Field
[0001] This disclosure relates to heating units capable of rapidly heating the substrate
to essentially uniform temperature across the surface and to articles and methods
employing such heating units.
Introduction
[0002] Self-contained heat sources are employed in a wide-range of industries, from food
industries for heating food and drink to outdoor recreation industries for providing
hand and foot warmers to medical applications for inhalation devices. Many self-contained
heating sources are based on either an exothermic chemical reaction or on ohmic heating.
For example, self-heating units that produce heat by an exothermic chemical reaction
often have at least two compartments, one for holding a heat producing composition
and one for holding an activating solution. The two compartments are separated by
a frangible seal that when broken allows mixing of the components to initiate an exothermic
reaction to generate heat (see for example
U.S. Patent Nos. 5,628,304;
4,773,389;
6,289,889). This type of non-combustible, self-heating unit is suitable for heating food, drink,
or cold toes and fingers, since the heat production is relatively mild.
Another common source for self-contained heat is ohmic heating. In ohmic heating a
current is passed through an electrically resistive material to generate heat that
is transmitted to an adjacent article. This mode of heat production has been employed
to vaporize or heat a volatile substance, for example tobacco, for inhalation by a
user. Cigarette holders and pipe bowls having an electrical resistance coil to generate
heat in order to volatilize tobacco flavors have been described (
U.S. Patent Nos. 2,104,266;
4,922,901;
6,095,143). Heating of drugs other than tobacco by ohmic heating have also been described.
For example,
WO 94/09842 to Rosen describes applying a drug to an electrically resistive surface and heating
the surface to vaporize the drug for inhalation. Ohmic heating has the advantage of
facilitating precise control of the energy applied to determine the heat generated.
However, in many ohmic heating systems, and in particular for small systems where
limited energy is available, such as, for example, when using batteries, there can
be a substantial delay on the order of seconds or minutes between the time heating
is initiated and maximum temperature is achieved. Moreover, for small devices, such
as for example, portable medical devices, where the power source comprises a battery,
ohmic heating can be expensive and bulky.
[0003] Another approach for providing a controlled amount of heat is using electrochemical
interactions. Here, components that interact electrochemically after initiation in
an exothermic reaction are used to generate heat. Exothermic electrochemical reactions
include reactions of a metallic agent and an electrolyte, such as a mixture of magnesium
granules and iron particles as the metallic agent, and granular potassium chloride
crystals as the electrolyte. In the presence of water, heat is generated by the exothermic
hydroxylation of magnesium, where the rate of hydroxylation is accelerated in a controlled
manner by the electrochemical interaction between magnesium and iron, which is initiated
when the potassium chloride electrolyte dissociates upon contact with the liquid water.
Electrochemical interactions have been used in the smoking industry to volatilize
tobacco for inhalation (
U.S. Patent Nos. 5,285,798;
4,941,483;
5,593,792).
[0004] The aforementioned self-heating methods are capable of generating heat sufficient
to heat an adjacent article to several hundred degrees Celsius in a period of several
minutes. There remains a need in the art for a device capable of rapid heat production,
i.e., on the order of seconds and fractions of seconds, capable of heating with essential
uniformity an article to within a defined temperature range, and which is suitable
for use in articles to be used by people.
[0005] US 5,322,018 relates to an igniter that is said to provide rapid longitudinal and radial propagation
of the ignition reaction.
[0006] US 4,193,388 relates to a container which, it is said, can be designed to heat its outer surface
as to sterilize it, or to heat its inner surface and any contents therewithin.
Summary
[0007] This disclosure relates to the use of a layer of an essentially homogenous slurry
of a selected mass of a solid fuel according to claim 1.
[0008] This disclosure relates also to a method for providing an essentially homogenous
and uniform coating of dry solid fuel, according to claim 15, and to a heating unit
according to the claim 28.
[0009] It is to be understood that both the foregoing general description and the following
detailed description are exemplary and explanatory only and are not restrictive of
certain embodiments, as claimed.
Description of the Drawings
[0010]
Fig. 1A is a cross-sectional illustration of a heating unit according to certain embodiments.
Fig. 1B is a perspective illustration of a heating unit as disclosed herein, but not
an embodiment of the claimed invention.
Fig. 2A is a cross-sectional illustration of a heating unit having a cylindrical geometry
as disclosed herein, but not an embodiment of the claimed invention.
Fig. 2B is a perspective illustration of a heating unit having a cylindrical geometry
as disclosed herein, but not an embodiment of the claimed invention.
Fig. 2C is a cross-sectional illustration of a cylindrical heating unit similar to
the heating unit of Figs. 2A-2B but having a modified igniter design as disclosed
herein, but not an embodimenet of the claimed invention.
Fig. 2D is a cross-sectional illustration of a cylindrically-shaped heating unit that
includes a thermal shunt as disclosed herein but not an embodiment of the claimed
invention.
Fig. 3 is a schematic cross-sectional illustration of a chemical heating unit having
two pressure transducers for measuring the internal pressure during and after ignition
of the solid fuel.
Figs. 4A-4F are thermal images of a cylindrically-shaped heating unit measured using
an infrared thermal imaging camera at post-ignition times of 100 milliseconds (Fig.
4A), 200 milliseconds (Fig. 4B), 300 milliseconds (Fig. 4C), 400 milliseconds (Fig.
4D), 500 milliseconds (Fig. 4E), and 600 milliseconds (Fig. 4F).
Figs. 5A-5B are thermal images showing the temperature uniformity of the exterior
substrate surface expanse 400 milliseconds after ignition of two cylindrically-shaped
heating units.
Figs. 6A-6C show schematic illustrations of the generation of drug vapor from a drug
supply unit carrying a film of drug on the exterior substrate surface (Fig. 6A); ignition
of the heating unit (Fig. 6B); and generation of a wave of heat effective to vaporize
the drug film (Fig. 6C).
Figs. 7A-7E are high speed photographs showing the generation of thermal vapor from
a drug supply unit as a function of time following ignition of the solid fuel.
Fig. 8 shows a drug delivery device containing a heating unit as part of an inhalation
drug delivery device for delivery of an aerosol comprising a drug.
Figs. 9A-9C show drug supply units for use in drug delivery devices designed for delivering
multiple drug doses.
Figs 10A-10B show illustrations of a perspective view (Fig. 10A) and an assembly view
(Fig. 10B) of a thin film drug supply unit.
Figs. 11A-11B show cross-sectional illustrations of thin film drug supply units comprising
multiple doses.
Fig. 12 shows a relationship between the mass of a solid fuel coating and the peak
temperature of the exterior surface of a substrate according to certain embodiments.
Fig. 13A is an illustration of a cross-sectional view of a heating unit having an
impulse absorbing material disposed within the unit.
Fig.13B is an illustration of a cross-sectional view of a cylindrical heating unit
having an impulse absorbing material disposed within the unit.
Fig. 13C is an illustration of a cross-sectional view of a heating unit having an
impulse absorbing material and an additional pressure reducing element disposed with
the enclosure.
Fig. 14 shows the measured pressure within heating units comprising glass fiber mats
following ignition of the solid fuel.
Fig. 15 shows the temperature at various positions within a heating unit following
ignition of the solid fuel.
Fig. 16 is a schematic illustration of an igniter comprising an initiator composition
disposed on an electrically resistive heating element.
Fig.17 shows peak internal pressure within sealed heating units following ignition
of a thin film layer of solid fuel comprising a metal reducing agent and a metal-containing
oxidizer.
Fig. 18 shows the relationship of the yield and purity of an aerosol comprising a
specific pharmaceutical compound using different substrate temperatures obtained from
different masses of solid fuel.
Fig. 19 shows a temperature profile of a heating unit substrate following ignition
of the solid fuel.
Description of Various Embodiments
[0011] Unless otherwise indicated, all numbers expressing quantities of ingredients, reaction
conditions, and so forth used in the specification and claims are to be understood
as being modified in all instances by the term "about."
[0012] In this application, the use of the singular includes the plural unless specifically
stated otherwise. In this application, the use of "or" means "and/or" unless stated
otherwise. Also, terms such as "element" or "component" encompass both elements and
components comprising one unit and elements and components that comprise more than
one subunit unless specifically stated otherwise.
COATED SUBSTRATES AND TEMPERATURE CONTROL
[0013] Fig. 1A shows an example of a substrate
12, such as those used in this invention. The substrate can be formed from a thermally-conductive
material. Thermally-conductive materials are well known, and typically include, but
are not limited to, metals, such as aluminum, iron, copper, stainless steel, and the
like, alloys, ceramics, and filled polymers. The substrate can be formed from one
or more such materials and in certain embodiments, can have a multilayer structure.
For example, the substrate can comprise one or more films and/or coatings and/or multiple
sheets or layers of materials. In certain embodiments, portions of the substrate can
be formed from multiple sections. In certain embodiments, the multiple sections forming
the substrate of the heating unit can have different thermal properties. A substrate
can be of any appropriate geometry, the rectangular configuration shown in
Fig. 1A is merely exemplary. A substrate can also have any appropriate thickness and the
thickness of the substrate can be different in certain regions. Substrate
12, as shown in
Fig. 1A, has an interior surface
14 and an exterior surface
16. Heat can be conducted from interior surface
14 to exterior surface
16. An article or object placed adjacent or in contact with exterior surface
16 can receive the conducted heat to achieve a desired action, such as warming or heating
a solid or fluid object, effecting a further reaction, or causing a phase change.
In certain embodiments, the conducted heat can effect a phase transition in a compound
in contact, directly or indirectly, with exterior surface
16.
[0014] Solid fuels can be used to heat the substrates rapidly. The energy released during
an exothermic reaction using solid fuels can be used to provide the temperature rise
required to heat directly or indirectly a material adjacent to the exterior surface.
In certain embodiments, the substrate
12 has an expanse of a solid fuel
20, in direct contact with or adjoining interior surface
14.
[0015] The solid fuel can be any appropriate shape and have any appropriate dimensions.
For example, as shown in
Fig. 1A, solid fuel
20 can comprise a surface expanse
26 and side expanses
28, 30. As shown in
Fig. 1B, heating unit
40 comprises a substrate
42 having an exterior surface
44 and an interior surface
46. Solid fuel
48, is in the shape of a hollow rod extending the length of substrate
42 and exhibiting a diameter less than that of interior surface
46. It can be appreciated that a finned or ribbed exterior surface can provide a high
surface area that can be useful to facilitate heat transfer from the solid fuel to
an article or composition in contact with the surface.
[0016] The components of the solid fuel can react in an exothermic reaction to produce heat.
For example, the solid fuel can react in an exothermic oxidation-reduction reaction
or an intermetallic alloying reaction. An oxidation-reduction reaction refers to a
chemical reaction in which one compound gains electrons and another compound loses
electrons. The compound that gains electrons is referred to as an oxidizing agent,
and the compound that loses electrons is referred to as a reducing agent. An example
of an oxidation-reduction reaction is a chemical reaction of a compound with molecular
oxygen (O
2) or an oxygen-containing compound that adds one or more oxygen atoms to the compound
being oxidized. During the oxidation-reduction reaction, the molecular oxygen or the
oxygen-containing compound is reduced by the compound being oxidized. The compound
providing oxygen acts as the oxidizer or oxidizing agent. The compound being oxidized
acts as the reducing agent. Oxidation-reduction reactions can be exothermic, meaning
that the reactions generate heat. An example of an exothermic oxidation-reduction
reaction is the thermite reaction of a metal with a metal oxidizing agent. According
to the invention, a solid fuel comprises a metal reducing agent and a metal-containing
oxidizing agent.
[0017] The metal reducing agent and the oxidizing agent can be in the form of a powder.
The term "powder" refers to powders, particles, prills, flakes, and any other particulate
that exhibits an appropriate size and/or surface area to sustain self-propagating
ignition. For example, the powder can comprise particles exhibiting an average diameter
ranging from 0.1 µm to 200 µm.
[0018] A metal reducing agent can include, but is not limited to molybdenum, magnesium,
calcium, strontium, barium, boron, titanium, zirconium, vanadium, niobium, tantalum,
chromium, tungsten, manganese, iron, cobalt, nickel, copper, zinc, cadmium, tin, antimony,
bismuth, aluminum, and silicon. In certain embodiments, a metal reducing agent can
include aluminum, zirconium, and titanium. A metal reducing agent can comprise more
than one metal reducing agent.
[0019] An oxidizing agent can comprise oxygen, an oxygen based gas, and/or a solid oxidizing
agent. In this disclosure, an oxidizing agent comprises a metal-containing oxidizing
agent. A metal-containing oxidizing agent includes, but is not limited to, perchlorates
and transition metal oxides. Perchlorates can include perchlorates of alkali metals
or alkaline earth metals, such as, but not limited to, potassium perchlorate (KClO
4), potassium chlorate (KClO
3), lithium perchlorate (LiClO
4), sodium perchlorate (NaClO
4), and magnesium perchlorate [Mg(ClO
4)
2]. Transition metal oxides that function as oxidizing agents include, but are not
limited to, oxides of molybdenum, such as MoO
3, iron, such as Fe
2O
3, vanadium (V
2O
5), chromium (CrO
3, Cr
2O
3), manganese (MnO
2), cobalt (Co
3O
4), silver (Ag
2O), copper (CuO), tungsten (WO
3), magnesium (MgO), and niobium (Nb
2O
5). The metal-containing oxidizing agent can include more than one metal-containing
oxidizing agent.
[0020] In certain embodiments, the metal reducing agent forming the solid fuel can be selected
from zirconium and aluminum, and the metal-containing oxidizing agent can be selected
from MoO
3 and Fe
2O
3.
[0021] The ratio of metal reducing agent to metal-containing oxidizing agent can be selected
to determine the ignition temperature and the burn characteristics of the solid fuel.
An exemplary chemical fuel can comprise 75% zirconium and 25% MoO
3, percentage based on weight. In certain embodiments, the amount of metal with is
a reducing agent can range from 60% by weight to 90% by weight of the total dry weight
of the solid fuel. In certain embodiments, the amount of metal-containing oxidizing
agent can range from 10% by weight to 40% by weight of the total dry weight of the
solid fuel. The amount of oxidizing agent in the solid fuel can be related to the
molar amount of the oxidizers at or near the eutectic point for the fuel composition.
The oxidizing agent can be the major component and in others the metal reducing agent
can be the major component. Those of skill in the art are able to determine the appropriate
amount of each component based on the stoichiometry of the chemical reaction and/or
by routine experimentation. Also as known in the art, the particle size of the metal
and the metal-containing oxidizer can be varied to determine the burn rate, with smaller
particle sizes selected for a faster burn (see, for example,
U.S. Patent No. 5,603,350).
[0022] In certain embodiments, a solid fuel can comprise additive materials to facilitate,
for example, processing and/or to determine the thermal and temporal characteristics
of a heating unit during and following ignition of the solid fuel. An additive material
can be reactive or inert. An inert additive material will not react or will react
to a minimal extent during ignition and burning of the solid fuel. The additive can
comprise inorganic or organic materials.
[0023] In certain applications, particularly, where it is desirous to produce a minimal
amount of gas, such as for example, in a sealed heating unit, the additive material
can be inorganic materials. These inorganic materials can function as binders, adhesives,
gelling agents, thixotropic agents, and/or surfactants. Examples of gelling agents
include, but are not limited to, clays such as Laponite®, Montmorillonite, Cloisite®,
metal alkoxides, such as those represented by the formula R-Si(OR)
n and M(OR)
n where n can be 3 or 4, and M can be Ti, Zr, Al, B or other metals, and collidal particles
based on transition metal hydroxides or oxides. Examples of binding agents include,
but are not limited to, soluble silicates such as Na- or K-silicates, aluminum silicates,
metal alkoxides, inorganic polyanions, inorganic polycations, and inorganic sol-gel
materials, such as alumina or silica-based sols.
[0024] The solid fuel adheres to the surface of the substrate and the constituents of the
solid fuel adhere to each other, and maintain physical integrity. It can be useful
that the solid fuel remain adhered to the substrate surface and maintain physical
integrity during processing, storage, and use during which time the solid fuel coating
can be exposed to a variety of mechanical and environmental conditions. As discussed
above, several additives, such as those disclosed herein, can be incorporated into
the solid fuel to impart adhesion and physical robustness to the solid fuel coating.
[0025] The solid fuel can comprise Laponite®, and in particular Laponite® RDS, as an inert
additive material. Laponite® is a synthetic layered silicate, and in particular a
magnesium phyllosilicate, with a structure resembling that of the natural clay mineral
hectorite (Na
0.4Mg
2.7Li
0.3Si
4O
10(OH)
2). Laponite® RD is a commercial grade material which, when added to water, rapidly
disperses to form a gel when hydrated (Southern Clay Products, Gonzales, TX). Laponite®
RD has the following chemical analysis in weight percent: 59.5% SiO
2 : 27.5% MgO: 0.8% Li
2O : 2.8% Na
2O. Laponite® RDS (Southern Clay Products, Gonzales, TX) is a commercially available
sol-forming grade of Laponite® modified with a polyphosphate dispersing agent, or
peptizer, to delay rheological activity until the Laponite® RDS is added as a dispersion
into a formulation. A sol refers to a colloid having a continuous liquid phase in
which solid is suspended in a liquid. Laponite® RDS has the following chemical analysis
in weight percent: 54.5% SiO
2 : 26% MgO : 0.8% Li
2O : 5.6% Na
2O : 4.1% P
2O
5. In the presence of electrolytes, Laponites® can act as gelling and thixotropic agents.
Thixotropy refers to the property of a material to exhibit decreased viscosity under
shear.
[0026] When incorporated into a solid fuel composition comprising a metal which is a reducing
agent and a metal-containing oxidizing agent, such as any of those disclosed herein,
in addition to imparting gelling and thixotropic properties, Laponite® RDS can also
act as binder.
[0027] An example of the preparation of a solid fuel comprising Laponite® RDS and the application
of the solid fuel to a metal foil substrate are described in Example 1.
[0028] Other useful additive materials include glass beads, diatomaceous earth, nitrocellulose,
polyvinylalcohol, and other polymers that may function as binders. The solid fuel
can comprise more than one additive material. The components of the solid fuel comprising
the metal, oxidizing agent and/or additive material and/or any appropriate aqueous-
or organic-soluble binder, can be mixed by any appropriate physical or mechanical
method to achieve a useful level of dispersion and/or homogeneity. The solid fuel
can be degassed.
