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.
SYSTEMES ET PROCEDES D'ATTENUATION DE TOURBILLON DE FREIN
2016-12-09
Patent
Electronic Resource
French
European Patent Office | 2019
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