Fiber-reinforced syntactic foam composites and method of forming same

• US 4,595,623 A
• Filed: 05/07/1984
• Issued: 06/17/1986
• Est. Priority Date: 05/07/1984
• Status: Expired due to Term

• Current Assignee: Hughes Electronics Corporation (AT&T, Inc.)
• Original Assignee: Hughes Aircraft Company (Rtx Corporation)
• Inventors: Wittmann, Alois, Ritter, Robert E., Du Pont, Preston S., Freeman, Janet E.
• Primary Examiner(s): Foelak, Morton
• Application Number:
  US06/607,847
• Time in Patent Office: 771 Days
• Field of Search: 521/54, 523/218, 523/219, 428/195, 428/209
• US Class Current: 428/195.1
• CPC Class Codes: C08J 9/32 from compositions containing microballoons, e.g. syntactic foams
• CPC Class Codes: H01Q 15/14 Reflecting surfaces; Equivalent structures electromagnetic shields H01Q1/526
• CPC Class Codes: H05K 1/0313 Organic insulating material
• CPC Class Codes: H05K 1/0373 containing additives, e.g. fillers H05K1/036 takes precedence
• CPC Class Codes: Y10T 428/24802 Discontinuous or differential coating, impregnation or bond [e.g., artwork, printing, retouched photograph, etc.]
• CPC Class Codes: Y10T 428/24917 including metal layer

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.

Claims

1. 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.

2. 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.

3. The composite of claim 2 wherein the heat curable thermosetting resin comprises a mixture of an epoxy resin and a polyfunctional curing agent.

4. The composite of claim 3 wherein the epoxy resin is tetraglycidyl methylene dianiline.

5. The composite of claim 3 wherein the epoxy resin comprises a mixture of diglycidyl orthotoluidine and tetraglycidyl methylene dianiline.

6. The composite of claim 3 wherein the epoxy resin is the diglycidyl ether of Bisphenol A.

7. The composite of claim 3 wherein the epoxy resin is a phenol formaldehyde novolac polyglycidyl ether.

8. The composite of claim 3 wherein the polyfunctional curing agent is a polyamine.

9. The composite of claim 3 wherein the polyfunctional curing agent is a polycarboxylic acid anhydride.

10. The composite of claim 9 wherein the polycarboxylic acid curing agent is the maleic anhydride adduct of methyl cyclopentadiene.

11. The composite of claim 3 wherein the mixture further comprises benzyldimethylaniline as an accelerator.

12. 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.

13. The composite of claim 12 wherein the hollow microspheres are formed of glass and have an average diameter of about 50 micrometers.

14. The composite of claim 12 wherein the hollow microspheres comprise a mixture of glass microspheres and carbon microspheres.

15. 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.

16. 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.

17. The composite of claim 1 wherein said admixture further includes a coupling and wetting agent.

18. The composite of claim 1 wherein the admixture further includes solid microbeads.

19. 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.

20. 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.

21. 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.

23. An article of manufacture comprising a body formed from the composite material of claim 1.

24. 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.

25. The article of manufacture set forth in claim 24 wherein said article comprises a component in an antenna structure.

22. 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.

26. 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.

27. 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.

28. 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.

29. The method of claim 26 wherein the heat curable thermosetting resin is a mixture of an epoxy resin and a polyfunctional curing agent.

30. The method of claim 29 wherein the epoxy resin is tetraglycidyl methylene dianiline.

31. The method of claim 29 wherein the epoxy resin comprises a mixture of diglycidyl orthotoluidene and tetraglycidyl methylene dianiline.

32. The method of claim 29 wherein the epoxy resin is the diglycidyl ether of Bisphenol A.

33. The method of claim 29 wherein the epoxy resin is a phenol formaldehyde novolac polyglycidyl ether.

34. The method of claim 29 wherein the polyfunctional curing agent is a polyamine.

35. The method of claim 29 wherein the polyfunctional curing agent is a polycarboxylic acid anhydride.

36. The method of claim 35 wherein the polycarboxylic acid curing agent is the maleic anhydride adduct of methyl cyclopentadiene.

37. The method of claim 29 wherein the mixture further comprises benzyldimethylaniline as an accelerator.

38. The method of claim 26 wherein the hollow microspheres comprise glass microspheres.

39. The method of claim 26 wherein the fibers comprise graphite fibers.