发明名称 |
MOTION RESTRICTOR SYSTEM FOR AN AIRCRAFT ENGINE |
摘要 |
A method and apparatus comprising a first wall (122) and a plurality of longitudinal members (120). The first wall is for an inlet (110) of an aircraft engine (108). The plurality of longitudinal members connects the first wall to a structure for the aircraft engine. The plurality of longitudinal members has an orientation configured to reduce motion in the inlet. |
申请公布号 |
EP2750972(A1) |
申请公布日期 |
2014.07.09 |
申请号 |
EP20110757492 |
申请日期 |
2011.09.02 |
申请人 |
THE BOEING COMPANY |
发明人 |
STANESCU, ADRIAN;MAHANIAN, SABA |
分类号 |
B64D33/02;B64D27/00;B64D27/26 |
主分类号 |
B64D33/02 |
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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