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    • 3. 发明申请
    • WELLS TURBINE HAVING PASSIVE ROTOR BLADE DISPLACEMENT
    • 被动转动叶片调节韦尔斯涡轮机
    • WO2009071150A3
    • 2010-06-10
    • PCT/EP2008008754
    • 2008-10-16
    • VOITH PATENT GMBHARLITT RAPHAELBRONOWSKI HELMUTWEILEPP JOCHENENGELHARDT MICHAELSTARZMANN RALF
    • ARLITT RAPHAELBRONOWSKI HELMUTWEILEPP JOCHENENGELHARDT MICHAELSTARZMANN RALF
    • F03B13/24F03B13/06F03D1/06
    • F03B13/24F03B13/142F03D1/0675F05B2210/404F05B2260/74F05B2260/77F05B2260/78F05B2280/1021F05C2201/021Y02E10/32Y02E10/38Y02E10/721Y02E60/17
    • The invention relates to a Wells turbine comprising a hub carrying a plurality of rotor blades having a symmetrical, drop-shaped profile originating from a profile nose; the rotor blades are attached to the hub in a rotary fashion by means of a foot part such that the angle of incidence position is variable relative to the plane of rotation, wherein the associated rotational axis for each profile section intersects the chord line at a threading point located in a region between the profile nose and the aerodynamic center of the profile; the adjustment of the angle of incidence is made passively by the equilibrium occurring during the operation of the Wells turbine between the aerodynamic torques engaging on the rotor blades and the centrifugal force torques, wherein the average density of the rotor blades is selected at less than 2700 kg/m3 and/or mass distribution within the profile is structured such that the surface centrifugal torque or the rotor blades is reduced relative to a profile of a full material and/or the surface centrifugal torque of the rotor blades is at least partially compensated by compensatory weights disposed at a distance from the center and perpendicular to the chord line.
    • 本发明涉及一种韦尔斯涡轮机,其包括承载多个转子叶片与轮毂的水滴形,从配置文件鼻子,对称轮廓开始; 转子叶片由安装在轮毂上的脚的方式连接,以使桨距调节是可变的,以旋转平面,其中用于在穿线点的每个轮廓截面相关联的旋转轴线相交的弦,其位于轮廓鼻子和轮廓的气动中心之间的区域; 间距调整是通过在韦尔斯涡轮机上转子叶片调整攻击之间的平衡气动力矩和离心力扭矩,其中,所述转子叶片的平均密度小于2700公斤的操作而设计的简档在其内部质量分布被动地进行选择/立方米和/或 是表面离心转子叶片是相反的固体材料的轮廓被减小和/或表面离心转子叶片至少部分地由配重,其在从所述枢轴点的距离和被布置成垂直于轮廓弦偏移。