An electro-mechanical actuator in an aircraft brake may include a ball nut piston, and endcap coupled to the ball nut piston, a retaining ring coupled to the endcap, and a puck secured within the endcap. The puck may be permanently retained within the retaining ring. The retaining ring may be a split ring which is installed around a base of the puck. The puck may be inserted within a single-piece retaining ring, and the retaining ring may be bent over a base of the puck.
AIRCRAFT BRAKE PUCK ASSEMBLY
2016-05-05
Patent
Electronic Resource
English
PUCK ATTACHMENT MECHANISM FOR FLEXIBLE AIRCRAFT CONFIGURATION
European Patent Office | 2020
|Puck attachment mechanism for flexible aircraft configuration
European Patent Office | 2021
|