System and Method for Aircraft Braking System Usage Monitoring

• US 20070200427A1
• Filed: 05/03/2007
• Published: 08/30/2007
• Est. Priority Date: 12/04/2001
• Status: Active Grant

• Current Assignee: Hydro-Aire, Inc. (Crane Company)
• Original Assignee: Hydro-Aire, Inc. (Crane Company)
• Inventors: DEVLIEG, Garrett
• Granted Patent: US 7,416,059 B2
• Time in Patent Office: Days
• US Class Current: 303/20
• 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 traveled 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 brake temperature, and for generating a brake temperature signal indicating brake temperature; and

means for receiving said brake temperature signal and determining an estimate of usage of said aircraft brake based upon said brake temperature signal.

2. The system of claim 1, wherein said means for receiving said brake temperature signal and determining an estimate of usage further comprises means for estimating a degree to which each individual brake application contributes to wear based upon said temperature signal.