发明名称 |
METHODS TO MONITOR COMPONENTS OF AN AIRCRAFT LANDING SYSTEM |
摘要 |
Methods to monitor components of an aircraft landing system are disclosed herein. An example method includes determining a brake assembly temperature and determining a wheel temperature. The example method also includes retrieving an estimated increase in the wheel temperature from a data structure based on the wheel temperature and the brake assembly temperature. The example method further includes determining a maximum wheel temperature based on the wheel temperature and the estimated increase in the wheel temperature. |
申请公布号 |
US2015145703(A1) |
申请公布日期 |
2015.05.28 |
申请号 |
US201314088087 |
申请日期 |
2013.11.22 |
申请人 |
The Boeing Company |
发明人 |
Martin Casandra Jolene |
分类号 |
B64D45/00 |
主分类号 |
B64D45/00 |
代理机构 |
|
代理人 |
|
主权项 |
1. A method comprising:
determining a first temperature of a wheel of an aircraft; determining a second temperature of a brake assembly operatively coupled to the wheel; associating the first temperature with one of a plurality of predetermined ranges of wheel temperatures; associating the second temperature with one of a plurality of predetermined ranges of brake assembly temperatures; determining an estimated increase in the first temperature associated with the one of the ranges of wheel temperatures and the one of the ranges of brake assembly temperatures; and determining a maximum temperature of the wheel based on the first temperature and the estimated increase in the first temperature. |
地址 |
Chicago IL US |