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 |
EP2846023(A1) |
申请公布日期 |
2015.03.11 |
申请号 |
EP20140172649 |
申请日期 |
2014.06.17 |
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;B64D33/02 |
主分类号 |
F02C7/047 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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