[0029] In addition, to the enhanced binding properties of the solid fuels with additive,
other advantages of using inorganic additives include stability of the additive up
to very high temperatures and lack of, or minimal release of, any toxic gases by the
additive. In an enclosed system, this lack of additional gas production from the inorganic
additive also reduces or minimizes the possibility of rupture of the enclosed heating
unit.
[0030] Tables 1A-1E summarize solid fuel compositions including the additives used. The
weight ratio of the components comprising certain solid fuel compositions are provided.
Table 1A: Examples of Solid Fuel Compositions (wt%)
| Component |
Fuel #1 |
Fuel #2 |
Fuel #3 |
Fuel #4 |
Fuel #5 |
Fuel #6 |
Fuel #7 |
Fuel #8 |
| Zirconium (Zr) |
70-90 |
|
|
|
|
20-40 |
20-30 |
|
| Titanium (Ti) |
|
70-92 |
|
|
|
|
|
60-80 |
| Iron (Fe) |
|
|
70-90 |
|
|
|
|
|
| Magnesium (Mg) |
|
|
|
20-40 |
40-60 |
|
|
|
| Boron (B) |
|
|
|
|
|
|
|
20-40 |
| Potassium perchlorate (KClO4) |
10-30 |
8-30 |
10-30 |
|
|
|
|
|
| Lead Oxide (PbO) |
|
|
|
|
40-60 |
|
|
|
| Tungsten Oxide (WO3) |
|
|
|
|
|
60-80 |
|
|
| Barium Chromate (BaCrO4) |
|
|
|
|
|
|
70-80 |
|
| Teflon |
|
|
|
60-80 |
|
|
|
|
Table 1B: Examples of Solid Fuel Compositions (wt%)
| Component |
Fuel #9 |
Fuel #10 |
Fuel #11 |
Fuel #12 |
Fuel #13 |
Fuel #14 |
Fuel #15 |
Fuel #16 |
| Zirconium (Zr) |
|
|
|
21 |
|
|
10-50 |
|
| Titanium (Ti) |
60-80 |
|
70-92 |
|
82 |
55 |
33-81 |
|
| Iron (Fe) |
|
|
0-84 |
|
|
|
|
|
| Aluminum (Al) |
|
20-40 |
|
|
|
20 |
|
|
| Nickel (Ni) |
|
60-80 |
|
|
|
|
|
|
| Boron (B) |
|
|
|
|
|
25 |
|
|
| Potassium perchlorate (KClO4) |
|
|
8-30 |
|
|
|
9-17 |
50 |
| Potassium chlorate (KClO3) |
|
|
|
|
18 |
|
|
|
| Tungsten Oxide (WO3) |
20-40 |
|
|
|
|
|
|
|
| Barium Chromate (BaCrO4) |
|
|
|
64 |
|
|
|
|
| Zirconium Carbide (ZrC) |
|
|
|
|
|
|
|
50 |
| Diatomaceous Earth |
|
|
|
15 |
|
|
|
|
Table 1C: Examples of Solid Fuel Compositions (wt%)
| Component |
Fuel #17 |
Fuel #18 |
Fuel #19 |
Fuel #20 |
Fuel #21 |
Fuel #22 |
Fuel #23 |
Fuel #24 |
| Zirconium (Zr) |
|
50-65 |
|
|
50-72 |
30-80 |
65 |
55-70 |
| Titanium (Ti) |
|
|
20-70 |
|
|
|
|
|
| Boron (B) |
|
|
|
15 |
|
|
|
|
| Potassium Perchlorate (KClO4) |
52.5 |
|
|
|
|
|
|
|
| Molybdenum Oxide (MoO3) |
|
0-50 |
30-80 |
|
|
20-70 |
|
25-33 |
| Iron Oxide (Fe2O3) |
|
0-50 |
|
85 |
28-50 |
|
25 |
|
| Zirconium Hydride (ZrH2) |
47.5 |
|
|
|
|
|
|
|
| Diatomaceous Earth |
|
balance |
|
|
|
|
10 |
5-12 |
Table 1D: Examples of Solid Fuel Compositions (wt%)
| Component |
Fuel #25 |
Fuel #26 |
Fuel #27 |
Fuel #28 |
Fuel #29 |
Fuel #30 |
Fuel #31 |
Fuel #32 |
Fuel #33 |
| Zirconium (Zr) |
35-50 |
63-69 |
70 |
34 |
66.5-69 |
66.5-74.6 |
54-66.5 |
69 |
69 |
| Titanium (Ti) |
20-35 |
|
|
|
|
|
|
|
|
| Molybdenum Oxide MoO3 |
30 |
27-29.5 |
30 |
54 |
28.5-29 |
24.87-29 |
28.5-34 |
29.85 |
29.85 |
| Nitrocellulose |
|
|
excess |
|
|
0.53-4.5 |
|
0.5 |
0.5 |
| Cab-O-Sil |
|
4-7.5 |
|
|
|
|
|
|
|
| Glass Fiber |
|
|
|
12 |
|
|
|
|
0.65 |
| Glass Microsphere |
|
|
|
|
|
|
|
0.65 |
|
| Polyvinyl Alcohol |
|
|
|
|
2.5-4.5 |
|
|
|
|
| High Vacuum Grease |
|
|
|
|
|
|
5-12 |
|
|
Table 1E: Examples of Solid Fuel Compositions (wt%)
| Component |
Fuel #34 |
Fuel #35 |
Fuel #36 |
Fuel #37 |
Fuel #38 |
Fuel #39 |
Fuel #40 |
Fuel #41 |
Fuel #42 |
Fuel #43 |
| Zirconium (Zr) |
66.5-69 |
69.65 |
69.7-74.6 |
49-59.5 |
|
|
47-70 |
|
40 |
20 |
| Magnesium (Mg) |
|
|
|
|
|
40 |
|
|
|
|
| Aluminum (Al) |
|
|
|
|
36-70 |
|
|
50-55 |
30 |
|
| Silicon (Si) |
|
|
|
|
|
|
|
|
|
30 |
| Potassium chlorate (KClO3) |
|
|
|
|
|
|
0-3 |
|
|
|
| Bismuth Oxide (Bi2O3) |
|
|
|
|
|
|
|
|
|
50 |
| Molybdenum Oxide (MoO3) |
28.5-29 |
29.85 |
24.9-29.8 |
21-25.5 |
30-64 |
40 |
23.1-38 |
45-50 |
30 |
|
| Diatomaceous Earth |
|
|
|
19-25 |
|
|
balance or excess |
|
|
|
| Nitrocellulose |
|
|
|
0.5 |
|
|
0.4-2 |
1 |
|
|
| Glass Beads |
|
|
|
|
|
20 |
|
|
|
|
| Carboxymethyl cellulose |
|
|
|
|
|
|
|
|
|
excess |
| Polyvinyl alcohol |
|
|
0.5 |
|
|
|
|
|
|
|
| 40% Aqueous SiO2 |
2-5 |
|
|
|
|
|
|
|
|
|
| Viton-A |
|
0.5 |
|
|
|
|
|
|
|
|
[0031] While the use of additives in the solid fuel can improve the binding properties of
the solid fuel, it also can improve the ease of use and manufacturability of substrates
coated with such fuel. In particular, use of additives can make it possible to use
wet-coating techniques, such as, for example, but not limitation, dip coating, spray
coating, roller coating, gravure coating, reverse roll coating, gap coating e.g. with
a wire wound coating rod e.g. in a bar coater, metering rod coating, slot die coating,
curtain coating, and air knife coating, as means for deposition of a fuel powder on
a substrate surface, such as, for example, either inside, or on, a cylindrical type
surface such as the internal surface of the substrate in
Fig. 1B, or on a flat surface such as a foil as is shown in
Fig 10A.
[0032] The use of solid fuel slurries with additives for coating a substrate can provide
for better mixing of the materials, enhanced adherence properties, and more control
over the even disbursement of the solid fuel on a surface. While preparing a physical
mixture of solid fuel powders as an essentially homogeneous layer around the walls
of a cylindrical device can be done, it is problematic, especially if the materials
used have differences in densities, particle sizes, shapes, surface volume ratios;
and lack chemically attractive surface-surface interactions. (Essentially homogeneous
is defined, for purposes herein, as essentially uniform; and when applied to a mixture
of two or more components, it refers to a basically uniform distribution of the various
different particles throughout the mixture. This is in contrast to a heterogeneous
mixture of components where various components tend to aggregate and there is settling
out of the higher density particles.) Use of a core for dispersing mixtures of fuel
powders to an interior surface of a substrate, allows one to control the gap or layer
thickness of the solid fuel layer, however, it does not prevent other problems such
as segregation of the particles in the mixture. Inadequate homogeneity as to the fuel
mixture itself, due to ineffective mixing can result in inconsistent heating of the
exterior surface of the substrate. Mixing can be facilitated and even automated when
done as a slurry as opposed to a dry powder.
[0033] Additionnally, lack of homogeneity as to the fuel thickness on, or in, contact with
an interior surface of a substrate can also result in inconsistent heating of the
exterior surface of a substrate. Coating adherence and ease of application can be
enhanced by the use of slurries with additives.
[0034] The solid fuel is disposed on a substrate as a coating or thin layer, wherein the
thickness of the thin layer of solid fuel ranges from 0.00254 cm (0.001 inches) to
0.0762 cm (0.030 inches) by use of wet coating.
[0035] Substrates such as, for example, substrates
510 shown in
Fig. 10A, can be coated to a nearly homogeneous thickness to form a thin coating or a thin
layer of solid fuel
512 on the interior region of the substrate corresponding to the exterior surface on
which the drug
514 is disposed. The thickness of the substrate, its thermal conductivity, its heat capacity,
the thickness of the thin layer of solid fuel
512, and the composition of solid fuel
512 can determine the maximum temperature (peak temperature) as well as the temporal
and spatial dynamics of the temperature profile produced by the burning of the solid
fuel.
[0036] Studies using thin solid fuel layers having a thickness ranging from 0.00254 cm (0.001
inches) to 0.0227 cm (0.005 inches) demonstrate that the maximum temperature reached
by a thin film substrate on which the solid fuel is disposed can be linear with the
mass of solid fuel applied. For example, as shown in
Fig. 12 for several different solid fuel compositions, for a 0.00254 cm (0.001 inch) to 0.00762
cm (0.0003 inch) thick layer of Zr/MoO
3 solid fuel having a mass ranging from 0.13 g to 0.25 g, the maximum temperature reached
by the substrate during burn is linear. Other studies with solid fuel layers having
a mass ranging from 0.12 g to 0.24 g demonstrate linearity over a temperature ranging
from 375 °C to 625 °C. It will be appreciated that one skilled in the art can establish
similar relationships for other solid fuel compositions and configurations. Such studies
demonstrate that the temperature reached by the substrate when the solid fuel is burned
can be established by controlling the amount of solid fuel applied to the substrate.
[0037] Measurements of the substrate surface temperature after firing demonstrate that thin
coatings or layers of a solid fuel comprising a metal reducing agent and a metal-containing
oxidizing agent can produce uniformity of temperature on the exterior surface of the
substrate. Uniformity of temperature is defined herein to exist when the temperature
in degrees Celsius of the exterior surface of the substrate, corresponding to the
fuel coated area of the interior surface of the substrate, is within a standard deviation
of 50° C from the average surface temperature obtained, as measured within 100 milliseconds
after completion of propagation of the ignited fuel flame front. A temperature profile
of a substrate forming a heating unit substantially as shown in
Figs. 10A and
10B and described in Example 9 following ignition of the solid fuel is shown in
Fig. 19.
Fig. 19 shows the average surface temperature at various positions across two dimensions
of a 3.302 cm x 3.302 cm (1.3 inch x 1.3 inch) substrate 0.25 seconds following ignition
of a 0.0041 cm (0.00163 inch) thick coating of solid fuel. The average surface temperature
of the effective heated area was about 400°C.
[0038] In certain applications, such as for example, vaporization of a drug off the substrate
of a heating unit, uniformity of heating of the substrate is critical as it facilitates
the production of an aerosol comprising a high purity drug or pharmaceutical composition
and maximizes the yield of drug initially deposited on the substrate forming an aerosol.
HEATING UNITS
[0039] An embodiment of a heating unit is shown in
Fig. 1A. Heating unit
10 comprises a substrate
12 with a thin layer or coating of solid fuel
20 in contact with the interior surface
14 of substrate
12. Solid fuel is ignited to generate a self-sustaining oxidation-reduction reaction.
Once a portion of the solid fuel is ignited, the heat generated by the oxidation-reduction
reaction can ignite adjacent unburned fuel until all of the fuel is consumed in the
process of the chemical reaction. The exothermic oxidation-reduction reaction can
be initiated by the application of energy to at least a portion of the solid fuel.
Energy absorbed by the solid fuel or by an element in contact with the solid fuel
can be converted to heat. When the solid fuel becomes heated to a temperature above
the auto-ignition temperature of the reactants, e.g. the minimum temperature required
to initiate or cause self-sustaining combustion in the absence of a combustion source
or flame, the oxidation-reduction reaction will initiate, igniting the solid fuel
in a self-sustaining reaction until the fuel is consumed.
[0040] Energy can be applied to ignite the solid fuel using a number of methods. For example,
a resistive heating element can be positioned in thermal contact with the solid fuel,
which when a current is applied, can heat the solid fuel to the auto-ignition temperature.
An electromagnetic radiation source can be directed at the solid fuel, which when
absorbed, can heat the solid fuel to its auto-ignition temperature. An electromagnetic
source can include lasers, diodes, flashlamps and microwave sources. RF or induction
heating can heat the solid fuel source by applying an alternating RF field that can
be absorbed by materials having high magnetic permeability, either within the solid
fuel, or in thermal contact with the solid fuel. The source of energy can be focused
onto the absorbing material to increase the energy density to produce a higher local
temperature and thereby facilitate ignition. In certain embodiments, the solid fuel
can be ignited by percussive forces.
[0041] The auto-ignition temperature of a solid fuel comprising a metal which is a reducing
agent and a metal-containing oxidizing agent as disclosed herein can range of 400
°C to 500 °C. While such high auto-ignition temperatures facilitate safe processing
and safe use of the solid fuel under many use conditions, for example, as a portable
medical device, for the same reasons, to achieve such high temperatures, a large amount
of energy must be applied to the solid fuel to initiate the self-sustaining reaction.
Furthermore, the thermal mass represented by the solid fuel can require that an impractically
high temperature be applied to raise the temperature of the solid fuel above the auto-ignition
temperature. As heat is being applied to the solid fuel and/or a support on which
the solid fuel is disposed, heat is also being conducted away. Directly heating a
solid fuel can require a substantial amount of power due to the thermal mass of the
solid fuel and support.
[0042] As is well known in the art, for example, in the pyrotechnic industry, sparks can
be used to safely and efficiently ignite fuel compositions. Sparks refer to an electrical
breakdown of a dielectric medium or the ejection of burning particles. In the first
sense, an electrical breakdown can be produced, for example, between separated electrodes
to which a voltage is applied. Sparks can also be produced by ionizing compounds in
an intense laser radiation field. Examples of burning particles include those produced
by friction and break sparks produced by intermittent electrical current. Sparks of
sufficient energy incident on a solid fuel can initiate the self-sustaining oxidation-reduction
reaction.
[0043] When sufficiently heated, the exothermic oxidation-reduction reaction of the solid
fuel can produce sparks, as well as radiation energy. Thus, reliable, reproducible
and controlled ignition of the solid fuel can be facilitated by the use of an initiator
composition capable of reacting in an exothermic oxidation-reduction reaction. The
initiator composition can comprise the same or similar reactants as those comprising
the solid fuel. The initiator composition can be formulated to maximize the production
of sparks having sufficient energy to ignite a solid fuel. Sparks ejected from an
initiator composition can impinge upon the surface of the solid fuel, causing the
solid fuel to ignite in a self-sustaining exothermic oxidation-reduction reaction.
The igniter can comprise a physically small, thermally isolated heating element on
which is applied a small amount of an initiator composition capable of producing sparks
or the initiator composition can be placed directly on the fuel itself and ignited
by a variety of means, including, for example, optical or percussive.
[0044] As shown in
Fig. 1A, heating unit
10 can include an initiator composition
50 which can ignite a portion of solid fuel
20. As shown in
Fig. 1A, initiator composition
50 can be positioned proximate to the center region
54 of solid fuel
20. Initiator composition
50 can be positioned at other regions of solid fuel
20, such as toward the edges. A heating unit can comprise more than one initiator composition
where the more than one initiator composition
50 can be positioned on the same or different side of solid fuel
20. Initiator composition
50 can be mounted in a retaining member
56 that is integrally formed with substrate
12 and/or secured within a suitably sized opening in substrate
12. Retaining member
56 and substrate
12 can be sealed to prevent release outside heating unit
10 of reactants and reaction products produced during ignition and burning of solid
fuel
20. Electrical leads
58a,
58b in electrical contact with initiator composition
50 can extend from retaining member
56 for electrical connection to a mechanism configured to activate (not shown) initiator
composition
50.
[0045] Initiator compositions capable of producing sparks upon exposure to heat, force,
or a spark are known, for example, in the pyrotechnic field and the photoflash industry.
An initiator composition can comprise at least one metal, such as those described
herein, and at least one oxidizing agent, such as, for example, a chlorate or perchlorate
of an alkali metal or an alkaline earth metal or metal oxide and others disclosed
herein. An initiator composition can include at least one binder and/or additive material
such as a gelling agent and/or binder. Examples of additive materials including gelling
agents and/or binders are disclosed herein. Additive materials can be useful in determining
certain processing, ignition, and/or burn characteristics of the initiator composition.
[0046] Fig.
2A shows a longitudinal cross-sectional illustration of a heating unit.
