Technical Field
[0001] This invention relates to electromagnetic radiation absorbing materials which comprise
dissipative particles dispersed in dielectric binders.
Background
[0002] Electromagnetic radiation absorbing materials typically comprise one or more kinds
of dissipative particles dispersed through a dielectric binder material. For example,
U.S. Patent 4,173,018 (Dawson et al.) discloses a material comprising an insulating
resin and solid iron spheres of 3 microns diameter, or solid glass spheres of 0.4
micron diameter having a single 1.3 micron thick iron coating, for a total diameter
of 3 microns. The particles comprise up to 90% of the weight of the composite material.
[0003] Substantially spherical solid particles of such sizes are often called "microspheres."
A variation on the microsphere is the "microbubble," a hollow microsphere made of
a material such as glass. Single thin film layers of nonmagnetic metal may be deposited
on glass microbubbles, and the product dispersed through polymeric hinders, as taught
in U.S. Patent 4,618,525 (Chamberlain et al.)
[0004] Singly layered microbubbles dispersed through polymeric hinders have been used in
electromagnetic shielding applications. For example, U.S. Patent 4,624,798 (Gindrup
et al.) describes a composite material in which the microbubbles form a network of
contacting particles, giving the bulk material sufficient electrical conductivity
to act as a radiation shield, i.e., like a sheet of conductive material.
Summary of Invention
[0005] The invention is a non-electrically-conductive electromagnetic radiation absorbing
material, comprising a plurality of dissipative particles and a dielectric binder
through which the dissipative particles are dispersed. Any of the dissipative particles
comprises: (a) a core particle; (b) a dissipative layer located on the surface of
the core particle; and (c) an insulating layer overlaying the dissipative layer at
a thickness between 0.5 and 10 nanometers.
Brief Description of the Drawing
[0006] Figure 1 is a cross sectional view of one embodiment of the invention.
[0007] Figure 2 is a graph of the calculated reflection magnitude of radiation normally
incident upon a surface of two embodiments of the invention, as a function of incident
radiation frequency.
Detailed Description
[0008] One preferred embodiment of the invention is a radiation absorbing tile. Figure 1
is a cross sectional view of this embodiment, in which such a tile 10 comprises a
radiation absorbing material 12. This absorbing material 12 is applied to the radiation-incident
side (in the figure, the upper side) of an optional second component, an electrically
conductive material 18. The electrically conductive material 18 is preferred because
it reflects radiation which is not fully absorbed back into the absorbing material
12 for further absorption. Also shown is an optional impedance matching material 16.
The impedance matching material 16 is preferred because it reduces reflection of the
incident radiation from the radiation-incident side of the absorbing material 12.
[0009] The absorbing material 12 comprises a plurality of doubly layered dissipative particles
11, dispersed in a dielectric binder material 14 by mixing or extrusion. Any of the
doubly layered dissipative particles 11 comprises a core particle 13, a dissipative
layer 15, and an insulating layer 17, the latter being the outermost layer.
[0010] The core particle material may be the same as the dielectric binder material, but,
in the usual case, the two materials will not be the same, as the criteria for choosing
the two materials do not exactly coincide.
[0011] The dissipative layer 15 is deposited on the core particle 13 by thin film deposition
techniques. The insulating layer 17 may be deposited on the dissipative layer 15 by
such deposition techniques, or it may be formed as a reaction product of the dissipative
layer 15. The remainder of this discussion assumes that each member of the plurality
of doubly layered particles has essentially the same thickness of dissipative layer
15, but this is not required. Generally, thicker dissipative layers absorb more radiation
at higher frequencies. Thus, the need for either a broadband or narrowband absorber
will suggest an appropriate distribution of dissipative layer thicknesses.
[0012] The preferred core particles 13 have as low a dielectric constant and weigh as little
as possible. The core particles 13 may be essentially spherical particles, or acicular
fibers, or flakes. Optimum performance is achieved if the core particle size distribution
is narrow, and thus in the ideal case all the core particles 13 are the same size.
The core particles 13 are formed preferably from a ceramic or polymeric material.
