FIELD
[0001] The present disclosure relates to enhancing slagging in gas generants containing
copper by introducing large particle size endothermic slag-forming components.
BACKGROUND
[0002] This section provides background information related to the present disclosure which
is not necessarily prior art.
[0003] Passive inflatable restraint systems are used in a variety of applications, such
as motor vehicles. Certain types of passive inflatable restraint systems minimize
occupant injuries by using a pyrotechnic gas generant to inflate an airbag cushion
(
e.g., gas initiators and/or inflators) or to actuate a seatbelt tensioner (
e.g., micro gas generators), for example. Automotive airbag inflator performance and
safety requirements are continually increasing to enhance passenger safety, while
concurrently striving to reduce manufacturing costs.
[0004] Thus, increasing functionality of a propellant or a gas generant used in airbag inflators,
while improving performance and reducing costs of the entire airbag inflator system
has been an ongoing objective in design of inflatable restraint systems. Gas generant
selection involves addressing various factors, including meeting current industry
performance specifications, guidelines and standards, generating safe gases or effluents,
durational stability of the materials, and cost-effectiveness in manufacture, among
other considerations. Improved gas generator performance may be achieved in a variety
of ways, many of which ultimately depend on the gas generant formulation to provide
the desired properties.
[0005] Suitable gas generants provide sufficient gas mass flow in a desired time interval
to achieve a required work impulse for the inflating device. Further, gas generants
having lower flame temperatures are advantageous. In current designs of automotive
airbag inflators, a significant portion of the mass of the inflator is often relegated
to heat sink, in combination with filtration systems. This detrimentally impacts the
weight of the inflator and thus the efficiency of the system. Hence, for new advanced
inflator designs, it is desirable to reduce or minimize filter and heat sink requirements
as much as possible. As part of these new designs, cool burning gas generant formulations
are advantageous because they reduce heat sink requirements. Additionally, if filter
mass is to be reduced the cool burning gas generant must slag very well, meaning that
combustion products form a large integral mass that is retained inside the combustion
chamber during combustion and thus does not pass through the filter into the airbag.
Accordingly, enhancing formation of slag in various gas generants, especially in cool
burning gas generants would be highly desirable to produce lighter, more efficient
inflator designs.
[0006] EP1415963 discloses a gas generant composition comprising basic copper nitrate and 2 slag formers:
glass powder (10-50 microns) and aluminium hydroxide.
[0007] US2008/105342 discloses a gas generant composition comprising basic copper nitrate and aluminium
hydroxide, having a combustion temperature of <1400 °C. The aluminium hydroxide is
included in order to reduce the amount of nitrogen oxide and carbon monoxide produced.
[0008] US6964716 discloses a gas generant composition comprising guanidine nitrate, basic copper nitrate,
at least one perchlorate and aluminium hydroxide. It further discloses that the aluminium
hydroxide is used as a coolant and that its average particle size is 0.1-70 microns.
[0009] US5817972 discloses a gas generant composition comprising dicyandiamide and sodium nitrate
which results in 19.5% slag after burning. It further discloses the introduction of
20% of Fe2O3 with an average particle size of 200 microns as a coolant and residue
former into the composition, resulting in an enhanced slag formation (45.1%).
[0010] US6039820 discloses that aluminium hydroxide has a double function as a coolant and slag enhancer
in gas generating compositions.
SUMMARY
[0011] This section provides a general summary of the disclosure, and is not a comprehensive
disclosure of its full scope or all of its features.
[0012] The present disclosure pertains to gas generant compositions comprising copper having
improved slagging properties. The present invention provides a gas generant composition
comprising a fuel, an oxidizer comprising basic copper nitrate, and an endothermic
slag-forming component having an average particle size diameter of greater than or
equal to about 150 µm. The gas generant composition has a maximum flame temperature
at combustion (T
c) of less than or equal to about 1,900K (1,627°C).
[0013] In another variation, the present disclosure provides a gas generant composition
comprising a fuel, at least one oxidizer comprising basic copper nitrate, and an endothermic
slag-forming component comprising aluminum hydroxide having an average particle size
diameter of greater than or equal to about 150 µm. The gas generant composition has
a maximum flame temperature at combustion (T
c) of less than or equal to about 1,900K (1,627°C). In certain aspects, such a gas
generant composition may have a maximum flame temperature at combustion (T
c) of greater than or equal to about 1,350K (1,077°C) to less than or equal to about
1,450K (1,177°C).
[0014] The present invention further provides a method of enhancing slag formation for a
gas generant composition. The method comprises introducing an endothermic slag-forming
component having an average particle diameter size of greater than or equal to about
150 µm to a gas generant composition comprising a fuel and an oxidizer comprising
basic copper nitrate. The introducing of the endothermic slag-forming component enhances
slag formation during combustion of the gas generant composition by at least 50%,
wherein the gas generant composition has a maximum flame temperature at combustion
(Tc) of less than or equal to about 1,900K (1,627°C), the fuel is selected from the
group consisting of: guanidine nitrate, copper bis guanylurea dinitrate, hexamine
cobalt (III) nitrate, copper diammine bitetrazole, and combinations thereof, and the
endothermic slag-forming component is selected from the group consisting of: aluminum
hydroxide, hydromagnesite, Dawsonite, magnesium hydroxide, magnesium carbonate subhydrate,
Bohemite, calcium hydroxide, and combinations thereof.
[0015] Further areas of applicability will become apparent from the description provided
herein. The description and specific examples in this summary are intended for purposes
of illustration only and are not intended to limit the scope of the present disclosure.
DRAWINGS
[0016] The drawings described herein are for illustrative purposes only of selected embodiments
and not all possible implementations, and are not intended to limit the scope of the
present disclosure.
Figure 1 is a partial cross-sectional view of an exemplary passenger-side airbag module
including an inflator for an inflatable airbag restraint device.
Figure 2 shows an acceptable particle size distribution for a large particle size
endothermic slag-forming aluminum hydroxide for use in accordance with various aspects
of the present disclosure.
Figure 3 shows a macroscopic photograph of a slag formed from a conventional gas generant.
Figure 4 shows a microscopic photograph of the slag in Figure 3 formed from the comparative
example of a conventional gas generant. Magnification is at 50 times.
Figure 5 shows a macroscopic photograph of a slag formed from a gas generant prepared
in accordance with certain aspects of the present disclosure.
Figure 6 shows a microscopic photograph of the slag in Figure 5 formed from the gas
generant prepared in accordance with certain aspects of the present disclosure. Magnification
is at 50 times.
Figure 7 shows a photograph of a slag formed from a comparative conventional gas generant
in a post-fire inflator combustion chamber.
