| 发明名称 |
Aircraft Engine Anti-Icing (EAI) Barrier Assembly, System and Method |
| 摘要 |
There is provided an aircraft engine anti-icing (EAI) barrier assembly. The aircraft EAI barrier assembly has a slip joint subassembly having a forward end and an aft end. The forward end is configured for fixed attachment at a forward bulkhead of an engine of an aircraft, and an aft end with a sliding joint. The aircraft EAI barrier assembly has a barrier subassembly attached through an aft bulkhead and has two mount pads configured for joined sealed attachment around the aft end of the slip joint subassembly to form a barrier to an engine inlet of the engine. |
| 申请公布号 |
US2015176490(A1) |
申请公布日期 |
2015.06.25 |
| 申请号 |
US201313972902 |
申请日期 |
2013.08.21 |
| 申请人 |
The Boeing Company |
发明人 |
Trinh Haisan K.;Vogel Stuart W.;Breister Robert T.;Mauldin Jack W. |
| 分类号 |
F02C7/047;B64D15/02 |
主分类号 |
F02C7/047 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An aircraft engine anti-icing (EAI) barrier assembly comprising:
a slip joint subassembly having a forward end and an aft end, the forward end configured for fixed attachment at a forward bulkhead of an engine of an aircraft, and the aft end having a sliding joint; and, a barrier subassembly attached through an aft bulkhead, the barrier subassembly comprising two mount pads configured for joined sealed attachment around the aft end of the slip joint subassembly to form a barrier to an engine inlet of the engine. |
| 地址 |
Chicago IL US |
