发明名称 MODIFIED ATMOSPHERE MELT INFILTRATION
摘要 A ceramic matrix composite component for use in a gas turbine engine and method for making the same are described herein. The component comprising a body and an outer region. The body having a silicon containing ceramic composite. The outer region on an outer surface of the body.
申请公布号 US2016230570(A1) 申请公布日期 2016.08.11
申请号 US201615040527 申请日期 2016.02.10
申请人 Rolls-Royce High Temperature Composites Inc. ;Rolls-Royce Corporation 发明人 Harris Stephen L.;Shinavski Robert J.;Kidd Richard W.;Shim Sungbo;Lee Kang N.
分类号 F01D5/28;C04B35/80 主分类号 F01D5/28
代理机构 代理人
主权项 1. A ceramic matrix composite component for use in a gas turbine engine, the component comprising a body comprising a silicon containing ceramic composite; and an outer region on an outer surface of the body, the outer region comprising whiskers embedded in a matrix, the whiskers comprising silicon carbide, and the matrix comprising a majority of silicon metal.
地址 Huntington Beach CA US