发明名称 Disc rotor retraction system
摘要 A disc rotor blade retraction system includes a main blade spar (22) incorporating a hydraulic cylinder (54) and having a screw thread (34). A ball screw (24) is concentrically carried within the main blade spar and is operably connected to a ball nut (60) which has an outboard end connected to an intermediate spar (26) with a hydraulic piston (62) received for reciprocation in the hydraulic cylinder. A first geared actuator (20) engages the ball screw and a second geared actuator (30) engages the main blade spar screw thread. A hydraulic fluid accumulator (74) providing pressurized hydraulic fluid is connected to an outboard end of the hydraulic cylinder and a controller actuates the first and second geared actuators.
申请公布号 EP2492192(A2) 申请公布日期 2012.08.29
申请号 EP20120157385 申请日期 2012.02.28
申请人 THE BOEING COMPANY 发明人 PODGURSKI, DANIEL MICHAEL
分类号 B64C27/32 主分类号 B64C27/32
代理机构 代理人
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