System and method for aircraft braking system usage monitoring

• US 6,659,233 B2
• Filed: 12/04/2001
• Issued: 12/09/2003
• Est. Priority Date: 12/04/2001
• Status: Expired due to Term

• Current Assignee: Hydro-Aire, Inc. (Crane Company)
• Original Assignee: Hydro-Aire, Inc. (Crane Company)
• Inventors: DeVlieg, Garrett H.
• Primary Examiner(s): Schwartz, Christopher P.
• Application Number:
  US10/008,607
• Publication Number:
  US 20030102191A1
• Time in Patent Office: 735 Days
• Field of Search: 188/1.11 E, 188/1.11 L, 188/1.11 W, 244/111, 340/454, 162/08, 731/29, 731/30
• US Class Current: 188/1.11E
• CPC Class Codes: B60T 17/22 Devices for monitoring or checking brake systems; Signal devices
• CPC Class Codes: B60T 2270/406 Test-mode; Self-diagnosis
• CPC Class Codes: B60T 8/1703 for aircrafts
• CPC Class Codes: B60T 8/172 Determining control parameters used in the regulation, e.g. by calculations involving measured or detected parameters B60T8/17551 takes precedence
• CPC Class Codes: B60T 8/325 Systems specially adapted for aircraft
• CPC Class Codes: B60T 8/885 using electrical circuitry
• CPC Class Codes: F16D 66/028 with non-electrical sensors or signal transmission, e.g. magnetic, optical

Abstract

The system and method for monitoring wear of one or more aircraft parts, such as an aircraft brake, an aircraft tire, a standby system, and landing gear. One or more sensors are provided for sensing a parameter of usage, and an estimate of usage of the part can be determined based upon the signal indicating the sensed value of the parameter of usage of the aircraft part. A plurality of sensors can be provided for sensing usage of a plurality of parts of the aircraft, and the estimate of usage of the part can be stored for access of the estimate by ground personnel. As applied to monitoring wear of an aircraft brake, a linear brake wear indicator attached to the brake moves a discrete distance when the brake is actuated, and a linear position encoder measures the distance travelled by the linear brake wear indicator as an indication of brake usage. A wheel speed monitor may also be provided for measuring the aircraft wheel speed, for distinguishing between static brake applications and moving brake applications, based upon the wheel speed signal.

Claims

1. A system for monitoring wear of an aircraft brake, comprising:

at least one sensor for sensing a parameter of usage of an aircraft brake and for generating a signal indicating a sensed value of said parameter of usage of said aircraft brake, said at least one sensor comprising a linear brake wear indicator and a linear position encoder, said linear brake wear indicator being attached to the brake, wherein each time the brake is actuated, the linear brake wear indicator moves a discrete distance, and said linear position encoder measuring and generating a linear position signal indicating the distance travelled by the linear brake wear indicator as an indication of brake usage;

means for determining an estimate of usage of said brake based upon said linear position signal; and

a wheel speed monitor for generating a wheel speed signal indicating wheel speed of the aircraft, and wherein said means for determining an estimate of usage receives said wheel speed signal for distinguishing between static brake applications and moving brake applications based upon said wheel speed signal.

2. The system for monitoring wear of an aircraft brake of claim 1, wherein said linear brake wear indicator includes a plurality of longitudinally arranged markings, and said linear position encoder comprises an optical encoder for counting said markings passing by said optical encoder for determining the distance travelled by the linear brake wear indicator upon brake actuation, for indicating the distance travelled by the linear brake wear indicator as an indication of brake usage.

3. The system for monitoring wear of an aircraft brake of claim 1, wherein said linear brake wear indicator comprises a brake wear pin.

4. The system for monitoring wear of an aircraft brake of claim 1, wherein said linear brake wear indicator includes a plurality of longitudinally arranged digitized markings indicating longitudinal position on said linear brake wear indicator, and said linear position encoder comprises an optical encoder for encoding the digitized markings, for indicating the distance travelled by the linear brake wear indicator as an indication of brake usage.

5. The system for monitoring wear of an aircraft brake of claim 1, wherein said wheel speed monitor comprises a wheel speed sensor.

6. The system for monitoring wear of an aircraft brake of claim 1, wherein said wheel speed monitor comprises an aircraft speed sensor.

7. The system for monitoring wear of an aircraft brake of claim 1, wherein said means for determining an estimate of usage further comprises means for measuring the period of time elapsed during each brake application, and means for determining the distance over which each brake application occurs, based upon the wheel speed during each brake application and said period of time elapsed during each brake application, for determining the degree to which each individual brake application contributes to brake wear.