[0013] If essentially spherical particles are used for the core particles 13, the preferences
for low dielectric constant and low weight suggest (hollow) microbubbles, not (solid)
microspheres. The preferred inorganic material for the microbubbles is glass, but
polymeric materials are suitable. For glass microbubbles an average outer diameter
in the range of 10 to 500 microns, and a thickness (difference between inner and outer
average radii) of 1-2 microns, are suitable. The preferred range of average outer
diameters is 20 to 80 microns. The preferred glass microbubbles are identified by
Minnesota Mining and Manufacturing Company as "SCOTCHLITE" brand glass microbubbles.
[0014] Another technique for reducing the dielectric constant of the inorganic core particles
13 is to reduce their density. One method for this is to screen them through a sieve,
floating in methanol those which do not pass through, and discarding those which do
not float. When S60/10000 "SCOTCHLITE" brand microbubbles having a density of 0.60
g/cc were screened through a size #325 mesh sieve (44 micron diameter opening), this
process produced microbubbles having an average diameter of 70 microns, with 90% of
the diameters ranging between 50 and 88 microns. (This narrow particle size distribution
is preferred, but not affected by the floating in methanol.) About 23% by weight (8%
by volume) of the screened microbubbles did not float.
[0015] To allow doubly layered microbubbles to remain intact through dispersion into the
binder material, the unlayered microbubbles should be strong enough to remain uncrushed
when subjected to pressure of preferably at least about 6.9x10⁵ Pascal. The preferred
type S60/10000 "SCOTCHLITE" brand glass microbubbles are even stronger, resisting
a pressure up to about 6.9x10⁷ Pascal. Embodiments of the invention using these stronger
microbubbles in silicone rubber binders may have volume loading factors of up to 60%
without significant breakage of the doubly layered microbubbles.
[0016] If acicular fibers are used, polymeric materials may be used, but the preferred material
is either milled glass or the ceramic product identified by the Minnesota Mining and
Manufacturing Company as "NEXTEL" 440. The lattermost fibers have an average diameter
of 8 to 10 microns, and preferably have aspect ratios ranging from 1 to 40, as may
be made from longer fibers by chopping with a razor blade. If inorganic flakes are
used, the preferred material is mica.
[0017] The dissipative layer 15 is an inorganic material, which may be a metal or a semiconductor.
Preferred materials are tungsten, chromium, aluminum, copper, titanium, titanium nitride,
molybdenum disilicide, iron, iron suboxide, zirconium, and stainless steel.
[0018] The dissipative layer 15 is extremely thin relative to the core particle size. For
materials having metallic conductivity, the thickness is in the range of 0.05 nanometer
to 10 nanometers, and preferably about 0.4 nm to 2.0 nm, depending on the material
chosen. Layers of such extreme thinness are often termed "ultrathin" layers or films.
For semiconductive materials, which are less conductive than metals, the layer thickness
will be proportionately larger. The thickness of the inorganic layer 15 should be
uniform to within ten percent, and preferably to within five percent. In general,
this is accomplished by reducing the deposition rate and increasing the deposition
time.
[0019] An effective lower limit on the amount of material in the dissipative layer 15 follows
from the identity of the material. Relatively small amounts of material will not form
an ultrathin layer, but instead small "beads" in one or more locations on the surface
of the core particle 11. This reduces the absorption performance of the invention.
Thus, because materials differ in their tendencies to form beads, the identity of
the material effectively sets a lower limit on the amount of material required to
form an ultrathin layer at all. Therefore, for the purposes of this invention, the
term "ultrathin layer" describes a layer having a sufficient amount of material to
avoid forming beads on the layer substrate (which may be the core material, or another
ultrathin layer).
[0020] Even if an ultrathin layer is formed, it may be a "contiguous" layer, i.e., one in
which discontinuities larger than atomic size exist in the layer, but the discontinuities
are not so large that beads are formed on a substantial portion of the surface of
the layer substrate. However, in a preferred embodiment, the ultrathin layer is sufficiently
thick to cover the entire layer substrate in a continuous shell. The term "continuous"
includes ultrathin layers which have atomic-sized discontinuities, or "pinholes,"
which are so small that they do not eliminate electrical continuity because of electron
tunneling or other phenomena.
