Aircraft brake assembly retention mechanism

专利名称：Aircraft brake assembly retention

mechanism

发明人：BRIAN GENE HARKER申请号：AU7250894申请日：19940623公开号：AU676073B2公开日：19970227

摘要：The aircraft brake retention mechanism (40) comprises a retractable mechanism(41) having an enlarged circular head (42) , and a threaded shaft (43) received threadedlyin an end part (50) biased by a resilient mechanism (60). The head (42), shaft (43), end part(50) and resilient mechanism (60) are received within a radial opening (33) of a pistonhousing (30), with the end part (50) extending through the radial opening (33) and intoabutting engagement with a flange (13A) of the axle (13) . The piston housing (30) isconnected fixedly with a torque tube (20) so that the piston housing (30)/torque tube (20)and associated brake discs (34, 36) are retained axially by the axle flange (13A) which iscaptured axially between the end part (50) and torque tube (20) . The retractablemechanism (41) may be retracted manually and rotated to engage a surface (37A) of thepiston housing (30) and be retained in the; retracted position, so that the brake assembly(10) may be disengaged from the axle (13).

申请人：ALLIEDSIGNAL INC.

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