Figure 8 shows a photograph of slag formed from the gas generant prepared in accordance
with certain aspects of the present disclosure in a post-fire inflator combustion
chamber.
[0017] Corresponding reference numerals indicate corresponding parts throughout the several
views of the drawings.
DETAILED DESCRIPTION
[0018] Example embodiments will now be described more fully with reference to the accompanying
drawings.
[0019] Example embodiments are provided so that this disclosure will be thorough, and will
fully convey the scope to those who are skilled in the art. Numerous specific details
are set forth such as examples of specific components, devices, and methods, to provide
a thorough understanding of embodiments of the present disclosure. It will be apparent
to those skilled in the art that specific details need not be employed, that example
embodiments may be embodied in many different forms and that neither should be construed
to limit the scope of the disclosure. In some example embodiments, well-known processes,
well-known device structures, and well-known technologies are not described in detail.
[0020] The terminology used herein is for the purpose of describing particular example embodiments
only and is not intended to be limiting. As used herein, the singular forms "a," "an,"
and "the" may be intended to include the plural forms as well, unless the context
clearly indicates otherwise. As used herein, the term "and/or" includes any and all
combinations of one or more of the associated listed items. Although the terms first,
second, third, etc. may be used herein to describe various components, elements, regions,
layers and/or sections, these components, elements, regions, layers and/or sections
should not be limited by these terms. These terms may be only used to distinguish
one element, component, region, layer or section from another region, layer or section.
Terms such as "primary," "secondary," "first," "second," or and other numerical terms
when used herein do not imply a sequence or order unless clearly indicated by the
context. Thus, a first or primary component, element, region, layer or section discussed
below could be termed a secondary component, element, region, layer or section without
departing from the teachings of the example embodiments.
[0021] Throughout this disclosure, the numerical values represent approximate measures or
limits to ranges to encompass minor deviations from the given values and embodiments
having about the value mentioned as well as those having exactly the value mentioned.
Other than in the working examples provided at the end of the detailed description,
all numerical values of parameters (
e.
g., of quantities or conditions) in this specification, including the appended claims,
are to be understood as being modified in all instances by the term "about" whether
or not "about" actually appears before the numerical value. "About" indicates that
the stated numerical value allows some slight imprecision (with some approach to exactness
in the value; approximately or reasonably close to the value; nearly). If the imprecision
provided by "about" is not otherwise understood in the art with this ordinary meaning,
then "about" as used herein indicates at least variations that may arise from ordinary
methods of measuring and using such parameters.
[0022] As referred to herein, ranges are, unless specified otherwise, inclusive of endpoints
and include disclosure of all distinct values and further divided ranges within the
entire range. Thus, for example, a range of "from A to B" or "from about A to about
B" is inclusive of A and of B. Disclosure of values and ranges of values for specific
parameters (such as weight percentages, temperatures, molecular weights, etc.) are
not exclusive of other values and ranges of values useful herein. It is envisioned
that two or more specific exemplified values for a given parameter may define endpoints
for a range of values that may be claimed for the parameter. For example, if Parameter
X is exemplified herein to have value A and also exemplified to have value Z, it is
envisioned that Parameter X may have a range of values from about A to about Z. Similarly,
it is envisioned that disclosure of two or more ranges of values for a parameter (whether
such ranges are nested, overlapping or distinct) subsume all possible combination
of ranges for the value that might be claimed using endpoints of the disclosed ranges.
For example, if Parameter X is exemplified herein to have values in the range of 1-10,
or 2-9, or 3-8, it is also envisioned that Parameter X may have other ranges of values
including 1-9, 1-8, 1-3, 1-2, 2-10, 2-8, 2-3, 3-10, and 3-9. Example embodiments will
now be described more fully with reference to the accompanying drawings.
[0023] The present disclosure is drawn to gas generant compositions and methods for enhancing
slag formation in such gas generant compositions. Gas generants, also known as propellants,
gas-generating materials, and pyrotechnic materials are used in inflators of airbag
modules, such as a simplified exemplary airbag module 30 comprising a passenger compartment
inflator assembly 32 and a covered compartment 34 to store an airbag 36 of Figure
1. A gas generant material 50 burns to produce the majority of gas products that are
directed to the airbag 36 to provide inflation. Such devices often use a squib or
initiator 40 which is electrically ignited when rapid deceleration and/or collision
is sensed. The discharge from the squib 40 usually ignites an igniter material 42
that burns rapidly and exothermically, in turn, igniting a gas generant material 50.
[0024] The gas generant 50 can be in the form of a solid grain, a pellet, a tablet, or the
like. "Slag" or "clinker" is another name for solid combustion products formed during
combustion of the gas generant material. The composition of slag is mainly metals
and metal oxides. Ideally, the slag will maintain the original shape of the gas generant
(e.g., grain, pellet, or tablet) and be large and easily filtered. This is particularly
important when the inflator design includes a reduced mass filtration system for the
purpose of reducing the inflator size and weight such as can be used with cool burning
gas generant formulations. As shown in Figure 1, an exemplary conventional filter
system 52 is provided between gas generant 50 and airbag 36. The quality and toxicity
of the components of the gas produced by the gas generant 50, also referred to as
effluent, are important because occupants of the vehicle are potentially exposed to
these compounds. It is desirable to minimize the concentration of potentially harmful
compounds in the effluent.
[0025] Various different gas generant compositions (
e.g., 50) are used in vehicular occupant inflatable restraint systems. Gas generant material
selection involves various factors, including meeting current industry performance
specifications, guidelines and standards, generating safe gases or effluents, handling
safety of the gas generant materials, durational stability of the materials, and cost-effectiveness
in manufacture, among other considerations. It is preferred that the gas generant
compositions are safe during handling, storage, and disposal, and preferably are azide-free.
[0026] In various aspects, the gas generant typically includes at least one fuel component
and at least one oxidizer component, and may include other minor ingredients, that
once ignited combust rapidly to form gaseous reaction products (
e.g., CO
2, H
2O, and N
2). One or more fuel compounds undergo rapid combustion to form heat and gaseous products;
e.g., the gas generant burns to create heated inflation gas for an inflatable restraint
device or to actuate a piston. The gas-generating composition also includes one or
more oxidizing components, where the oxidizing component reacts with the fuel component
in order to generate the gas product.
[0027] Improved gas generator performance in an inflatable restraint system may be achieved
in a variety of ways, many of which ultimately depend on the gas generant formulation
to provide the desired properties. Ideally, a gas generant provides sufficient gas
mass flow in a desired time interval to achieve the required work impulse for an inflating
device (e.g., airbag) within the inflatable restraint system. Although a temperature
of gas generated by the gas generant influences the amount of work gases can do, high
gas temperatures may be undesirable because burns and related thermal damage can result.