[0021] The electromagnetic radiation absorption properties of the invention may be attributed
to the polarization of the dissipative layer 15. As the electric field component of
the incident radiation is oriented in one direction, the electrons in the dissipative
layer 15 tend to flow in the opposite direction, producing an electric current and
resistive heating. The energy required to support this heating is removed from the
electric field, and therefore the incident radiation is absorbed.
[0022] However, if the amount of material in the dissipative layer 15 is too great, depolarization
effects occur to reduce the effectiveness of the resistive heating process. The dipole
interaction induced by the electric field polarizes the excess material in the direction
opposite to the induced field (i.e., in the same direction as the incident electric
field), thus reducing the amount of induced electric current.
[0023] A way to identify a suitable range of thicknesses is to consider a parameter "B."
For spherically shaped dissipative particles 11, B is known as the "bubble parameter,"
and is the ratio of the product of the frequency of incident radiation and the core
particle radius, divided by the product of the thickness of the dissipative layer
and the conductivity of the dissipative layer. Generally the radiation frequency for
the intended application and the core particle radius are known, and the process conditions
varied to adjust the dissipative layer thickness and conductivity.
[0024] The conductivity of the ultrathin layer is not the same as the bulk conductivity
of the material from which the layer is made. This is because the electronic behavior
of ultrathin films is inherently different from that of bulk materials, and because
impurities entraped in the ultrathin layer have a great effect due to their proportionately
greater presence in the material.
[0025] Ultrathin film conductivity can be varied by adjusting composition (e.g., for iron
suboxide, the amount of oxygen introduced in the deposition chamber is controlled).
For metals, the ultrathin film conductivity is held approximately constant and the
thickness is controlled. Generally, thicker layers are desirable for higher incident
frequencies, and vice versa. For tungsten layered microbubbles, the optimum values
of B for the 1-20 GHz range follow from a 1 nm thick tungsten layer on a microbubble
of about 50 micron outer diameter.
[0026] The insulating layer 17 is preferably made of aluminum oxide, silicon dioxide, zirconium
oxide, or titanium dioxide. The choice of material for the dissipative layer 15 influences
the choice of material for the insulating layer 17. For example, when molybdenum disilicide
is used in the dissipative layer 15, silicon dioxide is the preferred material for
the insulating layer 17, because it may be formed by thermal oxidation of the outer
surface of the molybdenum disilicide, without direct deposition of a second layer.
A similar situation applies to zirconium oxide layered on zirconium, and titanium
dioxide layered on titanium or titanium nitride. Of course, in all these examples
the insulating layer 17 could be separately deposited on the inorganic layer 15. Thus,
in practice, the insulating layer 17 may be a reaction product of the dissipative
layer 15, but it need not be.
[0027] However formed, the insulating layer 17 overlays the inorganic layer 15 at a thickness
of about 1 to 10 nm, preferably about 2 nm. The insulating layer 17 allows the dissipative
particles 11 to be present in the absorbing material 12 at fairly high volume loading
ratios, despite possible contact between the particles. Such contact can cause the
absorbing material 12 to become effectively a conductive sheet which reflects, rather
than absorbs, radiation. The insulating layer 17 also helps prevent degradation of
the dissipative layer 15 due to oxidation or other processes. Ultrathin metal films
are expected to oxidize over time, which will result in a change to to the composite
material permittivity. With ultrathin tungsten films, measurable changes in powder
resistivity occur in a period of hours in some cases. The addition of the aluminum
suboxide layer results in a material with permitivity which is constant over a period
of months or more. As with the dissipative layer 15, the insulating layer 17 is an
ultrathin layer which may be contiguous, but in preferred embodiments it is continuous,
and uniform in thickness.
[0028] The dielectric binder 14 may be made from a ceramic, polymeric, or elastomeric material.
Ceramic binders are preferred for applications requiring exposure to high temperatures,
while polymeric binders are preferred for their flexibility and lightness. Many polymeric
binders are suitable, including polyethylenes, polypropylenes, polymethylmethacrylates,
urethanes, cellulose acetates, epoxies, and polytetrafluoroethylene (PTFE). Suitable
elastomeric binders are natural rubbers and synthetic rubbers, such as the polychloroprene
rubbers known by the tradename "NEOPRENE" and those based on ethylene propylene diene
monomers (EPDM). Other preferred binders are silicone compounds available from General
Electric Company under the designations RTV-11 and RTV-615.
