Aircraft rotor blade with passive tuned tab
    7.
    发明授权
    Aircraft rotor blade with passive tuned tab 失效
    飞机转子叶片与被动调谐片

    公开(公告)号:US4514143A

    公开(公告)日:1985-04-30

    申请号:US489675

    申请日:1983-04-28

    摘要: A structure (10) for reducing vibratory airloading in a rotor blade (12) with a leading edge (14) and a trailing edge (16) includes a cut-out portion (18) at the trailing edge. A substantially wedge shaped cross-section, inertially deflectable tab (20), also having a leading edge (22) and a trailing edge (24) is pivotally mounted in the cut-out portion. The trailing edge (24) of the tab (20) may move above and below the rotor blade (12). A torsion strap (26 or 64) applies force against the tab (20) when the trailing edge (24) of the tab (20) is above and below the rotor blade (12). A restraining member (92) is slidably movable along the torsion strap (64) to vary torsional biasing force supplied by the torsion bar (64) to the tab (20). A plurality of movable weights (82) positioned between plates (84) and (86) vary a center of gravity of the tab (20). Skin (74) of the tab (20) is formed from unidirectional graphite and fiberglass layers. Sliders (54 and 56), coupled with a pinned degree of freedom at rod (58) eliminate bending of tab (20) under edgewise blade deflection.

    摘要翻译: 用于减小具有前缘(14)和后缘(16)的转子叶片(12)中的振动空气负载的结构(10)包括在后缘处的切口部分(18)。 枢转地安装在切口部分中的具有前缘(22)和后缘(24)的基本楔形的横截面惯性偏转片(20)。 突片(20)的后缘(24)可以在转子叶片(12)的上方和下方移动。 当翼片(20)的后缘(24)位于转子叶片(12)的上方和下方时,扭力带(26或64)向翼片(20)施加力。 约束构件(92)可沿着扭力带(64)可滑动地移动,以便将由扭力杆(64)提供的扭转偏压力改变到翼片(20)。 定位在板(84)和(86)之间的多个可移动重物(82)改变突片(20)的重心。 翼片(20)的皮肤(74)由单向石墨和玻璃纤维层形成。 滑杆(54和56)与杆(58)上的固定自由度相结合,消除了沿边缘叶片偏转下翼片(20)的弯曲。

    Helicopter gimbal rotor
    9.
    发明授权
    Helicopter gimbal rotor 失效
    直升机云台转子

    公开(公告)号:US4569629A

    公开(公告)日:1986-02-11

    申请号:US655384

    申请日:1984-09-27

    摘要: Hub moment and driving torque is provided for a helicopter gimbal rotor by two-part flat springs that are in-plane with the rotor tilt point (P). The inboard end of an outward part of each spring is connected to the rotorshaft and the inboard end of an inward part of the spring is connected to the tiltable hub member. The outboard ends of the two spring parts are journaled together by an eccentric elastomeric joint that allows for spring foreshortening that accompanies rotor tilt.

    摘要翻译: 通过与转子倾斜点(P)处于平面的两部分平面弹簧为直升机万向转子提供轮毂力矩和驱动扭矩。 每个弹簧的向外部分的内侧端部连接到转轴,并且弹簧的向内部分的内侧端部连接到可倾斜的毂部件上。 两个弹簧部件的外侧端部通过一个偏心的弹性接头连在一起,该弹性接头允许伴随转子倾斜的弹簧缩短。