Fig. 2B shows a corresponding perspective illustration illustrating the unassembled individual
components shown in
Fig. 2A. As shown in
Fig. 2A, heating unit
60 can include a substrate
62 that is generally cylindrical in shape and terminates at one end in a tapered nose
portion
64 and at the other end in an open receptacle
66. Substrate
62 has interior and exterior surfaces
68,
70, respectively, which define an inner region
72. An inner backing member
74 can be cylindrical in shape and can be located within inner region
72. The opposing ends
76,
78 of backing member
74 can be open. Backing member
74 can comprise a heat-conducting or heat-absorbing material, depending on the desired
thermal and temporal dynamics of the heating unit. When constructed of a heat-absorbing
material, backing member
74 can reduce the maximum temperature reached by substrate
62 after ignition of the solid fuel
80.
[0047] Solid fuel
80 comprising, for example, any of the solid fuels described herein, can be confined
between substrate
62 and backing member
74 or can fill inner region
72. Solid fuel 80 can adjoin interior surface
68 of substrate
62.
[0048] Initiator composition
82 can be positioned in open receptacle
66 of substrate
62, and can be configured to ignite solid fuel
80. A retaining member
84 can be located in open receptacle
66 and can be secured in place using any suitable mechanism, such as for example, bonding
or welding. Retaining member
84 and substrate
62 can be sealed to prevent release of the reactants or reaction products produced during
ignition and burn of initiator composition
82 and solid fuel
80. Retaining member
84 can include a recess
86 in the surface facing inner region
72. Recess
86 can retain initiator composition
82. In certain embodiments, an electrical stimulus can be applied directly to initiator
composition
82 via leads
88,
90 connected to the positive and negative termini of a power source, such as a battery
(not shown). Leads
88,
90 can be connected to an electrically resistive heating element placed in physical
contact with the initiator composition
82 (not shown). In certain embodiments, leads
88,
90 can be coated with the initiator composition
82.
[0049] Referring to
Fig. 2A, application of a stimulus to initiator composition
82 can result in the generation of sparks that can be directed from open end
78 of backing member
74 toward end
76. Sparks directed toward end
76 can contact solid fuel
80, causing solid fuel
80 to ignite. Ignition of solid fuel
80 can produce a self propagating wave of ignited solid fuel
80, the wave traveling from open end
78 toward nose portion
64 and back toward retaining member
84 held within receptacle end
66 of substrate
62. The self-propagating wave of ignited solid fuel
80 can generate heat that can be conducted from interior surface
68 to exterior surface
70 of substrate
62.
[0050] A heating unit is illustrated in
Fig. 2C. As shown in
Fig. 2C, heating unit
60 can comprise a first initiator composition
82 disposed in recess
86 in retaining member
84 and a second initiator composition
94 disposed in open end
76 of backing member
74. Backing member
74, located within inner region
72, defines an open region
96. Solid fuel
80 is disposed within the inner region between substrate
62 and backing member
74. Sparks generated upon application of an electrical stimulus to first initiator composition
82, through leads
88,
90, can be directed through open region
96 toward second initiator composition
94, causing second initiator composition
94 to ignite and generate sparks. Sparks generated by second initiator composition
94 can then ignite solid fuel
80, with ignition initially occurring toward the nose portion of substrate
62 and traveling in a self propagating wave of ignition to the opposing end.
[0051] The igniter can comprise a support and an initiator composition disposed on the support.
The support can be thermally isolated to minimize the potential for heat loss. In
this way, dissipation of energy applied to the combination of assembly and support
can be minimized, thereby reducing the power requirements of the energy source, and
facilitating the use of physically smaller and less expensive heat sources. In certain
applications, for example, with battery powered portable medical devices, such considerations
can be particularly useful. It can be useful that the energy source be a small low
cost battery, such as a 1.5 V alkaline battery. The initiator composition can comprise
a metal reducing agent and metal-containing oxidizing agent.
[0052] A metal reducing agent can include, but is not limited to molybdenum, magnesium,
calcium, strontium, barium, boron, titanium, zirconium, vanadium, niobium, tantalum,
chromium, tungsten, manganese, iron, cobalt, nickel, copper, zinc, cadmium, tin, antimony,
bismuth, aluminum, and silicon. A metal reducing agent can include aluminum, zirconium,
and titanium. A metal reducing agent can comprise more than one metal reducing agent.
An oxidizing agent can comprise oxygen, an oxygen based gas, and/or a solid oxidizing
agent. An oxidizing agent can comprise a metal-containing oxidizing agent. A metal-containing
oxidizing agent includes, but is not limited to, perchlorates and transition metal
oxides. Perchlorates can include perchlorates of alkali metals or alkaline earth metals,
such as but not limited to, potassium perchlorate (KClO
4), potassium chlorate (KClO
3), lithium perchlorate (LiClO
4), sodium perchlorate (NaClO
4), and magnesium perchlorate [Mg(ClO
4)
2]. Transition metal oxides that function as oxidizing agents include, but are not
limited to, oxides of molybdenum, such as MoO
3, iron, such as Fe
2O
3, vanadium (V
2O
5), chromium (CrO
3, Cr
2O
3), manganese (MnO
2), cobalt (Co
3O
4), silver (Ag
2O), copper (CuO), tungsten (WO
3), magnesium (MgO), and niobium (Nb
2O
5). The metal-containing oxidizing agent can include more than one metal-containing
oxidizing agent.
[0053] The ratio of metal reducing agent to metal-containing oxidizing agent can be selected
to determine the appropriate burn and spark generating characteristics. The amount
of oxidizing agent in the initiator composition can be related to the molar amount
of the oxidizers at or near the eutectic point for the fuel composition. The oxidizing
agent can be the major component and in others the metal reducing agent can be the
major component. Those of skill in the art are able to determine the appropriate amount
of each component based on the stoichiometry of the chemical reaction and/or by routine
experimentation. Also as known in the art, the particle size of the metal and the
metal-containing oxidizer can be varied to determine the burn rate, with smaller particle
sizes selected for a faster burn (see, for example, WO 2004/011396).
[0054] An initiator composition can comprise additive materials to facilitate, for example,
processing, enhance the mechanical integrity and/or determine the burn and spark generating
characteristics. The additive materials can be inorganic materials and can function
as binders, adhesives, gelling agents, thixotropic, and/or surfactants. Examples of
gelling agents include, but are not limited to, clays such as Laponite®, Montmorillonite,
Cloisite®, metal alkoxides such as those represented by the formula R-Si(OR)
n and M(OR)
n where n can be 3 or 4, and M can be Ti, Zr, Al, B or other metals, and colloidal
particles based on transition metal hydroxides or oxides. Examples of binding agents
include, but are not limited to, soluble silicates such as Na- or K-silicates, aluminum
silicates, metal alkoxides, inorganic polyanions, inorganic polycations, inorganic
sol-gel materials such as alumina or silica-based sols. Other useful additive materials
include glass beads, diatomaceous earth, nitrocellulose, polyvinylalcohol, guor gum,
ethyl cellulose, cellulose acetate, polyvinylpyrrolidone, fluorocarbon rubber (Viton)
and other polymers that can function as a binder. The initiator composition can comprise
more than one additive material. The components of the initiator composition comprising
the metal, metal-containing oxidizing agent and/or additive material and/or any appropriate
aqueous- or organic-soluble binder, can be mixed by any appropriate physical or mechanical
method to achieve a useful level of dispersion and/or homogeneity. Additive materials
can be useful in determining certain processing, ignition, and/or burn characteristics
of the initiator composition. The particle size of the components of the initiator
can be selected to tailor the ignition and burn rate characteristics as is known in
the art (see for example
U.S. Patent No. 5,739,460).
[0055] An initiator composition can comprise at least one metal, such as those described
herein, and at least one oxidizing agent, such as, for example, a chlorate or perchlorate
of an alkali metal or an alkaline earth metal or metal oxide and others disclosed
herein.
[0056] Examples of initiator compositions include compositions comprising 10% Zr : 22.5%
B : 67.5% KClO
3.; 49.0% Zr : 49.0 % MoO
3 and 2.0% nitrocellulose, and 33.9% Al : 55.4% MoO
3 : 8.9% B : 1.8 nitrocellulose; 26.5% Al : 51.5% MoO
3 : 7.8%B : 14.2% Viton, in weight percent.
[0057] Other initiator compositions can be used. For example, an initiator composition that
can ignite upon application of a percussive force comprises a mixture of sodium chlorate
(NaClO
3), phosphorous (P), and magnesium oxide (MgO).
[0058] Energy sufficient to heat the initiator composition to the auto-ignition temperature
can be applied to the initiator composition and/or the support on which the initiator
composition is disposed. The energy source can be any of those disclosed herein, such
as resistive heating, radiation heating, inductive heating, optical heating, and percussive
heating. In applications wherein the initiator composition is capable of absorbing
the incident energy, the support can comprise a thermally insulating material. The
incident energy can be applied to a thermally conductive support that can heat the
initiator composition above the auto-ignition temperature by thermal conduction.
[0059] The energy source can be an electrically resistive heating element. The electrically
resistive heating element can comprise any material that can maintain integrity at
the auto-ignition temperature of the initiator composition. The heating element can
comprise an elemental metal such as tungsten, an alloy such as Nichrome, or other
material such as carbon. Materials suitable for resistive heating elements are known
in the art. The resistive heating element can have any appropriate form. For example,
the resistive heating element can be in the form of a wire, filament, ribbon or foil.
The electrical resistance of the heating unit can range from 2 Ω to 4 Ω. The appropriate
resistivity of the heating element can at least in part be determined by the current
of the power source, the desired auto ignition temperature, or the desired ignition
time. The auto-ignition temperature of the initiator composition can range from 200
°C to 500 °C. The resistive heating element can be electrically connected, and suspended
between two electrodes electrically connected to a power source.
[0060] The support can comprise one or more heating units.
[0061] An igniter comprising a resistive heating element is illustrated in
Fig. 16. As shown in
Fig. 16, resistive heating element
716 is electrically connected to electrodes
714. Electrodes
714 can be electrically connected to an external power source such as a battery (not
shown). As shown in
Fig. 16, electrodes
714 are disposed on a laminate material
712 such as a printed circuit material. Such materials and methods of fabricating such
flexible or rigid laminated circuits are well known in the art. Laminate material
712 can comprise a material that will not degrade at the temperatures reached by resistive
heating element
716, by the exothermic reaction including sparks generated by initiator composition
718, and at the temperature reached during burning of the solid fuel. For example, laminate
712 can comprise Kapton®, a fluorocarbon laminate material or FR4 epoxy/fiberglass printed
circuit board. Resistive heating element
716 is positioned in an opening
713 in laminate
712. Opening
713 thermally isolates resistive heating element
716 to minimize thermal dissipation and facilitate transfer of the heat generated by
the resistive heating element to the initiator composition, and can provide a path
for sparks ejected from initiator composition
718 to impinge upon a solid fuel (not shown).
[0062] As shown in
Fig. 16, initiator composition
718 is disposed on resistive heating element
716.
[0063] The following procedure was used to apply the initiator composition to resistive
heating elements.
[0064] A 0.002 cm (0.0008 inch) diameter Nichrome wire was soldered to Cu conductors disposed
on a 0.005 inch thick FR4 epoxy/fiberglass printed circuit board (Onanon). The dimensions
of the igniter printed circuit board were 4.62 x 0.64 cm (1.82 inches by 0.25 inches).
Conductor leads can extend from the printed circuit board for connection to a power
source. In certain embodiments, the electrical leads can be connected to an electrical
connector.
[0065] The igniter printed circuit board was cleaned by sonicating (Branson 8510R-MT) in
DI water for 10 minutes, dried, sprayed with acetone and air dried.
[0066] The initiator composition comprised 0.68 grams nano-aluminum (40-70 nm diameter,
Argonide Nanomaterial Technologies, Sanford, FL), 1.23 grams of nano-MoO
3 (EM-NTO-U2; Climax Molybdenum, Henderson, CO), and 0.2 grams of nano-boron (33,2445-25G;
Aldrich). A slurry comprising the initiator composition was prepared by adding 8.6
mL of 4.25% Viton/A500 (4.25 grams Viton in 100 mL amyl acetate (Mallinckrodt)) solution.
[0067] A 1.1 uL drop of slurry was deposited on the heating element, dried for 20 minutes,
and another 0.8 uL drop of slurry comprising the initiator composition was , deposited
on the opposite side of the heating element.
[0068] Application of 3.0 V through a 1,000µF capacitor from two A76 alkaline batteries
to the Nichrome heating element ignited the Al : MoO
3 : B initiator composition within 1 to 50 msec, typically within 1 to 6 msec. When
positioned within 0.12" inches of the surface of a solid fuel comprising a metal reducing
agent and a metal-containing oxidizing agent such as, for example, a fuel comprising
76.16% Zr: 19.04% MoO
3 : 4.8% Laponite® RDS, the sparks produced by the initiator composition ignited the
solid fuel to produce a self-sustaining exothermic reaction. A 1 µL drop of the slurry
comprising the initiator composition can be deposited onto the surface of the solid
fuel adjacent the initiator composition disposed on the resistive heating element
to facilitate ignition of the solid fuel.
[0069] The initiator composition comprising Al : MoO
3 : B adhered to the Nichrome wire and maintained physical integrity following mechanical
and environmental testing including temperature cycling (-25 °C ↔ 40 °C), drop testing,
and impact testing.
[0070] As shown in
Fig. 2D heating units can include a thermal shunt
98, shown in
Fig. 2D as a cylindrical rod disposed within the heating unit. The thermal shunt can be incorporated
into the solid fuel expanse as a particulate, the thermal shunt can comprise the backing
member and/or the thermal shunt can be a separate element as shown. The thermal shunt
can be in direct contact with the solid fuel and/or can indirectly contact the solid
fuel. A thermal shunt can be capable of absorbing heat such that incorporation of
a thermal shunt in a heating unit can control or reduce the maximum temperature reached
by the exterior surface of the substrate forming the heating unit. For example, the
thermal shunt can comprise a material capable of undergoing a phase change at or above
the ignition temperature of the solid fuel. Examples of phase change materials include
low melting point metals such as tin, low melting point alloys such as Wood's metal
and leadtin alloys, inorganic salts, and mixtures thereof. The thermal shunt can comprise
a material that can release absorbed heat to prolong the heating time of the heating
unit. A thermal shunt can comprise at least one material exhibiting a high heat capacity,
such as, for example, copper, aluminum, stainless steel and glass. Examples of materials
that can release absorbed heat include sugars, waxes, metal salts and other materials
capable of melting during burning of the solid fuel and then undergoing crystallization
as the heating unit cools, thus generating exothermic heat of crystallization, and
mixtures thereof. Other materials capable of functioning as thermal shunts include
porous and fibrous materials such as porous ceramic membranes and/or fiber mats, and
the like. Such materials can exhibit a high surface area that can facilitate heat
transfer from the reactants and reaction products to the material matrix. In certain
applications, the porous and/or fibrous materials do not react with the reactants
or reaction products produced during ignition and burn, and do not degrade and/or
produce gaseous products at the temperatures achieved by the heating unit. The thermal
shunt material can comprise fibers including, but not limited to, metal fibers, silica
fibers, glass fibers, graphite fibers, and/or polymer fibers.
[0071] In certain embodiments, the heating unit described and illustrated in
Fig. 1A can be used in applications wherein rapid heating is useful. In certain embodiments,
a portion of the substrate can reach a maximum (peak) temperature in less than three
seconds (3 sec), in certain embodiments less than 1 second (1 sec), in certain embodiments
less than 500 milliseconds, and in certain embodiments less than 250 milliseconds.
[0072] A heating unit substantially as illustrated in
Fig. 2B was fabricated to measure the temperature of the exterior surface of the substrate
following ignition of a solid fuel. Referring to
Fig. 2B, cylindrical substrate
62 was approximate 3.81 cm (1.5 inches) in length and the diameter of open receptacle
66 was 1.524 cm (0.6 inches). Solid fuel
80 comprising 75% Zr : 25% MoO
3 in weight percent was placed in the inner region in the space between the backing
member
74 and the interior surface of substrate
62. A first initiator composition
82 comprising 5 mg of 10% Zr : 22.5% B : 67.5% KClO
3 in weight percent was placed in the depression of the retaining member and 10 mg
of a second initiator composition
94 of 10% Zr : 22.5% B : 67.5% KClO
3 in weight percent was placed in the open end
76 of backing member
74 near the tapered portion of heating unit
60. Electrical leads
88,
90 from two 1.5 V batteries provided a current of 0.3 Amps to ignite first initiator
composition
82, thus producing sparks to ignite second initiator composition
94. Both initiators were ignited within 1 to 20 milliseconds following application of
the electrical current. Sparks produced by second initiator composition
94 ignited solid fuel
80 in the tapered nose region
64 of the cylinder. Thermocouples placed on the exterior surface of substrate
62 were used to monitor the substrate surface temperature as a function of time. The
exterior substrate surface reached a maximum temperature of 400 °C in less than 100
milliseconds.
[0073] Upon ignition of the solid fuel, an exothermic oxidation-reduction reaction produces
a considerable amount of energy in a short time, such as for example, in certain embodiments
less than 1 second, in certain embodiments less than 500 milliseconds, and in certain
embodiments less than 250 milliseconds. Examples of exothermic reactions include electrochemical
reactions and metal oxidation-reduction reactions. When used in enclosed heating units,
by minimizing the quantity of reactants and the reaction conditions the reaction can
be controlled but can result in a slow release of heat and/or a modest temperature
rise. However, in certain applications, it can be useful to rapidly heat a substrate
to temperatures in excess of 200 °C within 1 second or less. Such rapid intense thermal
pulses can be useful for vaporizing pharmaceutical compositions to produce aerosols.
A rapid intense thermal pulse can be produced using an exothermic oxidation-reduction
reaction and in particular a thermite reaction involving a metal and a metal-containing
oxidizing agent. Concomitant with the rapid generation of heat, there can be a rapid
generation of gaseous products and unreacted reactants with high translational energies.
When sealed within an enclosure, the exothermic oxidation-reduction reaction can generate
a significant increase in pressure.
[0074] Energy produced by the exothermic reaction, whether thermal, optical, mechanical,
e.g. particle ejection, or chemical can generate a significant pressure when contained
with a sealed enclosure. In certain embodiments, a solid fuel capable of reacting
in an exothermic oxidation-reduction reaction can be used to form a heating unit.