[0029] The dielectric binder could be a made from thermosetting or thermoplastic material.
Thermosetting materials, once heated, irreversibly cure and cannot be remelted to
be reformed. Thermoplastic materials can be repeatedly heated and reformed. In either
case, the materials may be heated and set into a form by one or more forces external
to the binder. Typically the force is due to heat conduction, or pressure, but it
may be the influence of gravity or a vacuum. In this respect the binders suitable
for the present invention differ from the "conformable" materials taught in U.S. Patent
4,814,546 (Whitney et al.), which require molecular forces internal to the binder
(such as a mechanical stress in a stretchable material) to be responsible for the
change in shape of the absorber.
[0030] Many types of adhesives have the required thermoplastic or thermosetting properties.
An adhesive is a material which forms intimate contact with a surface such that mechanical
force can be transferred across the contact interface. Suitable thermoplastic and
thermosetting adhesives include (but are not limited to) polyamides, polyethylenes,
polypropylenes, polymethylmethacrylates, urethanes, cellulose acetates, vinyl acetates,
epoxies, and silicones.
[0031] Alternatively, the conformable materials mentioned above are also suitable for other
embodiments of the invention. For example, a thermoplastic heat-shrinkable binder
may be formed from cross-linked or oriented crystallizable materials such as polyethylene,
polypropylene, and polyvinyl chloride; or from amorphous materials such as silicones,
polyacrylates, and polystyrenes. Solvent-shrinkable or mechanically stretchable binders
may be elastomers such as natural rubbers or synthetic rubbers such as reactive diene
polymers; suitable solvents are aromatic and aliphatic hydrocarbons. Specific examples
of such materials are taught in U.S. Patent 4,814,546 (Whitney et al.).
[0032] The binder may be homogenous, or a matrix of interentangled fibrils, such as the
PTFE matrix taught in U.S. Patent 4,153,661 (Ree et al.). In general, an absorber
of this embodiment is formed in a fibrillation process involving the formation of
a water-logged paste of doubly layered particles and PTFE particles, intensive mixing
at about 50° to about 100°C, biaxial calendering at about 50° to about 100°C, and
drying at about 20° to about 100°C. The composite of PTFE fibrils and particles has
the high tensile strength of the PTFE matrix.
[0033] To be effective, the absorbing material 12 should have a thickness in the direction
of radiation propagation greater than about one-fourtieth (2.5 percent) of the wavelength
absorbed. The invention is suitable for absorbing radiation over as broad an incident
frequency range as possible in the region of approximately 2 to 40 GHz. This implies
a thickness greater than the order of about 0.2 mm. Thicker layers generally provide
greater absorption, but the increased weight and reduced flexibility are not desired
in many applications. Thus, while layers having thicknesses up to one-fourth (25 percent)
of the absorbed wavelength are possible, they are not preferred. For example, in the
same frequency region this upper thickness limit is on the order of about 37.5 mm,
but sufficient absorption can be obtained with layers on the order of 2.0 mm or less
in thickness.
[0034] The absorbing material 12 may have a reduced specific gravity, which will produce
a reduction in weight of the tile 10. Volume loading factors for composites based
on carbonyl iron microspheres typically range from forty to sixty-five percent, and
the specific density of iron is 7.9 grams/cm². In the present invention the volume
loading factor is in the range of thirty to sixty-five percent, but the specific density
of the doubly layered particles is far less, in the range of 0.10 to 0.60 g/cm². For
example, consider an absorber with sixty percent volume loading of particles and a
binder of specific gravity 1.0. If the absorber is constructed according to the present
invention, the specific gravity of the inventive absorber will be from 0.40 to 0.46.
For a similar but non-inventive absorber comprising iron spheres, the specific gravity
will be 5.1, or about eleven to thirteen times as much as the inventive absorber.
This shows that the metal on the particles of the present invention is used very efficiently,
i.e., it is only about 0.01% (by weight) of the inventive absorber, but about 92%
(by weight) of the non-inventive absorber comprising iron spheres.
