Claims
- 1. A method for providing a cold work surface using a porous ceramic composite to carry cryogen, comprising the steps of:
- (a) preparing a ceramic composite by felting a mat of ceramic particles from a slurry and binding the particles together with a sol-gel binder, wherein the mat has a working surface and wherein the particles are selected from microparticles or a mixture of microparticles and fibers, the fibers being about 0-99 wt % of the particles;
- (b) preparing a covering coating on the working surface; and
- (c) cooling the coating by wicking cryogen to the coating through the mat.
- 2. The method of claim 1 wherein the coating is impact resistant and comprises about 5-60 wt % borosilicate glass under the trademark PYREX glass powder mixed with colloidal silica, mullite, single crystal ceramic whiskers, and trona.
- 3. The method of claim 1 wherein the coating includes a superconductive metal oxide and wherein the cooling cools the superconductive metal oxide below its superconducting transition temperature.
- 4. A method of preparing a coating on a porous mat of ceramic particles, comprising the steps of:
- (a) felting a mat of ceramic particles from a slurry, the particles being microparticles or a mixture of microparticles and fibers wherein the fibers comprise 0-99 wt % of the particles;
- (b) binding the particles in the mat with a sol-gel binder, the mat having a working surface; and
- (c) applying a coating on the working surface.
- 5. A method according to claim 4 wherein said coating comprises superconducting metal oxides or precursors thereof.
- 6. A method according to claim 4 wherein said coating is applied by sputtering, plasma deposition, or by application as a paint.
- 7. A method according to claim 4 further comprising applying a substrate to the working surface by sputtering, plasma desposition, or by application as a paint, wherein the coating is applied thereafter to the substrate on the working surface.
- 8. A method according to claim 4 wherein said coating comprises a metal or metal oxide.
- 9. A method according to claim 4 wherein said coating comprises glass.
- 10. The method of claim 4 wherein the coating is metal, glass, or ceramic.
- 11. The method of claim 4 wherein the coating is an impact-resistant surface comprising about 5-60 wt % borosilicate glass under the trademark PYREX glass powder mixed with colloidal silica, mullite, single crystal ceramic whiskers, and trona.
- 12. The method of claim 11 further comprising the step of apply a metal on the impact-resistant coating.
- 13. The method of claim 4 wherein the particles include ceramic whiskers to increase the compressive strength and modulus of the mat.
Parent Case Info
This application is a divisional application based upon U.S. patent application Ser. No. 07/404,015, filed Mar. 13, 1995, now U.S. Pat. No. 5,587,228, which is a division of application Ser. No. 08/124,419, filed July, 28, 1993, now U.S. Pat. No. 5,441,682, which is a continuation of application based upon U.S. patent application Ser. No. 07/527,600, filed May 23, 1990, now abandoned, which is 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 (5)
Number |
Date |
Country |
750073 |
Aug 1933 |
FRX |
485730 |
Oct 1953 |
ITX |
62-33651 |
Feb 1987 |
JPX |
1-143108 |
Jun 1989 |
JPX |
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 Jet Propulsion Laboratory. |
Divisions (2)
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Number |
Date |
Country |
Parent |
404015 |
Mar 1995 |
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Parent |
124419 |
Jul 1993 |
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Continuations (1)
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Number |
Date |
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Parent |
527600 |
May 1990 |
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Continuation in Parts (3)
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Number |
Date |
Country |
Parent |
381498 |
Jul 1989 |
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Parent |
698496 |
Feb 1985 |
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Parent |
667496 |
Oct 1984 |
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