公开(公告)号：US1585797A

公开(公告)日：1926-05-25

申请号：US1585797D

CPC分类号： F16F7/06 ,  F16F7/065

公开(公告)号：US5542505A

公开(公告)日：1996-08-06

申请号：US452062

申请日：1995-05-26

申请人： Mark Kempf

发明人： Mark Kempf

IPC分类号： E05D11/08 ,  F16D49/02 ,  F16F7/06 ,  F16D63/00

CPC分类号： F16D49/02 ,  E05D11/084 ,  F16F7/065 ,  Y10T16/5389 ,  Y10T16/54038

摘要： A torque limiting device that includes a shaft and a wrap extending around the shaft. The wrap is frictionally engaged with the shaft, and the wrap has an inner and an outer surface. The device further includes a restraining mechanism enclosing the wrap such that there is contact between the restraining mechanism and the outer surface of the wrap, and such that the restraining mechanism prevents the wrap from rotating relative to the retraining mechanism as the shaft is rotated in either one of two opposing rotational directions.

摘要翻译： 扭矩限制装置，其包括轴和围绕轴延伸的包裹物。 包裹物与轴摩擦接合，并且包裹物具有内表面和外表面。 该装置还包括限制机构，其包围包裹物，使得约束机构和包裹物的外表面之间存在接触，并且使得约束机构防止卷轴相对于再培训机构旋转，因为轴在任一 两个相反的旋转方向之一。

公开(公告)号：US20190048959A1

公开(公告)日：2019-02-14

申请号：US16159633

申请日：2018-10-13

申请人： The Boeing Company

发明人： Michael T. Fox ,  Jeffrey M. Roach ,  Eric A. Howell

IPC分类号： F16F7/06 ,  F16F15/12 ,  F16F15/121 ,  F16F7/10 ,  B64C9/02

CPC分类号： F16F7/065 ,  B64C9/02 ,  F16F7/1022 ,  F16F15/1204 ,  F16F15/1208 ,  F16F15/1216

摘要： There is provided a translational inerter assembly for damping movement of a flight control surface of an aircraft with a support structure. The translational inerter assembly includes a press fit element rotatably disposed within the flight control surface. The translational inerter assembly further includes an inertia element disposed in the press fit element. The translational inerter assembly further includes a torsion bar coupled to the inertia element and to the support structure of the aircraft, such that when the flight control surface rotates, the inertia element translates, and movement of the flight control surface is dampened.

公开(公告)号：US20180135717A1

公开(公告)日：2018-05-17

申请号：US15867940

申请日：2018-01-11

申请人： The Boeing Company

发明人： Michael T. Fox ,  Jeffrey M. Roach ,  Eric A. Howell

IPC分类号： F16F7/06 ,  F16F15/12 ,  B64C9/02 ,  F16F15/121

CPC分类号： F16F7/065 ,  B64C9/02 ,  F16F7/1022 ,  F16F15/1204 ,  F16F15/1208 ,  F16F15/1216

摘要： There is provided a translational inerter assembly for damping movement of a flight control surface of an aircraft. The assembly has a press fit element fixedly disposed within a first end of the flight control surface and rotatably movable with the flight control surface. The assembly further has an inertia element coupled to and installed in the press fit element. The assembly further has a torsion bar having a torsion bar first end coupled to and installed in the inertia element, and having a torsion bar second end fixedly attached to a support structure of the aircraft. Rotation of the flight control surface causes translational movement of the inertia element, via the press fit element, along a hinge axis of the flight control surface and along the torsion bar, resulting in the translational inerter assembly damping movement of the flight control surface.

公开(公告)号：US11754129B2

公开(公告)日：2023-09-12

申请号：US17436403

申请日：2020-02-13

申请人： Schaeffler Technologies AG & Co. KG

发明人： Wolfgang Volk

IPC分类号： F16D41/20 ,  F16F15/12 ,  F16F15/121 ,  F16F7/06 ,  F16D13/12 ,  F16D13/08 ,  B23P19/04

CPC分类号： F16D41/206 ,  B23P19/048 ,  F16F15/1203 ,  F16D13/08 ,  F16D13/12 ,  F16D2250/0084 ,  F16D2300/12 ,  F16F7/065 ,  F16F15/1216 ,  F16F2226/04

摘要： A method for installing a wrap spring includes providing a first sleeve with a first longitudinal axis extending in an axial direction and a lateral surface, and the wrap spring designed to frictionally abut the lateral surface. The wrap spring includes a nominal diameter and a central axis. The method includes applying the wrap spring in a relaxed state to the lateral surface at an angle α between the central axis and the first longitudinal axis, elastically twisting the wrap spring to change the nominal diameter while the wrap spring contacts the lateral surface, reducing the angle α, threading the wrap spring onto the first sleeve, and relaxing the wrap spring to establish frictional contact with the lateral surface.

公开(公告)号：US06216972B1

公开(公告)日：2001-04-17

申请号：US09382919

申请日：1999-08-25

申请人： Martin Röhrle

发明人： Martin Röhrle

IPC分类号： B60R2228

CPC分类号： B60R22/3413 ,  B60R2022/286 ,  B60R2022/287 ,  B60R2022/289 ,  F16F1/16 ,  F16F7/065

摘要： A device for force limitation with an annular housing in which a guide path is formed, comprises a carrier arranged inside the housing concentrically therewith, which is rotatable relative to the housing, and a traction means which is secured on the carrier, extends along a part of its length in the guide path and can be withdrawn from the guide path by rotation of the carrier relative to the housing and can be wound onto the the carrier.

摘要翻译： 一种用于限制力的装置，其中形成有导向路径的环形壳体包括与壳体同心地布置在壳体内的载体，其可相对于壳体旋转，并且固定在载体上的牵引装置沿着部件 其长度在引导路径中并且可以通过载体相对于壳体的旋转而从引导路径中撤出，并且可以被卷绕到载体上。