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
09.12.2016
Patent
Elektronische Ressource
Französisch
Europäisches Patentamt | 2019
|Europäisches Patentamt | 2015
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