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