发明名称 Telescopic actuator for deploying landing gear of aircraft, has retaining unit with step provided at auxiliary rod`s end and sleeve axially displaceable by motor, where retaining unit retains rod in retracted position inside main rod
摘要 <p>The actuator has a cylinder (1) defining a cavity in which a main rod (2) is mounted, and an auxiliary rod (20) mounted to slide telescopically in the main rod along a sliding axis between retracted and an extended positions. A controlled retaining unit retains the rod (20) in the retracted position inside the main rod and includes a catch (30). The unit has a step (31) provided at an end of the rod (20) and a locking sleeve (32) axially displaceable by an unlocking motor (33) from locking position and release position. An independent claim is also included for a method of using an actuator.</p>
申请公布号 FR2895482(A1) 申请公布日期 2007.06.29
申请号 FR20050013298 申请日期 2005.12.23
申请人 MESSIER BUGATTI SOCIETE ANONYME 发明人 BUCHETON DANIEL
分类号 F16H25/20;B64C25/20;B64C25/30 主分类号 F16H25/20
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