For example, solid fuel as disclosed herein can be used to thermally vaporize a drug
coating to produce an aerosol of a drug for medical applications. In certain applications,
such as in portable medical devices, it can be useful to contain the pyrothermic materials
and products of the exothermic reaction and other chemical reactions resulting from
the high temperatures within the enclosure. While containing the exothermic reaction
can be accomplished by adequately sealing the enclosure to withstand the internal
pressures resulting from the burning of the solid fuel as well as an initiator composition
if present, it can be useful to minimize the internal pressure to ensure the safety
of the heating device and facilitate device fabrication.
[0075] The pressure within the substrate can increase during and after ignition and burning
of the initiator composition and the solid fuel. The increase in pressure can depend,
at least in part, on the amount and composition of the solid fuel, the relative amounts
of the fuel components, the density and/or degree of compaction of the solid fuel,
the particle size of the fuel components, the configuration of the substrate, the
amount of initiator, and/or the composition of the initiator. A solid fuel, an initiator
composition, and a substrate configuration can be selected to control the pressure
increase and maintain the maximum pressure within a useful operating range. The initiator
composition and solid fuel can produce gas phase reaction products during ignition
and burn. Thus, the pressure within the substrate can be managed by minimizing the
amount of initiator composition and solid fuel disposed within the heating unit. One
of skill can experimentally determine the minimum amount of initiator composition
needed to reliably ignite the solid fuel. One of skill can also determine the properties,
configuration, and placement of the solid fuel within a heating unit to achieve a
useful substrate temperature.
[0076] The internal pressure of a heating unit can be managed or reduced by constructing
the substrate, backing, and any other internal components from materials that produce
minimal gas products at elevated temperatures. Pressure can be managed or reduced
by providing an interior volume wherein gas can be collected and/or vented when the
initiator and solid fuel are burned. The interior volume can include a porous or fibrous
material having a high surface area and a large interstitial volume. The interstitial
volume can contain a gas generated as a result of the initiator and solid fuel reactions
and can thereby reduce the pressure within the enclosure and collisions of the reactants
and reaction products with the matrix of the porous or fibrous material can efficiently
transfer the internal and translational energy.
[0077] The internal pressure of a heating unit during and after burning of an initiator
composition and a solid fuel can vary depending on the parameters discussed above.
The internal pressure of heating units was measured using the fixture illustrated
in
Fig. 3. As shown in
Fig. 3, heating unit
300 comprises a substantially-cylindrically shaped substrate
302 having a closed nose portion
304 and an open receiving end
306. A backing member
308 is disposed within the interior region of substrate
302. Backing member
308 is cylindrical in shape but of overall smaller dimensions than that of substrate
302. Tapered nose portion
310 defines an opening
312 in backing member
308. Opposing end
314 from tapered nose portion
310 of backing member
308 is open. The interior surface of substrate
302 and the exterior surface of backing member
308 define an annular shell or a gap into which a solid fuel
316 can be disposed. A plug
320 is sized for insertion into open receiving end
306 of substrate
302 and is securely sealed by an O-ring
322. Electrodes
324 in contact with an initiator composition (not shown) disposed within heating unit
300 extend through plug
320 for electrical connection to a power source (not shown) external to heating unit
300. Pressure transducer
326 for measuring the steady state pressure via line
328 within heating unit
300 can be mounted on plug
320. A dynamic pressure transducer
330 can be provided for monitoring the pressure within heating unit
300 via line
332.
[0078] A heating unit equipped with two pressure transducers, as illustrated in
Fig. 3, was used to simultaneously measure the dynamic pressure and steady state pressure
within a heating unit of a type as shown in
Fig. 2. For dynamic pressure measurement, a high frequency shock wave/blast ICP pressure
sensor (PCB, model 113A24, maximum pressure = 7.0x10
6 Pa (1,000 psig)) combined with a line powered ICP signal conditioner (PCB, model
484B06) was used. For steady state pressure measurement, a subminiature millivolt
output type pressure transducer (Omega Engineering, model PX600-500GV, maximum pressure
= 3.5x10
6Pa (500 psig)) and a high performance strain gauge indicator with analog output (PCB,
DP41-S-A) were used. Signals generated by the pressure transducers were recorded and
stored using two oscilloscopes. To minimize the influence of pressure measurement
on the performance of the heating unit, the volume of lines
328 and
332 were designed so as not to exceed 2% of the total unfilled internal volume of the
heating unit. The measured internal pressure ranged from 7.9x10
5Pa to 2.3x10
6Pa (100 psig to 300 psig), and depended primarily on the compositions of the solid
fuel. The contribution of the initiator composition to the internal pressure was a
maximum 7.9x10
5Pa (100 psig).
[0079] Measurments of the peak internal pressure within sealed heating units, of a type
as shown in
Fig. 10, following ignition of a thin film layer of solid fuel comprising a metal reducing
agent and a metal-containing oxidizer are shown in
Fig. 17. The experimental arrangement used to generate the results shown in
Fig.17 is described in Example 2.
Fig. 17 shows that the peak pressure within a heating unit can range from 1.7x10
5Pa to 3.8x10
5Pa (10 psig to 40 psig) and correlates with the peak temperature of the exterior surface
of the substrate. Also, as shown in
Fig. 17, the peak pressure within the heating unit, as well as the peak temperature of the
substrate surface can for the particular heating units measure, depend on the composition
of the solid fuel, and the thickness of the foil substrate.
[0080] The internal pressure within a heating unit can also be managed or reduced by incorporating
materials capable of absorbing, adsorbing or reacting with gas phase reaction products.
The surface of the material may intrinsically be capable of absorbing. adsorbing or
reacting with the gaseous products, or can be coated or decorated with, for example,
elements, compounds and/or compositions. The immediate burst of pressure resulting
from the solid fuel burn can be reduced by locating an impulse absorbing material
and/or coating within the heating unit. A heating unit comprising an impulse absorbing
material is schematically illustrated in
Fig. 13.
[0081] Figs. 13A-C show a thermally conductive substrate
210, such as metal foil on which is disposed a coating of a solid fuel
212. Solid fuel
212 comprises a metal which is a reducing agent and a metal-containing oxidizing agent
capable of forming an oxidation-reduction reaction. In
Figs. 13A-
C thermally conductive substrate
210 is sealed using a sealant
220 to an enclosure
218 to form the heating unit. Sealant
220 can be an adhesive or any other methods for forming a seal, such as for example,
welding, soldering, fastening or crimping. An impulse absorbing material
214 is disposed between the interior surface of enclosure
218 and the interior surfaces of substrate
210 and the solid fuel
212. As shown in
Figs. 13A-C, impulse absorbing material fills the interior volume defined by the interior surfaces
of the heating unit. The impulse absorbing material can fill a portion of the interior
volume defined by the interior surfaces of the heating unit (not shown). The thickness
of the impulse absorbing material, e.g. the dimension between the interior surface
of solid fuel
212 and the interior surface of enclosure
218 can be any appropriate thickness to reduce the initial pressure impulse resulting
from the burning of solid fuel
212 to an appropriate level. The appropriate thickness can vary at least in part on the
amount of solid fuel, the solid fuel composition, and/or the physical characteristics
of the impulse absorbing material such as porosity, density, and composition and the
maximum acceptable pressure within the enclosure. It will be appreciated that above
a certain thickness, additional impulse absorbing material can have limited effect
on reducing the peak pressure within the heating unit. The impulse absorbing material
can comprise one or more materials and one or more layers of impulse absorbing material.
In certain applications wherein multiple layers of impulse absorbing materials are
used, each layer can comprise the same or different material. In
Fig 13C, an element
216 overlays impulse absorbing material
214. Element
216 can be the same or a different impulse absorbing material, and can include a getter.
Fig 13B illustrates a cross-sectional view of a cylindrical heating unit comprising a substrate
210, a layer of solid fuel
212, and a central region filled with an impulse absorbing material
214.
[0082] The impulse absorbing material can comprise a material which can absorb the thermal
and translational energy of the reactants and reaction products produced during burning
of the solid fuel, and if present, an initiator composition. An initiator composition
comprising, for example, any of the initiator compositions disclosed herein, can be
incorporated into the sealed heating unit to initiate the self-sustaining exothermic
reaction of the solid fuel. An impulse absorbing material can present a high surface
area to absorb the pressure impulse of thermally and translationally hot molecules
and which does not react at the temperatures reached within the heating unit during
and following the burn of the solid fuel. Examples of such materials include porous
materials such as ceramic membranes, and fibrous materials such as fiber mats. Hot
molecules physically and/or thermally ejected from the burning solid fuel can pass
through the interstitial spaces defined by porous or fibrous matrix to access a large
surface area, which upon collision, can facilitate transfer of thermal and translational
energy to the matrix of the impulse absorbing material, thereby reducing the peak
pressure within the heating unit.
[0083] Examples of porous membranes include, but are not limited to ceramic membranes, fluorocarbon
membranes, alumina membranes, polymer membrane and membranes formed from sintered
metal powders. Examples of fibrous materials include, but are not limited to, glass,
silica, carbon, graphite, metals, and high temperature resistant polymers. Sponge
materials can also be used. The porosity and density of the impulse absorbing material
can be selected to reduce the peak pressure by an appropriate amount. For a given
amount of solid fuel, composition of solid fuel, and heating unit dimensions, the
appropriate porosity and density of the impulse absorbing material can be determined
empirically. It can be useful to have the pores sufficiently large to facilitate entry
of the thermally and translationally hot molecules to the interior of an impulse absorbing
material, or to one or more additional layers of impulse absorbing materials with
different porosity and/or composition to facilitate transfer of energy from the hot
molecules to the impulse absorbing material.
[0084] The effect of incorporating glass fiber mats on the internal pressure of a heating
unit is shown in
Fig. 14. Glass fiber mats were placed over a coating of solid fuel comprising an average mass
of 177 mg of 80% Zr: 20% MoO
3 disposed on a 0.01 cm (0.004 inch) thick stainless steel foil, and the pressure within
the enclosure measured following ignition of the solid fuel. Each glass fiber mat
was 0.1 cm (0.040 inches) thick. As shown in
Fig. 14, glass fiber mats significantly reduced the peak internal pressure of the heating
unit. When a single mat was used, the maximum pressure within the sealed enclosure
was 2.5x10
5Pa (22 psig) when two mats were used the maximum pressure was 1.9x10
5Pa (13 psig), and when 5 mats were used, the peak pressure was 1.6x10
5Pa (9 psig).
[0085] The ability of glass fiber mats to reduce the temperature within a heating unit is
shown in
Fig. 15. The same experimental arrangement as described for
Fig. 14 was used. The peak temperature measured between the solid fuel and the first mat
was about 515 °C and 325 °C, between the first and second mats was about 200°C and
180 °C, and between the second and third mats was less than 100 °C, thus demonstrating
that the internal and translational energy of the reactants and reaction products
is transferred to the impulse absorbing materials.
[0086] As demonstrated by the results shown in
Fig. 14, the residual pressure, e.g. the pressure 10 seconds or more after solid fuel ignition,
in the heating unit was insensitive to the presence of an impulse absorbing material.
Without being limited by theory, the residual pressure can be the result of gases
evolved and/or produced during the burning of the solid fuel. Possible gas sources
include hydrogen bonded to the metal reducing agent, and unreacted oxygen produced
during the oxidation reaction and unreacted gaseous intermediates. For example, oxygen
generated by the metal-containing oxidizing agent may not immediately react with the
metal reducing agent, but rather can proceed through several gaseous reaction intermediates.
[0087] The residual pressure within a heating unit can be reduced by including materials
capable of gettering the residual gaseous reaction products. Such materials can be
included with the impulse absorbing material, intrinsic to the impulse absorbing material,
and/or applied to the impulse absorbing material as a coating, deposit, layer, and
the like. The getter can be coated or deposited onto a support disposed within a heating
unit and/or on one or more interior surfaces of the heating unit.
[0088] Getters are materials capable of absorbing, adsorbing and/or reacting with gases
and can be used to improve and/or maintain a vacuum, and/or to purify gases. Absorption
refers to the process by which one material is retained by another, such as the attachment
of molecules of a gas or vapor to a solid surface by physical forces. Adsorption refers
to the increase in the concentration of a dissolved substance at the interface of
a condensed and a gaseous or liquid phase. Getters are used for example in the semiconductor
industry to reduce residual gases in high vacuum systems. In certain embodiments,
getters capable of removing hydrogen gas, H
2, and molecular oxygen, O
2, can include, but are not limited to, compositions including metals and nonmetals,
such as Ta, Zr, Tb, Ti, Al, Mg, Ba, Fe, and P. Examples of getters useful for removing
H
2 gas include, but are not limited to, sintered Zr/graphite powders, Zr/ Al compositions,
Zr/V/Fe, polymer-bound getters such as PdO/zeolite dispersed in a polymer matrix,
and polydiene hydrogenation catalyst compositions. Iron-based and polymeric getters
have been developed to absorb O
2. Carbon and/or graphite based materials can be used to adsorb and/or absorb H
2 and O
2. A getter can also adsorb, absorb and/or react with volatile intermediate products
or the unreacted reactants of the exothermic oxidation-reduction reaction such as,
for example, MoO
x, CO, CO
2, and N
2.
[0089] A getter can be applied to a substrate by any appropriate method. It can be useful
to provide a large surface area of getter to rapidly and efficiently reduce the residual
gas pressure. This can be accomplished, for example, by providing a getter formed
from a porous material, such as a sintered powder, or a fibrous material. The getter
can be applied to the surface of a porous or fibrous material.
[0090] Certain applications of heating units were used to examine the burn propagation speed
of the solid fuel following ignition. The burn propagation speed refers to the speed
of the burn front, which separates unburned and burned solid fuel regions. The burn
propagation speed can be determined at least in part by the solid fuel composition,
the particle size of the components of the solid fuel, the density or level of compaction
of the solid fuel, the shape and dimensions of the solid fuel, the material forming
the heating unit, and/or any internal components such as a backing member. The temporal
and spatial characteristics of the burn propagation speed for cylindrically-shaped
heating units were evaluated by monitoring the surface temperature of heating units
using an infrared thermal imaging camera (FLIR Systems, Thermacam SC3000).
[0091] Thermal images of a cylindrically-shaped heating unit measured by infrared thermal
imaging as a function of time, in milliseconds, are shown in
Figs. 4A-4F. The construction of the heating unit used to produce the thermal images is provided
in Example 3. The substrate was 1.5 cm in diameter and 4.5 cm in length In
Figs. 4A-4F, two images are shown in each panel. In both images, white areas in color correspond
to a surface temperature of 500 °C and black areas correspond to a surface temperature
of 25 °C. The top image corresponds to a front view of the heating unit and the lower
image corresponds to a rear view of the heating unit, which was obtained from a reflection
in a mirror mounted behind the unit.
Fig. 4A shows the extent of the self-propagating wave of ignited solid fuel 100 milliseconds
after ignition.
Figs. 4B-4E, taken at 200, 300, 400, and 500 milliseconds after ignition, respectively, show that
the wave of ignited fuel continued to propagate along the axial direction of the heating
unit. The image shown in
Fig. 4F was taken at 600 milliseconds after ignition, at which time the entire surface of
the substrate was heated, indicating that the solid fuel was consumed. The data gathered
from this and other studies using various solid fuel compositions and heating unit
configurations demonstrated that the burn propagation speed can range from 1.5 cm/sec
to 50 cm/sec. Thus, the speed at which heat is transferred to a substrate forming
the heating unit can be tailored as useful for certain applications.
[0092] In other studies, heating units as described in Examples 4A and 4B were fabricated
and the surface temperature uniformity was evaluated by infrared thermal imaging.
Heating units prepared for these studies differed from those used in the investigation
of burn propagation speed only in the mass ratio of metal and oxidizing agent used
to form the solid fuel. Thermal images taken 400 milliseconds after igniting the solid
fuel are shown in
Figs. 5A-5B. The image shown in
Fig. 5A corresponds to a heating unit comprising the solid fuel composition described in
Example 4A and the image in
Fig. 5B to a heating unit comprising the solid fuel composition described in Example 4B.
The dimensions of the heated area were 1.5 cm by 4.5 cm. The exterior substrate surface
of the heating unit used to produce the image shown in
Fig. 5B is more uniform than that of the heating unit shown in
Fig. 5A. The substrate surface temperature can be more uniform in heating units designed
for axial flame propagation. In certain applications, the substrate surface temperature
is considered uniformly heated if no more than 10% of the exterior surface exhibits
a temperature 50 °C to 100 °C less than the average temperature of the remaining 90%
of the exterior surface.
[0093] In certain embodiments, it can be useful that at least a portion of the exterior
surface of the substrate be heated to a uniform temperatures, and that the heated
portion be heated at a similar rate. Uniform heating of at least a portion of the
substrate can be facilitated by reducing the thermal mass of the substrate in the
region to be heated and/or by controlling the amount of solid fuel generating heat.
Uniform heating of the exterior surface of the substrate can be useful for vaporizing
a compound disposed on the exterior substrate surface in a short period of time to
form an aerosol comprising the vaporized compound having high yield and purity. As
an example, uniform heating of a 3.3cm by 3.3cm (1.3 inch by 1.3 inch) substrate area
can be achieved by applying a 0.0041 ± 0.00093cm (0.00163± 0.000368 inch) thick layer
of solid fuel onto a 0.01cm (0.004 inch) thick foil. Upon ignition, the surface of
the foil opposing the surface on which 0.18 g of the solid fuel is applied can reach
a maximum temperature of 440 °C over the 3.3cm by 3.3cm (1.3 inch by 1.3 inch) area
at 250 msec after ignition. As will be appreciated by one of skill in the art, the
fuel thickness selected will depend on the fuel composition, the foil thickness, and
the desired temperature.
[0094] Examples 5-7 provide heating units prepared and evaluated for pressure during burn,
burn propagation speed, and substrate temperature uniformity. The heating unit described
in Example 5 was comprised of a solid fuel composition of Zr, MoO
3, KClO
3, nitrocellulose, and diatomaceous earth. After remote ignition of the solid fuel
from the tip of the heating unit (opening
312 in
Fig. 3), the internal pressure increased to 150 psig during the burn period of 0.3 seconds.
One minute after burn, the residual pressure was under 5.2x10
5Pa (60 psig). The burn propagation speed was measured by infrared thermal imaging
to be 13 cm/sec. With respect to surface temperature uniformity, no obvious cold spots
were observed. (A cold spot, for purposes of Examples 5-7 herein, is defined as a
portion of the surface exhibiting a temperature which is 50 °C to 100 °C less than
the average temperature of the remaining 90% of the exterior surface.)
