Patent ID: 9745054
Date: 2017-08-29
CPC Classifications: B64C

Claim:
1. An aircraft landing gear assembly comprising: a main strut arranged to be movably coupled to an aircraft; an axle coupled to the main strut; a first brake assembly mounted on the axle; an adaptor member mounted on the axle, the adaptor member defining a brake rod connection point; a brake rod coupled to the adaptor member at the brake rod connection point and coupled to the landing gear assembly at an anchor point so as to inhibit rotation of the adaptor member about an axis of the axle; and an adaptor linkage coupled to the first brake assembly and to the adaptor member, the adaptor linkage being arranged to inhibit rotation of the first brake assembly about the axis of the axle relative to the adaptor member, and being arranged to permit movement between the first brake assembly and the adaptor member in one or more other degree of freedom.