发明申请
- 专利标题: MODULAR INTEGRATED DEVICE FOR ROTOR BLADE CONTROL
- 专利标题(中): 用于转子叶片控制的模块化集成装置
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申请号: US13025394申请日: 2011-02-11
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公开(公告)号: US20120207602A1公开(公告)日: 2012-08-16
- 发明人: Claude G. Matalanis , Andrzej Ernest Kuczek , Zaffir A. Chaudhry , Brian E. Wake , Vijaya Ramaraju Lakamraju , Alan Matthew Finn , Fanping Sun , Ulf J. Jonsson
- 申请人: Claude G. Matalanis , Andrzej Ernest Kuczek , Zaffir A. Chaudhry , Brian E. Wake , Vijaya Ramaraju Lakamraju , Alan Matthew Finn , Fanping Sun , Ulf J. Jonsson
- 申请人地址: US CT Stratford
- 专利权人: SIKORSKY AIRCRAFT CORPORATION
- 当前专利权人: SIKORSKY AIRCRAFT CORPORATION
- 当前专利权人地址: US CT Stratford
- 主分类号: B64C27/473
- IPC分类号: B64C27/473
摘要:
A rotor blade assembly includes a rotor blade including one or more pockets and a housing located on the rotor blade within one or more pockets. The housing is secured to the rotor blade via one or more dovetail joints. A drive mechanism for a control surface of a rotor blade includes an actuator and a rocker operably connected to the actuator. At least one hinge rod is operably connected to the rocker and operably connected to a control surface at a control surface pivot. The drive mechanism translates substantially linear motion of the actuator into rotational motion of the control surface about the control surface pivot.
公开/授权文献
- US09278755B2 Modular integrated device for rotor blade control 公开/授权日:2016-03-08
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