发明名称 TURBOJET ENGINE NACELLE WITH CLOSURE COOPERATING WITH A CLOSING BLOCKING ELEMENT
摘要 The present disclosure relates to a turbofan nacelle comprising a cowl and a service structure, both being annular shapes in two halves. The cowl and the service structure are hinged on axes in respective halves to be opened during maintenance and closed during operation. In particular, a first annular half of the service structure supports a strike and a second annular half of the service structure supports a mobile bolt on a lever, such that the assembly constitutes a lock for closing the service structure. The lever engages with a locking member of a free edge of one half of the cowl, which is retracted when the lever is in the normal closed position thereof and active otherwise.
申请公布号 EP2920077(A1) 申请公布日期 2015.09.23
申请号 EP20130801677 申请日期 2013.11.18
申请人 AIRCELLE 发明人 RENAULT, CÉDRIC
分类号 F01D25/24;B64D29/06;B64D29/08;E05C19/14 主分类号 F01D25/24
代理机构 代理人
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