发明名称 VARIABLE PITCH PROPELLER MODULE FOR AN AERO GAS TURBINE ENGINE POWERPLANT
摘要 A variable pitch propeller module includes first and second multi-bladed propellers arranged to be driven in opposite rotational directions by a reduction gear mechanism, via shafts. First and second drums are rotatably mounted on the hubs of the first and second propellers and the drums are arranged to rotate the blades of the propellers. A hydraulic motor is mounted coaxially on and rotates with the second propeller, the hydraulic motor being arranged to drive the drums by via a pitch change gear assembly. A hydraulic fluid feed tube extends coaxially through the reduction gear mechanism and both propellers to supply hydraulic fluid to the hydraulic motor. An annular sleeve is positioned coaxially on the tube. The hydraulic fluid feed tube has passages and the sleeve has passages which are aligned to allow hydraulic fluid to flow to the hydraulic motor to vary the pitch of both blades. The feed tube and sleeve are moved axially to control the flow of hydraulic fluid to the hydraulic motor.
申请公布号 US5090869(A) 申请公布日期 1992.02.25
申请号 US19900507578 申请日期 1990.04.11
申请人 ROLLS-ROYCE PLC 发明人 WRIGHT, WILLIAM B.
分类号 B64C11/30;F02C6/02;F02C6/20 主分类号 B64C11/30
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