Invention Grant
- Patent Title: Brake actuator for an aircraft wheel hydraulic brake
- Patent Title (中): 用于飞机车轮液压制动器的制动执行器
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Application No.: US14645792Application Date: 2015-03-12
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Publication No.: US09476473B2Publication Date: 2016-10-25
- Inventor: Vincent Gonzalez , Jacques Bussiere
- Applicant: MESSIER-BUGATTI-DOWTY
- Applicant Address: FR Velizy Villacoublay
- Assignee: MESSIER-BUGATTI-DOWTY
- Current Assignee: MESSIER-BUGATTI-DOWTY
- Current Assignee Address: FR Velizy Villacoublay
- Agency: Sughrue Mion, PLLC
- Priority: FR1452887 20140401
- Main IPC: F16D65/38
- IPC: F16D65/38 ; F16D65/58 ; F16D55/24 ; B64C25/44 ; B64C25/42 ; F16D65/54 ; F16D55/40 ; F16D65/18 ; F16D121/04

Abstract:
A brake actuator comprising a sleeve (1), a piston (3) sealingly slidably mounted in the sleeve to apply a braking force, the piston being provided with an internal cage (21), and a wear compensating device (10) which defines a retracted position of the piston in the sleeve by means of an axially mobile stop which is able to be moved forward by the piston during the application of a braking force and/in frictional relationship with a fixed part (12) of the wear compensating device attached to the sleeve. The mobile stop comprises a radially deformable bushing (16) which cooperates with an olive (15) which is attached to a distal end of the fixed part of the wear compensating device. The bushing comprises means for guiding its proximal end (17) against an internal face of the internal cage (21).
Public/Granted literature
- US20150275992A1 BRAKE ACTUATOR FOR AN AIRCRAFT WHEEL HYDRAULIC BRAKE Public/Granted day:2015-10-01
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