[0035] The absorbing material 12 is non-electrically conductive, i.e., it has a high DC
resistivity. If the resistivity is too low, the absorber 12 effectively becomes a
conductive sheet, which reflects radiation instead of absorbing it. The resistivity
of iron, for example, is about 10⁻⁵ ohm-cm at room temperature. Insulators typically
have resistivities of 10¹² ohm-cm or more. Samples of the absorbing material 12 having
60 percent volume loading of layered microbubbles had measured resistivities of greater
than 2x10⁸ ohm-cm at room temperature, indicating that they were non-conductive.
[0036] Any electrically conductive material is suitable for the optional electrically conductive
material 18. The absorbing material 15 may be bound to the electrically conductive
material 18 by extruding the former onto the latter and allowing the former to cure.
Many thermoplastic binders are suitable for extrusion, especially polyvinylchlorides,
polyamides, and polyurethanes. The electrically conductive material 18 may be a wire
or cable in lieu of the flat sheet shown in Figure 1. Alternatives to extrusion include
the use of adhesives, and processes involving in-place thermal casting.
[0037] In any embodiment of the invention, impedance matching of the absorbing material
to the incident medium (usually air) is preferred, but not required. Impedance matching
is done by a material which maximizes transmission of incident radiation to the absorbing
layer. In the embodiment of Figure 1, an optional impedance matching material 16 is
shown as a component of the tile 10. The impedance matching material 16 is bound to
the radiation incident side of the absorbing material 12. Co-extrusion and the use
adhesives are suitable processes for binding the materials together. The dimensions,
weight, and other properties of the impedance matching material 16 are considered
in the design of a complete tile 10.
[0038] A suitable impedance matching layer 16 is a layer of polymeric material having high
volumes of trapped air, such as air-filled, bare, glass microbubbles embedded in the
polymeric binder materials described above. For example, a suitable impedance matching
material comprises 5 to 25 volume percent type S60/10000 "SCOTCHLITE" brand glass
microbubbles, dispersed in a synthetic rubber such as that made from the EPDM resin
identified by E.I duPont de Nemours Company as "NORDEL" brand type 1440.
[0039] Furthermore, a laminated structure, each lamina individually constructed according
to the description above, is possible. For example, one lamina may be an absorber
comprising doubly layered glass microbubbles, a second lamina may be an absorber comprising
doubly layered ceramic fibers, and a third lamina may be an absorber comprising doubly
layered inorganic flakes. Preferably two to five layers are used. The total thickness
of the laminated structure may be as great as 40 centimeters, although generally each
lamina will meet the thickness limitations described above. Use of a laminated structure
allows the absorption profile of the composite structure to be "tuned" to a particular
frequency range and bandwidth of interest.
[0040] The invention need not be in the form of a flat sheet as shown in Figure 1. For a
cylindrical conductor, for example, a pre-sized flexible cylindrical shell absorber
is preferred to minimize possible stretching, cracking, or delamination of a flat
laminated sheet. The pre-formed cylindrical shell could be slit along its length,
wrapped around the conductor (or slid along the long axis of the conductor) with little
distortion, and then adhered into place. The seam formed by the edges of the slit
should be sealed.
[0041] The exact choices of materials depend on the final absorption versus frequency characteristics
desired, and the physical application required. The choices of materials also dictate
the procedure and equipment required to assemble the absorber, as illustrated by the
following examples.
Examples 1 to 8: Aluminum Suboxide and Tungsten Layered Glass Bubbles
[0042] In each example batch, two hundred cubic centimeters of type S60/10000 "SCOTCHLITE"
brand glass microbubbles were screened through a 325 mesh (44 micron) sieve. The microbubbles
which did not pass the sieve were floated in methanol, and those that did not float
were discarded, the remainder then allowed to dry in air. The microbubbles retained
had an average diameter of 70 microns, with 90% of the microbubbles being between
50 and 88 microns, and an average surface area (determined by the BET method) of 0.33
m²/g.
[0043] The microbubbles were prepared using essentially the same method as taught in U.S.
