US4595623A
Expired / Lapsed
US
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Fiber-reinforced syntactic foam composites and method of forming same
Assignee: The AT&T MVPD Group LLC
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Filing: 1984-05-07
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Granted: 1986-06-17
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Expires: 2004-05-07
Abstract
Abstract Fiber-reinforced syntactic foam composites having a low specific gravity and a low coefficient of thermal expansion suitable for forming lightweight structures for spacecraft applications are prepared from a mixture of a heat curable thermosetting resin, hollow microspheres having a diameter of about 5 to 200 micrometers and fibers having a length less than or equal to 250 micrometers.
Inventors
- 👤 Preston S. Du Pont
- 👤 Janet E. Freeman
- 👤 Robert E. Ritter
- 👤 Alois Wittmann
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-02 19:07
CPC Classifications
H; H01; H01Q; H01Q15/00; H01Q15/14; C; C08; C08J; C08J9/00; C08J9/32; H05; H05K; H05K1/00; H05K1/02; H05K1/03; H05K1/0313; H05K1/0353; H05K1/0373; Y; Y10; Y10T; Y10T428/00; Y10T428/24; Y10T428/24802; Y10T428/24917
Claims Analysis
Total Claims: 42
Claim 1
Independent Claim
78 words
A fiber-reinforced syntactic foam composite having a specific gravity less than 1.0 and a coefficient of thermal expansion of about 25×10 -6 in/in/°F. (45×10 -6 cm/cm/°C.) or less and being suitable for use in the outer space environment, the composite being prepared from an admixture comprising a heat curable thermosetting resin, hollow microspheres having a diameter in the range of about 5 to about 200 micrometers and fibers having a length less than or equal to 250 micrometers.
Claim 2
Dependent Claim
78 words
A fiber-reinforced syntactic foam composite having a specific gravity less than 1.0 and a coefficient of thermal expansion of about 25×10 -6 in/in/°F. (45×10 -6 cm/cm/°C.) or less and being suitable for use in the outer space environment, the composite being prepared from an admixture comprising a heat curable thermosetting resin, hollow microspheres having a diameter in the range of about 5 to about 200 micrometers and fibers having a length less than or equal to 250 micrometers.
Claim 3
Dependent Claim
26 words
The composite of claim 1 wherein the resin comprises a material selected from the group consisting of an epoxy, a polyester and a condensate of formaldehyde.
Claim 4
Dependent Claim
23 words
The composite of claim 2 wherein the heat curable thermosetting resin comprises a mixture of an epoxy resin and a polyfunctional curing agent.
Claim 5
Dependent Claim
13 words
The composite of claim 3 wherein the epoxy resin is tetraglycidyl methylene dianiline.
Claim 6
Dependent Claim
19 words
The composite of claim 3 wherein the epoxy resin comprises a mixture of diglycidyl orthotoluidine and tetraglycidyl methylene dianiline.
Claim 7
Dependent Claim
16 words
The composite of claim 3 wherein the epoxy resin is the diglycidyl ether of Bisphenol A.
Claim 8
Dependent Claim
16 words
The composite of claim 3 wherein the epoxy resin is a phenol formaldehyde novolac polyglycidyl ether.
Claim 9
Dependent Claim
13 words
The composite of claim 3 wherein the polyfunctional curing agent is a polyamine.
Claim 10
Dependent Claim
15 words
The composite of claim 3 wherein the polyfunctional curing agent is a polycarboxylic acid anhydride.
Claim 11
Dependent Claim
19 words
The composite of claim 9 wherein the polycarboxylic acid curing agent is the maleic anhydride adduct of methyl cyclopentadiene.
Claim 12
Dependent Claim
14 words
The composite of claim 3 wherein the mixture further comprises benzyldimethylaniline as an accelerator.
Claim 13
Dependent Claim
28 words
The composite of claim 1 wherein the hollow microspheres are formed of a material selected from the group consisting of glass, silica, carbon, acrylate resins, and phenolic resins.