[0095] The heating unit prepared as described in Example 6 contained a solid fuel composition
comprised of Zr, MoO
3, and nitrocellulose. The gap or annular shell between the substrate and backing member
was 0.05cm (0.020 inches). The external surface of the backing member was coated with
initiator composition to increase the burn propagation speed. The solid fuel was remotely
ignited from the tip of the heating unit (opening
312 in
Fig. 3). The internal pressure increased to 1.45x10
6Pa (200 psig) during the reaction period of 0.25 seconds, and the residual pressure
was under 5.2x10
5Pa (60 psig). The burn propagation speed was 15 cm/sec. With respect to surface temperature
uniformity, no obvious cold spots were observed.
[0096] The heating unit prepared as described in Example 7 contained a solid fuel composition
of Al, MoO
3, and nitrocellulose. The solid fuel was placed in a 0.05 cm (0.020-inch) annular
shell gap between the substrate and the backing member. The solid fuel was directly
ignited near the plug. The internal pressure increased to 2.17x10
6Pa (300 psig) during the reaction period of less than 5 milliseconds. The residual
pressure was under 5.2x10
5Pa (60 psig). The exterior surface of the substrate was uniformly heated, with between
5 percent to 10 percent of the exterior surface exhibiting a temperature 50 °C to
100 °C less than that of the remaining exterior surface.
DRUG SUPPLY UNIT
[0097] Certain arrangements include a drug supply unit comprising, a heating unit as described
herein. A drug supply unit can be used in a drug delivery device where a drug is to
be thermally vaporized and then condensed for administration to a user. The drug condensate
can be administered by inhalation, nasal ingestion, or topically. Drug refers to any
compound for therapeutic use or non-therapeutic use, including therapeutic agents
and substances, Therapeutic agent refers to any compound for use in the diagnosis,
cure, mitigation, treatment, or prevention of disease, and any compound used in the
mitigation or treatment of symptoms of disease. Whereas, substances refer to compounds
used for a non-therapeuttc use, typically for a recreational or experimental purpose.
[0098] Figs. 6A-6C schematically illustrate cross-sectional views of a drug supply unit
100 comprising a heating unit similar to that described in
Fig. 2B. More specifically,
Figs. 6A-6C illustrate a drug supply unit
100 having a film of drug disposed on the exterior substrate surface
(Fig. 6A); ignition of the heating unit
(Fig. 6B); and generation of a wave of heat effective to vaporize the drug film
(Fig. 6C). With initial reference to
Fig. 6A, drug supply unit
100 comprises a heating unit
102, similar to that described in
Fig. 2B. In
Figs. 6A-B, a substantially cyllindrically-shaped, heat-conductive substrate
104 has an exterior surface
106 and an interior surface
108, which define an inner region
112. A film
110 of drug can be disposed on all or a portion of exterior surface
106.
[0099] Film
110 can be applied to exterior substrate surface
106 by any appropriate method and can depend at least in part on the physical properties
of the drug and the final thickness of the film. Methods of applying a drug to the
exterior substrate surface include, but are not limited to, brushing dip coating,
spray coating, screen printing, roller coating, inkjet printing, vapor-phase deposition,
spin coating, and the like. The drug can be prepared as a solution comprising at least
one solvent and applied to the exterior surface. A solvent can comprise a volatile
solvent such as, for example, but not limitation, acetone or isopropanol. The drug
can be applied to the exterior surface of the substrate as a melt. The drug can be
applied to a support having a release coating and transferred to a substrate from
the support. For drugs that are liquid at room temperature, thickening agents can
be admixed with the drug to produce a viscous composition comprising the drug that
can be applied to the exterior substrate surface by any appropriate method, including
those described herein. A film of compound can be formed during a single application
or can be formed during repeated applications to increase the final thickness of the
film. The final thickness of a film of drug disposed on the exterior substrate surface
can be less than 50 µm, less than 20 µm and less than 10 µm, the film thickness can
range from 0.02 µm to 20 µm, and can range from 0.1 µm to 10 µm.
[0100] The film can comprise a therapeutically effective amount of at least one drug. Therapeutically
effective amount refers to an amount sufficient to affect treatment when administered
to a patient or user in need of treatment. Treating or treatment of any disease, condition,
or disorder refers to arresting or ameliorating a disease, condition or disorder,
reducing the risk of acquiring a disease, condition or disorder, reducing the development
of a disease, condition or disorder or at least one of the clinical symptoms of the
disease, condition or disorder, or reducing the risk of developing a disease, condition
or disorder or at least one of the clinical symptoms of a disease or disorder. Treating
or treatment also refers to inhibiting the disease, condition or disorder, either
physically, e.g. stabilization of a discernible symptom, physiologically, e.g., stabilization
of a physical parameter, or both, and inhibiting at least one physical parameter that
may not be discernible to the patient. Further, treating or treatment refers to delaying
the onset of the disease, condition or disorder or at least symptoms thereof in a
patient which may be exposed to or predisposed to a disease, condition or disorder
even though that patient does not yet experience or display symptoms of the disease,
condition or disorder. In certain embodiments, the drug film can comprise one or more
pharmaceutically acceptable carriers, adjuvants, and/or excipients. Pharmaceutically
acceptable refers to approved or approvable by a regulatory agency of the Federal
or a state government or listed in the U.S Pharmacopoeia or other generally recognized
pharmacopoeia for use in animals, and more particularly in humans.
[0101] As shown in
FIGS. 6A-6C, substrate
104 of drug supply unit
100 can define an inner region
112 in which a solid fuel
114 can be disposed. As shown, solid fuel
114 can be disposed as an annular shell defined by interior substrate surface
108 and an inner, cylindrical backing member
118. A first initiator composition
120 can be located at one end of cylindrical backing member
118 and a second initiator composition
122 can be located at the opposing end of cylindrical backing member
118. First initiator composition
120 can be in physical contact with an electrically resistive heating element via electrical
leads
124,
126 to a power source (not shown).
[0102] As shown in
Figs. 6B, application of an electrical current provided by a power source (not shown) to leads
124,
126 can cause initiator composition
120 to produce sparks, such as sparks
128,
130 that can be directed toward second initiator composition
122. Ignition of second initiator composition
122 can ignite solid fuel
114 in the region indicated by arrows
132,
134. Igniting solid fuel
114 in the region indicated by arrows
132,
134 effectuates a self-propagating wave of burning solid fuel, as schematically illustrated
in
Fig. 6C. In
Fig. 6C, the self-propagating burn is indicated by arrows
136,
138,
140,
142 with the solid fuel burn propagating from the point of ignition through the solid
fuel. As the solid fuel burns, heat can be produced that can be conducted through
substrate
104 causing vaporization of drug film
110 disposed on external substrate surface
106. In
Fig. 6C, thermally vaporized drug is illustrated as the "cloud" of drug
144. As illustrated in
Fig. 6C, vaporization of the drug occurs in the direction of arrows
136,
138,
140,
142, where the film nearest the ignition point of the solid fuel is vaporized first,
followed by vaporization in regions along the length of drug supply unit
100. As shown in
Fig. 6C, thermally vaporized drug
144 is illustrated at the tapered region of drug supply unit
100, and drug film not yet vaporized from the exterior surface
106 is illustrated at point
110.
[0103] Figs. 7A-7E represent high-speed photographs showing the thermal generation of a vapor from a
drug supply unit similar to that described in
Figs. 6A-6C.
Fig. 7A shows a heat-conductive substrate 4 cm in length coated with a 3 µm to 5 µm thick
film of the therapeutic agent alprazolam. The drug-coated substrate was placed in
a chamber through which a stream of air was flowing in an upstream-to-downstream direction,
indicated by the arrow in
Fig. 7A, at a rate of 15 L/min. Solid fuel contained in the heating unit was ignited to heat
the substrate. The progression of drug vaporization from the exterior surface of the
drug supply unit was monitored using real-time photography.
Figs. 7B-7E show the sequence of thermal vaporization at time intervals of 150 msec, 250 msec,
500 msec, and 1,000 msec, following ignition of an initiator composition, respectively.
The cloud of thermal vapor formed from the drug film is visible in the photographs.
Complete vaporization of the drug film was achieved in less than 1,000 msec.
[0104] The drug supply unit is configured such that the solid fuel heats a portion of the
exterior surface of the substrate to a temperature sufficient to thermally vaporize
the drug within at least 3 seconds following ignition of the solid fuel, within 1
second following ignition of the solid fuel, within 800 milliseconds following ignition
of the solid fuel, within 500 milliseconds following ignition of the solid fuel, or
within 250 milliseconds following ignition of the solid fuel.
[0105] A drug supply unit can generate an aerosol comprising a drug that can be inhaled
directly by a user and/or can be mixed with a delivery vehicle, such as a gas, to
produce a stream for delivery, e.g., via a spray nozzle, to a topical site for a variety
of treatment regimens, including acute or chronic treatment of a skin condition, administration
of a drug to an incision site during surgery, or to an open wound.
[0106] Rapid vaporization of a drug film can occur with minimal thermal decomposition of
the drug. For example less than 10% of the drug is decomposed during thermal vaporization,
or less than 5% of the drug is decomposed during thermal vaporization. A drug can
undergo a phase transition to a liquid state and then to a gaseous state, or can sublime,
i.e., pass directly from a solid state to a gaseous state. A drug can include a pharmaceutical
compound. The drug can comprise a therapeutic compound or a non-therapeutic compound.
A non-therapeutic compound refers to a compound that can be used for recreational,
experimental, or pre-clinical purposes. Classes of drugs that can be used include,
but are not limited to, anesthetics, anticonvulsants, antidepressants, antidiabetic
agents, antidotes, antiemetics, antihistamines, anti-infective agents, antineoplastics,
antiparkisonian drugs, antirheumatic agents, antipsychotics, anxiolytics, appetite
stimulants and suppressants, blood modifiers, cardiovascular agents, central nervous
system stimulants, drugs for Alzheimer's disease management, drugs for cystic fibrosis
management, diagnostics, dietary supplements, drugs for erectile dysfunction, gastrointestinal
agents, hormones, drugs for the treatment of alcoholism, drugs for the treatment of
addiction, immunosuppressives, mast cell stabilizers, migraine preparations, motion
sickness products, drugs for multiple sclerosis management, muscle relaxants, nonsteroidal
anti-inflammatories, opioids, other analgesics and stimulants, opthalmic preparations,
osteoporosis preparations, prostaglandins, respiratory agents, sedatives and hypnotics,
skin and mucous membrane agents, smoking cessation aids, Tourette's syndrome agents,
urinary tract agents, and vertigo agents.
[0107] Examples of anesthetic include ketamine and lidocaine.
[0108] Examples of anticonvulsants include compounds from one of the following classes:
GABA analogs, tiagabine, vigabatrin; barbiturates such as pentobarbital; benzodiazepines
such as clonazepam; hydantoins such as phenytoin; phenyltriazines such as lamotrigine;
miscellaneous anticonvulsants such as carbamazepine, topiramate, valproic acid, and
zonisamide.
[0109] Examples of antidepressants include amitriptyline, amoxapine, benmoxine, butriptyline,
clomipramine, desipramine, dosulepin, doxepin, imipramine, kitanserin, lofepramine,
medifoxamine, mianserin, maprotoline, mirtazapine, nortriptyline, protriptyline, trimipramine,
venlafaxine, viloxazine, citalopram, cotinine, duloxetine, fluoxetine, fluvoxamine,
milnacipran, nisoxetine, paroxetine, reboxetine, sertraline, tianeptine, acetaphenazine,
binedaline, brofaromine, cericlamine, clovoxamine, iproniazid, isocarboxazid, moclobemide,
phenyhydrazine, phenelzine, selegiline, sibutramine, tranylcypromine, ademetionine,
adrafinil, amesergide, amisulpride, amperozide, benactyzine, bupropion, caroxazone,
gepirone, idazoxan, metralindole, milnacipran, minaprine, nefazodone, nomifensine,
ritanserin, roxindole, S-adenosylmethionine, escitalopram, tofenacin, trazodone, tryptophan,
and zalospirone.
[0110] Examples of antidiabetic agents include pioglitazone, rosiglitazone, and troglitazone.
[0111] Examples of antidotes include edrophonium chloride, flumazenil, deferoxamine, nalmefene,
naloxone, and naltrexone.
[0112] Examples of antiemetics include alizapride, azasetron, benzquinamide, bromopride,
buclizine, chlorpromazine, cinnarizine, clebopride, cyclizine, diphenhydramine, diphenidol,
dolasetron, droperidol, granisetron, hyoscine, lorazepam, dronabinol, metoclopramide,
metopimazine, ondansetron, perphenazine, promethazine, prochlorperazine, scopolamine,
triethylperazine, trifluoperazine, triflupromazine, trimethobenzamide, tropisetron,
domperidone, and palonosetron.
[0113] Examples of antihistamines include astemizole, azatadine, brompheniramine, carbinoxamine,
cetrizine, chlorpheniramine, cinnarizine, clemastine, cyproheptadine, dexmedetomidine,
diphenhydramine, doxylamine, fexofenadine, hydroxyzine, loratidine, promethazine,
pyrilamine and terfenidine.
[0114] Examples of anti-infective agent include compounds selected from one of the following
classes: antivirals such as efavirenz; AIDS adjunct agents such as dapsone; aminoglycosides
such as tobramycin; antifungals such as fluconazole; antimalarial agents such as quinine;
antituberculosis agents such as ethambutol; β-lactams such as cefmetazole, cefazolin,
cephalexin, cefoperazone, cefoxitin, cephacetrile, cephaloglycin, cephaloridine; cephalosporins,
such as cephalosporin C, cephalothin; cephamycins such as cephamycin A, cephamycin
B, and cephamycin C, cephapirin, cephradine; leprostatics such as clofazimine; penicillins
such as ampicillin, amoxicillin, hetacillin, carfecillin, carindacillin, carbenicillin,
amylpenicillin, azidocillin, benzylpenicillin, clometocillin, cloxacillin, cyclacillin,
methicillin, nafcillin, 2-pentenylpenicillin, penicillin N, penicillin O, penicillin
S, penicillin V, dicloxacillin; diphenicillin; heptylpenicillin; and metampicillin;
quinolones such as ciprofloxacin, clinafloxacin, difloxacin, grepafloxacin, norfloxacin,
ofloxacine, temafloxacin; tetracyclines such as doxycycline and oxytetracycline; miscellaneous
anti-infectives such as linezolide, trimethoprim and sulfamethoxazole.
[0115] Examples of anti-neoplastic agents include droloxifene, tamoxifen, and toremifene.
[0116] Examples of antiparkisonian drugs include amantadine, baclofen, biperiden, benztropine,
orphenadrine, procyclidine, trihexyphenidyl, levodopa, carbidopa, andropinirole, apomorphine,
benserazide, bromocriptine, budipine, cabergoline, eliprodil, eptastigmine, ergoline,
galanthamine, lazabemide, lisuride, mazindol, memantine, mofegiline, pergolide, piribedil,
pramipexole, propentofylline, rasagiline, remacemide, ropinerole, selegiline, spheramine,
terguride, entacapone, and tolcapone.
[0117] Examples of antirheumatic agents include diclofenac, hydroxychloroquine and methotrexate.
[0118] Examples of antipsychotics include acetophenazine, alizapride, amisulpride, amoxapine,
amperozide, aripiprazole, benperidol, benzquinamide, bromperidol, buramate, butaclamol,
butaperazine, carphenazine, carpipramine, chlorpromazine, chlorprothixene, clocapramine,
clomacran, clopenthixol, clospirazine, clothiapine, clozapine, cyamemazine, droperidol,
flupenthixol, fluphenazine, fluspirilene, haloperidol, loxapine, melperone, mesoridazine,
metofenazate, molindrone, olanzapine, penfluridol, pericyazine, perphenazine, pimozide,
pipamerone, piperacetazine, pipotiazine, prochlorperazine, promazine, quetiapine,
remoxipride, risperidone, sertindole, spiperone, sulpiride, thioridazine, thiothixene,
trifluperidol, triflupromazine, trifluoperazine, ziprasidone, zotepine, and zuclopenthixol.
[0119] Examples of anxiolytics include alprazolam, bromazepam, oxazepam, buspirone, hydroxyzine,
mecloqualone, medetomidine, metomidate, adinazolam, chlordiazepoxide, clobenzepam,
flurazepam, lorazepam, loprazolam, midazolam, alpidem, alseroxlon, amphenidone, azacyclonol,
bromisovalum, captodiamine, capuride, carbcloral, carbromal, chloral betaine, enciprazine,
flesinoxan, ipsapiraone, lesopitron, loxapine, methaqualone, methprylon, propanolol,
tandospirone, trazadone, zopiclone, and zolpidem.
[0120] An example of an appetite stimulant is dronabinol.
[0121] Examples of appetite suppressants include fenfluramine, phentermine and sibutramine.
[0122] Examples of blood modifiers include cilostazol and dipyridamol.
[0123] Examples of cardiovascular agents include benazepril, captopril, enalapril, quinapril,
ramipril, doxazosin, prazosin, clonidine, labetolol, candesartan, irbesartan, losartan,
telmisartan, valsartan, disopyramide, flecanide, mexiletine, procainamide, propafenone,
quinidine, tocainide, amiodarone, dofetilide, ibutilide, adenosine, gemfibrozil, lovastatin,
acebutalol, atenolol, bisoprolol, esmolol, metoprolol, nadolol, pindolol, propranolol,
sotalol, diltiazem, nifedipine, verapamil, spironolactone, bumetanide, ethacrynic
acid, furosemide, torsemide, amiloride, triamterene, and metolazone.
[0124] Examples of central nervous system stimulants include amphetamine, brucine, caffeine,
dexfenfluramine, dextroamphetamine, ephedrine, fenfluramine, mazindol, methyphenidate,
pemoline, phentermine, sibutramine, and modafinil.
[0125] Examples of drugs for Alzheimer's disease management include donepezil, galanthamine
and tacrin.
[0126] Examples of drugs for cystic fibrosis management include CPX, IBMX, XAC and analogues;
4-phenylbutyric acid; genistein and analogous isoflavones; and milrinone.
