Brake actuator for aircraft wheel hydraulic brake

A brake actuator for an aircraft hydraulic brake, which is intended to be added into a cavity of a brake ring, the actuator comprising:

• a liner (1) designed to be housed sealingly in the cavity of the ring;
• a piston (3) mounted to slide sealingly in the liner along an axis of sliding (X) so as to apply a braking force on friction pads when a fluid is introduced under pressure into the cavity, and having a determined operational travel between a retracted position and a position where the operational travel is exhausted;
• and
• a wear compensation device (10) which defines a position to which the piston retreats into the liner by means of a mobile stop (13) that can be moved forward by the piston as a braking force is applied;
• and
• an elastic return member (16) returning the piston towards the retracted position bearing against the mobile stop;
• wherein the mobile stop is constituted by a friction member (13) rubbing against the liner, such that one face of the friction member serves as a stop defining the retracted position of the piston, and another face of the friction member serves as a support for the elastic return member, the elastic return member being operative, when compressed by the piston, to push back the mobile stop in the event that the piston is not in contact with the friction pads while its operational travel is already exhausted, and in which the elastic return member is a helical spring (16) whose coils meet during application of the braking force if an operational travel of the piston is exhausted before the piston touches the friction pads.