Patent 4,618,525 (Chamberlain, et al.). They were tumbled in a vacumn chamber while
being sputter coated with a vapor of tungsten for 120 minutes. The sputtering cathode
was a water-cooled rectangular target, 12.7 x 20.3 cm in size. The direct current
planar magnetron method was used. The argon sputtering gas pressure was 0.53 Pascal,
and the background pressure was about 1.33x10⁻³ Pascal. Table 1 lists various parameters
and results for the example batches.
Table 1
Example |
Applied Power kW |
Weight Percentage |
Thickness nm |
1-5 |
0.19 |
0.80 |
1.3 |
6 |
0.16 |
0.55 |
0.9 |
7 |
0.26 |
0.98 |
1.6 |
8 |
0.18 |
0.67 |
1.1 |
[0044] The weight percentage of the dissipative tungsten layer was determined by dissolving
portions of the batches in dilute hydrofloric acid in combination with nitric, hydrochloric,
or sulfuric acid as appropriate. The resulting solutions were analyzed by Inductively
Coupled Argon Plasma Atomic Emission Spectroscopy.
[0045] The average thickness of each tungsten layer was calculated from the weight percentage
of metal and the specific surface area of the uncoated microbubbles as:
- t =
- average layer thickness, nm
- W =
- weight percentage of layer
- D =
- density of layer material
(for tungsten, 19.3 g/cm³)
- S =
- surface area of microbubbles (m²/g)
[0046] Each batch was then sputtered by the same process with an aluminum target, while
admitting oxygen into the chamber in the vicinity of the particles at a rate of 4.0
cc/min. This produced an insulative layer of non-stoichiometric aluminum oxide of
approximately 2.0 nm thickness.
[0047] The doubly layered particles were hand mixed into an epoxy binder using a lab spatula
and a 30 ml beaker. The binder material was type 5 "SCOTCHCAST" Electrical Resin supplied
by the Minnesota Mining and Manufacturing Company. This product is a two-part room
temperature cure epoxy consisting of two parts (by weight) of a diglycidal ether of
bisphenol A to one part (by weight) of a 20 weight percent solution of diethylene
triamine in an aromatic oil. The mixtures were placed under vacumn for about 10 minutes
to removed air entrapped while mixing.
[0048] The volume loadings of the particles in the resin were 60% for Examples 1 and 6-8,
and 50.0%, 53.5%, 57.0%, and 60.5% for Examples 2-5 respectively.
[0049] The mixtures were spread and pressed between two 75x25 mm glass microscope slides,
using 1 mm spacers, and allowed to cure at room temperature for 12 hours, after which
the slides were removed. This produced eight samples of hardened radiation absorbing
materials.
[0050] The hardened composites were removed from the slides and machined into a flat annular
rings. Each ring had an outside diameter of 7.0mm±0.0076mm, an inside diameter of
3.5mm±0.0076mm, and a known thickness of approximately 1mm. They were placed, at a
position known to ± 0.1mm, in a 6cm long coaxial airline connected to a Hewlett-Packard
Model 8510A precision microwave measurement system. The annular plastic substrates
used to hold the rings in place had a relative permittivity of 2.58 and a relative
permeability of 1.00.
[0051] Two hundred one step mode measurements from 0.1 to 20.1 GHz were made on each ring.
Measurements of the transmission and reflection of the radiation by the sample were
used to calculate the real and imaginary parts of the permittivities and permeabilities
of the samples as a function of incident frequency.
[0052] The calculated permitivity and permeability values for Example 1 were used to generate
Figure 2, which shows (at "A") the predicted reflection magnitude of radiation incident
normal to a 2.18 mm thick layer of the composite material over a conductive ground
plane. The results predict the desired broad and strong absorption response, at least
5 dB over a range from about 7.5 to 20 Ghz, and at least 10dB over a range from about
9.5 to about 11.5 GHz.
[0053] Also shown (at "B") is the beneficial effect of adding an impedance matching layer
to the composite material, specifically a 2.66 mm thick layer of homogeneous material
having a dielectric constant of 2.6. Absorption response is both broadened and deepened,
to least 5 dB over a range from about 6.5 to over 20 Ghz, and at least 10dB over a
range from about 7.5 to over 20 GHz. Two ranges of at least 15 dB absorption are predicted:
the first from 8 to 12 Ghz, with a maximum of nearly 30dB at about 9 Ghz, and the
second from 13 to 19 GHz, with a local maximum of over 20 dB at about 17 GHz.
