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.
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机译：本发明涉及一种用于减小在制动过程中产生的飞机车轮/制动器组件的振动的方法，该制动器包括通过该车轮由车轮旋转驱动的转子盘（ 2 b ）。固定在车轮上并啮合在转子盘和定子盘（）的槽口（ 3 b ）中的杆（ 5 ）的数量2 a ）通过固定在齿轮箱扭矩管（ 1 ）上的榫（ 5 ）保持旋转不动。制动并啮合到定子圆盘的槽口（ 3 a ）中，槽口的侧面由支架（ 7 ）保护。该方法包括选择摩擦系数小于或等于0.6的托架/榫on对和/或托架/钢筋对。
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