Claims
- 1. A ceramic composite which is the product of the process of:
- (a) forming a slurry of ceramic components in a liquid, the components including microparticles in the size range between about 5-200 micrometers and selected from the group consisting of hollow microballoons, diatoms, solid microparticles and mixtures thereof;
- (b) felting a wet mat of the ceramic components from the slurry;
- (c) drying the wet mat;
- (d) infusing a ceramic sol-gel binder into the dry mat;
- (e) gelling and curing the binder at a temperature of no more than about 600.degree. F. to form a glass to hold the felted ceramic components in a rigid, porous, low-density, ceramic form;
- (f) optionally, infusing additional binder into the mat to increase the density and strength; and
- (g) optionally, gelling and curing the subsequent infusions of binder.
- 2. The composite of claim 1 wherein the ceramic components are diatoms.
- 3. The composite of claim 1 wherein the ceramic components are microballoons.
- 4. The composite of claim 1 wherein the ceramic components are a mixture of fibers and microparticles.
- 5. The composite of claim 1 wherein the ceramic components include whiskers to increase the product's strength.
- 6. The composite of claim 1 wherein the first infusion of binder is gelled in air while subsequent infusions are gelled in ammonia.
- 7. The composite of claim 1 wherein the steps of infusing and gelling are done a sufficient number of times to produce a product having a density of about 7-23 lbs/ft.sup.3.
- 8. A ceramic composite, which is the product made by:
- (a) slurrying hollow ceramic microballoons with water;
- (b) felting the microballoons out of the slurry to form a wet mat;
- (c) drying the mat;
- (d) infusing a sol-gel ceramic binder into the dried mat to form bridges between the microparticles;
- (e) gelling the binder; and
- (f) curing the gelled binder at a temperature no greater than about 600.degree. F. to form a glass that interconnects the microballoons into a rigid, porous product.
- 9. The composite of claim 8 further comprising the step of adding ceramic fibers to the microballoons in the slurry.
- 10. The composite of claim 8 further comprising the step of adding ceramic whiskers to the microballoons in the slurry.
- 11. The composite of claim 8 further comprising the steps of adding diatoms to the microballoons in the slurry.
- 12. The composite of claim 8 wherein the binder is an alumina sol-gel.
- 13. The composite of claim 9 wherein the microballoons have a diameter of about 5-50 micrometers and the fibers have a length of about 0.3-4 in and a diameter of about 1-10 micrometers.
- 14. The composite of claim 10 wherein the whiskers have a diameter of about 0.4-1.0 micrometer and an aspect ratio up to about 100:1.
- 15. The composite of claim 10 wherein the whiskers constitute about 5-10 wt % of the combined weight of the microballoons and whiskers.
- 16. The composite of claim 10 wherein the whiskers are silicon carbide.
Parent Case Info
This application is a divisional application based upon U.S. patent application Ser. No. 08/124,419, filed Jul. 28, 1993, now U.S. Pat. No. 5,441,682, which was a continuation of U.S. patent application Ser. No. 07/527,600, filed May 23, 1990 which was a continuation-in-part of U.S. patent application Ser. No. 07/381,498, filed Jul. 18, 1989, now abandoned, which in turn is a continuation-in-part of U.S. patent application Ser. No. 06/698,496, filed Feb. 5, 1985 now U.S. Pat. No. 5,041,321, which in turn is a continuation-in-part of U.S. patent application Ser. No. 06/667,496, filed Oct. 18, 1984, now U.S. Pat. No. 4,634,918, all of which are incorporated by reference.
US Referenced Citations (31)
Foreign Referenced Citations (3)
Number |
Date |
Country |
720073 |
Aug 1933 |
FRX |
485730 |
Oct 1953 |
ITX |
71759 |
Apr 1928 |
SEX |
Non-Patent Literature Citations (3)
Entry |
NASA Tech Brief (Nov. 1989), p. 52 "Ceramic Wick for Capillary--Pumped Heat Pipe", by Goddard Space Flight Center. |
NASA Tech Brief (Sep. 89), p. 84, "Capillary Pumped Heat Transfer Loop", by Marshall Space Flight Center. |
NASA Tech Brief (Sep. 1989), p. 94, "Two-Pipe Heat-Transfer Loop", by NASA Jep Propulsion Laboratory. |
Divisions (1)
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Number |
Date |
Country |
Parent |
124419 |
Jul 1993 |
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Continuations (1)
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Number |
Date |
Country |
Parent |
527600 |
May 1990 |
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Continuation in Parts (3)
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Number |
Date |
Country |
Parent |
381498 |
Jul 1989 |
|
Parent |
698496 |
Feb 1985 |
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Parent |
667496 |
Oct 1984 |
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