发明名称 AIRCRAFT LANDING GEAR ASSEMBLY
摘要 An aircraft landing gear assembly (10) includes a main strut and an axle (18b) on which wheel and brake assemblies (20b, 22b) are mounted. An adaptor member (30) is mounted on a mounting pin and arranged to define a brake rod anchor point (28). The adaptor member is coupled to a part of the landing gear assembly so as to react brake torque and can be formed from a different material than a portion of the main strut.
申请公布号 CA2909027(A1) 申请公布日期 2016.04.16
申请号 CA20152909027 申请日期 2015.10.13
申请人 MESSIER-DOWTY LIMITED 发明人 SEXTON, MATTHEW;SCHMIDT, ROBERT KYLE
分类号 B64C25/34;B64C25/42;B64C25/58 主分类号 B64C25/34
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