Patent · US Active

Method and system for controlling aircraft braking on a runway

US8972141B2 · kind B2 · utility

1Cited by
2References
17Claims
0Family size

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Key dates

Filing dateMar 28, 2013
Grant dateMar 3, 2015
Priority date
Expiry dateApr 25, 2033

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB60T8/1703
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A method to control braking of an aircraft on a landing runway including: selecting a dummy runway state corresponding to a level of adhesion of wheels of the aircraft to a runway which is lower, over an entire speed range of the aircraft while braking on a runway, than an adhesion level of the wheels of the aircraft to the landing runway; calculating a set point of a deceleration value for the aircraft on the landing runway based on the landing runway for the selected dummy runway state, wherein the calculated set point corresponds to maximum braking value of the aircraft, and controlling the braking of the aircraft using the set point.

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