Examples 9 to 11: Silicon Dioxide and Molybdenum Disilicide Layered Glass Bubbles
[0054] The procedures of Examples 1 to 8 were followed, except as noted below, with the
following results:
(1) The glass microbubbles were screened through a 400 mesh (38 micron) sieve; those
retained had an average diameter of 45 microns, with 90% of the microbubbles being
between 33 and 64 microns, and an average surface area of 0.46 m²/g.
(2) The microbubbles were sputter coated with a vapor of molybdenum disilicide (density
6.31 g/cm³), at a rate of 110 nm/min, at an applied power of 0.8 kW.
(3) The weight percentage of the dissipative MoSi₂ layer was 0.49%.
(4) The average thickness of each MoSi₂ layer was calculated to be 1.7 nm.
(5) Each batch was then heated in air for two hours for 200, 300, and 400 degrees
Celsius for Examples 9 to 11, respectively. This forms a electrically insulating layer
of silicon dioxide.
(6) The volume loadings of the particles in the resin were 60% for each of Examples
9-11.
[0055] Qualitative inspection of the calculated permittivity vs. frequency curves indicated
little or no performance difference between the curves of Examples 9 and 10. However,
a significant decrease in permittivity (both real and imaginary parts), by approximately
a factor of two for each part, evenly across the radiation range, was shown by the
curve of Example 11. We believe that this decreased performance is due to excessive
oxidation of the molybdenum disilicide into silicon dioxide, effectively reducing
the amount of molybdenum disilicide available for radiation absorption.
[0056] But, a material having an excessively large real part of the permittivity can exhibit
undue reflection of the incident radiation at the material surface. In all three cases
the magnitude of the imaginary part of the permittivity was at least one-tenth that
of the real part, over much if not all of the 2-20 GHz range, indicating acceptable
absorption performance. Therefore, on balance, we believe that each of Examples 9-11
would be a suitable absorber.
Example 12: Aluminum Suboxide and Tungsten Layered Mica Flakes
[0057] The procedures of Examples 1 to 8 were followed, except as noted below, with the
following results:
(1) Mica flakes obtained from Suzorite Mica Products, Inc., and designated 200HK,
were used. This product contains particles which are no larger than 75 microns, have
a density of 2.9 g/cm³, and have an average surface area of 2.8 m²/g.
(2) The mica flakes (460 g) were sputter coated with a vapor of tungsten for 180 minutes
at an applied power of 1.1 kW.
(3) The weight percentage of the dissipative tunsten layer was 1.7%.
(4) The average thickness of each tungsten layer was calculated to be 0.3 nm.
(5) The tungsten coated mica flakes were then sputter coated with aluminum suboxide
to a thickness of about 2 nm.
(6) The volume loadings of the particles in the resin was 15%.
[0058] Qualitative inspection of the calculated permeability vs. frequency curves indicated
acceptable absorption performance.
Example 13: Aluminum Suboxide and Tungsten Layered Milled Glass Fibers
[0059] The procedures of Examples 1 to 8 were followed, except as noted below, with the
following results:
(1) Milled glass fibers obtained from Owens Corning Company, and designated "FIBERGLAS,"
were used. This product contained glass fibers with a diameter of 16 microns, and
lengths from about 1 to 300 microns. They had a density of 2.56 g/cm³, and an average
surface area of 0.17 m²/g.
(2) The glass fibers (202 g) were sputter coated with a vapor of tungsten for 135
minutes at an applied power of 0.5 kW.
(3) The weight percentage of the dissipative tunsten layer was 0.45%.
(4) The average thickness of each tungsten layer was calculated to be 1.2 nm.
(5) The tungsten coated glass fibers were then sputter coated with aluminum suboxide
to a thickness of about 2 nm.
(6) The volume loadings of the particles in the resin was 33%.
[0060] Qualitative inspection of the calculated permeability vs. frequency curves indicated
acceptable absorption performance.