Claim 14
Dependent Claim
22 words
The composite of claim 12 wherein the hollow microspheres are formed of glass and have an average diameter of about 50 micrometers.
Claim 15
Dependent Claim
18 words
The composite of claim 12 wherein the hollow microspheres comprise a mixture of glass microspheres and carbon microspheres.
Claim 16
Dependent Claim
25 words
The composite of claim 1 wherein the fibers are formed of a material selected from the group consisting of graphite, glass, carbon, nylon, and polyamide.
Claim 17
Dependent Claim
27 words
The composite of claim 15 wherein the fibers are formed of graphite and have a length of about 50 micrometers and a diameter of about 8 micrometers.
Claim 18
Dependent Claim
15 words
The composite of claim 1 wherein said admixture further includes a coupling and wetting agent.
Claim 19
Dependent Claim
12 words
The composite of claim 1 wherein the admixture further includes solid microbeads.
Claim 20
Dependent Claim
48 words
The composite of claim 1 which comprises about 35 to about 65 percent by volume microspheres and about 3 to about 10 percent by volume fibers, the balance being a matrix comprised of the heat cured resin throughout which the microspheres and fibers are dispersed and bonded together.
Claim 21
Dependent Claim
29 words
The composite of claim 19 which additionally comprises about 2 to about 8 percent by volume of solid microbeads having a diameter of about 2 to about 8 micrometers.
Claim 22
Dependent Claim
76 words
The composite of claim 1 wherein: (a) the heat curable thermosetting resin comprises a mixture of diglycidyl orthotoluidene, tetraglycidyl methylene dianiline, nadic methyl anhydride, and benzyldimethylaniline; (b) the hollow microspheres are glass microspheres having a mean diameter of 50 micrometers; (c) the fibers are graphite fibers having a length of about 50 micrometers and a diameter of about 8 micrometers; and (d) the admixture further comprises solid glass microbeads having a median diameter of 3 micrometers.
Claim 23
Dependent Claim
90 words
A fiber-reinforced syntactic foam composite having a specific gravity less than 1.0 and a coefficient of thermal expansion of about 13×10 -6 in/in/°F. (23×10 -6 cm/cm/°C.) or less and being suitable for use in the outer space environment, said composite comprising: (a) a heat curable thermosetting epoxy resin comprising a mixture of tetraglycidyl methylene dianiline, nadic methyl anhydride, and benzyldimethylaniline; (b) hollow glass microspheres having a mean diameter of about 75 micrometers; and (c) graphite fibers having a length of about 150 micrometers and a diameter of about 8 micrometers.
Claim 24
Dependent Claim
90 words
A fiber-reinforced syntactic foam composite having a specific gravity less than 1.0 and a coefficient of thermal expansion of about 13×10 -6 in/in/°F. (23×10 -6 cm/cm/°C.) or less and being suitable for use in the outer space environment, said composite comprising: (a) a heat curable thermosetting epoxy resin comprising a mixture of tetraglycidyl methylene dianiline, nadic methyl anhydride, and benzyldimethylaniline; (b) hollow glass microspheres having a mean diameter of about 75 micrometers; and (c) graphite fibers having a length of about 150 micrometers and a diameter of about 8 micrometers.
Claim 25
Dependent Claim
15 words
An article of manufacture comprising a body formed from the composite material of claim 1.
Claim 26
Dependent Claim
25 words
The article of manufacture set forth in claim 23 which further comprises a layer of electrically conductive material adhered to selected surfaces of the body.
Claim 27
Dependent Claim
19 words
The article of manufacture set forth in claim 24 wherein said article comprises a component in an antenna structure.
