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    • 3. 发明公开
    • Improved vibration absorber
    • Schwingungsdämpfer。
    • EP0323768A1
    • 1989-07-12
    • EP88402925.7
    • 1988-11-22
    • BARRY WRIGHT CORPORATION
    • Brumme, ReinholdDesons, Roger
    • F16F13/00
    • F16F13/08
    • The invention concerns a vibration absorber intended to be disposed between two devices.
      The absorber is of the type comprising a casing (1) solid with one of the said devices, two bell-shaped membranes (2, 3) of a resiliently deformable material, mounted in coaxial relationship and axially aligned inside the casing, with the tops thereof facing each other, and connected through their bases to the said casing, and a rod (7) intended to be solid with the other device, coaxially passing through the said membranes, and connected to the membranes so that a relative motion of the rod with respect to the casing provokes a resilient deformation of at least one membrane and is characterized in that both membranes (2, 3) are solid with the rod (7) at their tops (4) and in that their radially outer peripheral surfaces delimit a tight chamber (14) inside the casing (1) of a constant volume and which is filled with a liquid.
      The invention is useful in the cases where a weak overtension is desired.
    • 本发明涉及旨在设置在两个装置之间的减振器。 所述吸收体是包括具有一个所述装置的壳体(1)的类型的壳体(1),两个可弹性变形材料的钟形膜(2,3)以同轴的关系安装并且在壳体内轴向对准,顶部 并且通过它们的底座连接到所述壳体,以及与另一装置固定的杆(7),同轴地穿过所述膜并连接到膜,使得杆的相对运动 相对于套管引起至少一个膜的弹性变形,其特征在于两个膜(2,3)在其顶部(4)处具有杆(7)是固体的,并且其径向外周表面限定一个 (1)内的紧固室(14),其具有恒定体积并且填充有液体。 本发明在需要弱过大的情况下是有用的。
    • 4. 发明公开
    • Apparatus for securing an electronic unit to an avionics tray
    • 用于将电子装置保存到航空纸盘的装置
    • EP0105609A3
    • 1986-03-12
    • EP83305061
    • 1983-09-01
    • BARRY WRIGHT CORPORATION
    • Roake, Joseph Charles
    • G12B09/10H05K07/14
    • G12B9/10H05K7/1412Y10T29/53209Y10T29/53257Y10T29/53283Y10T74/18696
    • Apparatus for removing and securing a plug-in electronic unit or the like to or from an avionics tray comprises a threaded spindle carrying a transverse pin at one end thereof and having an arrangement of three concentric sleeves located about the spindle. Stop members are provided to limit the movement of the sleeves in both axial directions along the threaded spindle. A rotatable grip is fitted about the innermost of the three concentric sleeves at that end of the sleeve remote from the transverse pin. A ring member is positioned about the middle of the three sleeves and cooperates with an extended flange of the latter to define an annular recess which contains a resilient element. A torque- limiting arrangement is provided between the rotatable grip and a cooperating surface portion of the middle of the three sleeves. The outermost sleeve has, at its end closest to the transverse pin, a radial flange which together with said ring member defines an annular recess capable of receiving a hook forming part of the attachment mechanism of an electronic unit. In use, rotation of the rotatable grip allows an electronic unit to be inserted into an avionics tray with a predetermined degree of force, this being adjusted via the torque limiting arrangement. Rotation of the rotatable grip in the opposite sense effects removal of the electronic unit from the avionics tray.
    • 8. 发明公开
    • Laminated bearing
    • Laminatlager。
    • EP0306027A2
    • 1989-03-08
    • EP88114292.1
    • 1988-09-01
    • BARRY WRIGHT CORPORATION
    • Finney, Robert H.
    • F16F1/40B64C27/35B64C27/41
    • F16F1/41B64C27/35B64C27/41
    • An improved bearing designed for use in a link assembly of a coupling assembly used for coupling a first member to a second member in an aircraft is disclosed. The bearing comprises a plurality of alternating layers of a resilient, elastomeric material and a non-extensible material coaxially formed around a common axis. Each of the innermost and outermost layers of is adapted to be coupled to a respective one of the members, and has at least a center portion in which each of the inner radial and outer radial surfaces of the center portion of each innermost and outermost layers is formed as a surface of revolution around the axis with a curvature having an axial cross-sectional shape defined by different centers of curvature so as to reduce the compression induced shear strain carried by the innermost and outermost layers when the layers are subjected to compression induced shear.
    • 公开了一种设计用于联接组件的改进的轴承,其用于将飞行器中的第一构件联接到第二构件。 轴承包括多个交替的弹性弹性体材料层和围绕公共轴同轴地形成的不可伸展材料。 最内层和最外层的每一个适于联接到相应的一个构件,并且至少具有中心部分,其中每个最内层和最外层的中心部分的内径向外径面和外径向表面中的每一个 形成为围绕轴线的旋转表面,具有由不同曲率中心限定的轴向横截面形状的曲率,以便当层受到压缩诱导剪切时减小最内层和最外层承受的压缩诱导剪切应变 。