In addition, high gas temperatures can also potentially lead to an excessive reliance
or sensitivity of the gas to heat transfer and excessively rapid deflation profiles,
which can likewise be undesirable. For example, a cool burning gas generant having
combustion flame temperatures of less than approximately 1,900K (1,627°C) has been
shown to enable inflator devices with reduced filtration, which operate in a manner
that provides adequate restraint and protection, without the risk of burns or injury
to an automobile occupant in the event of a crash. Thus, minimizing flame temperature
is advantageous. In certain aspects of the present technology, a high flame temperature
may be considered anything in excess of about 1,900K (1,627°C) at combustion.
[0028] In order to mitigate the effects of high flame temperatures, in conventional inflatable
restraint system gas generators, a significant portion of mass of an inflator is often
relegated to heat sink in combination with filtration. This impacts the efficiency
of the system and, most significantly, the weight of the inflator. Consequently, in
certain aspects, it is desirable to provide a gas generant formulation for an inflatable
restraint system that can achieve a high gas output at a high mass flow rate at relatively
low flame temperatures. Furthermore, it would be desirable to employ a gas generant
formulation that has enhanced slag forming abilities, so that attendant filter components
can be reduced within the inflator component to further improve efficiency. Other
important variables in inflator gas generant design include improving gas generant
performance with respect to gas yield, relative quickness (as determined by observed
burning rate), and cost.
[0029] Advanced inflator design concepts incorporate reduced filter and heat sink mass,
as well as reduced containment wall thickness coupled with fiberglass/resin reinforcement
to achieve significant weight reduction in the inflator. Use of cool burning gas generant
formulations reduces heat sink requirements. Additionally, because filter mass is
reduced, it is desirable to have a cool burning gas generant that slags very well.
By "slagging" it is meant that certain solid combustion products generated during
burning of the gas generant form a large integral solid mass that is retained inside
the combustion chamber during combustion, rather than passing through the filter into
the airbag. Traditional slagging agents have been used to achieve this effect. A slagging
agent is a compound or material, usually inert to combustion, that melts at combustion
temperatures and agglomerates or collects all of the solid combustion products together.
Examples of conventional slagging agents are silicon dioxide, aluminum oxide, glass
and other metal oxides that melt at or near the combustion flame temperature.
[0030] In various aspects, the present disclosure provides a relatively cool burning gas
generant composition that comprises a fuel and an oxidizer. In certain embodiments,
the gas generant composition comprises a fuel and an oxidizer comprising copper. In
further embodiments, the gas generant comprises a fuel and an oxidizer comprising
basic copper nitrate. In certain aspects, the gas generant composition has a maximum
flame temperature at combustion (T
c) of less than or equal to about 1,900K (1,627°C) and in certain other aspects, optionally
less than or equal to about 1,700K (1,427°C). In accordance with various aspects of
the present teachings, a large particle size endothermic slag-forming component is
introduced to the gas generant composition to significantly enhance formation of slag
when such a gas generant component is combusted. The endothermic slag-forming component
particles preferably have an average particle size diameter of greater than or equal
to about 150 µm. In certain aspects, the endothermic slag-forming component has a
decomposition temperature in a range of greater than or equal to about 180°C to less
than or equal to about 450°C, meaning that the compound decomposes endothermically
within this temperature range, for example, by releasing water or carbon dioxide.
[0031] In certain preferred variations, the endothermic slag-forming component comprises
a large particle size aluminum hydroxide (Al(OH)
3). However, in alternative variations, the following compounds may be employed as
endothermic slag-forming components in gas generant compositions comprising copper:
hydromagnesite (Mg
5(CO
3)
4(OH)
2·4H
2O), Dawsonite (NaAl(OH)
2CO
3), magnesium hydroxide (Mg(OH)
2), magnesium carbonate subhydrate (MgOCO
2·H
2O
(0.3)), Bohemite (AlO(OH)), calcium hydroxide (Ca(OH)
2), and combinations thereof. Each of these compounds decomposes endothermically within
the desired temperature range of greater than or equal to about 180°C to less than
or equal to about 450°C, as set forth in Table 1 below.
Table 1
| Compound |
Chemical Formula |
Decomposition Temperature °C |
| Aluminum Hydroxide |
Al(OH)3 |
180 - 200 |
| Hydromagnesite |
Mg5(CO3)4(OH)2·4H20 |
220 - 240 |
| Dawsonite |
NaAl(OH)2CO3 |
240 - 260 |
| Magnesium Hydroxide |
Mg(OH)2 |
300 - 320 |
| Magnesium Carbonate Subhydrate |
MgOCO2·H2O(0.3) |
340 - 350 |
| Bohemite |
AlO(OH) |
340 - 350 |
| Calcium Hydroxide |
Ca(OH)2 |
430- 450 |
[0032] The endothermic slag-forming component has specific particle size requirements to
provide certain benefits associated with the inventive technology. In certain embodiments,
the endothermic slag-forming component comprises a large particle size aluminum hydroxide
(Al(OH)
3). The inventive technology contemplates use of aluminum hydroxide having very specific
particle size properties, which greatly improves slag formation while also cooling
a copper-containing gas generant flame temperature (
e.g., a maximum combustion flame temperature lowered to about 1,350K (1,077°C) - 1,450K
(1,177°C).
[0033] In certain variations, endothermic slag-forming component particles (e.g., aluminum
hydroxide particles) have a large particle size. By "large particle size," it is meant
that an average particle size diameter of the endothermic slag-forming component particles
(e.g., aluminum hydroxide particles) is greater than or equal to 150 micrometers (µm),
optionally greater than or equal to about 175 µm, optionally greater than or equal
to about 200 µm, optionally greater than or equal to about 225 µm, optionally greater
than or equal to about 250 µm, optionally greater than or equal to about 275 µm, and
in certain variations greater than or equal to about 300 µm. The particle size distribution
for the endothermic slag-forming component particles may have a 10% value of greater
than or equal to about 100 µm (micrometers); optionally greater than or equal to about
115 µm. In certain variations, the particle size distribution has an average (50%)
particle size of greater than or equal to about 150 µm, while also having a 10% value
of greater than or equal to about 100 µm. Furthermore, particle size distributions
of endothermic slag-forming component particles with 90% values of 200 to 300 µm also
provide desired advantages associated with certain aspects of the present teachings.
