ELECTRIC TAXIING SYSTEM OF AIRCRAFT AND METHOD FOR CONTROLLING THE SYSTEM

摘要

An electric taxiing system of an aircraft (1) includes: a wheel (5a, 7a) of anaircraft (1); a taxiing motor (5b, 7b) which is rotated together with thewheel (5a, 7a) inlanding of the aircraft (1) to apply breaking force to the wheel (5a, 7a) andto generateregenerative power according to the breaking force, and which rotates thewheel (5a, 7a)in taxiing of the aircraft (1); and a power supply control unit (27) whichsupplies theregenerative power to an electric element of the aircraft (1), the electricelement (9b,11b, 13b, 15b, 29a, 31a) being driven in order for the aircraft (1) to performlanding orre-takeoff after cancelling landing.