[0127] Examples of diagnostic agents include adenosine and aminohippuric acid.
[0128] Examples of dietary supplements include melatonin and vitamin-E.
[0129] Examples of drugs for erectile dysfunction include tadalafil, sildenafil, vardenafil,
apomorphine, apomorphine diacetate, phentolamine, and yohimbine.
[0130] Examples of gastrointestinal agents include loperamide, atropine, hyoscyamine, famotidine,
lansoprazole, omeprazole, and rebeprazole.
[0131] Examples of hormones include: testosterone, estradiol, and cortisone.
[0132] Examples of drugs for the treatment of alcoholism include naloxone, naltrexone, and
disulfiram.
[0133] Examples of drugs for the treatment of addiction it is buprenorphine.
[0134] Examples of immunosupressives includemycophenolic acid, cyclosporin, azathioprine,
tacrolimus, and rapamycin.
[0135] Examples of mast cell stabilizers include cromolyn, pemirolast, and nedocromil.
[0136] Examples of drugs for migraine headache include almotriptan, alperopride, codeine,
dihydroergotamine, ergotamine, eletriptan, frovatriptan, isometheptene, lidocaine,
lisuride, metoclopramide, naratriptan, oxycodone, propoxyphene, rizatriptan, sumatriptan,
tolfenamic acid, zolmitriptan, amitriptyline, atenolol, clonidine, cyproheptadine,
diltiazem, doxepin, fluoxetine, lisinopril, methysergide, metoprolol, nadolol, nortriptyline,
paroxetine, pizotifen, pizotyline, propanolol, protriptyline, sertraline, timolol,
and verapamil.
[0137] Examples of motion sickness products include diphenhydramine, promethazine, and scopolamine.
[0138] Examples of drugs for multiple sclerosis management include bencyclane, methylprednisolone,
mitoxantrone, and prednisolone.
[0139] Examples of muscle relaxants include baclofen, chlorzoxazone, cyclobenzaprine, methocarbamol,
orphenadrine, quinine, and tizanidine.
[0140] Examples of nonsteroidal anti-inflammatory drugs include aceclofenac, acetaminophen,
alminoprofen, amfenac, aminopropylon, amixetrine, aspirin, benoxaprofen, bromfenac,
bufexamac, carprofen, celecoxib, choline, salicylate, cinchophen, cinmetacin, clopriac,
clometacin, diclofenac, diflunisal, etodolac, fenoprofen, flurbiprofen, ibuprofen,
indomethacin, indoprofen, ketoprofen, ketorolac, mazipredone, meclofenamate, nabumetone,
naproxen, parecoxib, piroxicam, pirprofen, rofecoxib, sulindac, tolfenamate, tolmetin,
and valdecoxib.
[0141] Examples of opioid drugs include alfentanil, allylprodine, alphaprodine, anileridine,
benzylmorphine, bezitramide, buprenorphine, butorphanol, carbiphene, cipramadol, clonitazene,
codeine, dextromoramide, dextropropoxyphene, diamorphine, dihydrocodeine, diphenoxylate,
dipipanone, fentanyl, hydromorphone, L-alpha acetyl methadol, lofentanil, levorphanol,
meperidine, methadone, meptazinol, metopon, morphine, nalbuphine, nalorphine, oxycodone,
papaveretum, pethidine, pentazocine, phenazocine, remifentanil, sufentanil, and tramadol.
[0142] Examples of other analgesic drugs include apazone, benzpiperylon, benzydramine, caffeine,
clonixin, ethoheptazine, flupirtine, nefopam, orphenadrine, propacetamol, and propoxyphene.
[0143] Examples of opthalmic preparation drugs include ketotifen and betaxolol.
[0144] Examples of osteoporosis preparation drugs alendronate, estradiol, estropitate, risedronate
and raloxifene.
[0145] Examples of prostaglandin drugs include epoprostanol, dinoprostone, misoprostol,
and alprostadil.
[0146] Examples of respiratory agents include albuterol, ephedrine, epinephrine, fomoterol,
metaproterenol, terbutaline, budesonide, ciclesonide, dexamethasone, flunisolide,
fluticasone propionate, triamcinolone acetonide, ipratropium bromide, pseudoephedrine,
theophylline, montelukast, zafirlukast, ambrisentan, bosentan, enrasentan, sitaxsentan,
tezosentan, iloprost, treprostinil, and pirfenidone
[0147] Examples of sedative and hypnotic drugs include butalbital, chlordiazepoxide, diazepam,
estazolam, flunitrazepam, flurazepam, lorazepam, midazolam, temazepam, triazolam,
zaleplon, zolpidem, and zopiclone.
[0148] Examples of skin and mucous membrane agents include isotretinoin, bergapten and methoxsalen.
[0149] Examples of smoking cessation aids include nicotine and varenicline.
[0150] An example of a Tourette's syndrome agent includes pimozide.
[0151] Examples of urinary tract agents include tolteridine, darifenicin, propantheline
bromide, and oxybutynin.
[0152] Examples of vertigo agents include betahistine and meclizine.
[0153] A drug can further comprise substances to enhance, modulate and/or control release,
aerosol formation, intrapulmonary delivery, therapeutic efficacy, therapeutic potency,
stability, and the like. For example, to enhance therapeutic efficacy a drug can be
co-administered with one or more active agents to increase the absorption or diffusion
of the first drug through the pulmonary alveoli, or to inhibit degradation of the
drug in the systemic circulation. A drug can be co-administered with active agents
having pharmacological effects that enhance the therapeutic efficacy of the drug.
A drug can comprise compounds that can be used in the treatment of one or more diseases,
conditions, or disorders. A drug can comprise more than one compound for treating
one disease, condition, or disorder, or for treating more than one disease, condition,
or disorder.
THIN FILM DRUG SUPPLY UNIT
[0154] A thin film drug supply unit is illustrated in
Figs. 10A-
10B.
Fig. 10A illustrates a perspective view, and
Fig. 10B an assembly view of a thin film drug supply unit
500. Thin film drug supply unit
500 comprises, as shown in
Fig. 10B, a thin film heating unit
530 on which is disposed a drug
514 to be thermally vaporized. As shown in
Fig.10A, thin film heating unit
530 comprises a first and a second substrate
510, and a spacer
518.
[0155] As shown, first and second substrates
510 include an area comprising solid fuel
512 disposed on the interior surface, and an area comprising a drug
514 to be vaporized disposed on the exterior surface. First and second substrates
510 can comprise a thermally conductive material such as those described herein, including,
for example, metals, ceramics, and thermally conductive polymers. Substrates
510 can comprise a metal, such as, but not limited to, stainless steel, copper, aluminum,
and nickel or an alloy thereof. Substrates can have one or more layers, and the multiple
layers can comprise different materials. For example, a substrate can comprise multiple
layers of laminated metal foils, and/or can comprise thin films of one or more materials
deposited on the surface. The multiple layers can be used for example to determine
the thermal properties of the substrate and/or can be used to determine the reactivity
of the surface with respect to a compound disposed on the exterior surface. A multilayer
substrate can have regions comprising different materials. The thickness of substrates
510 can be thin to facilitate heat transfer from the interior to the exterior surface
and/or to minimize the thermal mass of the device. In certain embodiments, a thin
substrate can facilitate rapid and homogeneous heating of the exterior surface with
a lesser amount of solid fuel compared to a thicker substrate. Substate
510 can also provide structural support for solid fuel
512 and drug film
514. In certain embodiments, substrates
510 can comprise a metal foil. The thickness of substrates
510 can range from 0.00254 cm to 0.05 cm (0.001 inches to 0.020 inches), in certain embodiments
from 0.00254 cm to 0.0254 cm (0.001 inches to 0.010 inches) from 0.005 cm to 0.015
cm (0.002 inches to 0.006 inches), and from 0.005 cm to 0.0127 cm (0.002 inches to
0.005 inches). The use of lesser amounts of solid fuel can facilitate control of the
heating process as well as facilitate miniaturization of a drug supply unit.
[0156] The thickness of substrates
510 can vary across the surface. For example, a variable thickness can be useful for
controlling the temporal and spatial characteristics of heat transfer and/or to facilitate
sealing of the edges of substrates
510, for example, to spacer
518, opposing substrate
510, or to another support (not shown). In certain embodiments, substrates
510 can exhibit a homogeneous or nearly homogeneous thickness in the region of the substrate
on which solid fuel
512 and drug
514 are disposed to facilitate achieving a homogeneous temperature across that region
of the substrate on which the solid fuel is disposed. Homogeneous heating of the substrate
can facilitate the production of an aerosol comprising a high purity of a drug or
pharmaceutical composition and maximize the yield of drug initially deposited on the
substrate forming an aeresol.
[0157] Substrates
510 can comprise an area of solid fuel
512 disposed on the interior surface, e.g. the surface facing opposing substrate
510. An appropriate amount of solid fuel
512 can in part be determined by the thermal vaporization or sublimation temperature
of the drug, the amount of drug to be vaporized, the thickness and thermal conductivity
of the substrate, the composition of the solid fuel, and the temporal characteristics
of the intended thermal vaporization process. Solid fuel
512 can be applied to substrate
510 using any appropriate method. For example, solid fuel
512 can be applied to substrate
510 by brushing, dip coating, screen printing, roller coating, spray coating, inkjet
printing, stamping, spin coating, and the like. To facilitate processing, solid fuel
510 can comprise at least one additive material, and/or a solvent, as disclosed herein.
In certain embodiments, solid fuel
512 can be formed as a preformed sheet that can be cut to a specific dimension and subsequently
applied to substrate
510. The solid fuel can be applied to a support, and transferred to a substrate as a
preformed section. In this disclosure solid fuel
512 is applied to a portion of substrates
510 as a thin film or layer.
[0158] Solid fuel
512 can comprise a mixture of Zr/MoO
3, Zr/Fe
2O
3, Al/MoO
3, or Al/Fe
2O
3. In certain embodiments, the amount of metal which is a reducing agent can range
from 60 wt% to 90 wt%, and the amount of metal-containing oxidizing agent can range
from 40 wt% to 10 wt%. Higher ratios of metal reducing agent can cause the solid fuel
to burn slower and at a lower temperature, whereas lower ratios of metal reducing
agent can cause the solid fuel to burn faster and reach a higher maximum temperature.
Regardless of the weight percent ratios of the metal reducing agent and metal-containing
oxidizing agent, a solid fuel can comprise a stoichiometric amount of metal which
is a reducing agent and metal-containing oxidizing agent. For example, the balanced
Zr : Fe
2O
3 metal oxidation-reduction reaction can be written as:
3 Zr + 2 Fe
2O
3 → 3 ZrO
2 + 4 Fe
A stoichiometric amount of Zr : Fe
2O
3 for this reaction is 1 : 1.67 by weight.
[0159] Drug
514 can be disposed on the exterior surface of substrates
510. The amount of drug
514 disposed on the exterior surface of substrate
510 can be any appropriate amount. For example, the amount of drug
514 can be a therapeutically effective amount. A therapeutically effective amount can
be determined by the potency of the drug, the clinical indications, and the mode of
administration. Thin film drug supply unit can be configured to thermally vaporize
more than 95% of the drug, and in certain applications, greater than 98% of the drug,
with minimal degradation of the drug. The aerosol formed using a drug supply unit
can comprise greater than 90% of a drug applied to a substrate, and in certain applications
greater than 95% of a drug applied to a substrate. The yield and purity of the aerosol
can be controlled by and selected based on the temporal characteristics and magnitude
of the thermal impulse transferred to the compound.
[0160] The relationship of the yield and purity of an aerosol comprising a pharmaceutical
compound on the substrate temperature and mass of solid fuel for certain embodiments
is shown in
Fig. 18. Thin film drug supply units substantially as shown in
Figs. 10A and
10B, and described in Example 9 were used to produce the measurements shown in
Fig. 18. The experimental arrangement used to analyze the percent yield and percent purity
of the aerosol comprising a vaporized drug is described in Example 10. As shown in
Fig. 18, at substrate temperatures ranging from about 355° C to about 425° C, the percent
yield of drug forming the aerosol was greater than about 85% and the percent purity
was greater than about 90%. The percent yield refers to the ratio of the total solid
weight of the aerosol to the weight of the drug initially deposed on the substrate
times 100. Factors that can reduce the percent yield include incomplete vaporization
of the drug and redeposition of the drug on the substrate.
[0161] The percent purity, with respect to the aerosol purity, refers to the fraction of
drug composition in the aerosol/ the fraction of drug composition in the aerosol plus
drug degradation products times 100. Thus purity is relative with regard to the purity
of the starting material. For example, when the starting drug or drug composition
used for substrate coating contained detectable impurities, the reported purity of
the aerosol does not include those impurities present in the starting material that
were also found in the aerosol, e.g., in certain cases if the starting material contained
a 1% impurity and the aerosol was found to contain the identical 1% impurity, the
aerosol purity may nevertheless be reported as >99 % pure, reflecting the fact that
the detectable 1% purity was not produced during the vaporization-condensation aerosol
generation process.
[0162] Factors that can reduce the percent purity of the aerosol include degradation of
the drug during thermal vaporization. Depending at least in part on the composition
and thermal properties of a particular drug or pharmaceutical composition, the appropriate
thermal vaporization temperature to produce an aerosol comprising the particular drug
or pharmaceutical composition having high yield and purity can be determined as set
forth in
U.S. application Serial No. 10/718,982, filed November 20, 2003.
[0163] Drug
514 can be applied to substrate
510 using any appropriate method, such as for example, brushing, dip coating, screen
printing, roller coating, spray coating, inkjet printing, stamping, vapor deposition,
and the like. Drug
514 can also be applied to a support having a release layer and transferred to substrate
510. Drug
514 can be suspended in a volatile solvent such as, for example, but not limited to,
acetone or isopropanol to facilitate application. A volatile solvent can be removed
at room temperature or at elevated temperature, with or without application of a vacuum.
The solvent can comprise a pharmaceutically acceptable solvent. Residual solvent can
be reduced to a pharmaceutically acceptable level.
[0164] Drug
514 can be disposed on substrate
510 in any appropriate form such as a solid, viscous liquid, liquid, crystalline solid,
or powder. The film of drug can be crystallized after disposition on the substrate.
[0165] As shown in
Figs. 10A-10B, a drug supply unit can comprise an igniter
520. Igniter
520 can comprise an initiator composition
522 disposed on an electrically resistive heating element connected to electrical leads
disposed between two strips of insulating materials (not shown). The electrical leads
can be connected to a power source (not shown). Initiator composition
522 can comprise any of the initiator compositions or compositions described herein.
The ignition temperature of initiator composition can range from 200 °C to 500 °C.
The electrically resistive material can comprise a material capable of generating
heat when electrical current is applied. For example, the electrically resistive material
can be a metal such as nichrome, tungsten or graphite. An initiator composition can
be disposed on the surface of the electrically resistive material such that when the
electrically resistive material is heated to the ignition temperature of the initiator
composition, the initiator composition can ignite to produce sparks. An initiator
composition can be applied to the electrically resistive heating element by depositing
a slurry comprising the initiator composition and drying. An initiator composition
can be deposited on a solid fuel at a position such that when assembled, the initiator
composition forming the igniter is adjacent to the initiator composition deposited
on the solid fuel. Having initiator composition on at least a portion of the solid
fuel can increase the speed of ignition and the reliability of the ignition process.
[0166] The electrically resistive heating element can be connected to electrical conductors.
The heating element can be soldered or electrically connected to conductors, such
as, Cu conductors or graphite ink traces, disposed on an electrically insulating substrate,
such as a polyimide, polyester, or fluoropolymer. The conductors can be disposed between
two opposing layers of the electrically insulating material such as flexible or rigid
printed circuit board materials. The heating element on which an initiator composition
is disposed can be exposed through an opening in the end of ignition assembly
520.
[0167] Igniter
520 can be positioned with respect to solid fuel
512 such that sparks produced by initiator composition
522 can be directed toward solid fuel area
512, causing solid fuel
512 to ignite and burn. Initiator composition
522 can be located in any position such that sparks produced by the initiator can cause
solid fuel
512 to ignite. The location of initiator composition
522 with respect to solid fuel
512 can determine the direction in which solid fuel 5
12 burns. For example, initiator composition
522 can be located to cause solid fuel
512 to burn in any direction with respect to the airflow including in the same direction
of airflow, opposite the direction of airflow, or normal the direction of airflow.
The direction of solid fuel burn with respect to airflow can influence the average
particle diameter of particulates comprising the thermally vaporized drug forming
the aerosol. For example, solid fuel burn opposite the direction of airflow can produce
smaller diameter particles than when the direction of solid fuel burn is in the same
direction as the airflow. The dynamics of solid fuel burn can be influenced by other
parameters such as the spatial and temporal characteristics of the surface temperature,
and the extent to which vaporized drug is redeposited on the substrate and/or other
surfaces such as a housing in which the drug supply unit is incorporated.
[0168] Thin film drug supply unit
500 can comprise more than one igniter
520 and/or each igniter
520 can comprise more than one initiator composition
522.
[0169] It can be useful to minimize the amount of initiator composition used, so as to reduce
the amount of gas and other reaction products potentially generated by the initiator
composition during burn.