One suitable example of a large particle size aluminum hydroxide has a particle size
distribution 10% value of about 115 µm, a 50% value of about 158 µm (thus an average
particle size diameter of 158 µm), and a 90% value of about 288 µm. An example of
such an acceptable particle size for an aluminum hydroxide that fulfills the requirements
for use in accordance with the present technology is shown in Figure 2, which has
an average particle size diameter as described just above. Thus, relatively large
particles provide the desirable slagging ability to the gas generant compositions
comprising copper.
[0034] In accordance with various aspects of the present disclosure, gas generants are provided
that have desirable compositions that result in superior performance characteristics
in an inflatable restraint device, while reducing overall cost of gas generant and
inflator assembly production. Thus, in accordance with various aspects of the present
teachings, an improved cool burning gas generant composition is provided that has
a maximum combustion temperature (T
c) (also expressed as maximum combustion flame temperature) of less than or equal to
about 1,900K (1,627°C). In certain variations, the maximum combustion temperature
is less than or equal to about 1,800K (1,527°C), optionally less than or equal to
about 1,700K (1,427°C), optionally less than or equal to about 1,600K (1,327°C) and
in certain variations, less than or equal to about 1,500K (1,227°C). In various embodiments,
it is preferred that the flame temperature during combustion for a cool burning gas
generant is greater than or equal to about 1,300K (1,027°C) to less than or equal
to about 1,700K (1,427°C).
[0035] Additionally, in various aspects, the gas generant may have a high mass density in
various embodiments. For example, in certain embodiments, the gas generant has a theoretical
mass density of greater than or equal to about 2 g/cm
3, optionally greater than or equal to about 2.25 g/cm
3, optionally greater than or equal to about 2.5 g/cm3, and in certain variations,
optionally greater than or equal to about 2.75 g/cm
3.
[0036] Further, in accordance with the present disclosure, the gravimetric gas yield of
the gas generant is relatively high. For example, in certain embodiments, the gravimetric
gas yield is greater than or equal to about 1.8 moles/100 grams of gas generant. In
other embodiments, the gravimetric gas yield is greater than or equal to about 1.9
moles/100 g of gas generant, optionally greater than or equal to about 2.0 moles/100
g of gas generant, optionally greater than or equal to about 2.1 moles/100 g of gas
generant, optionally greater than or equal to about 2.2 moles/100 g of gas generant,
optionally greater than or equal to about 2.3 moles/100 g of gas generant, optionally
greater than or equal to about 2.4 moles/100 g of gas generant, optionally greater
than or equal to about 2.5 moles/100 g of gas generant, and in certain variations,
optionally greater than or equal to about 2.6 moles/100 g of gas generant. The product
of gravimetric gas yield and density is a volumetric gas yield.
[0037] In other aspects, the volumetric gas yield of a gas generant according to certain
variations of the present disclosure is optionally greater than or equal to about
5.0 moles/100 cm
3 of gas generant. In other embodiments, the volumetric gas yield is greater than or
equal to about 5.1 moles/100 cm
3 of gas generant, optionally greater than or equal to about 5.2 moles/100 cm
3 of gas generant, optionally greater than or equal to about 5.3 moles/100 cm
3 of gas generant, optionally greater than or equal to about 5.4 moles/100 cm
3 of gas generant, optionally greater than or equal to about 5.5 moles/100 cm
3 of gas generant, and in certain variations, optionally greater than or equal to about
5.6 moles/100 cm
3 of gas generant.
[0038] Thus, the present technology provides enhanced slag formation for cool burning gas
generants. Thus, in certain aspects, the disclosure provides a gas generant composition
comprising copper having good slag forming capabilities. For example, the gas generant
composition may comprise at least one fuel, at least one oxidizer comprising copper,
a large particle size endothermic slag-forming component, and optionally minor amounts
of conventional gas generant additives. Materials are generally categorized as gas
generant fuels due to their relatively low burn rates, and are often combined with
one or more oxidizers in order to obtain desired burn rates and gas production. As
appreciated by those of skill in the art, such a fuel component may be combined with
additional components in the gas generant, such as co-fuels or oxidizers. Most fuels
known in the art can be used with the present technology and are generally selected
to impart certain desirable characteristics to the gas generant formulation, such
as gas yield, burning rate, thermal stability, and low cost. These fuels can be organic
compounds containing two or more of the elements: carbon (C), hydrogen (H), nitrogen
(N), and oxygen (O). The fuels can also include transition metal salts and transition
metal nitrate complexes. In certain variations, preferred transition metals are copper
and/or cobalt. In accordance with certain aspects of the present teachings, a fuel
is selected for the inventive gas generant compositions so that when combusted with
certain oxidizers comprising copper, such as basic copper nitrate, a resulting maximum
combustion flame temperature (T
c) falls within a range of greater than or equal to about 1,400K (1,127°C) to less
than or equal to 1,900K (1,627°C).
[0039] Examples of fuels useful for gas generants according to the present teachings are
selected from the group consisting of guanidine nitrate, copper bis guanylurea dinitrate,
hexamine cobalt (III) nitrate, copper diammine bitetrazole, and combinations thereof.
Fuels may be used singly or in combination with other co-fuels to impart the desired
combustion characteristics. A suitable gas generant composition optionally includes
greater than or equal to about 25% to less than or equal to about 70% by weight; optionally
greater than or equal to about 30% to less than or equal to about 55% of all fuel
components in the total gas generant composition .
[0040] The gas generant formulations according to various aspects of the present teachings
include an oxidizer comprising copper as a main oxidizer. A particularly suitable
oxidizer for the gas generant compositions of the present disclosure is basic copper
nitrate. Basic copper nitrate has a high oxygen-to-metal ratio and good slag forming
capabilities upon burn. By way of example, a suitable gas generant composition optionally
includes greater than or equal to about 25% to less than or equal to about 75% by
weight of the oxidizer, such as basic copper nitrate; optionally greater than or equal
to about 30% to less than or equal to about 60% by weight of the oxidizer, such as
basic copper nitrate, in the total gas generant composition.
[0041] The gas generant may include combinations of oxidizers, such that the oxidizer comprising
copper may be nominally considered to be a primary oxidizer, so that additional oxidizers
are referred to as a secondary oxidizer, and the like. In certain variations, the
gas generant composition may comprise an oxidizer comprising a perchlorate-containing
compound (a compound including a perchlorate group (ClO
4-)). In certain variations, the gas generant compositions may be substantially free
of perchlorate-containing compounds. However, if such perchlorate-containing compounds
are present in relatively small amounts, alkali, alkaline earth, and ammonium perchlorates
are contemplated for use in the gas generant compositions. Particularly suitable perchlorate
oxidizers include alkali metal perchlorates and ammonium perchlorates, such as ammonium
perchlorate (NH
4ClO
4), sodium perchlorate (NaClO
4), potassium perchlorate (KClO
4), lithium perchlorate (LiClO
4), magnesium perchlorate (Mg(ClO
4)
2), and combinations thereof. If perchlorate oxidizers are present in the gas generant,
it is preferably at less than about 3% by weight of the total gas generant composition.
