发明公开
- 专利标题: ROTOR SYSTEM WITH PITCH FLAP COUPLING
- 专利标题(中): 皮瓣及电站转子系统
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申请号: EP07875057.7申请日: 2007-11-12
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公开(公告)号: EP2084055A1公开(公告)日: 2009-08-05
- 发明人: SCHMALING, David N. , CABRERA, Pedro L.
- 申请人: Sikorsky Aircraft Corporation
- 申请人地址: 6900 Main Street P.O. Box 9729 Stratford, CT 06615 US
- 专利权人: Sikorsky Aircraft Corporation
- 当前专利权人: Sikorsky Aircraft Corporation
- 当前专利权人地址: 6900 Main Street P.O. Box 9729 Stratford, CT 06615 US
- 代理机构: Klunker . Schmitt-Nilson . Hirsch
- 优先权: US560008 20061115
- 国际公布: WO2008147448 20081204
- 主分类号: B63H1/06
- IPC分类号: B63H1/06
摘要:
An articulated rotor system with a servo-flap rotor control system locates the focal point of a blade retention spherical elastomeric bearing inboard of a joint in the servo-flap pitch control tube which separates the flap hinge and supports the servo-flap pitch control tube on a single pivot bearing within a blade retention spindle. Rotor blade flapping produces relative movements between the servo-flap pitch control tube and the blade retention spindle which is converted through a servo-flap drive linkage into servo-flap pitch motions to provide flap/pitch coupling which reduces steady and transient blade flapping.
公开/授权文献
- EP2084055B1 ROTOR SYSTEM WITH PITCH FLAP COUPLING 公开/授权日:2014-10-15
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