发明名称 Rotor with aerodynamically modelled blade for helicopter or wind turbine - includes resonator mass guided in curved path so during rotor rotation centrifugal force acting on mass is provided by force driving mass back to rest position
摘要 The rotor (1) has a shaft mounted rotatably in a frame, bearing, on a free end zone, a hub to which the blade is fixed. The blade zone is remote from the hub and has a mechanical resonator, the eigen frequency of which is the same as the resonance frequency of the blade to be suppressed. The resonator has a mass moving reciprocally around a middle position in the plane. The mass moves guided in a curved path, the middle zone of which has the greatest distance from the rotation axis of the rotor. During rotor rotation, the centrifugal force acting on the mass is partially provided by the force driving the mass back to the rest position defined by the middle zone.
申请公布号 NL1008027(C2) 申请公布日期 1998.10.01
申请号 NL19981008027 申请日期 1998.01.14
申请人 AERPAC UK LTD. 发明人 RICHARD YEMM;HENDRIK JAN HEERKES
分类号 B64C27/51;B64C27/625;F03D1/06;F03D7/02;F03D11/00;F16F7/10;F16F15/03 主分类号 B64C27/51
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