发明名称 NACELLE DE TURBOREACTEUR, DESTINEE A EQUIPER UN AERONEF
摘要 <p>An actuating device is provided for a locking system which locks one of half-shells of a jet engine nacelle with respect to the other half-shell. The actuating device includes a fixed body in which an actuating rod is translationally and rotationally mounted with respect to the rod's longitudinal axis, and the fixed body has a track cooperating with a follower projecting from the actuating rod. In particular, the actuating rod includes a first end equipped with a handle and a second end connected to the locking system. The track has a middle part running parallel to the longitudinal axis, a first end part and a second end part formed on each side of the middle part, each of the end parts running perpendicular to the longitudinal axis.</p>
申请公布号 FR2920133(B1) 申请公布日期 2009.10.30
申请号 FR20070005917 申请日期 2007.08.20
申请人 AIRCELLE SOCIETE ANONYME 发明人 SOULIER PASCAL MARIE PAUL MARCEL;DE SORBAY AURELIE
分类号 B64D29/00;E05B1/00;E05B13/00;E05C3/04 主分类号 B64D29/00
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