Brake actuator for aircraft wheel hydraulic brake

Patent metadata

Field	Value
Publication number	US-9739325-B2
Application number	US-201514945660-A
Country	US
Kind code	B2
Filing date	Nov 19, 2015
Priority date	Dec 12, 2014
Publication date	Aug 22, 2017
Grant date	Aug 22, 2017

Abstract

The invention relates to a brake actuator for an aircraft hydraulic brake, which is intended to be added into one of the cavities 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, a wear compensation device ( 10 ) which defines a position to which the piston retreats into the liner by means of a mobile stop ( 11 ) 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. According to the invention, the mobile stop is reduced to a friction member rubbing against the liner, such that one of the faces of the friction member serves as a stop defining the retracted position of the piston, and the other of the faces serves as a support for the elastic return member, the elastic member having, when compressed, a sufficient increase in force in order to be able 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.

First claim

The invention claimed is:

1. A brake actuator for an aircraft hydraulic brake, which is intended to be added into one of the cavities 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;
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 serves as a support for the elastic return member, the elastic 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.

2. The brake actuator according to claim 1 , in which the piston has a proximal end ( 4 ) that is closed and fluid tight.

3. 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.

4. The brake actuator according to claim 3 , in which the piston has a proximal end ( 4 ) that is closed and fluid tight.

Assignees

• Messier Bugatti Dowty

Inventors

• Robin Jean-Baptiste
• Lucienne Robin

Classifications

• F16D65/54

  by means of direct linear adjustment · CPC title

• B64C25/42

  Arrangement or adaptation of brakes · CPC title

• F16D2129/02

  Fluid-pressure · CPC title

• F16D2125/04

  Cylinders · CPC title

• F16D65/186

  with full-face force-applying member, e.g. annular · CPC title