1. A non-electrically-conductive electromagnetic radiation absorbing material, comprising
a plurality of dissipative particles and a dielectric binder through which the dissipative
particles are dispersed, in which any of the dissipative particles comprises:
(a) a core particle;
(b) a dissipative layer made of an inorganic material, located on the surface of the
core particle; and
(c) an insulating layer overlaying the dissipative layer.
2. The absorbing material of claim 1 in which the core particle is chosen from the group
consisting of microsphere, microbubble, fiber, and flake.
3. The absorbing material of claim 2 in which the core particle is a glass microbubble
having an average outer diameter between 10 and 500 microns.
4. The absorbing material of claim 3 in which the core particle is a glass microbubble
having an average outer diameter between 20 and 80 microns.
5. The absorbing material of claim 1 in which the inorganic material of the dissipative
layer is chosen from the group consisting of metals and semiconductors.
6. The absorbing material of claim 5 in which the inorganic material of the dissipative
layer is chosen from the group consisting of tungsten, chromium, aluminum, copper,
titanium, titanium nitride, molybdenum disilicide, iron, iron suboxide, zirconium,
and stainless steel.
7. The absorbing material of claim 1 in which the dissipative layer has a thickness between
0.05 and 10 nanometers.
8. The absorbing material of claim 1 in which the dissipative layer averages approximately
0.4 to 2 nanometers in thickness.
9. The absorbing material of claim 1 in which the dissipative layer contiguously overlays
the core particle.
10. The absorbing material of claim 1 in which the dissipative layer continuously overlays
the core particle.
11. The absorbing material of claim 1 in which the thickness of the dissipative layer
is uniform to within ten percent.
12. The absorbing material of claim 1 in which the insulating layer comprises a material
chosen from the group consisting of aluminum suboxide, silicon dioxide, zirconium
oxide, and titanium dioxide.
13. The absorbing material of claim 1 in which the insulating layer is approximately about
2 nanometers thick.
14. The absorbing material of claim 1 in which the insulating layer contiguously overlays
the dissipative layer.
15. The absorbing material of claim 1 in which the insulating layer continuously overlays
the dissipative layer.
16. The absorbing material of claim 1 in which the insulating layer comprises a material
which is a reaction product of the inorganic material of the dissipative layer.
17. The absorbing material of claim 1 in which the dielectric binder is ceramic.
18. The absorbing material of claim 1 in which the dielectric binder is polymeric.
19. The absorbing material of claim 18 in which the the polymeric binder comprises a polymer
chosen from the group consisting of polyethylenes, polypropylenes, polymethylmethacrylates,
urethanes, cellulose acetates, and polytetrafluoroethylene.
20. The absorbing material of claim 18 in which the polymeric binder comprises a polymer
chosen from the group consisting of thermosetting polymeric adhesives and thermoplastic
polymeric adhesives.
21. The absorbing material of claim 18 in which the polymeric binder comprises a polymer
chosen from the group consisting of heat-shrinkable polymers, solvent-shrinkable polymers,
and mechanically-stretchable polymers.
22. The absorbing material of claim 1 in which the dielectric binder is elastomeric.
23. The absorbing material of claim 1 in which the plurality of dissipative particles
are dispersed in the dielectric binder at a volume loading between 65 and 15 percent.
24. The absorbing material of claim 1 in which the core particles are glass microbubbles
and the plurality of dissipative particles are dispersed in the dielectric binder
at a volume loading between 60 and 30 percent.
25. The combination of the absorbing material of claim 1 and an electrically conductive
material bound directly adjacent to the absorbing material.
26. The combination of the absorbing material of claim 1 and an impedance matching material
bound to a radiation incident side of the absorbing material.
27. A laminated construction comprising two or more laminae of an electromagnetic radiation
absorbing material, each lamina independently meeting the limitations of claim 1.
28. A method of making an electromagnetic radiation absorbing material, comprising the
steps of:
(a) providing an electrically conductive particle comprising a core particle which
has an ultrathin layer of a dissipative material;
(b) producing a stable, ultrathin layer of insulating material overlaying the dissipative
material; and
(c) embedding the result of (b) into a dielectric binder material.
29. The method of claim 28, in which the insulating material of step (b) comprises a reaction
product of the dissipative material of step (a).
30. The method of claim 29, in which step (b) comprises introducing oxygen to the dissipative
material.