发明名称 Main rotor shaft mounted hydraulic pressure system
摘要 A rotor system includes a hydraulic pressure system located within a rotor shaft along an axis or rotation. The hydraulic pressure system is within the rotating field such that fluid pressure is generated and supplied from within the rotational field without the need to cross a rotational interface. Differential rotation between the rotor shaft and a standpipe rotates a hydraulic pump body relative a hydraulic pump shaft. The hydraulic pressure system is contained within a support structure so as to be readily mounted and removed from the rotor hub for replacement or maintenance. A gear system is mounted to the support structure between the standpipe and the hydraulic pump shaft to step-up or step-down the relative rotation between the rotor shaft and the standpipe.
申请公布号 US6908286(B2) 申请公布日期 2005.06.21
申请号 US20030617194 申请日期 2003.07.10
申请人 SIKORSKY AIRCRAFT CORPORATION 发明人 LESKOW DAVID J.;EADIE WILLIAM J.
分类号 B64C27/32;B64C27/615;B64C27/64;(IPC1-7):B63H1/00 主分类号 B64C27/32
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