发明名称 Articulable rotational coupling for an aircraft
摘要 An airfoil surface control system includes a movable surface. An actuator, 28, is coupled to the surface. The airfoil surface control system includes a motor, 22. A torque tube assembly, 26, operatively couples the motor, 22, and actuator, 28, and includes first and second shafts, 30, 32, coupled by a universal joint. The universal joint, 36, is configured to provide a first maximum angle between the first and second shafts, 30, 32. A stop is configured to provide a second maximum angle between the first and second shafts, 30, 32, that is less than the first maximum angle.
申请公布号 EP2664811(B1) 申请公布日期 2016.03.02
申请号 EP20130167349 申请日期 2013.05.10
申请人 HAMILTON SUNDSTRAND CORPORATION 发明人 HILL, DAVID G.
分类号 F16D3/40;B64C13/28;F16D3/84 主分类号 F16D3/40
代理机构 代理人
主权项
地址