By way of example, a perchlorate containing oxidizer is present in certain embodiments
at about 0.1% to about 3% by weight; and optionally about 0.5 to about 2% by weight
of the gas generant.
[0042] As discussed above, in accordance with the present technology, the gas generant composition
further comprises an endothermic slag-forming component having a large particle size.
In certain variations, the endothermic slag-forming component is selected from the
group consisting of: aluminum hydroxide, hydromagnesite, Dawsonite, magnesium hydroxide,
magnesium carbonate subhydrate, Bohemite, calcium hydroxide, and combinations thereof.
In various aspects, the endothermic slag-forming component may be present at greater
than or equal to about 5% by weight to less than or equal to about 20% by weight of
a total gas generant composition; optionally at greater than or equal to about 7%
to less than or equal to about 18%; optionally at greater than or equal to about 8%
to less than or equal to about 16%; and in certain variations, greater than or equal
to about 10% to less than or equal to about 15% by weight of a total gas generant
composition.
[0043] If desired, a gas generant composition may optionally include additional components
known to those of skill in the art. Such additives typically function to improve the
handling or other material characteristics of the slag which remains after combustion
of the gas generant material; and improve ability to handle or process pyrotechnic
raw materials. By way of non-limiting example, additional ingredients for the gas
generant composition may be selected from the group consisting of: flow aids, pressing
aids, metal oxides, and combinations thereof. If minor ingredients are included in
the gas generant, they may be cumulatively present at less than or equal to about
4% by weight of the total gas generant composition. By way of example, such an additive
may be selected from the group consisting of: flow aids, press aids, metal oxides,
and combinations thereof is present in a gas generant composition, in certain variations
each respective additive is present at greater than or equal to 0% to less than or
equal to about 3% by weight; optionally greater than or equal to about 0.1% to less
than or equal to about 2% by weight, and in certain variations, optionally greater
than or equal to about 0.5% to less than or equal to about 1% by weight of the gas
generant, so that the total amount of additives is less than or equal to about 4%.
[0044] Press aids used during compression processing, include lubricants and/or release
agents, such as graphite, calcium stearate, magnesium stearate, molybdenum disulfide,
tungsten disulfide, graphitic boron nitride, may be optionally included in the gas
generant compositions, by way of non-limiting example. Conventional flow aids may
also be employed, such as high surface area fumed silica.
[0045] The gas generant compositions may optionally include a metal oxide that serves as
a viscosity modifying compound or an additional slag forming agent (in addition to
the endothermic slag-forming component described above). Suitable metal oxides may
include silicon dioxide, cerium oxide, ferric oxide, titanium oxide, zirconium oxide,
bismuth oxide, molybdenum oxide, lanthanum oxide and the like.
[0046] A gas generant composition according to certain aspects of the present disclosure
comprises a fuel component, an oxidizer comprising basic copper nitrate, and an endothermic
slag-forming component having an average particle size diameter of greater than or
equal to about 150 µm. Such a gas generant composition preferably has a maximum flame
temperature at combustion (T
c) of less than or equal to about 1,900K (1,627°C). The gas generant composition may
further comprise a co-oxidizer, such as a perchlorate-based compound. In certain variations,
a gas generant composition comprises greater than or equal to about 5% to less than
or equal to about 70% by weight of the gas generant composition, an oxidizer comprising
basic copper nitrate present at greater than or equal to about 25% to less than or
equal to about 75% by weight of the gas generant composition, a co-oxidizer comprising
a perchlorate-based compound present at greater than or equal to 0% to less than or
equal to about 3% by weight of the gas generant composition, and an endothermic slag-forming
component having an average particle size diameter of greater than or equal to about
150 µm present at greater than or equal to about 5% to less than or equal to about
20% by weight of the gas generant composition. In certain variations, the gas generant
composition may further comprise an additive selected from the group consisting of:
flow aids, press aids, metal oxides, and combinations thereof, wherein a cumulative
amount of the additive(s) is greater than or equal to 0% to less than or equal to
about 4% of the gas generant composition. The inventive gas generant formulations
are cool burning and show a significant improvement in slagging, as will be discussed
in greater detail below.
[0047] In other variations, a gas generant composition comprises a fuel selected from the
group consisting of: guanidine nitrate, copper bis guanylurea dinitrate, hexamine
cobalt (III) nitrate, copper diammine bitetrazole, and combinations thereof, present
at greater than or equal to about 25% to less than or equal to about 70% by weight.
The gas generant also comprises an oxidizer comprising basic copper nitrate present
at greater than or equal to about 25% to less than or equal to about 75% by weight
of the gas generant composition. In certain aspects, the gas generant composition
may further comprise a co-oxidizer, such as a perchlorate-based compound present at
greater than or equal to 0% to less than or equal to about 3%. Further, the gas generant
includes an endothermic slag-forming component having an average particle size diameter
of greater than or equal to about 150 µm selected from the group consisting of: aluminum
hydroxide, hydromagnesite, Dawsonite, magnesium hydroxide, magnesium carbonate subhydrate,
Bohemite, calcium hydroxide, and combinations thereof, which is present at greater
than or equal to about 5% to less than or equal to about 20% by weight of the gas
generant composition. In certain variations, the gas generant composition comprises
an additive selected from the group consisting of: flow aids, press aids, metal oxides,
and combinations thereof, where a cumulative amount of the additive(s) is greater
than or equal to 0% to less than or equal to about 4% of the gas generant composition.
Such a gas generant composition preferably has a maximum flame temperature at combustion
(T
c) of less than or equal to about 1,900K (1,627°C) and can achieve a resultant flame
temperature of between about 1,350K (1,077°C) to 1,450K (1,177°C).
[0048] In certain other variations, a gas generant composition comprises a fuel comprising
guanidine nitrate present at greater than or equal to about 25% to less than or equal
to about 70% by weight. The gas generant also includes an oxidizer comprising basic
copper nitrate at greater than or equal to about 25% to less than or equal to about
75% by weight of the gas generant composition. In certain variations, a co-oxidizer
is optionally present, for example a co-oxidizer that comprises a perchlorate-based
compound present at greater than or equal to 0% to less than or equal to about 3%
by weight of the gas generant composition. Further, the gas generant includes an endothermic
slag-forming component comprising aluminum hydroxide (Al(OH)
3) having an average particle size diameter of greater than or equal to about 150 µm
present at greater than or equal to about 5% to less than or equal to about 20% by
weight of the gas generant composition. In certain variations, such a gas generant
composition optionally comprises an additive selected from the group consisting of:
flow aids, press aids, metal oxides, and combinations thereof, where a cumulative
amount of the additive(s) is greater than or equal to 0% to less than or equal to
about 4% of the gas generant composition. Such a gas generant composition preferably
has a maximum flame temperature at combustion (T
c) of less than or equal to about 1,900K (1,627°C) and can achieve a resultant flame
temperature of between about 1,350K (1,077°C) to 1,450K (1,177°C).