Claim 28
Independent Claim
152 words
A method for fabricating a fiber-reinforced syntactic foam composite which comprises the steps of: (a) admixing a heat curable thermosetting resin, hollow microspheres having a diameter in the range of about 5 to about 200 micrometers and fibers having a length less than or equal to 250 micrometers to form a mixture of the resin, microspheres and fibers; and (b) curing the mixture of the resin, microspheres, and fibers in a mold of predetermined geometry to a thermoset state to provide a composite structure containing about 35 to about 65 volume percent microspheres and about 3 to about 10 volume percent fibers disposed throughout the resin matrix, and the resin comprising the balance of the composite, wherein the composite has a specific gravity of less than 1.0 and a coefficient of thermal expansion about 13×10 -6 in/in/°F. (23×10 -6 cm/cm/°C.) or less and is suitable for use in the outer space environment.
Claim 29
Independent Claim
152 words
A method for fabricating a fiber-reinforced syntactic foam composite which comprises the steps of: (a) admixing a heat curable thermosetting resin, hollow microspheres having a diameter in the range of about 5 to about 200 micrometers and fibers having a length less than or equal to 250 micrometers to form a mixture of the resin, microspheres and fibers; and (b) curing the mixture of the resin, microspheres, and fibers in a mold of predetermined geometry to a thermoset state to provide a composite structure containing about 35 to about 65 volume percent microspheres and about 3 to about 10 volume percent fibers disposed throughout the resin matrix, and the resin comprising the balance of the composite, wherein the composite has a specific gravity of less than 1.0 and a coefficient of thermal expansion about 13×10 -6 in/in/°F. (23×10 -6 cm/cm/°C.) or less and is suitable for use in the outer space environment.
Claim 30
Dependent Claim
68 words
The method of claim 26 wherein the admixing comprises: (a) forming a liquid dispersion of the microspheres and fibers in a coupling agent; (b) filtering the dispersion to separate the microspheres and fibers from the liquid as a filtration residue; (c) drying the residue to provide a mixture of microspheres and fibers coated with the coupling agent; and (d) admixing the coated microspheres and fibers with the resin.
Claim 31
Dependent Claim
37 words
The method of claim 27 wherein: (a) the microspheres are hollow glass microspheres; (b) the fibers are graphite fibers; (c) the coupling agent is selected from the group consisting of a silane compound and a titanate compound.
Claim 32
Dependent Claim
23 words
The method of claim 26 wherein the heat curable thermosetting resin is a mixture of an epoxy resin and a polyfunctional curing agent.
Claim 33
Dependent Claim
13 words
The method of claim 29 wherein the epoxy resin is tetraglycidyl methylene dianiline.
Claim 34
Dependent Claim
19 words
The method of claim 29 wherein the epoxy resin comprises a mixture of diglycidyl orthotoluidene and tetraglycidyl methylene dianiline.
Claim 35
Dependent Claim
16 words
The method of claim 29 wherein the epoxy resin is the diglycidyl ether of Bisphenol A.
Claim 36
Dependent Claim
16 words
The method of claim 29 wherein the epoxy resin is a phenol formaldehyde novolac polyglycidyl ether.
Claim 37
Dependent Claim
13 words
The method of claim 29 wherein the polyfunctional curing agent is a polyamine.
Claim 38
Dependent Claim
15 words
The method of claim 29 wherein the polyfunctional curing agent is a polycarboxylic acid anhydride.
Claim 39
Dependent Claim
19 words
The method of claim 35 wherein the polycarboxylic acid curing agent is the maleic anhydride adduct of methyl cyclopentadiene.
Claim 40
Dependent Claim
14 words
The method of claim 29 wherein the mixture further comprises benzyldimethylaniline as an accelerator.
Claim 41
Dependent Claim
12 words
The method of claim 26 wherein the hollow microspheres comprise glass microspheres.
Claim 42
Dependent Claim
11 words
The method of claim 26 wherein the fibers comprise graphite fibers.
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1989-06-16 | 1989-12-16 | 1990-06-17 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1993-06-16 | 1993-12-16 | 1994-06-17 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1997-06-16 | 1997-12-16 | 1998-06-17 | $7700.00 | Window Closed / Lapsed |