8. The system for monitoring wear of an aircraft brake of claim 1, further comprising means for storing said estimate of usage of said brake for access of said estimate by ground personnel.

9. The system for monitoring wear of an aircraft brake of claim 1, wherein said at least one sensor for sensing a parameter comprises a plurality of sensors for sensing usage of a plurality of brakes of the aircraft, and said means for determining an estimate of usage comprises a central computer.

10. The system for monitoring wear of an aircraft brake of claim 1, further comprising means for sensing brake temperature, and for generating a temperature signal indicating brake temperature that is received by said means for determining an estimate of usage, and wherein said estimate of usage is based upon said temperature signal.

11. The system for monitoring wear of an aircraft brake of claim 10, wherein said means for determining an estimate of usage further comprises means for estimating the degree to which each individual brake application contributes to wear based upon said temperature signal.

12. A system for monitoring wear of an aircraft tire, comprising:

a wheel speed monitor generating a wheel speed signal indicating wheel speed of the aircraft;

means for sensing aircraft yaw generating a yaw signal indicating aircraft yaw; and

means for determining an estimate of usage of said tire based upon said wheel speed signal and said yaw signal, and distinguishing between static brake applications and moving brake applications based upon said wheel speed signal.

13. The system for monitoring wear of an aircraft tire of claim 12, wherein said wheel speed monitor comprises a wheel speed sensor.

14. The system for monitoring wear of an aircraft tire of claim 12, wherein said wheel speed monitor comprises an aircraft speed sensor.

15. A system for monitoring wear of an aircraft standby system, comprising

means for sensing input power to said standby system and generating an input power signal;

means for measuring the period of time elapsed during each usage of said standby system and generating an elapsed time signal; and

means for determining an estimate of usage of said aircraft standby system based upon said input power signal and said elapsed time signal.

16. A system for monitoring wear of an aircraft landing gear, comprising:

means for sensing load on said landing gear and generating a load signal;

means for measuring the period of time elapsed during each usage of said landing gear generating an elapsed time signal; and

means for determining an estimate of usage of said aircraft landing gear based upon said load signal and said elapsed time signal.

17. A system for monitoring wear of an aircraft brake, comprising:

at least one linear brake wear indicator attached to the brake, wherein each time the brake is actuated, the linear brake wear indicator moves a discrete distance;

a linear position encoder for measuring and generating a linear position signal indicating the distance travelled by the linear brake wear indicator as an indication of brake usage, and wherein said means for determining an estimate of usage determines an estimate of usage of said brake based upon said linear position signal;

means for determining an estimate of usage of said brake based upon said signal indicating said sensed value of said parameter of usage of said aircraft brake; and

a wheel speed monitor for generating a wheel speed signal indicating wheel speed of the aircraft, wherein said means for determining an estimate of usage receives said wheel speed signal for distinguishing between static brake applications and moving brake applications based upon said wheel speed signal.

18. The system for monitoring wear of an aircraft brake of claim 17, wherein said linear brake wear indicator includes a plurality of longitudinally arranged markings, and said linear position encoder comprises an optical encoder for counting said markings passing by said optical encoder for determining the distance travelled by the linear brake wear indicator upon brake actuation, for indicating the distance travelled by the linear brake wear indicator as an indication of brake usage.

19. The system for monitoring wear of an aircraft brake of claim 17, wherein said linear brake wear indicator comprises a brake wear pin.

20. The system for monitoring wear of an aircraft brake of claim 17, wherein said linear brake wear indicator includes a plurality of longitudinally arranged digitized markings indicating longitudinal position on said linear brake wear indicator, and said linear position encoder comprises an optical encoder for encoding the digitized markings, for indicating the distance travelled by the linear brake wear indicator as an indication of brake usage.

21. The system for monitoring wear of an aircraft brake of claim 17, wherein said wheel speed monitor comprises a wheel speed sensor.

22. The system for monitoring wear of an aircraft brake of claim 17, wherein said wheel speed monitor comprises an aircraft speed sensor.

23. The system for monitoring wear of an aircraft brake of claim 17, wherein said means for determining an estimate of usage further comprises means for measuring the period of time elapsed during each brake application, and means for determining the distance over which each brake application occurs, based upon the wheel speed during each brake application and said period of time elapsed during each brake application, for determining the degree to which each individual brake application contributes to brake wear.

