| 发明名称 |
AIRCRAFT LANDING GEAR ASSEMBLY INCLUDING A HEALTH AND USAGE MONITORING SYSTEM (HUMS) AND METHOD |
| 摘要 |
A health and monitoring system or “HUMS” mounted within a hollow structural subassembly of an aircraft landing gear assembly, the subassembly having an access port for access to the HUMS without requiring disassembly of the structural subassembly so as to require jacking up the aircraft. |
| 申请公布号 |
US2017113811(A1) |
申请公布日期 |
2017.04.27 |
| 申请号 |
US201615297723 |
申请日期 |
2016.10.19 |
| 申请人 |
Safran Landing Systems UK Limited |
发明人 |
Cokonaj Valerijan |
| 分类号 |
B64D45/00;B64C25/60;B64C25/10 |
主分类号 |
B64D45/00 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An aircraft landing gear assembly for supporting an aircraft, the landing gear assembly comprising:
a first structural subassembly which defines a cavity and an access port for providing access to the cavity from the exterior of the first subassembly while, in use, the landing gear assembly is supporting the aircraft on the ground; and one or more health and monitoring system (HUMS) components removably coupled to the first structural subassembly within the cavity. |
| 地址 |
Gloucester GB |
