发明名称 |
Method for manufacturing ceramic matrix composite structures |
摘要 |
Methods are disclosed herein to fabricate high-strength ceramic matrix composite (CMC) structures by combining, in one example, pre-impregnated (prepreg) material with a pre-ceramic polymer. The prepreg is processed to a first density, and the densification is completed with repeated polymer infiltration and pyrolysis (PIP) cycles of the pre-ceramic polymer to fabricate a CMC structure. Advantageously, the present invention allows for fabrication of ceramic matrix composites more efficiently and to a larger scale than previously available. |
申请公布号 |
US8859037(B2) |
申请公布日期 |
2014.10.14 |
申请号 |
US200511034134 |
申请日期 |
2005.01.12 |
申请人 |
The Boeing Company |
发明人 |
Stout Jeffrey B.;Pelletier Gerard D. |
分类号 |
B05D7/00 |
主分类号 |
B05D7/00 |
代理机构 |
Haynes and Boone, LLP |
代理人 |
Haynes and Boone, LLP |
主权项 |
1. A method of fabricating a ceramic matrix composite structure, comprising:
laying-up a carbon/carbon (C/C) pre-impregnated (prepreg) fabric on a tool; curing the C/C prepreg fabric to provide a cured material consisting of resin char and carbon black; adding carbon nano-structures to the resin char; carbonizing the cured material to provide a carbonized reinforcement part; applying a pre-ceramic polymer to the carbonized reinforcement part; and pyrolyzing the applied pre-ceramic polymer to fabricate a ceramic matrix composite structure. |
地址 |
Chicago IL US |