Aircraft brake cooling fan control system

Patent metadata

Field	Value
Publication number	US-10197124-B2
Application number	US-201615173167-A
Country	US
Kind code	B2
Filing date	Jun 3, 2016
Priority date	Jun 4, 2015
Publication date	Feb 5, 2019
Grant date	Feb 5, 2019

Abstract

An aircraft includes a power source arranged to provide AC electrical power of varying frequency, and a brake cooling fan including an impeller which is driven by an electric motor powered by said AC electrical power for cooling brakes of the aircrafts wheels. The brake cooling fan has an operable mode when the frequency of said AC electrical power meets certain criteria indicating that the frequency of the AC power is suitable for powering the motor, and an inoperable mode to protect against unsuitable operation of the motor. The brake cooling fan may then be safely powered with AC power direct from a wild frequency power network on the aircraft without needing a power inverter or constant power supply generator.

First claim

The invention claimed is:

1. A method of cooling at least two aircraft wheel brakes on an aircraft, wherein the method includes:
powering a plurality of brake cooling fans with AC power from a wild frequency power network on the aircraft, whilst ensuring that the frequency of the AC power meets certain criteria, wherein each of the plurality of brake cooling fan is associated with a different aircraft wheel brake of the at least two aircraft wheel brakes on the aircraft, and
controlling one or more of the plurality of brake cooling fans independently of one or more of the other ones of the plurality of brake cooling fans.

2. The method according to claim 1 , wherein the method includes a step of detecting that the one or more of the brake cooling fans, or parts associated therewith, is faulty, and then disabling operation of the one or more of the brake cooling fans independently of other of the brake cooling fans.

3. The method according to claim 1 , wherein the method includes detecting a fault associated with one or more of the brake cooling fans, or associated with the current supplied to the one or more of the brake cooling fans, and then recording in an electronic log data descriptive of the detected fault.

4. The method according to claim 1 , wherein the step of powering the plurality of brake cooling fans with AC power is performed automatically, under the control of a control system and in response to a determination that the certain criteria is met.

5. The method according to claim 1 , further comprising receiving data via an electronic data communications network on the aircraft and using the data to assess whether or not to power the brake cooling fan with the AC power from the wild frequency power network.

6. The method according to claim 1 , wherein the method includes a step of a control system determining whether or not to power the brake cooling fan in dependence on data received over an AFDX network on the aircraft, such data including data concerning the frequency of the AC power.

7. The method according to claim 1 , wherein the step of ensuring that the frequency of the AC power meets the certain criteria includes assessing whether or not the frequency is less than a maximum amount.

8. The method according to claim 1 , wherein the step of ensuring that the frequency of the AC power meets the certain criteria includes assessing whether or not the frequency has been less than a threshold amount for a certain period of time.

9. The method according to claim 1 , wherein the step of powering the plurality of brake cooling fans with the AC power is performed in dependence on a measure of the temperature of one or more of the brakes to be cooled by the fans.

10. The method according to claim 1 , wherein the step of controlling one or more of the brake cooling fans includes controlling at least one of the brake cooling fans in dependence on a measure of the temperature of the brake or brakes to be cooled by the fan.

11. A method of cooling an aircraft wheel brake on an aircraft, wherein the method includes a control system automatically powering a brake cooling fan with the AC power from a wild frequency power network on the aircraft in dependence on a measure of brake temperature whilst ensuring that the frequency of the AC power meets certain criteria.

12. The method according to claim 11 , wherein the aircraft includes a plurality of brake cooling fans, and the method is performed such that each of the brake cooling fans of the plurality of fans is powered by the AC power from the wild frequency power network on the aircraft whilst ensuring that the frequency of the AC power meets a certain criteria.

13. The method according to claim 12 , wherein the method includes a step of controlling one or more of the brake cooling fans independently of one or more of the other ones of the brake cooling fans.

14. The method according to claim 13 , wherein the method includes a step of detecting that one or more of the brake cooling fans, or parts associated therewith, are faulty, and then disabling operation of the one or more of the brake cooling fans independently of other ones of the brake cooling fans.

15. The method according to claim 14 , wherein the method includes detecting a fault associated with one or more of the brake cooling fans, or associated with the current supplied to one or more of the brake cooling fans, and then recording in an electronic log data descriptive of the fault.

16. A method to cool aircraft wheel brakes on an aircraft, the method includes:
powering brake cooling fans with AC power from a wild frequency power network on the aircraft, wherein each of the powered brake cooling fan cools a different one of the aircraft wheel brakes;
monitoring the frequency of the AC power;
determining if the frequency meets a first criteria;
shutting off power to all of the brake cooling fans if the frequency does not meet the first criteria;
monitoring the brake cooling fans and determining whether each of the brake cooling fans meets a second criteria; and
independently controlling at least one of the brake cooling fans separately of the other ones of the brake cooling fans based on whether the at least one of the brake cooling fans meets the second criteria.

17. The method according to claim 16 , wherein the second criteria relates to a level of current flowing to each of the brake cooling fans.

18. The method according to claim 16 , wherein the second criteria relates to a temperature of each of the wheel brakes, and the step of independently controlling at least one of the brake cooling fans includes shutting off AC power to the at least one of the brake cooling fans for which the associated wheel brake has a temperature lower than a threshold temperature.

19. A control system to cool aircraft wheel brakes on an aircraft, wherein a plurality of the aircraft wheel brakes are cooled by a respective brake cooling fans which are powered by a wild frequency power network on the aircraft, wherein the control system is configured to:
power the brake cooling fans with AC power from the wild frequency power network on the aircraft, wherein each of the powered brake cooling fan cools a different one of the aircraft wheel brakes;
monitor the frequency of the AC power;
determine whether the frequency meets a first criteria;
shut off power to all of the brake cooling fans if the frequency does not meet the first criteria;
monitor the brake cooling fans and determine whether each of the brake cooling fans meets a second criteria; and
independently control at least one of the brake cooling fans separately of the other ones of the brake cooling fans based on whether the at least one of the brake cooling fans meets the second criteria.

20. The control system according to claim 19 , wherein the second criteria relates to a level of current flowing to each of the brake cooling fans.

21. The control system according to claim 19 , wherein the second criteria relates to a temperature of each of the wheel brakes, and the control system is configured to independently control at least one of the brake cooling fans by shutting off the AC power to the at least one of the brake cooling fans for which the associated wheel brake has a temperature lower than a threshold temperature.

Assignees

• Airbus Operations Ltd

Inventors

• Bill Andrew Raymond

Classifications

• H02H3/46

  responsive to frequency deviations · CPC title

• F16D2065/787

  Pumps · CPC title

• F16D65/847 Primary

  with open cooling system, e.g. cooled by air · CPC title

• F16D65/78 Primary

  Features relating to cooling · CPC title

• F04D27/008

  Stop safety or alarm devices, e.g. stop-and-go control; Disposition of check-valves · CPC title