发明名称 Modular propeller blade pitch actuation system
摘要 A modular, easily replaceable, pitch actuation system is removably secured within the hub of an aircraft. The modular system houses a driving system which provides a rotational output to set the pitch of propeller blades mounted to the hub, and a pitch changing system that controls the driving system. The driving system includes a high-speed, low-torque hydraulic motor that drives an harmonic drive to amplify the torque of the motor. The pitch changing system includes an actuator which positions a valve that controls the hydraulic motor, and a nulling gear which repositions the valve and acts as a pitch lock.
申请公布号 US4750862(A) 申请公布日期 1988.06.14
申请号 US19860936046 申请日期 1986.11.28
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 BARNES, PHILIP E.;KUSIAK, EDWARD H.
分类号 B64C11/32;B64C11/30;B64C11/40;(IPC1-7):B64C11/38 主分类号 B64C11/32
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