[0170] Igniter
520 can comprise a mechanism configured to direct transmitted radiation to an initiator
composition capable of absorbing and being heated by the transmitted radiation, to
produce sparks. For example, the radiation can be infrared, visible, or ultraviolet
radiation such as produced by a diode laser, light emitting diode, or flashlamp. Radiation
produced by a radiation source can be transmitted through a waveguide such as an optical
fiber, and directed to an initiator or the radiation source can be incorporated into
the ignition assembly
522 with electrical conductors for connecting to an external power source. The transmission
device can include elements such as lenses for focusing the transmitted radiation
onto the initiator composition. The radiation can be directed to an initiator composition
disposed within the heating unit through a window. The transmitted radiation can be
directed onto an absorber or a material capable of absorbing the radiation, which
can be the initiator composition, or an element on which the initiator composition
is disposed. The initiator composition can comprise at least one metal such as, but
not limited to, zirconium, titanium, or aluminum, and at least one solid oxidizer
such as, but not limited to, MoO
3, KClO
4, CuO, or WO
3. The initiator composition can comprise any of those disclosed herein.
[0171] As shown in
Fig 10A, thin film drug supply unit
500 can have a spacer
518. Spacer
518 can retain igniter
520. Spacer
518 can provide a volume or space within the interior of thin film heating unit
500 to collect gases and byproducts generated during the burn of the initiator composition
522 and solid fuel
512. The volume produced by spacer
518 can reduce the internal pressure within thin film drug supply unit
500 upon ignition of the fuel. The volume can comprise a porous or fibrous material such
as a ceramic, or fiber mat in which the solid matrix component is a small fraction
of the unfilled volume. The porous or fibrous material can provide a high surface
area on which reaction products generated during the burning of the initiator composition
and the solid fuel can be absorbed, adsorbed or reacted. The pressure produced during
burn can in part depend on the composition and amount of initiator composition and
solid fuel used. The spacer can be less than 0.7 cm (0.3 inches) thick or less than
0.5 cm (0.2 inches) thick. The maximum internal pressure during and following burn
can be less than 3,5.10
5 Pa (50 psig), less than 1,4.10
5 Pa (20 psig), less than 0,7.10
5 Pa (10 psig), or less than 0,4.10
5 Pa (6 psig). The spacer can be a material capable of maintaining structural and chemical
properties at the temperatures produced by the solid fuel burn. The spacer can be
a material capable of maintaining structure and chemical properties up to a temperature
of about 100°C. It can be useful that the material forming the spacer not produce
and/or release or produce only a minimal amount of gases and/or reaction products
at the temperatures to which it is exposed by the heating unit. Spacer
518 can comprise a metal, a thermoplastic, such as, for example, but not limitation,
a polyimide, fluoropolymer, polyetherimide, polyether ketone, polyether sulfone, polycarbonate,
other high temperature resistant thermoplastic polymers, or a thermoset, and which
can optionally include a filler.
[0172] Spacer
518 can comprise a thermal insulator such that the spacer does not contribute to the
thermal mass of the thin film drug supply unit thereby facilitating heat transfer
to the substrate on which drug
514 is disposed. Thermal insulators or impulse absorbing materials such as mats of glass,
silica, ceramic, carbon, or high temperature resistant polymer fibers can be used.
Spacer
518 can be a thermal conductor such that the spacer functions as a thermal shunt to control
the temperature of the substrate.
[0173] Substrates
510, spacer
518 and igniter
520 can be sealed. Sealing can retain any reactants and reaction products released by
burning of initiator composition
522 and solid fuel
514, as well as provide a self-contained unit. As shown in
Fig. 10A, substrates
510 can be sealed to spacer
518 using an adhesive
516. Adhesive
516 can be a heat sensitive film capable of bonding substrates
510 and spacer
518 upon the application of heat and pressure. Substrates
510 and spacer
518 can be bonded using an adhesive applied to at least one of the surfaces to be bonded,
the parts assembled, and the adhesive cured. The access in spacer
518 into which igniter
520 is inserted can also be sealed using an adhesive. Other methods for forming a seal
can be used such as for example, welding soldering, or fastening.
[0174] The elements forming the thin film drug supply unit
500 can be assembled and sealed using thermoplastic or thermoset molding methods such
as insert molding and transfer molding.
[0175] An appropriate sealing method can, at least in part be determined by the materials
forming substrate
510 and spacer
518. Drug supply unit
500 can be sealed to withstand a maximum pressure of less than 3,5.10
5 Pa (50 psig), less than 1,4.10
5 Pa (20 psig) or less than 0,7.10
5 Pa (10 psig) The materials used to form the seal can maintain structural integrity
at the temperature reached by the article. The materials used can exhibit minimal
degradation and produce minimal gaseous reaction products at the temperature reached
by the heating unit
MULTIDOSE DRUG SUPPLY UNITS
[0176] A drug supply unit can be configured for use in single-use devices or in multi-use
devices.
Figs. 9A-9B illustrate drug supply units configured for use in a drug delivery device designed
for multiple uses. As shown in
Fig. 9A, a tape
406 in the form of a spool or reel
400 comprises a plurality of drug supply units
402,
404. The plurality of drug supply units
402,
404 can comprise a heating unit on which is disposed a thin film of a drug to be thermally
vaporized. Each of the plurality of drug supply units
402,
404 can comprise the same features as those described herein, for example, in
Fig. 1A and/or
Fig. 1B. Tape
406 can comprise a plurality of heating units. Each heating unit can comprise a solid
fuel, an initiator composition, and a substrate.
[0177] Thin film drug supply units are schematically illustrated in
Figs. 11A-11B,
Figs. 11A-11B illustrate certain arrangements wherein the thin film drug supply units
600 are in the form of a tape
650 comprising multiple layers. As shown in
Fig. 11A, tape
650 comprises a first layer
601 having openings in which a drug to be thermally vaporized
610 is disposed. A second layer
602 underlying first layer
601 separates drug
610 from solid fuel
620 disposed within a third layer
603 underlying second layer
602. Second layer
602 can be thermally conductive such that heat can be efficiently transferred from solid
fuel
620 to compound
610. Second layer
602 can be any of the metals described herein. Regions comprising solid fuel
620 underlie regions comprising drug
610. The amount of solid fuel
620 can be an amount sufficient to thermally vaporize drug
610. The dimensions and geometry of the region comprising solid fuel
620 can be any appropriate dimension. Third layer
603 can comprise a volume
640 to collect reaction products generated during burn of solid fuel
620 and thereby reduce the pressure within thin film drug supply unit
600. Volume
640 can comprise a material capable of absorbing, adsorbing of reacting with reaction
products produced during burning of the solid, such as a porous ceramic or fibrous
material. Third layer
603 can comprise a material in which the mechanical properties are substantially maintained
and which will not appreciably chemically degrade up to the temperatures reached by
the drug supply unit
600. Third layer
603 can comprise a metal or a polymer such as polyimide, fluoropolymer, polyetherimide,
polyether ketone, polyether sulfone, polycarbonate, or other high temperature resistance
polymers.
[0178] Tape
650 can comprise an upper and lower layer (not shown) configured to physically and/or
environmentally protect compound
610 and solid fuel
620. The upper and/or lower protective layers can comprise, for example, a metal foil,
a polymer, or can comprise a multilayer comprising metal foil and polymers. In certain
embodiments, protective layers can exhibit low permeability to oxygen, moisture, and/or
corrosive gases. All or portions of a protective layer can be removed prior to use
to expose compound
610 and solid fuel
620. To vaporize compound
610, solid fuel
620 can be ignited by energy from an external source (not shown) to generate heat that
can be conducted through second layer
602 to thermally vaporize compound
610. Examples of initiators include those discussed herein such as, but not limited to,
sparks or electrical resistance heating, Use of a protective layer can facilitate
use of drug
610 in the form of a powder or liquid.
[0179] Fig. 11B shows a cross-sectional view of a tape
670 comprising thin film drug supply units
600, which in addition to the element recited for
Fig. 11A, further comprise an initiator composition
630. Tape
670 has multiple layers including first layer
601 within which compound
610 is disposed, second layer
602 separating first layer
601 and third layer 603. Layer
603 retains solid fuel
620 and in certain embodiments, a volume
640. Openings in a fourth layer
604 define a gap separating solid fuel
620 disposed in third layer 603, and initiator composition
630 disposed within regions of a fifth layer
605. Initiator composition
630 can comprise any of the initiator compositions disclosed herein. Initiator
630 can adjoin an electrically resistive heating element
682 disposed within a sixth layer
606 and connected to electrical conductors
680 also disposed within sixth layer 606. As shown, a seventh layer
607 overlies sixth layer 606 and comprises openings
617 to facilitate electrical connection between electrical conductors
680 and a power source (not shown).
[0180] In an exemplary operation, tape
670 can be advanced to locale at least one region comprising drug
610 within an airway (not shown) and to connect respective electrical contacts
680, with a power source (not shown). Upon activation of the power source, the electrical
current can heat resistive element
682 to ignite initiator composition
630 and produce sparks. Sparks directed across gap
645 can ignite solid fuel
620. Heat generated by the ignition of solid fuel
620 can be conducted through second layer
602 thermally vaporizing compound
610 to form an aerosol comprising drug
610 within the airway.
[0181] Another drug supply article configured for the delivery of multiple doses is illustrated
in
Fig 9B.
Fig. 9B shows a plurality of individual drug-supply units provided on a card
410. Drug supply units
412,
414,
416, each consist of a solid fuel contained between a backing member and a substrate,
such as substrate
418 on unit
412. A film of drug can be coated onto substrate
418. Card
410 can be loaded into a suitable device configured to ignite at least one drug supply
unit at a time. Ignition can be, for example by sparks, as disclosed herein. To provide
a subsequent dose, card
410 can be rotated to advance a fresh drug supply unit.
[0182] Fig. 9C shows a cartridge
420 containing a plurality of cylindrically-shaped drug supply units
422,
424,
426,
428. The drug supply units can be as described herein, and comprise a solid fuel contained
within an enclosure comprising a substrate. The external surface of the substrate
can be coated with a film of drug. Each drug supply unit can be successively advanced
into position in a drug delivery device chamber for ignition of the solid fuel, vaporization
of the drug, and administration to a user.
DRUG DELIVERY DEVICES
[0183] Drug delivery devices comprising a housing defining an airway, a heating unit as
disclosed herein, a drug disposed on a portion of the exterior surface of a substrate
of the heating unit, wherein the portion of the exterior surface comprising the drug
is configured to be disposed within the airway, and an initiator configured to ignite
the solid fuel are disclosed Drug delivery devices can incorporate the heating units
and drug supply units disclosed herein. The drug delivery device comprises a housing
defining an airway. The housing can define an airway having any appropriate shape
or dimensions and can comprise at least one inlet and at least one outlet. The dimensions
of an airway can at least in part be determined by the volume of air that can be inhaled
through the mouth or the nostrils by a user in a single inhalation, the intended rate
of airflow through the airway, and/or the intended airflow velocity at the surface
of the substrate that is coupled to the airway and on which a drug is disposed. Airflow
can be generated by a patient inhaling with the mouth on the outlet of the airway,
and/or by inhaling with the nostrils on the outlet of the airway. Airflow can be generated
by injecting air or a gas into the inlet such as for example, by mechanically compressing
a flexible container filled with air and/or gas, or by releasing pressurized air and/or
gas into the inlet of the airway. Generating an airflow by injecting air and/or gas
into the airway can be useful in drug delivery devices intended for topical administration
of an aerosol comprising a drug.
[0184] A housing can be dimensioned to provide an airflow velocity through the airway sufficient
to produce an aerosol of a drug during thermal vaporization. The airflow velocity
can be at least 1 m/sec in the vicinity of the substrate on which the drug is disposed.
[0185] A housing can be dimensioned to provide a certain airflow rate through the airway.
The airflow rate through the airway can range from 10 L/min to 120 L/min. An airflow
rate ranging from 10 L/min to 120 L/min can be produced during inhalation by a user
when the outlet exhibits a cross-sectional area ranging from 0.1 cm
2 to 20 cm
2. The cross-sectional area of the outlet can range from 0.5 cm
2 to 5 cm
2, and in certain embodiments, from 1 cm
2 to 2 cm
2.
[0186] An airway can comprise one or more airflow control valves to control the airflow
rate and airflow velocity in airway. An airflow control valve can comprise, but is
not limited to, at least one valve such as an umbrella valve, a reed valve, a flapper
valve, or a flapping valve that bends in response to a pressure differential, and
the like. An airflow control valve can be located at the outlet of the airway, at
the inlet of the airway, within the airway, and/or can be incorporated into the walls
of housing defining the airway An airflow control valve can be actively controlled,
for example can be activated electronically such that a signal provided by a transducer
located within the airway can control the position of the valve; or passively controlled,
such as, for example, by a pressure differential between the airway and the exterior
of the device
[0187] Drug delivery devices configured for inhalation delivery of thermal vapor generated
from a drug supply unit are illustrated in
Fig. 8. Inhalation device
150 has an upper external housing member
152 and a lower external housing member
154 that snap fit together. The downstream end of each housing member can be gently tapered
for insertion into a users mouth, as shown on upper housing member
152 at downstream end
156. The upstream end of the upper and lower housing members can be Slotted
158, as shown in the upper housing member
152, to provide for air intake when a user inhales. When fitted together, upper and lower
housing members
152,
154 define a chamber
160. A drug supply unit
162 can be positioned within chamber
160. Drug supply unit
162 comprises a tapered, substantially cylindrical substrate
164 having an external surface
168 on which is disposed a film
166 of drug. The interior surface
170 of the substrate and a portion of the inner, cylindrical backing member
172 are shown in the cut-away section of drug supply unit
162. Solid fuel
174 is located within the annular shell region defined by backing member
172 and interior substrate surface
170. At least one initiator composition can be provided for the heating unit, and shown
in
Fig. 8, an initiator composition can be positioned (not shown) in the upstream end of the
device where the air intake occurs. The initiator composition can be configured to
ignite solid fuel
174 by the application of electrical current to an ohmic heating element connected to
a battery (not shown) located in end piece
176. Activation of the initiator composition can produce spans that are confined within
a space defined by backing member
172 and thus can be directed toward the downstream end of the drug supply unit indicated
at point
178. Sparks reaching the tapered nose portion at downstream end
178 can ignite solid fuel
174. Solid fuel
174 then burns in a downstream-to-upstream direction,
i.e. from point
178 toward the air intake end of the device at point
158, generating a wave of heat in the downstream-to-upstream direction that vaporizes
drug film
166 disposed on exterior substrate surface
168. Thus, the direction of solid fuel burn and the direction of thermal drug vapor generation
are opposite the direction of airflow through chamber
160 of the inhalation device.
METHODS FOR PRODUCING AND USING AEROSOLS
[0188] Methods of producing an aerosol of a compound using the heating units, drug supply
units, and drug delivery devices disclosed herein are described. The aerosol produced
by an apparatus can comprise a therapeutically effective amount of a drug. The temporal
and spatial characteristics of the heat applied to thermally vaporize the compound
disposed on the substrate and the air flow rate can be selected to produce an aerosol
comprising a drug having certain characteristics. For example, for intrapulmonary
delivery it is known that aerosol particles having a mean mass aerodynamic diameter
ranging from 0.01 µm to 0.1 µm and ranging from 1 µm to 3.5 µm can facilitate efficient
transfer of drugs from alveoli to the systemic circulation. In applications wherein
the aerosol is applied topically, the aerosol can have the same or different characteristics.
[0189] Methods for producing an aerosol comprise: (i) providing an airflow over a drug disposed
on a portion of an exterior surface of a substrate forming a drug supply unit, wherein
the drug supply unit comprises a heating unit as disclosed herein and the drug disposed
on a portion of the exterior surface of the substrate, wherein the portion of the
exterior surface comprising the drug is disposed within the airway; and an initiator
composition configured to ignite the solid chemical fuel; and (ii) thermally vaporizing
and condensing the drug to form an aerosol of the drug in the airway. The drug may
be disposed on the surface of the substrate as a thin film.
[0190] Methods of treating a disease in a patient in need of such treatment comprising administering
to the patient an aerosol comprising a therapeutically effective amount of a drug,
wherein the aerosol is produced by the methods and devices disclosed herein are described.
The aerosol can be administered by inhalation through the mouth, by nasal ingestion,
and/or by topical application.
[0191] Other embodiments will be apparent to those skilled in the art. It is intended that
the specification and examples be considered as exemplary only.
Examples
[0192] In the examples below, the following abbreviations have the following meanings. If
an abbreviation is not defined, it has its generally accepted meaning.
- wt%
- weight percent
- psig
- pounds per square inch, gauge
- DI
- deionized
- mL
- milliliters
- msec
- milliseconds
- L/min
- liters per minute
- µm
- micrometer
Example 1
Preparation of Solid Fuel with Laponite
[0193] The following procedure was used to prepare solid fuel coatings comprising 76.16%
Zr : 19.04% MoO
3: 4.8% Laponite® RDS.
[0194] To prepare wet Zirconium (Zr), the as-obtained suspension of Zr in DI water (Chemetall,
Germany) was agitated on a roto-mixer for 30 minutes. Ten to 40 mL of the wet Zr was
dispensed into a 50 mL centrifuge tube and centrifuged (Sorvall 6200RT) for 30 minutes
at 3,200 rpm. The DI water was removed to leave a wet Zr pellet.
[0195] To prepare a 15% Laponite® RDS solution, 85 grams of DI water was added to a beaker.
While stirring, 15 grams of Laponite® RDS (Southern Clay Products, Gonzalez, TX) was
added, and the suspension stirred for 30 minutes.
[0196] The reactant slurry was prepared by first removing the wet Zr pellet as previously
prepared from the centrifuge tube and placed in a beaker. Upon weighing the wet Zr
pellet, the weight of dry Zr was determined from the following equation: Dry Zr (g)
= 0.8234 (Wet Zr (g))- 0.1059.
[0197] The amount of molybdenum trioxide to provide a 80:20 ratio of Zr to MoO
3 was then determined, e.g, MoO
3 =Dry Zr (g) / 4, and the appropriate amount of MoO
3 powder (Accumet, NY) was added to the beaker containing the wet Zr to produce a wet
Zr : MoO
3 slurry. The amount of Laponite® RDS to obtain a final weight percent ratio of dry
components of 76.16% Zr : 19.04% MoO
3: 4.80% Laponite® RDS was determined. Excess water to obtain a reactant slurry comprising
40% DI water was added to the wet Zr and MoO
3 slurry. The reactant slurry was mixed for 5 minutes using an IKA Ultra-Turrax mixing
motor with a S2SN-8G dispersing head (setting 4). The amount of 15% Laponite® RDS
previously determined was then added to the reactant slurry, and mixed for an additional
5 minutes using the IKA Ultra-Turrax mixer. The reactant slurry was transferred to
a syringe and stored for at least 30 minutes prior to coating.
