发明名称 Rotor blade
摘要 A rotor blade made of fiber-reinforced synthetic resin has a profile which, at least in the region of the blade tip is designed so as to be twistable by actuators about the rotor blade longitudinal axis. The torsion skin of the rotor blade in the region of the blade tip is designed anisotropically in the sense of a tension/torsion coupling and a controllable actuator, which acts in a longitudinal direction of the rotor blade upon the rotor blade tip, is disposed in the rotor blade spar. To achieve anisotropy, the torsion skin is a uni-directional winding having a winding angle of less than 45 DEG relative to the rotor blade longitudinal axis. The winding angle is dependent upon the force-to-displacement ratio of the actuator and may lie between 18 DEG and 40 DEG . In the region of the blade tip, the anisotropic torsion skin is disposed resting loosely on the rotor blade spar.
申请公布号 US5730581(A) 申请公布日期 1998.03.24
申请号 US19960691459 申请日期 1996.08.02
申请人 DEUTSCHE FORSCHUNGSANSTALT FUR LUFT-UND RAUMFAHRT E.V. 发明人 BUTER, ANDREAS;PIENING, MATTHIAS
分类号 B64C27/615;F03D1/06;F03D7/02;(IPC1-7):F04D29/18 主分类号 B64C27/615
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