Brake condition monitoring

• US 7,506,941 B2
• Filed: 05/16/2006
• Issued: 03/24/2009
• Est. Priority Date: 08/04/2000
• Status: Expired due to Term

• Current Assignee: Meggitt Aerospace Ltd. (Meggitt PLC)
• Original Assignee: Meggitt Aerospace Ltd. (Meggitt PLC)
• Inventors: Miller, Richard John, Bailey, David Alexander, Marshall, Ross John, Griffin, Nicholas Charles
• Primary Examiner(s): RODRIGUEZ, PAMELA
• Application Number:
  US11/383,568
• Publication Number:
  US 20060191751A1
• Time in Patent Office: 1,043 Days
• Field of Search: 188/1.11 W, 188/1.11 L, 188/1.11 E, 188/1.11 R, 188/79.51, 188/79.52, 340/449, 340/453, 340/454, 374/7, 374/110, 374/111, 374/135, 374/163, 374/179, 377/15, 377/25, 701/29, 701/30, 303/122, 303/122.03, 303/122.02, 303/122.08, 303/DIG.3, 244/110.A, 244/111
• US Class Current: 303/191
• CPC Class Codes: B60T 17/22 Devices for monitoring or checking brake systems; Signal devices
• CPC Class Codes: B60T 17/221 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 Class Codes: B64C 25/42 Arrangement or adaptation of brakes
• CPC Class Codes: B64F 5/60 Testing or inspecting aircraft components or systems
• CPC Class Codes: F16D 2066/001 Temperature
• CPC Class Codes: F16D 2066/003 Position, angle or speed
• CPC Class Codes: F16D 2066/005 Force, torque, stress or strain
• CPC Class Codes: F16D 2066/006 without direct measurement of the quantity monitored, e.g. wear or temperature calculated form force and duration of braking
• CPC Class Codes: F16D 66/02 Apparatus for indicating wear
• CPC Class Codes: G06Q 40/12 Accounting

Abstract

A system and method for monitoring the usage of brake members of an aircraft braking system. The system makes a separate record of each brake actuation in which there is relative movement of the brake member'"'"'s facing friction surfaces which causes wear, determines the types of brake usage and operates a pricing/payment scheme to charge for brake usage.

Claims

1. An aircraft braking system maintenance program operating system for a hydraulic aircraft braking system comprising brake members having facing friction surfaces adapted to contact each other during brake actuations, the operating system comprising:

a brake control system operable to detect brake inputs and brake outputs during brake actuations while an aircraft is in motion with relative rotational movement taking place between contacting frictional surfaces of the brake members;

a processing system operable to compare said brake outputs with expected brake outputs for respective brake inputs and selectively provide maintenance action signals based on the comparison of said brake outputs with said expected brake outputs.

2. An aircraft braking system maintenance program operating system as claimed in claim 1, wherein said processing system comprises an onboard computing unit.

3. An aircraft braking system maintenance program operating system as claimed in claim 1, wherein said processing system comprises an onboard facility and a ground based facility for receiving signals from said onboard facility which ground based facility is operable to generate said maintenance action signals.

4. An aircraft braking system maintenance program operating system as claimed in claim 1, wherein said processing system is operable to generate maintenance action signals that allow for a predetermined lead-time for supply of components for the aircraft braking system.

5. An aircraft braking system maintenance program operating system as claimed in claim 1, wherein said processing system comprises software for incorporating the processing system into brake control hardware of an aircraft.

6. An aircraft braking system maintenance program operating system as claimed in claim 1, operable to generate said expected brake outputs based on the brake outputs detected by the brake control system.

7. An aircraft braking system maintenance program operating system as claimed in claim 1, comprising at least one detector for detecting said brake outputs and providing signals indicative of said brake outputs, said brake outputs being at least one of a set comprising brake torque, brake temperature, vibration, acoustic signature, wheel deceleration and brake odor.

8. An aircraft comprising an aircraft braking system maintenance program operating system according to claim 1.

9. A method of operating an aircraft braking system maintenance program operating system, said method comprising:

monitoring signals representative of at least one parameter affected by brake inputs and outputs during brake actuations of a hydraulic aircraft braking system while an aircraft is in motion with relative rotational movement taking place between contacting frictional surfaces of the aircraft braking system;

identifying changes in said signals that are indicative of at least one of a predetermined braking system wear condition and a predetermined braking system fault condition; and

instigating a maintenance action in response to the identification of at least one of a said predetermined braking system wear condition or said predetermined braking system fault condition.

