After a cup bearing (13a) is incorporated into a circular hole (11c) of a coupling arm portion (10c) forming a yoke, a notch (25) having a V-shaped cross section is formed in a portion near the periphery of the circular hole (11c) on an outer side surface of the coupling arm portion (10c). Thereafter, a thin-walled portion (27) having a substantially trapezoidal cross section formed in a radially inner portion of the notch (25) in an opening edge portion of the circular hole (11c) is plastically deformed inward in a radial direction to form a staking portion (14a). Therefore, it is possible to achieve a method of assembling a joint cross type universal joint and a joint cross type universal joint which can form the staking portion for preventing the cup bearing from falling off without complicating the staking work.


    Access

    Download


    Export, share and cite



    Title :

    Method for assembling cruciform universal joint, and cruciform universal joint


    Contributors:

    Publication date :

    2021-06-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F16D COUPLINGS FOR TRANSMITTING ROTATION , Nicht schaltbare Kupplungen / B62D MOTOR VEHICLES , Motorfahrzeuge



    METHOD FOR ASSEMBLING CRUCIFORM UNIVERSAL JOINT, AND CRUCIFORM UNIVERSAL JOINT

    TAGUCHI YUICHIRO | European Patent Office | 2019

    Free access

    Roll Damping of Cruciform-Tailed Missiles

    Donald W. Eastman | AIAA | 1986


    Mathematical modeling of cruciform parachute deployment

    Androsenkov, V. A. / Zaichuk, R. M. / Ponomarev, A. T. | Online Contents | 2007


    Fatigue Strength Assessment of Cruciform Joints

    Fricke, W. / Wernicke, R. | British Library Conference Proceedings | 2001


    Roll damping of cruciform-tailed missiles

    EASTMAN, D. W. | AIAA | 1986