[0198] The Zr : MoO
3: Lapomite® RDS reactant slurry was then coated onto stainless steel foils. Stainless
steel foils were first cleaned by sonication for 5 minutes in a 3,2% bv solution of
Ridoline 298 in DI water at 60°C. Stainless steel foils were masked with 0.546cm (0.215
inch) wide Mylar®such that the center portion of each 0.01cm (0.004 inch) thick 304
stainless steel foil was exposed. The foils were placed on a vacuum chuck having 0.008
inch thick shims at the edges. Two (2) mL of the reactant slurry was placed at one
edge of the foil. Using a Sheen Auto-Draw Automatic Film Applicator 1137 (Sheen Instruments)
the reactant slurry was coated onto the foils by drawing a #12 coating rod at an auto-draw
coating speed of up to 50 mm/sec across the surface of the foils to deposit approximately
an 0.075 cm (0.006 inch) thick layer of the Zr: MoO
3: Laponite® RDS reactant slurry. The coated foils were then placed in a 40 °C forced-air
convection oven and dried for at least 2 hours. The masks were then removed from the
foils to leave a coating of solid fuel on the center section of each foil
[0199] The solid fuel coatings comprising Laponite® RDS adhered to the stainless steel foil
surface and maintained physical integrity following mechanical and environmental testing
including temperature cycling (-25 °C↔40 °C), accelerated humidity exposure (40 °C
/75% RH), drop testing impact testing, and flexure testing.
Example 2
Measurement of Internal Pressure
[0200] Thin film heating units were used to measure the peak internal pressure and the peak
temperature of the exterior surface of the substrate following ignition of the solid
fuel.
[0201] The thin film heating units were substantially as described in Example 9 below and
as illustrated in Figs. 10A and 10B. Two 5.08 x 5.08 square cm (2 x 2 square inch),
0.01cm (0.004 inch) thick 304 stainless steel foils formed the substrates. A solid
fuel comprising 76.16 wt% Zr, 19.04% MoO
3, 4.8% Laponite® RDS and water was coated onto the interior surface of the stainless
steel substrates. The thickness of the solid fuel layer was 0.0045cm ± 0.00076cm (0.0018
± 0.0003 inches). The layer of solid fuel covered an area of 10.9 cm
2 (1.69 in
2) and after drying, the weight of the solid fuel disposed on the interior surface
of each substrate was 0.165 to 0.190 grams. The spacer comprised a 0.61cm (0.24 inch)
thick section of polycarbonate (Makrolon). The ignition assembly comprised a FR-4
printed circuit board having a 0.076 cm (0.03 inch) diameter opening at the end to
be disposed within an enclosure defined by the spacer and the substrates. A 0.002cm
(0.0008 inch) diameter Nichrome wire was soldered to electrical conductors on the
printed circuit board and positioned across the opening. An initiator composition
comprising 26.5% Al, 51.4% MoO
3 7.7%B and 143% Viton A500 weight percent was deposited onto the Nichrome wire and
dried.
[0202] To assemble the thin film drug supply unit, the Nichrome wire comprising the initiator
composition was positioned at one end of the solid fuel area. A bead of epoxy (Epo-Tek
353 ND; Epoxy Technology) was applied to both surfaces of the spacer, and the spacer,
substrates and the ignition assembly positioned and compressed. The epoxy was cured
at a temperature of 100 °C for 3 hours.
[0203] To ignite the solid fuel, a 0.4 amp current was applied to the electrical conductors
connected to the Nichrome wire.
[0204] The peak internal pressure was measured using a pressure sensor (Motorola, MPXA42S0A).
The external surface temperature was measured using IR camera (FLIR, Therma CAM SC3000).
Example 3
Thermal Images of Heating Unit
[0205] A solid fuel consisting of a mixture of zirconium (40.6 wt%), MoO
3 (21.9 wt%), and KClO
3 (1.9 wt%), nitrocellulose (0.6 wt%), and diatomaceous earth (35 wt%) was prepared.
The solid fuel was placed in a 0.076cm (0.030-inch) gap between a stainless steel
substrate (0.038cm (0.015 inch) wall thickness) and a stainless steel backing member
(0.038cm (0.015 inch) wall thickness). The diameter of the substrate was 1.43cm (9/16inch).
The fuel was ignited, and thermal images of the heating unit were taken as a function
of time after ignition. The results are shown in
Figs. 4A-4F.
Example 4
Thermal Images of Heating Units to Evaluate Surface Temperature Uniformity
[0206] A. A solid fuel consisting of a mixture of zirconium (53.8 wt%), MoO
3 (23.1 wt%), and KClO
3 (2.3 wt%), nitrocellulose (0.8 wt%) and diatomaceous earth (20 wt%), was prepared.
The solid fuel mixture was placed in a 0.076cm (0.030-inch) gap between a stainless
steel substrate (0.038cm (0.015 inch) wall thickness) and a stainless steel backing
member (0.038cm (0.015 inch) wall thickness). The diameter of the substrate was 1.43cm
(9/16 inch). The fuel was ignited, and a thermal image of the heating unit was taken
400 milliseconds after ignition. The image is shown in
Fig. 5A.
[0207] B. A solid fuel consisting of a mixture of zirconium (46.9 wt%), MoO
3 (25.2 wt%), KClO
3 (2.2 wt%), nitrocellulose (0.7 wt%), and diatomaceous earth (25.0 wt%) was prepared.
The solid fuel was placed in a 0.076cm (0.030-inch) gap between a stainless steel
substrate (0.038cm (0.015 inch) wall thickness) and a stainless steel backing member
(0.038cm (0.015 inch) wall thickness). The diameter of the substrate was 1.43cm (9/16
inch). The fuel was ignited, and a thermal image of the heating unit was taken 400
milliseconds after ignition. The image is shown in
Fig. 5B.
Example 5
Exemplary Heating Unit
[0208] A solid fuel consisting of a mixture of zirconium (46.9 wt%), MoO
3 (25.2 wt%), and KClO
3 (2.2 wt%), grain size 100-325 mesh, along with nitrocellulose (0.7 wt%) and diatomaceous
earth (25.0 wt%) was prepared. The solid fuel was placed in a 0.076cm (0.030-inch)
gap between a stainless steel substrate (0.038cm (0.015 inch) wall thickness) and
a stainless steel backing member (0.038cm (0.015 inch) wall thickness). The diameter
of the substrate was 1.43cm (9/16 inch) The solid fuel was remotely ignited from the
tip of the heating unit. During and after burn, the pressure in the cylindrical substrate
was measured as described herein. The burn propagation speed and the surface temperature
uniformity were evaluated by infrared imaging.
[0209] The internal pressure increased to 1.14 x 10
6Pa (150 psig) during the reaction period of 0.3 seconds. The residual pressure was
under 5.2 x 10
5 Pa (60 psig). The burn propagation speed was 13 cm/sec. With respect to surface temperature
uniformity, no obvious cold spots were observed.
Example 6
Exemplary Heating Unit
[0210] A solid fuel consisting of a mixture of zirconium (69.3 wt%) and MoO
3 (29.7 wt%), grain size 100-325 mesh, along with nitrocellulose (1.0 wt%) was prepared.
The solid fuel mixture was placed in a 0.05cm (0.020-inch) gap between a stainless
steel substrate (0.05cm (0.020 inch) wall thickness) and a stainless steel backing
member (0.05cm (0.020 inch) wall thickness). The outside of the backing member was
coated with initiator to increase burn propagation speed. The primary fuel was remotely
ignited from the tip of the heating unit. During and after burn, the pressure in the
cylindrical substrate was measured as described herein. The burn propagation speed
and the surface temperature uniformity were evaluated by infrared imaging.
[0211] The internal pressure increased to 1.48 x 10
6Pa (200 psig) during the reaction period of 0.25 seconds. The residual pressure was
under 5.2 x 10
5Pa (60 psig). The burn propagation speed was 15 cm/sec, With respect to surface temperature
uniformity, no obvious cold spots were observed.
Example7
Exemplary Heating unit
[0212] A solid fuel consisting of a mixture of aluminium (49.5 wt%) and MoO
3 (49.5 wt%), grain size 100-325 mesh, along with nitrocellulose (1.0 wt%) was prepared,
The solid fuel mixture was placed in a 0.05cm (0.020-inch) gap between a stainless
steel substrate (0.05cm (0.020 inch) wall thickness) and a stainless steel backing
member 0.05cm (0.020 inch) wall thickness). The primary fuel was directly ignited
near the plug. During and after burn, the pressure in the cylindrical substrate was
measured as described herein. The surface temperature uniformity was evaluated by
infrared imaging.
[0213] The internal pressure increased to 2.17 x 10
6Pa (300 psig) during the reaction period of less than 5 milliseconds. The residual
pressure was under 5.2 x 10
5Pa (60 psig). The exterior surface expanse was uniformly heated, with between 5-10
percent of the surface being 50 °C to 100°C cooler than the rest of the expanse.
Example 8
Wet Processing for Zirconium Fuel Slurry
[0214] The following procedure was used to prepare fuel compositions comprising Zr and MoO
3 for a thin film drug supply unit. Wet Zr particles, 46.7 wt%, having a 2 µm to 3
µm particle size were obtained from Chemetall, GmbH, Germany. The Zr particles were
rinsed with DI water, following which the excess water was decanted. DI water, 5.1
wt%, was added to the Zr and the mixture centrifuged. Excess water was decanted. Dry
MoÔ
3, 20 wt%, (Climax Molybdenum Co., AZ) and DI water was then added to the washed Zr,
and the mixture homogenized for 2 minutes with a high shear mixer (IKA, Germany).
A 15% aqueous solution of Laponite® RDS, 2.5 wt%, (Southern Clay Products, Inc., Texas)
was added and the mixture homogenized with a high shear mixer for an additional 5
minutes. The Zr : MO
3 solid fuel slurry was transferred to a syringe or holding vessel for subsequent coating.
The wet Zr included 8.5 wt% water and the Laponite® RDS gel included 14 wt% water.
The weight percents represent the percent weight of the total wet composition.
Example 9
Exemplary Thin Film Drug Supply Unit
[0215] A thin film drug supply unit according to
Figs. 10A-10B was fabricated and the performance evaluated, Two, 5.08 x 5.08 square cm, 0.01cm
(2 x 2 square inch, 0.004 inch) thick 304 stainless steel foils formed the substrates.
A solid fuel comprising 76.16 wt% Zr and 19.04% MoO
3 and 4.8% Laponite® RDS and water was coated onto the interior surface of the stainless
steel substrates. The thickness of the solid fuel layer was 0.0046cm ± 0.00076cm (0.0018
± 0.0003 inches). The layer of solid fuel covered an area 10.9cm
2 (1.69 in
2) and after drying, the weight of the solid fuel disposed on the interior surface
of each substrate was 0.165 to 0.190 grams. An ∼6 µm thick thin film of a drug was
deposited onto a 7.81cm
2 (1.21 in
2) area of the exterior substrate surfaces using spray coating. The drug was dissolved
in a 15 mg/ml solution of isopropanol or acetone to facilitate processing. The thin
film of drug was dried at ambient conditions and 1.5 mg to 3.0 mg of drug was deposited
on the exterior surface of each substrate. The spacer comprised a 0.61cm (0.24 inch)
thick section of polycarbonate (Makronlon). The ignition assembly comprised a FR-4
printed circuit board having a 0.076cm (0.03 inch) diameter opening at the end to
be disposed within an enclosure defined by the spacer and the substrates. A 0.002cm
(0.0008 inch) diameter Nichrome wire was soldered to electrical conductors on the
printed circuit board and positioned across the opening. An initiator composition
comprising 26.5% Al, 51.4% MoO
3, 7.7%B and 14.3% Viton A500 weight percent was deposited onto the Nichrome wire and
dried.
[0216] To assemble the thin film drug supply unit, the Nichrome wire comprising the initiator
composition was positioned at one end of the solid fuel area A bead of epoxy (Epo-Tek
353 ND, Epoxy Technology) was applied to both surfaces of the spacer, and the spacer,
substrates and the ignition assembly positioned and compressed. The epoxy was cured
at a temperature of 100 °C for 3 hours.
[0217] To ignite the solid fuel, a 0.4 Amp current was applied to the electrical conductors
connected to the Nichrome wire.
[0218] The airflow in the airway used for the measurements ranged from 14 L/min to 28 L/min
corresponding to an airflow velocity of 1.5 m/sec and 3 m/sec, respectively.
[0219] Measurements an such drug supply units demonstrated that the exterior surface of
the substrate reached temperatures in excess of 400 °C in less than 150 milliseconds
following activation of the initiator at which time the drug was completely thermally
vaporized. The maximum pressure within the enclosure was less than 0,7.10
5 Pa (10 psig) In separate measurement, it was demonstrated that the enclosure was
able to withstand a static pressure in excess of 4.10
5 Pa (60 psig) at room temperature. The burn propagation speed across the expanse of
solid fuel was measured to be 25 cm/sec. The particulates forming the aerosol comprised
greater than 95% of the drug, and greater than 90% of the drug originally deposited
on the substrates formed the aerosol.
Example 10
Measurement of Aerosol Purity and Yield
[0220] Drug supply units substantially as described in Example 9 and illustrated in
Figs. 10A and 10B were used to measure the percent yield and percent purity of aerosols.
[0221] Two, 5.08x5.08 square cm, 0.01cm (2 x 2 square inch, 0.004 inch) thick 304 stainless
steel foils formed the substrates. A solid fuel comprising 76.16 wt% Zr, 19.04% MoO
3, 4.8% Laponite® RDS and water was coated onto the interior surface of the stainless
steel substrates. The thickness of the solid fuel layer was 0.0046cm ± 0.00076cm (0.0018
± 0.0003 inches). The layer of solid fuel covered an area of 10.9cm
2 (1.69 in
2) and after drying, the weight of the solid fuel disposed on the interior surface
of each substrate was 0.165 to 0.190 grams. An ∼6 µm thick thin film of a drug was
deposited onto a 7.81cm
2 (1.21 in
2) area of the exterior substrate surfaces using spray coating. The drug was dissolved
in a 15 mg/ml solution of isopropanol or acetone to facilitate processing. The thin
film of drug was dried at ambient conditions and 1.5 mg to 3.0 mg of drug was deposited
on the exterior surface of each substrate. The spacer comprised a 0.61cm (0.24 inch)
thick section of polycarbonate (Makronlon). The ignition assembly comprised a FR-4
printed circuit board having a 7.62cm (0.03 inch) diameter opening at the end to be
disposed within an enclosure defined by the spacer and the substrates. A 0.002cm (0.0008
inch) diameter Nichrome wire was soldered to electrical conductors on the printed
circuit board and positioned across the opening. An initiator composition comprising
26.5% Al, 51.4% MoO
3, 7.7%B and 14.3% Viton A500 weight percent was deposited onto the Nichrome wire and
dried.
[0222] To assemble the thin film drug supply unit, the Nichrome wire comprising the initiator
composition was positioned at one end of the solid fuel area. A bead of epoxy (Epo-Tek
353 ND, Epoxy Technology) was applied to both surfaces of the spacer, and the spacer,
substrates and the ignition assembly positioned and compressed. The epoxy was cured
at a temperature of 100 °C for 3 hours.
[0223] To ignite the solid fuel, a 0.4 Amp current was applied to the electrical conductors
connected to the Nichrome wire.
[0224] The airflow in the airway used for the measurements ranged from 14 L/min to 28 L/min
corresponding to an airflow velocity of 1.5 m/sec and 3 m/sec, respectively.
[0225] After volatilization, the aerosol was captured on a mat for quantification of yield
and analysis of purity. The quantity of material recovered on the mat was used to
determine a percent yield, based on the mass of drug coated onto the substrate. Any
material deposited on the housing or the remaining on the substrate was also recovered
and quantified to determine a percent total recovery ((mass of drug on the mat + mass
of drug remaining on substrate and housing)/mass of drug coated onto substrate). For
compounds without UV absorption GC/MS or LC/MS was used to quantify the recovery.
[0226] The percent purity was determined using HPLC UV absorption at 250 nm. However, as
one of skill in the art recognizes, the purity of a drug-containing aerosol may be
determined using a number of different methods. It should be noted that when the term
"purity" is used, it refers to the percentage of aerosol minus the percent byproduct
produced in its formation. Byproducts for example, are those unwanted products produced
during vaporization. For example, byproducts include thermal degradation products
as well as any unwanted metabolites of the active compound or compounds. Examples
of suitable methods for determining aerosol purity are described in
Sekine et al., Journal of Forensic Science 32:1271-1280 (1987) and in
Martin et al., Journal of Analytic Toxicology 13:158-162 (1989).
[0227] One suitable method involves the use of a trap. In this method, the aerosol is collected
in a trap in order to determine the percent or fraction of byproduct. Any suitable
trap may be used. Suitable traps include mats, glass wool, impingers, solvent traps,
cold traps, and the like. Mats are often most desirable. The trap is then typically
extracted with a solvent, e.g. acetonitrile, and the extract subjected to analysis
by any of a variety of analytical methods known in the art, for example, gas, liquid,
and high performance liquid chromatography particularly useful.
[0228] The gas or liquid chromatography method typically includes a detector system, such
as a mass spectrometry detector or an ultraviolet absorption detector. Ideally, the
detector system allows determination of the quantity of the components of the drug
composition and of the byproduct, by weight. This is achieved in practice by measuring
the signal obtained upon analysis of one or more known mass(es) of components of the
drug composition or byproduct (standards) and then comparing the signal obtained upon
analysis of the aerosol to that obtained upon analysis of the standard(s), an approach
well known in the art.
[0229] In many cases, the structure of a byproduct may not be known or a standard for it
may not be available. In such cases, one may calculate the weight fraction of the
byproduct by assuming it has an identical response coefficient (e.g. for ultraviolet
absorption detection, identical extinction coefficient) to the drug component or components
in the drug composition. When conducting such analysis, byproducts present in less
than a very small fraction of the drug compound, e.g. less than 0.1 % or 0.03% of
the drug compound, are typically excluded. Because of the frequent necessity to assume
an identical response coefficient between drug and byproduct in calculating a weight
percentage of byproduct, it is often more desirable to use an analytical approach
in which such an assumption has a high probability of validity. In this respect, high
performance liquid chromatography with detection by absorption of ultraviolet light
at 225 nm is typically desirable. UV absorption at 250 nm may be used for detection
of compounds in cases where the compound absorbs more strongly at 250 nm or for other
reasons one skilled in the art would consider detection at 250 nm the most appropriate
means of estimating purity by weight using HPLC analysis. In certain cases where analysis
of the drug by UV are not viable, other analytical tools such as GC/MS or LC/MS may
be used to determine purity.