发明名称 |
Aircraft landing gear assembly |
摘要 |
<p>An aircraft landing gear assembly comprising an impact protection boot (17) mounted to a landing gear component, the impact protection boot comprising: a resilient inner impact energy absorption layer (20) which engages the component (10); and an outer protective layer (22) which substantially covers the impact energy absorption layer, wherein the inner layer is more compressible than the outer layer. The boot has first and second ends which are tied to each other by a connector which exerts oppositely directed forces on the first and second ends respectively, the forces being directed around the circumference of the boot so as to tighten the boot against the landing gear component.</p> |
申请公布号 |
EP2366622(A2) |
申请公布日期 |
2011.09.21 |
申请号 |
EP20110156316 |
申请日期 |
2011.02.28 |
申请人 |
AIRBUS OPERATIONS LIMITED |
发明人 |
CLARK, LESLIE JOHN;WEST, COLIN JOHN;SUTTON, DAVID ALISTAIR |
分类号 |
B64C25/32;B64C25/60 |
主分类号 |
B64C25/32 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|