24. A system for monitoring wear of an aircraft brake, comprising:

at least one linear brake wear indicator attached to the brake, wherein each time the brake is actuated, the linear brake wear indicator moves a discrete distance;

a linear position encoder for measuring and generating a linear position signal indicating the distance travelled by the linear brake wear indicator as an indication of brake usage, and wherein said means for determining an estimate of usage determines an estimate of usage of said brake based upon said linear position signal;

means for determining an estimate of usage of said brake based upon said signal indicating said sensed value of said parameter of usage of said aircraft brake; and

means for sensing brake temperature, and for generating a temperature signal indicating brake temperature that is received by said means for determining an estimate of usage, and wherein said estimate of usage is based upon said temperature signal.

25. The system for monitoring wear of an aircraft brake of claim 24, wherein said means for determining an estimate of usage further comprises means for estimating the degree to which each individual brake application contributes to wear based upon said temperature signal.

26. A method for monitoring wear of at least one aircraft brake, comprising:

providing a linear brake wear indicator attached to the brake, wherein each time the brake is actuated, the linear brake wear indicator moves a discrete distance; and

measuring the linear position of said linear brake wear indicator and generating a linear position signal indicating the distance travelled by the linear brake wear indicator as an indication of brake usage;

determining an estimate of usage of said at least one aircraft brake based upon said linear position signal; and

generating a wheel speed signal indicating wheel speed of the aircraft, and distinguishing between static brake applications and moving brake applications based upon said wheel speed signal.

27. The method for monitoring wear of at least one aircraft brake of claim 26, further comprising means for sensing brake temperature, and for generating a temperature signal indicating brake temperature that is received by said means for determining an estimate of usage, and wherein said estimate of usage is based upon said temperature signal.

28. The method for monitoring wear of at least one aircraft brake of claim 27, wherein said step of determining an estimate of usage further comprises estimating the degree to which each individual brake application contributes to wear based upon said temperature signal.

29. The method for monitoring wear of at least one aircraft brake of claim 26, wherein said linear brake wear indicator includes a plurality of longitudinally arranged markings, and said steps of measuring the linear position of said linear brake wear indicator and generating a linear position signal comprise providing an optical encoder for counting said markings passing by said optical encoder for determining the distance travelled by the linear brake wear indicator upon brake actuation, for indicating the distance travelled by the linear brake wear indicator as an indication of brake usage.

30. The method for monitoring wear of at least one aircraft brake of claim 26, wherein said linear brake wear indicator includes a plurality of longitudinally arranged digitized markings indicating longitudinal position on said linear brake wear indicator, and said steps of measuring the linear position of said linear brake wear indicator and generating a linear position signal comprise providing an optical encoder for encoding the digitized markings, for indicating the distance travelled by the linear brake wear indicator as an indication of brake usage.

31. The method for monitoring wear of at least one aircraft brake of claim 26, wherein said step of generating a wheel speed signal comprises providing a wheel speed sensor for indicating wheel speed of the aircraft.

32. The method for monitoring wear of at least one aircraft brake of claim 26, wherein said step of generating a wheel speed signal comprises determining wheel speed based upon speed of the aircraft speed.

33. The method for monitoring wear of at least one aircraft brake of claim 26, wherein said step of determining an estimate of usage further comprises measuring the period of time elapsed during each brake application, and determining the distance over which each brake application occurs, based upon the wheel speed during each brake application and said period of time elapsed during each brake application, to determine the degree to which each individual brake application contributes to brake wear.

34. The method for monitoring wear of at least one aircraft brake of claim 26, further comprising the step of storing said estimate of usage of said at least one aircraft brake for access of said estimate by ground personnel.

35. A method for monitoring wear of at least one aircraft tire, comprising:

generating a wheel speed signal indicating wheel speed of the aircraft;

sensing aircraft yaw and generating a yaw signal indicating aircraft yaw;

determining an estimate of usage of said at least one aircraft tire based upon said wheel speed signal and said yaw signal; and

distinguishing between static brake applications and moving brake application based upon said wheel speed signal.

36. A method for monitoring wear of at least one aircraft standby system, comprising:

sensing input power to said standby system and generating an input power signal; and

measuring the period of time elapsed during each usage of standby system and generating an elapsed time signal; and

determining an estimate of usage of said at least one aircraft standby system based upon said input power signal and said elapsed time signal.

37. A method for monitoring wear of at least one aircraft landing gear, comprising:

sensing load on said landing gear and generating a load signal;

measuring the period of time elapsed during each usage of said landing gear and generating an elapsed time signal; and

determining an estimate of usage of said at least one aircraft landing gear based upon said load signal and said elapsed time signal.

38. A method for monitoring wear of at least one aircraft part, comprising

sensing a plurality of parameters for a plurality of aircraft parts and generating a plurality of signals indicating a plurality of sensed values of said plurality of parameters of usage of said plurality of aircraft parts;

and

determining a plurality of estimates of usage of said plurality of aircraft parts based upon said plurality of signals.