Patent · US Active

High traction on demand aircraft landing gear system

US9457895B1 · kind B1 · utility

1Cited by
9References
19Claims
0Family size

Assignee

Inventors

Key dates

Filing dateMay 1, 2013
Grant dateOct 4, 2016
Priority date
Expiry dateDec 11, 2033

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY10T29/49492
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A traction-on-demand landing gear tire control system and methods are presented. An outer tire of an aircraft wheel is depressurized to a depressurized state in response to a non-optimal aircraft landing condition. An inner tire of the aircraft wheel contacts the outer tire in response to the depressurized state, and a plurality of traction studs are deployed to protrude from the outer tire in response to the inner tire contacting the outer tire.

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