Methods to monitor components of an aircraft landing system

Patent metadata

Field	Value
Publication number	US-9242739-B2
Application number	US-201314088087-A
Country	US
Kind code	B2
Filing date	Nov 22, 2013
Priority date	Nov 22, 2013
Publication date	Jan 26, 2016
Grant date	Jan 26, 2016

Abstract

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.

First claim

What is claimed is:

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.

2. The method of claim 1 further comprising determining if the maximum temperature is greater than a predetermined threshold temperature.

3. The method of claim 2 further comprising generating an alert if the maximum temperature is greater than the predetermined threshold temperature.

4. The method of claim 2 , wherein the predetermined threshold temperature is less than a temperature at which a fuse plug of the wheel is to melt.

5. The method of claim 1 , wherein determining the estimated increase in the first temperature comprises retrieving the estimated increase in the first temperature from a table.

6. The method of claim 1 , wherein the estimated increase in the first temperature is based on experimentally determined heating patterns of one or more aircraft wheels.

7. A method, comprising:
determining a brake assembly temperature;
determining a wheel temperature;
retrieving an estimated increase in the wheel temperature from a data structure based on the wheel temperature and the brake assembly temperature; and
determining a maximum wheel temperature based on the wheel temperature and the estimated increase in the wheel temperature.

8. The method of claim 7 , wherein retrieving the estimated increase in the wheel temperature comprises:
determining which one of a plurality of wheel temperature ranges and which one of a plurality of brake assembly temperature ranges in the data structure include the wheel temperature and the brake assembly temperature, respectively; and
retrieving the estimated increase in the wheel temperature associated with the one of the wheel temperature ranges and the one of the brake assembly temperature ranges.

9. The method of claim 7 further comprising:
determining if the maximum wheel temperature is greater than a first predetermined threshold temperature; and
generating an alert if the maximum wheel temperature is greater the first predetermined threshold temperature.

10. The method of claim 9 further comprising:
monitoring the wheel temperature;
monitoring the brake assembly temperature; and
removing the alert if the wheel temperature decreases below a second predetermined threshold temperature and the brake assembly temperature is below a third predetermined threshold temperature.

11. The method of claim 7 further comprising:
monitoring the wheel temperature;
determining if the wheel temperature peaks;
if the wheel temperature peaks, comparing only the wheel temperature to a first predetermined threshold temperature; and
communicating an alert if the wheel temperature is greater than the first predetermined threshold temperature.

12. The method of claim 7 , wherein determining the brake assembly temperature comprises determining the brake assembly temperature via a first temperature sensor disposed on a brake assembly operatively coupled to a wheel, and wherein determining the wheel temperature comprises determining the wheel temperature via a second temperature sensor disposed on the wheel.

13. A method, comprising:
determining a brake assembly temperature;
determining a wheel temperature; and
determining if a fuse plug disposed on a wheel is at risk of melting based on the brake assembly temperature, the wheel temperature, and estimated heating patterns of the wheel.

14. The method of claim 13 wherein determining if the fuse plug is at risk of melting comprises:
determining an estimated maximum temperature of the wheel based on the brake assembly temperature, the wheel temperature, and the estimated heating patterns; and
determining if the estimated maximum temperature of the wheel is greater than a predetermined threshold temperature.

15. The method of claim 14 , wherein determining the estimated maximum temperature of the wheel comprises retrieving an estimated increase in the wheel temperature from a data structure, wherein the estimated increase in the wheel temperature is determined based on one of the estimated heating patterns.

16. The method of claim 13 , wherein determining if the fuse plug is at risk of melting comprises:
comparing the brake assembly temperature to a predetermined brake assembly temperature; and
comparing the wheel temperature to a predetermined threshold temperature if the brake assembly temperature is less than the predetermined brake assembly temperature.

17. The method of claim 13 , wherein determining if the fuse plug is at risk of melting comprises:
determining if the wheel temperature is a peak wheel temperature; and
comparing the wheel temperature to a predetermined threshold temperature if the wheel temperature is the peak wheel temperature; and
determining that the fuse plug is at risk of melting if the wheel temperature is greater than the predetermined threshold temperature.

18. The method of claim 13 further comprising generating an alert if the fuse plug is at risk of melting.

19. The method of claim 18 further comprising removing the alert if the wheel temperature is decreasing, the wheel temperature is below a first predetermined temperature, and the brake assembly temperature is below a second predetermined temperature.

20. The method of claim 13 , wherein determining the brake assembly temperature comprises determining the brake assembly temperature via a first temperature sensor disposed on a brake assembly operatively coupled to the wheel, and wherein determining the wheel temperature comprises determining the wheel temperature via a second temperature sensor disposed on the wheel.

Assignees

• Boeing Co

Inventors

• Martin Casandra Jolene

Classifications

• B64D45/00 Primary

  Aircraft indicators or protectors not otherwise provided for · CPC title

• F16D2066/001

  Temperature · CPC title

• F16D66/00

  Arrangements for monitoring working conditions, e.g. wear, temperature · CPC title

• B60T8/1703

  for aircrafts · CPC title

• B60T17/221

  Procedure or apparatus for checking or keeping in a correct functioning condition of brake systems (hydraulic pressure systems in general F15B19/00, F15B21/04; testing structures or apparatus G01M) · CPC title