发明名称 Drive system for the retraction/extension of variable diameter rotor systems
摘要 A drive system for a variable diameter rotor (VDR) system includes a plurality of rotor blade assemblies with inner and outer rotor blade segments. The outer blade segment being telescopically mounted to the inner blade segment. The VDR retraction/extension system includes a drive housing mounted at the root of each blade. The housing supports a spool assembly, a harmonic gear set and an electric motor. The spool assembly includes a pair of counter rotating spools each of which drive a respective cable which extends through the interior of the inboard rotor blade section and around a pulley mounted to the outboard rotor blade section. In operation, the electric motor drives the harmonic gear set which rotates the counter rotating spools. Rotation of the spools causes the cables to be wound onto or off their respective spool consequently effecting retraction/extension of the pulley and the attached outboard rotor blade section relative the inboard rotor blade section. As each blade drive system is independently driven by a separate electrical motor, each independent VDR blade assembly is independently positionable.
申请公布号 US6655915(B2) 申请公布日期 2003.12.02
申请号 US20020136124 申请日期 2002.05.01
申请人 SIKORSKY AIRCRAFT CORPORATION 发明人 GMIRYA YURIY
分类号 B64C11/28;B64C27/28;B64C27/473;B64C29/00;(IPC1-7):B64C11/28 主分类号 B64C11/28
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