[0049] In yet other variations, a gas generant composition according to certain aspects
of the present disclosure consists essentially of a fuel component, an oxidizer comprising
basic copper nitrate, and an endothermic slag-forming component having an average
particle size diameter of greater than or equal to about 150 µm. Such a gas generant
composition preferably has a maximum flame temperature at combustion (T
c) of less than or equal to about 1,900K (1,627°C). In certain variations, a gas generant
composition consists essentially of greater than or equal to about 25% of a fuel to
less than or equal to about 70% by weight of the gas generant composition, an oxidizer
comprising basic copper nitrate present at greater than or equal to about 25% to less
than or equal to about 75% by weight of the gas generant composition, a co-oxidizer
comprising a perchlorate-based compound present at greater than or equal to 0% to
less than or equal to about 3% by weight of the gas generant composition, and an endothermic
slag-forming component having an average particle size diameter of greater than or
equal to about 150 µm present at greater than or equal to about 5% to less than or
equal to about 20% by weight of the gas generant composition and an optional additive
selected from the group consisting of: flow aids, press aids, metal oxides, and combinations
thereof, wherein a cumulative amount of the additive(s) is greater than or equal to
0% to less than or equal to about 4% of the gas generant composition.
[0050] In other variations, a gas generant composition consists essentially of a fuel selected
from the group consisting of: guanidine nitrate, copper bis guanylurea dinitrate,
hexamine cobalt (III) nitrate, copper diammine bitetrazole, and combinations thereof;
an oxidizer comprising basic copper nitrate; a co-oxidizer comprising a perchlorate-based
compound present at greater than or equal to 0% to less than or equal to about 3%
by weight of the gas generant composition; an endothermic slag-forming component having
an average particle size diameter of greater than or equal to about 150 µm selected
from the group consisting of: aluminum hydroxide, hydromagnesite, Dawsonite, magnesium
hydroxide, magnesium carbonate subhydrate, Bohemite, calcium hydroxide, and combinations
thereof; and an optional additive selected from the group consisting of: flow aids,
press aids, metal oxides, and combinations thereof. Such a gas generant composition
preferably has a maximum flame temperature at combustion (T
c) of less than or equal to about 1,900K (1,627°C) and can achieve a resultant flame
temperature of between about 1,350K (1,077°C) to 1,450K (1,177°C).
[0051] In yet other variations, a gas generant composition consists essentially of a fuel
selected from the group consisting of: guanidine nitrate, copper bis guanylurea dinitrate,
hexamine cobalt (III) nitrate, copper diammine bitetrazole, and combinations thereof,
present at greater than or equal to about 25% to less than or equal to about 70% by
weight; an oxidizer comprising basic copper nitrate present at greater than or equal
to about 25% to less than or equal to about 75% by weight of the gas generant composition;
a co-oxidizer comprising a perchlorate-based compound present at greater than or equal
to 0% to less than or equal to about 3% by weight of the gas generant composition;
an endothermic slag-forming component having an average particle size diameter of
greater than or equal to about 150 µm selected from the group consisting of: aluminum
hydroxide, hydromagnesite, Dawsonite, magnesium hydroxide, magnesium carbonate subhydrate,
Bohemite, calcium hydroxide, and combinations thereof, which is present at greater
than or equal to about 5% to less than or equal to about 20% by weight of the gas
generant composition; and an optional additive selected from the group consisting
of: flow aids, press aids, metal oxides, and combinations thereof, where a cumulative
amount of the additive(s) is greater than or equal to 0% to less than or equal to
about 4% of the gas generant composition. Such a gas generant composition preferably
has a maximum flame temperature at combustion (T
c) of less than or equal to about 1,900K (1,627°C) and can achieve a resultant flame
temperature of between about 1,350K (1,077°C) to 1,450K (1,177°C).
[0052] In certain other variations, a gas generant composition consists essentially of a
fuel comprising guanidine nitrate, an oxidizer comprising basic copper nitrate, a
co-oxidizer comprising a perchlorate-based compound, an endothermic slag-forming component
comprising aluminum hydroxide (Al(OH)
3) having an average particle size diameter of greater than or equal to about 150 µm,
and an optional additive selected from the group consisting of: flow aids, press aids,
metal oxides, and combinations thereof. Such a gas generant composition preferably
has a maximum flame temperature at combustion (T
c) of less than or equal to about 1,900K (1,627°C).
[0053] In other embodiments, a gas generant composition consists essentially of a fuel comprising
guanidine nitrate, an oxidizer comprising basic copper nitrate, an endothermic slag-forming
component comprising aluminum hydroxide (Al(OH)
3) having an average particle size diameter of greater than or equal to about 150 µm,
and an optional additive selected from the group consisting of: flow aids, press aids,
metal oxides, and combinations thereof. In certain variations, the fuel comprising
guanidine nitrate is present at greater than or equal to about 25% to less than or
equal to about 70% by weight. The oxidizer comprising basic copper nitrate can be
present at greater than or equal to about 25% to less than or equal to about 75% by
weight of the gas generant composition. Further, the aluminum hydroxide is present
at greater than or equal to about 5% to less than or equal to about 20% by weight
of the gas generant composition. The additive or additives may be present in a cumulative
total amount of greater than or equal to 0% to less than or equal to about 4% of the
gas generant composition. Such a gas generant composition preferably has a maximum
flame temperature at combustion (T
c) of less than or equal to about 1,900K (1,627°C).
Example 1
[0054] Experiments are performed to determine the effect of aluminum hydroxide particle
size on slag formation in a representative gas generant formulation. Comparative Example
1 has a conventional smaller size of aluminum hydroxide particle, while Example 2
is prepared in accordance with certain aspects of the present teachings. The ingredients
for the gas generant and their properties for both Comparative Example 1 and Example
2 are given in Table 2.
