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 |