The invention relates to a method for attenuating vibrations of an aircraft wheel/brake assembly arising during braking, the brake comprising rotor discs (2b) rotationally driven with the wheel by means of bars (5) secured to the wheel and engaging in notches (3b) of the rotor discs, and stator discs (2a) which are kept rotationally immobile by means of tenons (5) secured to a torque tube (1) of the brake and engaged in notches (3a) of the stator discs, the notches having flanks that are protected by brackets (7). The method involves selecting bracket/tenon pair and/or bracket/bar pairs with a coefficient of friction less than or equal to 0.6.
PROCÉDÉ D'ATTÉNUATION DES VIBRATIONS DES ROUES FREINÉES D'AÉRONEF
METHOD OF ATTENUATING VIBRATIONS OF BRAKED AIRCRAFT WHEELS
VERFAHREN ZUR VIBRATIONSDÄMPFUNG GEBREMSTER LUFTFAHRZEUGRÄDER
28.09.2022
Patent
Elektronische Ressource
Französisch
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