Table 2
| Ingredient |
Comparative Example 1 |
Example 2 |
| % basic copper nitrate |
38.68 |
38.68 |
| % guanidine nitrate |
17.27 |
17.27 |
| % copper bis guanylurea dinitrate |
28.84 |
28.84 |
| % glass fibers |
0.88 |
0.88 |
| % aluminum hydroxide |
14.32 |
14.32 |
| 10% Particle Size Distribution (PSD) Aluminum Hydroxide |
54 µm |
115 µm |
| 50% PSD Aluminum Hydroxide |
87 µm |
158µm |
| 90% PSD Aluminum Hydroxide |
152 µm |
228 µm |
| Flame Temperature K |
1,400 |
1,400 |
[0055] The respective formulations are prepared and pressed into 0.5" diameter by 0.43"
cylinders at 12,000 lbs force. These samples are prepared by spray drying a formulation
containing guanidine nitrate, basic copper nitrate, copper bis guanylurea dinitrate,
and glass fibers. The spray dried formulation is then dry blended with the different
particle size aluminum hydroxide and pressed into the 0.5 x 0.43" diameter cylinder.
Cylinders are then burned in a 1 liter enclosed bomb under 3,000 psi nitrogen. Slag
from Comparative Example 1, although in the shape of the original cylinder, had very
low density and fell apart to the touch. Slag from Example 2 maintains the shape of
the original cylinder, has good density, and does not fall apart when handling. Macroscopic
and microscope pictures of slag from Comparative Example 1 and Example 2 are shown
in Figures 3-4 (Comparative Example 1) and 5-6 (Example 2), respectively. Magnification
is 50X in the microscopic pictures in Figures 4 and 6.
[0056] The combustion slag in Figure 4 shows spheres of molten copper and spheres of aluminum
oxide loosely associated with each other, which results in very weak slag that falls
apart and can breach the filter and enter the airbag during deployment. The combustion
slag in Figure 6 shows large spheres of aluminum oxide coated and surrounded by a
molten copper matrix. This results in slag with greater structural strength that resists
coming apart and breaching the filter during combustion. While not limiting the present
disclosure to any particular theory, it is believed that a larger particle size aluminum
hydroxide stays cooler longer during combustion, for example, due to reduced surface
area and slower heat transfer, as compared to smaller particles of aluminum hydroxide.
The cooler surfaces thus can provide a site for molten copper to condense on as it
is formed resulting in an improved slagging product.
Example 2
[0057] Gas generants of Comparative Example 1 and Example 2 described in the context of
Example 1 are also pressed into 0.25" diameter x 0.060" tablets, loaded into a driver
side automotive airbag inflator, and deployed into a 60 liter tank. After deployment,
the tank is washed down and the wash water collected. The insoluble particulate is
captured on a filter and weighed after drying. Any soluble particulate is precipitated
by evaporation of the wash water and weighed. The total particulate escaping the combustion
filter is determined by adding the weights of the soluble and insoluble particulate
found in the tank. This value is called the "tank wash value."
[0058] Tank wash values for gas generants from Comparative Example 1 and Example 2 are given
in Table 3.
Table 3
| |
Comparative Example 1 |
Example 2 |
| Tank Wash (g) |
2.5 - 3.9 |
0.5 - 0.9 |
[0059] As shown in Table 3, the amount of particulate escaping the filter is greatly reduced
when using the inventive gas generant from Example 2 (having a large particle size
aluminum hydroxide), as compared to gas generant from Comparative Example 1 (having
a small particle size aluminum hydroxide). For example, a minimum reduction of tank
wash value (and thus enhancement of slag formation) is 64%, while a maximum reduction
of tank wash value is 87%. An average reduction in tank wash value is 78%. Thus, by
introducing large particle size aluminum hydroxide in accordance with certain aspects
of the present disclosure, a significant enhancement in slag formation occurs for
gas generant compositions.
[0060] The inflator combustion chambers from these tests are machined open and the combustion
slag is visually examined. Pictures of the post-fire combustion slags from Comparative
Example 1 and Example 2 are shown in Figures 7 and 8. As the pictures show, the slag
in Figure 7 from gas generant in Comparative Example 1 is very weak, most of it ending
up as a loose powder in the combustion chamber. The slag in Figure 8 from an inventive
gas generant in Example 2 is quite intact, maintaining the shape of the original tablets
with very little loose powder present.
[0061] Thus, in certain aspects, the present disclosure provides a method of enhancing slag
formation for a gas generant composition. The method comprises introducing an endothermic
slag-forming component having an average particle diameter size of greater than or
equal to about 150 µm to a gas generant composition that comprises copper. In certain
embodiments, the gas generant comprises a fuel and an oxidizer comprising copper.
In further embodiments, the gas generant comprises a fuel and an oxidizer comprising
basic copper nitrate. Any of the gas generant compositions described previously above
are contemplated. Similarly, any of the endothermic slag-forming components described
previously are contemplated for use in these methods. The introducing of the endothermic
slag-forming component enhances slag formation during combustion of the gas generant
composition by at least 50%, as measured by reduced tank wash values. In certain variations,
such methods desirably enhance slag formation by at least 55%, optionally by at least
60%, optionally by at least 63%, optionally by at least 64%, optionally by at least
65%, optionally by at least 70%, optionally by at least 75%, optionally by at least
78%, optionally by at least 80%, optionally by at least 85%, and in certain variations,
optionally by at least 87%.
[0062] In certain aspects, the gas generant composition to which the endothermic slag-forming
component is added has a maximum flame temperature at combustion (T
c) of less than or equal to about 1,900K (1,627°C), where the fuel is selected from
the group consisting of: guanidine nitrate, copper bis guanylurea dinitrate, hexamine
cobalt (III) nitrate, copper diammine bitetrazole, and combinations thereof. The endothermic
slag-forming component may be selected from the group consisting of: aluminum hydroxide,
hydromagnesite, Dawsonite, magnesium hydroxide, magnesium carbonate subhydrate, Bohemite,
calcium hydroxide, and combinations thereof. In certain variations, the maximum flame
temperature at combustion (T
c) of the gas generant is greater than or equal to about 1,350K (1,077°C) to less than
or equal to about 1,450K (1,177°C).
[0063] In certain preferred variations, the endothermic slag-forming component introduced
to the gas generant, which enhances slag formation, comprises aluminum hydroxide and
is present at greater than or equal to about 5% by weight to less than or equal to
about 20% by weight of a total gas generant composition. Thus, introducing a large
particle size aluminum hydroxide, for example, with an average particle diameter size
of greater than or equal to about 150 µm, into a gas generant provides a desirably
cool burning gas generant that has superior, enhanced slag formation.
