发明申请
- 专利标题: Hybrid actuator for helicopter rotor blade control flaps
- 专利标题(中): 用于直升机转子叶片控制翼片的混合致动器
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申请号: US11638980申请日: 2006-12-14
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公开(公告)号: US20080145221A1公开(公告)日: 2008-06-19
- 发明人: Fanping Sun , Zaffir A. Chaudhry , Jimmy Lih-Min Yeh , Michael G. O'Callaghan , Ulf J. Jonsson , Brian E. Wake , Robert H. Dold
- 申请人: Fanping Sun , Zaffir A. Chaudhry , Jimmy Lih-Min Yeh , Michael G. O'Callaghan , Ulf J. Jonsson , Brian E. Wake , Robert H. Dold
- 专利权人: SIKORKSY AIRCRAFT CORPORATION
- 当前专利权人: SIKORKSY AIRCRAFT CORPORATION
- 主分类号: F01D7/00
- IPC分类号: F01D7/00
摘要:
A helicopter rotor blade that has a blade body and a control flap secured to the blade body. The rotor blade has a first primary mover capable of generating a first linear motion that is sufficient to generate a high amplitude, low frequency motion of the control flap; and a second primary mover capable of generating a second linear motion that is sufficient to generate a small amplitude, high frequency motion of the control flap. Further, the rotor blade has a coupling transmission for combining the first linear motion with the second linear motion that generates a cumulative linear motion; and a second transmission device that causes the cumulative linear motion to rotate the control flap.
公开/授权文献
- US07762770B2 Hybrid actuator for helicopter rotor blade control flaps 公开/授权日:2010-07-27
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