Method of controlling a braking device electro - hydraulic of a set of wheels of the aircraft, and device for practicing said process óoeuvre.

摘要

The invention relates to the control of a braking device electro - hydraulic of a set of wheels of the aircraft, each wheel is equipped with a brake is actuated from the brake pedals by a servo - valve controlled electrically by a control unit which measurement data corresponding to the penetration of the said pedals. & br / according to the invention, when the aircraft is running at low speed, is fabricated separately the braking for the wheels (ri) of a first group and for the wheels (r) of a second group, with a law of variation of the control pressure as a function of the brake pedal depression, which is specific to each group of wheels. One of the two curves (l1) is a continuously increasing function involved over the entire active range of brake pedal depression (11), while the other braking relationship (l2) is a continuously increasing function that are involved only from a predetermined depression threshold of the said pedals.