ROTOR BLADE TIP PLAN FORM
    1.
    发明公开
    ROTOR BLADE TIP PLAN FORM 审中-公开
    GRUNDRISSFÜRROTORSCHAUFELSPITZE

    公开(公告)号:EP1991458A4

    公开(公告)日:2015-10-21

    申请号:EP06836361

    申请日:2006-10-17

    IPC分类号: B63H1/06 B64C27/46

    CPC分类号: B64C27/463

    摘要: A main rotor blade incorporating a rotor blade tip region having a tip chord and a tip taper such that the ratio of the main rotor blade chord to the tip chord is approximately 0.30. The tip taper ratio preferably providing an approximately 28% area of reduction in said outer 10% of said blade span. The tip region preferably further including a hover optimized high lift airfoil and a tip sweep that reaches a constant value of approximately 30 degrees along the quarter chord line.

    摘要翻译: 主转子叶片包括具有尖端弦和尖端锥形的转子叶片尖端区域,使得主转子叶片弦与尖端弦的比率大约为0.30。 尖端锥度比优选地在所述叶片跨度的所述外部10%中提供约28%的减小面积。 尖端区域优选地还包括悬停优化的高升力翼型件和沿着四分之一弦线达到大约30度的恒定值的尖端扫掠。

    ROTOR SYSTEM WITH PITCH FLAP COUPLING
    3.
    发明公开
    ROTOR SYSTEM WITH PITCH FLAP COUPLING 有权
    皮瓣及电站转子系统

    公开(公告)号:EP2084055A1

    公开(公告)日:2009-08-05

    申请号:EP07875057.7

    申请日:2007-11-12

    IPC分类号: B63H1/06

    摘要: An articulated rotor system with a servo-flap rotor control system locates the focal point of a blade retention spherical elastomeric bearing inboard of a joint in the servo-flap pitch control tube which separates the flap hinge and supports the servo-flap pitch control tube on a single pivot bearing within a blade retention spindle. Rotor blade flapping produces relative movements between the servo-flap pitch control tube and the blade retention spindle which is converted through a servo-flap drive linkage into servo-flap pitch motions to provide flap/pitch coupling which reduces steady and transient blade flapping.

    WIND TURBINE
    9.
    发明公开
    WIND TURBINE 审中-公开
    风力发电机组

    公开(公告)号:EP1824728A2

    公开(公告)日:2007-08-29

    申请号:EP05857006.0

    申请日:2005-11-23

    申请人: Jonsson, Stanley

    发明人: Jonsson, Stanley

    IPC分类号: B63H1/06

    摘要: A wind turbine, with: a rotatable frame; a plurality of airfoils mounted to the rotatable frame, wherein the airfoils extend parallel to an axis of rotation of the rotatable frame; a wind block positioned to restrict airflow over at least a portion of the rotatable frame; and at least one drive wheel in contact with the rotatable frame.