초록 ▼

A ceramic composition is provided to insulate ceramic matrix composites under high temperature, high heat flux environments. The composition comprises a plurality of hollow oxide-based spheres of various dimensions, a phosphate binder, and at least one oxide filler powder, whereby the phosphate bind

A ceramic composition is provided to insulate ceramic matrix composites under high temperature, high heat flux environments. The composition comprises a plurality of hollow oxide-based spheres of various dimensions, a phosphate binder, and at least one oxide filler powder, whereby the phosphate binder partially fills gaps between the spheres and the filler powders. The spheres are situated in the phosphate binder and the filler powders such that each sphere is in contact with at least one other sphere. The spheres may be any combination of Mullite spheres, Alumina spheres, or stabilized Zirconia spheres. The filler powder may be any combination of Alumina, Mullite, Ceria, or Hafnia. Preferably, the phosphate binder is Aluminum Ortho-Phosphate. A method of manufacturing the ceramic insulating composition and its application to CMC substrates are also provided.

대표청구항 ▼

1. A method of insulating a ceramic substrate when exposed to temperatures in excess of 1300° C. by positioning a ceramic-based material composition having a high temperature resistance and containing contacting hollow oxide-based spheres manufactured at high enough temperatures to make them stable

1. A method of insulating a ceramic substrate when exposed to temperatures in excess of 1300° C. by positioning a ceramic-based material composition having a high temperature resistance and containing contacting hollow oxide-based spheres manufactured at high enough temperatures to make them stable at 1600° C. over the ceramic substrate, which has a higher strength but lower temperature resistance than the ceramic-based material composition where the high temperature resistant ceramic-based material composition has an erosion resistance of approximately 4.5 g/kg to approximately 7.5 g/kg, when measured at 1100° C., a 15° impingement angle, and an erodent speed of 900 ft/s. 2. A method of insulating a ceramic substrate for use in a high temperature environment in excess of approximately 1300° C., comprising: positioning over the ceramic substrate, a ceramic-based material composition having a temperature resistance in excess of approximately 1300° C. and containing: a plurality of hollow oxide-based spheres, a phosphate binder, and at least one oxide filler material, the binder at least partially filling at least some gaps between the spheres and the filler material wherein the ceramic-based material composition has a lower strength but higher temperature resistance than the ceramic substrate. 3. The method of claim 2, where the high temperature resistant ceramic-based material composition is stable at temperatures up to approximately 1600° C. 4. The method of claim 2, where the high temperature resistant ceramic-based material composition has a coefficient of thermal expansion in the range of approximately 5.7×10-6mm/mm °C. to approximately 10×10-6mm/mm °C. 5. The method of claim 2, where at least some of the spheres are selected from one or more of the following: Mullite spheres, Alumina spheres, and stabilized Zirconia spheres. 6. The method of claim 5, where at least some of the Mullite spheres have a diameter in the range of approximately 0.4 to approximately 1.8 mm; at least some of the Alumina spheres have a diameter in the range of approximately 0.3 to approximately 1 mm; and at least some of the stabilized Zirconia spheres have a diameter in the range of approximately 0.6 to approximately 1.2 mm. 7. The method of claim 2, where the high temperature resistant ceramic-based material composition has an erosion resistance of approximately 4.5 g/kg to approximately 7.5 g/kg, when measured at 1100° C., and 15° impingement angle, and an erodent speed of 900 ft/s.