A landing gear tire traction 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 rotor 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 rotor contacting the outer tire.
CONTROLLED LANDING GEAR TIRE TRACTION SYSTEM
GESTEUERTES REIFENTRAKTIONSSYSTEM FÜR EIN FAHRWERK
SYSTÈME DE TRACTION COMMANDÉ DE PNEU DE TRAIN D'ATTERRISSAGE
10.01.2018
Patent
Elektronische Ressource
Englisch
TIRE MODELS IN AIRCRAFT LANDING GEAR SIMULATION
Taylor & Francis Verlag | 1992
|Tire parameters for landing-gear shimmy studies.
AIAA | 1969
|