发明名称 JAM RESISTANT BALL SCREW ACTUATOR
摘要 An actuator (10) is disclosed for movement between a retracted position and an extended position. The actuator (10) can be used to pivot a pylon (14) in a tilt rotor aircraft relative to the aircraft wing (12) between a helicopter mode and an aircraft mode. The actuator (10) is provided with an inner ball screw drive unit (20) and an outer ball screw drive unit (22) which provides for limited motion should one of the drive units jam. Further, the actuator (10) can be operated from either end of the actuator. Each ball screw (28, 52) in the actuator is associated with a tube (30, 54), preferably of carbon fiber composite, which forms a secondary load path if the screw fails.
申请公布号 EP0448711(A4) 申请公布日期 1993.03.31
申请号 EP19910900519 申请日期 1990.09.06
申请人 BELL HELICOPTER TEXTRON INC. 发明人 CAERO, JOSE, GERMAN 2301 SOUTH JEFFERSON DAVIS
分类号 B64C13/42;B64C27/28;B64C29/00;F16H25/22;(IPC1-7):B64C9/00 主分类号 B64C13/42
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