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 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|