Patent · US Active

System and method for aircraft braking system using monitoring

US7699408B2 · kind B2 · utility

4Cited by
46References
3Claims
0Family size

Assignee

Inventor

Key dates

Filing dateNov 12, 2008
Grant dateApr 20, 2010
Priority date
Expiry dateNov 13, 2028

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB60T2270/406
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

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.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.