Systems and methods for whirl mitigation in an aircraft braking system are provided. For example, an apparatus is provided comprising a brake disk stack including a torque tube having a first axial end and a second axial end, a back leg near a first axial end of the torque tube, and a circumferentially disposed spline extending from the back leg towards the second axial end of the torque tube.


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    Title :

    Systems and methods for brake whirl mitigation


    Contributors:
    TODD ROOK (author) / RAVINDRA UPPAR (author)

    Publication date :

    2018-06-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B60T Bremsanlagen für Fahrzeuge oder Teile davon , VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF / F16D COUPLINGS FOR TRANSMITTING ROTATION , Nicht schaltbare Kupplungen



    Nonlinear Transient Whirl Vibration Analysis of Aircraft Brake Systems

    Chang, C. F. / Confederation of European Aerospace Societies / AIAA et al. | British Library Conference Proceedings | 1999


    Local blade whirl and global rotor whirl interaction

    Petersen, Jørgen Thirstrup / Thomsen, Kenneth / Madsen, Helge Aagaard | TIBKAT | 1998



    Pitcairn whirl wing

    Larsen, A.E. | Engineering Index Backfile | 1940


    SYSTEMS AND METHODS FOR BRAKE PULL MITIGATION

    BADIRU IBRAHIM A | European Patent Office | 2019

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