发明名称 Dual frequency hub mounted vibration suppressor system
摘要 A vibration suppressor system includes an annular electric motor system which independently controls rotation of at least two masses about the axis of rotation to reduce in-plane vibration of the rotating system. A method of reducing vibrations in a rotary-wing aircraft includes independently controlling a relative angular position of a multiple of independently rotatable masses to reduce vibrations of a main rotor system.
申请公布号 US8403643(B2) 申请公布日期 2013.03.26
申请号 US20090353217 申请日期 2009.01.13
申请人 WELSH WILLIAM A.;SIKORSKY AIRCRAFT CORPORATION 发明人 WELSH WILLIAM A.
分类号 B64C27/00 主分类号 B64C27/00
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