| 发明名称 |
METHODS AND APPARATUS TO MONITOR COMPONENTS OF AN AIRCRAFT LANDING SYSTEM |
| 摘要 |
Methods and Apparatus to monitor components of an aircraft landing system are disclosed herein. An example method includes determining a first temperature of a wheel of an aircraft via a first temperature sensor, and determining a second temperature of a brake assembly operatively coupled to the wheel via a second temperature sensor. The example method further includes estimating a peak temperature of a fuse plug disposed on the wheel based on the first temperature and the second temperature. |
| 申请公布号 |
US2014269824(A1) |
申请公布日期 |
2014.09.18 |
| 申请号 |
US201313830109 |
申请日期 |
2013.03.14 |
| 申请人 |
The Boeing Company |
发明人 |
Miller Trent Daryl |
| 分类号 |
G01K3/04 |
主分类号 |
G01K3/04 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A method, comprising:
determining a first temperature of a wheel of an aircraft via a first temperature sensor; determining a second temperature of a brake assembly operatively coupled to the wheel via a second temperature sensor; and estimating a peak temperature of a fuse plug disposed on the wheel based on the first temperature and the second temperature. |
| 地址 |
US |
