Antiresonant suspension device for a helicopter
    1.
    发明授权
    Antiresonant suspension device for a helicopter 失效
    用于直升机的防静电悬挂装置

    公开(公告)号:US5190244A

    公开(公告)日:1993-03-02

    申请号:US794066

    申请日:1991-11-19

    申请人: Victor Y. Yana

    发明人: Victor Y. Yana

    摘要: The suspension device is interposed between the rotor and the fuselage of the helicopter for filtering the vibration exciting forces and moments coming from the rotor. In this helicopter, a speed reducer (1) is provided in a housing mounted on the fuselage (22) by rigid oblique bars (28). According to the invention, there are disposed around the housing of the speed reducer, in a number equal to the number of rigid oblique bars (28), monodirectional antiresonant means (20,21,23,23a,23b,25) connecting the upper ends of the rigid oblique bars (28) to the speed reducer (1).

    摘要翻译: 悬架装置设置在转子和直升机的机身之间,用于过滤来自转子的振动激励力和力矩。 在该直升机中,减速器(1)设置在通过刚性斜杆(28)安装在机身(22)上的壳体中。 根据本发明,围绕减速器的壳体设置数量等于刚性斜杆(28)的数量,单向反谐振装置(20,21,23,23a,23b,25)连接上部 刚性斜杆(28)的端部连接到减速器(1)。

    Anti-resonant suspension device having six degrees of freedom for a
helicopter
    2.
    发明授权
    Anti-resonant suspension device having six degrees of freedom for a helicopter 失效
    用于直升机具有六个自由度的反共振悬挂装置

    公开(公告)号:US4720060A

    公开(公告)日:1988-01-19

    申请号:US879217

    申请日:1986-06-27

    申请人: Victor Y. Yana

    发明人: Victor Y. Yana

    IPC分类号: B64C27/00 B64C27/04

    摘要: The device comprises four identical assemblies evenly spaced apart about the vertical axis of a speed reducer (1), offset 90.degree. from each other and each comprising an isotropic flexible beam (4) carrying a beating weight (14) and connected by its ends to the fuselage, this beam being perpendicular to the vertical axis, and rigid triangulation means (9, 10) connecting the speed reducer (1) to the beam (4) so as transmit its forces and its moments to the beam in a plane parallel to an offset from said vertical axis of the speed reducer (1).

    摘要翻译: 该装置包括围绕减速器(1)的垂直轴线均匀隔开的四个相同的组件,彼此偏移90°,并且每个组件包括承载跳动重物(14)的各向同性的柔性梁(4),并且其端部连接到 机身,该梁垂直于垂直轴,以及将减速器(1)连接到梁(4)上的刚性三角测量装置(9,10),以将其力和力矩传递到平行于 与减速器(1)的垂直轴线的偏移。

    Elastic strut having an integrated hydromechanical resonator in
particular for the suspension of a transmission box on a rotor aircraft
and a suspension device using such a strut
    3.
    发明授权
    Elastic strut having an integrated hydromechanical resonator in particular for the suspension of a transmission box on a rotor aircraft and a suspension device using such a strut 失效
    具有集成的液压机械谐振器的弹性支柱,特别用于转子飞机上的传动箱的悬架和使用这种支柱的悬架装置

    公开(公告)号:US4974794A

    公开(公告)日:1990-12-04

    申请号:US329752

    申请日:1989-03-28

    摘要: In this elastic strut incorporating a hydromechanical resonator having a weight/spring system of the type providing a hydraulic amplification of the displacement of the beating weight (7), the weight mounted between two opposed return springs constitutes a double-sided hollow piston slidably mounted on two coaxial opposed cylinders (6) in a closed chamber filled with a liquid (10) in an inner tubular element (1) disposed in an outer tubular element (2) with which it defines, at each end, a chamber (18, 26) filled with liquid onto which opens one of the cylinders (6), the elements (1, 2) constituting the body of the strut being coaxially movable relative to each other and fixed together at each of their ends in a sealed and elastic manner by bearings composed of an elastomer material.

    摘要翻译: 在该弹性支柱中,结合有具有重量/弹簧系统的液压机械共振器,该重量/弹簧系统提供对打浆锤(7)的位移的液压放大,安装在两个相对的复位弹簧之间的重物构成可滑动地安装在 两个同轴相对的气缸(6)在密封的腔室中,该腔体设置在外部管状元件(2)中的内部管状元件(1)中,液体(10)在每个端部限定一个腔室(18,26) )填充有液体,其上打开一个气缸(6),构成支柱主体的元件(1,2)可相对于彼此同轴地移动,并以密封和弹性方式固定在其每个端部处 轴承由弹性体材料组成。