1. Gasgeneratorzusammensetzung, umfassend:
einen Brennstoff;
ein Oxidationsmittel, das basisches Kupfernitrat umfasst; und
einen endothermen schlackenbildenden Bestandteil mit einem mittleren Teilchendurchmesser
von größer gleich ungefähr 150 µm, wobei die Gasgeneratorzusammensetzung eine maximale
Flammentemperatur bei der Verbrennung (Tc) von kleiner gleich ungefähr 1900 K (1627
°C) aufweist.
2. Gasgeneratorzusammensetzung nach Anspruch 1, wobei der endotherme schlackenbildende
Bestandteil eine Zersetzungstemperatur in einem Bereich von größer gleich ungefähr
180 °C bis kleiner gleich ungefähr 450 °C aufweist.
3. Gasgeneratorzusammensetzung nach Anspruch 1, wobei der endotherme schlackenbildende
Bestandteil zu einem Gewichtsanteil von mehr als oder gleich ungefähr 5 Gew.-% bis
weniger als oder gleich ungefähr 20 Gew.-% der Gesamt-Gasgeneratorzusammensetzung
vorliegt.
4. Gasgeneratorzusammensetzung nach Anspruch 1, wobei der endotherme schlackenbildende
Bestandteil aus der Gruppe ausgewählt ist bestehend aus: Aluminiumhydroxid, Hydromagnesit,
Dawsonit, Magnesiumhydroxid, Magnesiumcarbonat-Subhydrat, Böhmit, Calciumhydroxid
und Kombinationen daraus.
5. Gasgeneratorzusammensetzung nach Anspruch 1, wobei der Brennstoff aus der Gruppe ausgewählt
ist bestehend aus: Guanidinnitrat, Kupfer-bis-Guanylharnstoff-dinitrat, Hexammincobalt(III)-nitrat,
Kupferdiammin-bitetrazol und Kombinationen daraus.
6. Gasgeneratorzusammensetzung nach Anspruch 1, wobei das Oxidationsmittel, das basisches
Kupfernitrat umfasst, zu einem Gewichtsanteil von mehr als oder gleich ungefähr 30
% bis weniger als oder gleich ungefähr 70 Gew.-% der Gasgeneratorzusammensetzung vorliegt.
7. Gasgeneratorzusammensetzung nach Anspruch 1, wobei der endotherme schlackenbildende
Bestandteil einen mittleren Teilchendurchmesser von größer gleich ungefähr 200 µm
aufweist.
8. Gasgeneratorzusammensetzung nach Anspruch 1, wobei der Brennstoff zu einem Gewichtsanteil
von mehr als oder gleich ungefähr 25 % bis weniger als oder gleich ungefähr 70 Gew.-%
der Gesamt-Gasgeneratorzusammensetzung vorliegt; das Oxidationsmittel zu einem Gewichtsanteil
von mehr als oder gleich ungefähr 25 % bis weniger als oder gleich ungefähr 75 Gew.-%
der Gesamt-Gasgeneratorzusammensetzung vorliegt; der endotherme schlackenbildende
Bestandteil zu einem Gewichtsanteil von mehr als oder gleich ungefähr 5 % bis weniger
als oder gleich ungefähr 20 Gew.-% der Gesamt-Gasgeneratorzusammensetzung vorliegt;
und mehr als oder gleich 0 % bis weniger als oder gleich ungefähr 4 % von einem oder
mehreren Gasgeneratorzusätzen, ausgewählt aus der Gruppe bestehend aus: Fließhilfsmitteln,
Presshilfsmitteln, Metalloxiden und Kombinationen daraus.
9. Gasgeneratorzusammensetzung nach Anspruch 8, ferner umfassend ein Co-Oxidationsmittel,
das eine Verbindung auf Basis von Perchlorat umfasst, die zu einem Gewichtsanteil
von mehr als 0 % bis weniger als oder gleich ungefähr 3 Gew.-% der Gesamt-Gasgeneratorzusammensetzung
vorliegt.
10. Gasgeneratorzusammensetzung nach Anspruch 1, wobei der endotherme schlackenbildende
Bestandteil Aluminiumhydroxid mit einem mittleren Teilchendurchmesser von größer gleich
ungefähr 150 µm umfasst, und wobei die maximale Flammentemperatur bei der Verbrennung
(Tc) größer gleich ungefähr 1350 K (1077 °C) bis kleiner gleich ungefähr 1450 K (1177
°C) beträgt.
11. Gasgeneratorzusammensetzung nach Anspruch 1, wobei der endotherme schlackenbildende
Bestandteil Aluminiumhydroxid umfasst und einen mittleren Teilchendurchmesser von
größer gleich ungefähr 200 µm aufweist.
12. Verfahren zur Verbesserung der Schlackenbildung für eine Gasgeneratorzusammensetzung,
wobei das Verfahren Folgendes umfasst:
Einbringen eines endothermen schlackenbildenden Bestandteils mit einem mittleren Teilchendurchmesser
von größer gleich ungefähr 150 µm in eine Gasgeneratorzusammensetzung, die einen Brennstoff
und ein Oxidationsmittel umfasst, das basisches Kupfernitrat umfasst, wobei das Einbringen
des endothermen schlackenbildenden Bestandteils die Schlackenbildung während der Verbrennung
des Gasgeneratorzusammensetzung um mindestens 50 % verbessert,
wobei die Gasgeneratorzusammensetzung eine maximale Flammentemperatur bei der Verbrennung
(Tc) von kleiner gleich ungefähr 1900 K (1627 °C) aufweist, der Brennstoff aus der
Gruppe ausgewählt wird bestehend aus: Guanidinnitrat, Kupfer-bis-Guanylharnstoff-dinitrat,
Hexammin-Cobalt(III)-nitrat, Kupferdiammin-bitetrazol und Kombinationen daraus, und
der endotherme schlackenbildende Bestandteil aus der Gruppe ausgewählt wird bestehend
aus: Aluminiumhydroxid, Hydromagnesit, Dawsonit, Magnesiumhydroxid, Magnesiumcarbonat-Subhydrat,
Böhmit, Calciumhydroxid und Kombinationen daraus.
13. Verfahren nach Anspruch 12, wobei der endotherme schlackenbildende Bestandteil, der
die Schlackenbildung verbessert, Aluminiumhydroxid umfasst und zu einem Gewichtsanteil
von mehr als oder gleich ungefähr 5 Gew.-% bis weniger als oder gleich ungefähr 20
Gew.-% der Gesamt-Gasgeneratorzusammensetzung vorliegt.
14. Verfahren nach Anspruch 12, wobei durch das Einbringen des endothermen schlackenbildenden
Bestandteils die Schlackenbildung während der Verbrennung der Gasgeneratorzusammensetzung
um mindestens 60 % verbessert wird.