发明名称 Case with ballistic liner
摘要 A fan case for a gas turbine engine includes an outer case defined about an engine axis and a hard ballistic liner defined about the engine axis, the hard ballistic liner within the outer case.
申请公布号 US8827629(B2) 申请公布日期 2014.09.09
申请号 US201113024386 申请日期 2011.02.10
申请人 United Technologies Corporation 发明人 Voleti Sreenivasa R.;Lussier Darin S.;Naik Rajiv A.
分类号 F01B25/16;F01D21/04 主分类号 F01B25/16
代理机构 Carlson, Gaskey & Olds, P.C. 代理人 Carlson, Gaskey & Olds, P.C.
主权项 1. A case for a gas turbine engine comprising: an outer case defined about an engine axis, wherein said outer case is manufactured of a composite material; a hard ballistic liner defined about the engine axis, the hard ballistic liner within said outer case; an inner structure including a honeycomb layer extending along a radially innermost side of said case, wherein said honeycomb layer forms a boundary of a fan flow path and is axially spaced downstream of a trailing edge of a fan blade; and wherein a trailing edge of said hard ballistic liner is located axially upstream of a leading edge of said honeycomb layer.
地址 Hartford CT US