发明名称 Variable pitch propeller rotor
摘要 A bladed rotor comprises a rotor body 2 carrying blades 6, whose pitch can be varied by means of a pitch input shaft 10. The pitch input shaft 10 drives the respective blade 6 about a spanwise axis X of the blade through a harmonic drive reduction gear 14. The harmonic drive reduction gear 14 comprises a wave generator 16 which is fixed for rotation on the pitch input shaft 10 and a flex spline which meshes with a circular spline 20 and is secured to the blade 6.
申请公布号 US9302765(B2) 申请公布日期 2016.04.05
申请号 US201213458386 申请日期 2012.04.27
申请人 ROLLS-ROYCE plc 发明人 Thornton Stewart T.;Simms Paul;McFarlane Colin W R
分类号 B64C11/32;B64C11/30;B64D27/00 主分类号 B64C11/32
代理机构 Oliff PLC 代理人 Oliff PLC
主权项 1. A variable pitch bladed rotor comprising a rotor body carrying a plurality of blades, each blade having a blade root supported by bearings in a blade hub of the rotor body so as to be pivotable relative to the rotor body about respective spanwise pitch axes, each blade being drivably coupled to a pitch control mechanism by a respective pitch input shaft which is aligned with the pitch axis and which is drivingly connected to the blade by a harmonic drive reduction gear, the harmonic drive reduction gear comprising a circular spline in toothed engagement with a flex spline and a wave generator arranged to generate a travelling wave in the flex spline, wherein the circular spline is fixedly mounted on the blade hub and the flex spline is secured to the blade root.
地址 London GB
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