IP Library › Granted Patent US 11,407,259
Granted Patent B2
US 11,407,259 · App. 17/110,387 · Granted Aug 9, 2022

Method of monitoring the pressure of an aircraft tire

Inventor: Andrew Bill (Bristol, GB)
Assignee: AIRBUS OPERATIONS LIMITED
B60C23/0476B60C23/0408B60C23/0474B60C23/0486G01K11/00G01L17/00G01M17/02B60C2200/02
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Quick Facts
Patent No.
US 11,407,259
App. No.
17/110,387
Granted
Aug 9, 2022
Kind
B2
Abstract

A method of monitoring the pressure of a tire of an aircraft, the method including: taking two or more pressure readings from the tire at different times; calculating an estimated deflation rate based on the pressure readings; and calculating a time for the tire to deflate to a reference pressure level based on the estimated deflation rate. Two or more temperature readings are each associated with one of the pressure readings, and the estimated deflation rate is calculated by normalising each pressure reading based on its associated temperature reading and a common reference temperature to obtain a temperature-normalised pressure reading, and calculating the estimated deflation rate based on the temperature-normalised pressure readings. The estimated deflation rate is compared with a threshold, and a warning provided if the estimated deflation rate exceeds the threshold.

Claims (39)

1. An aircraft tire pressure monitoring system for monitoring the pressure of a tire of an aircraft, the apparatus comprising:

a sensor system comprising a pressure sensor for taking pressure readings from the tire at different times and a temperature sensor for taking temperature readings; and

a computer system configured to:

determine an estimated destination pressure based on a pressure reading from the pressure sensor, a temperature reading from the temperature sensor and a destination temperature; and,

provide a warning based on the estimated destination pressure.

2. The aircraft tire pressure monitoring system of claim 1 , wherein the computer system is configured to obtain the destination temperature from a weather forecast for the destination.

3. The aircraft tire pressure monitoring system of claim 1 , wherein the computer system is configured to compare the estimated destination pressure with a threshold, and provide a warning if the estimated destination pressure is less than the threshold.

4. The aircraft tire pressure monitoring system of claim 1 , further comprising a hand-held device, and wherein the hand-held device comprises the computer-system.

5. The aircraft tire pressure monitoring system of claim 4 , wherein the hand-held device is configured to receive the pressure readings and the temperature readings via a wireless connection.

6. The aircraft tire pressure monitoring system of claim 1 , further comprising a plurality of sensor systems such that each wheel of the aircraft has an associated sensor system.

7. The aircraft tire pressure monitoring system of claim 1 , wherein the computer system is configured to:

normalise each of two or more pressure readings from the pressure sensor based on an associated temperature reading from the temperature sensor and a reference temperature to obtain temperature-normalised pressure readings; and,

calculate an estimated deflation rate based on the temperature-normalised pressure readings.

8. The aircraft tire pressure monitoring system of claim 7 , wherein the computing system is configured to provide a warning based on the estimated deflation rate.

9. The aircraft tire pressure monitoring system of claim 7 , wherein the computer system is configured to estimate a time for the tire to deflate to a reference pressure level based on the estimated deflation rate.

10. The aircraft tire pressure monitoring system of claim 7 , wherein the computer system is configured to compare the estimated deflation rate with a threshold, and provide a warning if the estimated deflation rate exceeds the threshold.

11. A method of monitoring the pressure of a tire of an aircraft, the apparatus comprising:

obtaining a pressure reading and an associated temperature reading from the tire;

determining an estimated destination pressure based on a pressure reading from a pressure sensor, a temperature reading from a temperature sensor and a destination temperature; and,

providing a warning based on the estimated destination pressure.

12. The method of claim 11 , further comprising obtaining the destination temperature from a weather forecast for the destination.

13. The method of claim 12 , further comprising:

determining that the estimated pressure at the destination is less than a threshold; and,

providing a warning based on the determination that the estimated pressure at the destination is less than the threshold.

14. The method of claim 11 , further comprising receiving the pressure reading and the associated temperature reading via a wireless connection.

15. The method of claim 11 , further comprising obtaining a pressure reading and an associated temperature reading for each wheel of the aircraft.

16. The method of claim 11 , further comprising:

normalising each of two or more pressure readings based on an associated temperature reading and a reference temperature to obtain temperature-normalised pressure readings; and

calculating an estimated deflation rate based on the temperature-normalised pressure readings.

17. The method of claim 16 , further comprising providing a warning based on the estimated deflation rate.

18. The method of claim 16 , further comprising estimating a time for the tire to deflate to a reference pressure level based on the estimated deflation rate.

19. The method of claim 16 , further comprising:

determining that the estimated deflation rate exceeds a threshold; and,

providing a warning based on the determining that estimated deflation rate exceeds the threshold.

20. An aircraft tire pressure monitoring system for monitoring the pressure of a tire of an aircraft, comprising:

a sensor system comprising a pressure sensor for taking pressure readings from the tire and a temperature sensor for taking temperature readings; and

a hand-held device comprising a computer system configured to:

determine an estimated destination pressure based on a pressure reading from the pressure sensor, a temperature reading from the temperature sensor and a destination temperature; and,

compare the estimated destination pressure with a threshold, and provide a warning if the estimated pressure at the destination is less than the threshold.

Priority Claims (1)
GB 1504777 · Mar 20, 2015 · national
Continuity (3)
Continuation 16826427 · Mar 23, 2020
Continuation 15075532 · Mar 21, 2016
Related Publication 20210107323A1 · Apr 15, 2021
Cited By (1)
US 12,447,779