초록 ▼

A hybrid insulation material comprises of porous ceramic substrate material impregnated with nanoporous material and method of making the same is the topic of this invention. The porous substrate material has bulk density ranging from 6 to 20 lb/ft 3 and is composed of about 60 to 80 wt % silica (S

A hybrid insulation material comprises of porous ceramic substrate material impregnated with nanoporous material and method of making the same is the topic of this invention. The porous substrate material has bulk density ranging from 6 to 20 lb/ft 3 and is composed of about 60 to 80 wt % silica (SiO 2 ) 20 to 40 wt % alumina (Al 2 O 3 ) fibers, and with about 0.1 to 1.0 wt % boron-containing constituent as the sintering agent. The nanoporous material has density ranging from 1.0 to 10 lb/ft 3 and is either fully or partially impregnated into the substrate to block the pores, resulting in substantial reduction in conduction via radiation and convention. The nanoporous material used to impregnate the fiber substrate is preferably formed from a precursor of alkoxysilane, alcohol, water, and an acid or base catalyst for silica aerogels, and from a precursor of aluminum alkoxide, alcohol, water, and an acid or base catalyst for alumina aerogels.

대표청구항 ▼

1. An insulative material comprising:a porous substrate formed of sintered ceramic fibers,wherein said ceramic fibers compriseabout 60 wt % to about 80 wt % silica fibers;about 20 wt % to about 40 wt % alumina fibers; andabout 0.1 wt % to about 1.0 wt % boron-containing constituent; anda nanoporous

1. An insulative material comprising:a porous substrate formed of sintered ceramic fibers,wherein said ceramic fibers compriseabout 60 wt % to about 80 wt % silica fibers;about 20 wt % to about 40 wt % alumina fibers; andabout 0.1 wt % to about 1.0 wt % boron-containing constituent; anda nanoporous material impregnated within said porous substrate material. 2. The material of claim 1, wherein said ceramic fibers compriseabout 65 wt % to about 75 wt % silica fibers;about 25 wt % to about 35 wt % alumina fibers; andabout 0.1 wt % to about 0.5 wt % boron-containing powders. 3. The material of claim 1, wherein the material is in the form of a tile having a thickness defined by a first surface and a second surface which opposes said first surface. 4. The material of claim 3, wherein the physical arrangement of the ceramic fibers is substantially ordered and substantially parallel to the plane of at least one of said first and second surfaces of the tile. 5. The material of claim 4, wherein said first surface and said second surface are coplanar. 6. The material of claim 4, wherein the physical arrangement of the ceramic fibers is substantially parallel to the plane of said first surface of the tile. 7. The material of claim 1, wherein the ceramic fibers are chopped. 8. The material of claim 7, wherein the ceramic fibers have an average length between about 200 micron and about 500 micron. 9. The material of claim 6, wherein the ceramic fibers have an average diameter of between about 2 μm and about 5 μm. 10. The material of claim 8, wherein the ceramic fibers have an average diameter of about 3.0 μm. 11. The material of claim 1, wherein the nanoporous material is a silica based aerogel material. 12. The material of claim 11, wherein the silica aerogel material has a porosity of greater than 60%. 13. The material of claim 12, wherein the silica aerogel material has a density between about 1.0 and about 10.0 lbs/ft 3 . 14. The material of claim 12, wherein the silica aerogel material has a density of between about 5.0 lbs/ft 3 and about 6.0 lbs/ft 3 . 15. The material of claim 3, wherein the nanoporous material is a silica based aerogel material and the tile is either fully or partially impregnated with aerogel. 16. The material of claim 15, wherein the tile is impregnated with aerogel from the first surface of the tile through a portion of the thickness of the tile. 17. The material of claim 15, wherein the second surface of the tile is coated with reaction cured glass (RCG) and TUFI. 18. The material of claim 15, wherein the impregnated tile has a density of between about 8 and about 25 lbs/ft 3 . 19. The material of claim 1, wherein the nanoporous material is a alumina based aerogel material. 20. The material of claim 19, wherein the alumina aerogel material has a porosity of greater than 60%. 21. The material of claim 19, wherein the alumina aerogel material has a density between about 1.0 and about 10 lbs/ft 3 . 22. The material of claim 3, wherein the nanoporous material is an alumina based aerogel material and the tile is either partially or fully impregnated with aerogel. 23. The material of claim 22, wherein the second surface of the tile is coated with reaction cured glass (RCG) and TUFI. 24. The material of claim 21, wherein the impregnated tile has a density of between about 8 and about 25 lbs/ft 3 . 25. The material of claim 1, wherein said ceramic fibers compriseabout 67 wt % silica fibers;about 32.75 wt % alumina fibers; andabout 0.25 wt % boron carbide powders. 26. The material of claim 25, wherein the material is in the form of a tile having a thickness defined by a first surface and a second surface which opposes said first surface. 27. The material of claim 26, wherein the physical arrangement of the ceramic fibers is substantially ordered and substantially parallel to the plane of at least one of said first and second surfaces of the tile. 28. The material of claim 26, wherein said first s urface and said second surface are coplanar. 29. The material of claim 26, wherein the physical arrangement of the ceramic fibers is substantially ordered and substantially coplanar with said first surface of the tile. 30. The material of claim 25, wherein the ceramic fibers are chopped. 31. The material of claim 30, wherein the chopped fibers have an average length between about 200 micron to about 500 micron. 32. The material of claim 30, wherein the chopped fibers have an average diameter of between about 2 μm and about 5 μm. 33. The material of claim 30, wherein the chopped fibers have an average diameter of about 3.0 μm. 34. The material of claim 25, wherein the nanoporous material is a silica based aerogel material. 35. The material of claim 34, wherein the silica aerogel material has a porosity of greater than 60%. 36. The material of claim 35, wherein the silica aerogel material has a density between about 1.0 and about 10 lbs/ft 3 . 37. A method of producing an insulative material comprising:forming an aqueous slurry of mixed ceramic fibers wherein said fibers comprise about 60 wt % to about 80 wt % silica fibers; about 20 wt % to about 40 wt % alumina fibers; and about 0.1 wt % to about 1.0 wt % boron-containing constituent;removing at least a portion of the water from the slurry;pressing the ceramic fibers into a wet billet;removing residual water from the wet billet;fusing the ceramic fibers to one another to form a porous substrate; and,impregnating the porous substrate with an aerogel material. 38. The method of claim 37, wherein the step of impregnating the substrate comprises impregnating the substrate with a silica based aerogel. 39. The method of claim 38, further comprising the step of forming an aerogel precursor prior to impregnating the substrate. 40. The method of claim 39, wherein forming the precursor comprises mixing an alkoxysilane, an alcohol, water, and at least one of an acid and base catalyst. 41. The method of claim 40, wherein the alkoxysilane is tetra-methoxy silane (TMOS) and wherein the alcohol is methanol. 42. The method of claim 37, wherein the step of impregnating the substrate comprises impregnating the substrate with an alumina based aerogel. 43. The method of claim 42, further comprising the step of forming an aerogel precursor prior to impregnating the substrate. 44. The method of claim 43, wherein forming the precursor comprises mixing an alumina-tri-sec-butoxide an alcohol, water, and at least one of an acid and base catalyst. 45. The method of claim 37, further comprising curing the aerogel impregnated substrate under supercritical conditions. 46. The method of claim 45, wherein the step of curing the aerogel impregnated substrate under supercritical conditions comprises gradually heating the aerogel impregnated substrate to a temperature of about 625° F. and to a pressure of about 2000 psi over about a 6-9 hour period; and gradually returning to room temperature and pressure over about a 4 hour period.