10. A method as claimed in claim 9,comprising identifying said changes by comparing said signals representative of at least one parameter with expected values for the at least one parameter.

11. A method as claimed in claim 10,comprising determining said expected values by reference to historical values obtained from previous said signals representative of the at least one parameter.

12. A method as claimed in claim 9,wherein instigating a maintenance action comprises sending a maintenance action signal from an onboard location to a ground location.

13. A method as claimed in claim 9, wherein instigating a maintenance action comprises making an order for manufacture of at least one braking system component.

14. A method as claimed in claim 13, comprising making said order at a time ahead of a predicted required replacement date for said at least one braking system component according to a predetermined lead time for the manufacture thereof.

15. A method as claimed in claim 9, wherein instigating a maintenance action comprises making a request for supply of at least one braking system component.

16. A method as claimed in claim 15, comprising making said request at a time ahead of a predicted required replacement date for said at least one braking system component according to a predetermined lead time for the supply thereof.

17. Aircraft brake monitoring apparatus for monitoring usage of hydraulic aircraft brakes comprising carbon-carbon multi-discs and providing for maintenance of said hydraulic aircraft brakes said apparatus comprising:

at least one sensor for sensing a brake output parameter during brake actuations of said hydraulic aircraft brakes while an aircraft is in motion with the carbon-carbon multi-discs in engagement and in relative rotational movement and providing signals indicative of values of the sensed brake output parameter;

a processor for processing said signals to determine at least one of a brake wear condition and a brake fault condition; and

a signal provider for issuing a maintenance alert when at least one of said brake wear condition and a said brake fault condition is determined.

18. Apparatus according to claim 17, wherein at least one of said processor and said signal provider is disposed onboard an aircraft.

19. Apparatus according to claim 17, wherein at least one of said processor and said signal provider is a part of an aircraft brakes control system.

20. Apparatus according to claim 17, wherein the sensed brake output parameter is at least one of brake torque, brake temperature, vibration, acoustic signature, wheel deceleration and brake odor.

21. Apparatus according to claim 17, operable to generate expected brake output parameter values for respective brake inputs based on previously sensed brake output parameter values for the respective brake inputs and when said processor determines said at least one of a brake wear condition and a brake fault condition by comparing a current sensed brake output parameter value with an expected brake output parameter value for the respective brake input.

22. A monitoring system for monitoring the condition of a hydraulic aircraft braking apparatus having facing friction surfaces and actuation means for urging said surfaces towards one another and operating a maintenance program for said hydraulic aircraft braking apparatus, the monitoring system being operable for detecting and recording brake inputs and outputs during brake actuations of the braking apparatus during aircraft movement and being characterized in that it comprises distinguishing means for distinguishing, from other actuations, wear generating actuations in which said surfaces come into contact with one another and move relative to one another over the surfaces and generate significant wear of those surfaces, the monitoring system further comprising means capable of making available brake condition information dependent upon said wear generating actuations and selectively providing maintenance action signals based on said brake condition information.

23. A monitoring system according to claim 22, wherein said distinguishing means includes means for generating a signal according to an increase in temperature of the braking apparatus on actuation thereof and distinguishing between non-wear generating actuations which cause said increase below a threshold value and wear generating actuations which cause a said increase above the threshold value.

24. A monitoring system according to claim 23, including means for filtering and at least once differentiating the signals generated by said means for generating a signal.

25. A monitoring system according to claim 22, wherein the distinguishing means comprises signal processing means operable for distinguishing between wear generating and other actuations of the braking apparatus according to respective combinations of intensity and duration of the actuation and for predicting braking performance during future actuations.

26. A method for monitoring the condition of a hydraulic aircraft braking apparatus having facing friction surfaces and actuation means for urging said surfaces towards one another and operating a maintenance program for the hydraulic aircraft braking apparatus, the method including detecting and recording brake inputs and outputs during brake actuations of the braking apparatus during aircraft movement and being characterized in that it comprises distinguishing between wear generating actuations of the braking apparatus in which said surfaces come into contact with one another and move relative to one another over the said surfaces and generate significant wear of those surfaces and other actuations of the apparatus, providing brake condition information dependent upon said wear generating actuations and selectively providing maintenance action signals based on said brake condition information.