PITCH STABILIZER AND ROTARY-WING AIRCRAFT EQUIPPED WITH SUCH STABILIZER
    1.
    发明申请
    PITCH STABILIZER AND ROTARY-WING AIRCRAFT EQUIPPED WITH SUCH STABILIZER 有权
    配有稳定器的旋转稳定器和旋转式飞机

    公开(公告)号:US20140077026A1

    公开(公告)日:2014-03-20

    申请号:US14028690

    申请日:2013-09-17

    Applicant: Eurocopter

    Inventor: Frederic Beroul

    CPC classification number: B64C5/16 B64C5/02 B64C27/06 B64C27/82 B64C2027/8281

    Abstract: A pitch stabilizer [10] equipped with an upper stabilizer surface [15] and a lower stabilizer surface [20], with the upper stabilizer surface [15] being located in an upper plane [P1] and with the lower stabilizer surface [20] being located in a lower plane [P2], with the upper plane [P1] overhanging the lower plane [P2]. The upper stabilizer surface [15] is rotatable about an upper axis of rotation [AX1], with the said lower stabilizer surface [20] being rotatable about a lower axis of rotation [AX2], with the stabilizer means [10] having linking means [30] whereby a rotary movement of one stabilizer surface causes an equal rotary movement of the other stabilizer surface.

    Abstract translation: 配备有上稳定器表面[15]和下稳定器表面[20]的俯仰稳定器[10],其中上稳定器表面[15]位于上平面[P1]中并且具有下稳定器表面[20] 位于下平面[P2]中,上平面[P1]伸出下平面[P2]。 上稳定器表面15可以围绕旋转轴线[AX1]旋转,其中所述下稳定器表面20可以围绕下旋转轴线[AX2]旋转,稳定装置[10]具有连接装置 由此一个稳定器表面的旋转运动导致另一个稳定器表面的相等的旋转运动。

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