AIRCRAFT TURBINE ENGINE DRIVE LINE SHAFT COMPRISING A CONNECTING RING FOR DISASSEMBLING THE DRIVE LINE

    公开(公告)号:US20240003258A1

    公开(公告)日:2024-01-04

    申请号:US18252119

    申请日:2021-11-08

    IPC分类号: F01D5/02 F02C7/36

    CPC分类号: F01D5/026 F02C7/36 F16C3/023

    摘要: Disclosed is a main shaft for an aircraft turbine engine drive line extending longitudinally from front to rear along an axis and having a rear portion configured for receiving a front portion of a rear shaft by interlocking, the main shaft having: —a front retaining member and a rear retaining member together defining a prison and each having a central opening, —a connecting ring, located in the prison, having a rear end configured to be screwed to a front end of the rear shaft extending into the central opening of the rear retaining member, the connecting ring having a gripping member formed on the inner surface and accessible from a front portion of the main shaft by a tool extending via the central opening of the front retaining member.

    Vehicle drive train assembly
    3.
    发明授权

    公开(公告)号:US11840141B2

    公开(公告)日:2023-12-12

    申请号:US17306607

    申请日:2021-05-03

    IPC分类号: B60K17/24 F16C3/02

    CPC分类号: B60K17/24 F16C3/023

    摘要: A vehicle drive train assembly includes a propeller shaft and a nut. The nut has a first part and a second part. The first part is movable with respect to the propeller between an uninstalled position and an installed position of the nut. The second part is stationary with respect to the propeller shaft in the uninstalled position and the installed position.

    POWER TRANSMISSION SHAFT
    5.
    发明公开

    公开(公告)号:US20230332638A1

    公开(公告)日:2023-10-19

    申请号:US17788051

    申请日:2020-12-23

    摘要: A propeller shaft (PS) has a balance piece (9) on the outer peripheral side of a stub shaft body section (31) of a stub shaft (3), which is axially separated from both spline sections (25, 34), which are spline fitting sections. Due to this configuration, changes in the gap in both spline sections (25, 34) when the balance piece (9) is welded are minimized, and the occurrence of new rotational imbalance can be minimized. As a result, rotational imbalance in the propeller shaft (PS) due to the balance piece (9) can be corrected appropriately and easily.

    Torque transmitting shaft
    6.
    发明授权

    公开(公告)号:US11767875B2

    公开(公告)日:2023-09-26

    申请号:US17163434

    申请日:2021-01-30

    IPC分类号: F16C3/02 F16F15/121

    摘要: A torque transmitting shaft includes a first member and a second member. The first member extends along an axis and has an inner surface extending between a first end and a second end. The inner surface defines a plurality of first engagement elements disposed proximate the first end. The second member extends along the second axis and has a first end portion and an intermediate portion extending from the first end portion. An end of the intermediate portion is fixedly attached to the second end. The first end portion has a first spline portion and each member of the first spline portion is received within corresponding engagement elements of the plurality of first engagement elements.

    TORQUE TRANSMITTING SHAFT
    8.
    发明申请

    公开(公告)号:US20180202486A1

    公开(公告)日:2018-07-19

    申请号:US15923993

    申请日:2018-03-16

    IPC分类号: F16C3/02

    CPC分类号: F16C3/023

    摘要: A torque transmitting shaft includes a first member and a second member. The first member extends along an axis and has an inner surface extending between a first end and a second end. The inner surface defines a plurality of first engagement elements disposed proximate the first end. The second member extends along the second axis and has a first end portion and an intermediate portion extending from the first end portion. An end of the intermediate portion is fixedly attached to the second end. The first end portion has a first spline portion and each member of the first spline portion is received within corresponding engagement elements of the plurality of first engagement elements.