发明名称 Propeller pitch control system and apparatus
摘要 A plurality of propeller blades are mounted to an axially elongated tubular propeller hub (H1). Each blade is rotatable in position about a radial axis. An electromechanical linear actuator (A1) is housed within the hub for rotating the blades to change their pitch. The actuator includes a rod member (R1) fixed in position relative to the hub, a casing (C1) which can extend and retract relative to the rod member, a rotary electric motor (M1), and a planetary screw drive (SD1). The screw drive (SD1) drivingly interconnects the electric motor (M1) with the casing (C1) for causing the casing to move axially in response to operation of the motor. The actuator (A1) is connected to the propeller (P1) by a linkage (L1) so that movement of the casing causes the propellers to change their pitch. A second actuator (A2) may be housed within the hub (H1) and connected to the first actuator (A1) for providing redundancy in the event of failure of the first actuator.
申请公布号 US4591313(A) 申请公布日期 1986.05.27
申请号 US19830567054 申请日期 1983.12.30
申请人 THE BOEING COMPANY 发明人 MIYATAKE, HENRY J.;SAKURAI, SEIYA
分类号 B64C11/30;B64C11/44;(IPC1-7):B64C11/44 主分类号 B64C11/30
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