Method of taxiing an aircraft
View Patent ↗The invention provides a method of taxiing an aircraft having at least one nose undercarriage at the front of the aircraft and main undercarriages, each undercarriage having wheels, the method comprising the steps of: fitting at least one of the wheels carried by the nose undercarriage with a main taxiing motor member, and fitting at least one of the wheels carried by the main undercarriages with an auxiliary taxiing motor member; and in response to a taxiing order, powering the main taxiing motor member to cause the aircraft to taxi, and in particular if the driving force developed by the main taxiing motor member on the aircraft is insufficient, powering the auxiliary taxiing motor member, as required.
1. A method of taxiing an aircraft having at least one nose undercarriage at a front of the aircraft and main undercarriages to the rear of the nose undercarriage, each undercarriage having wheels, at least one of the wheels carried by the nose undercarriage is fitted with a main taxiing motor and at least one of the wheels carried by the main undercarriages is fitted with an auxiliary taxiing motor, the method comprising the steps of:
issuing a taxiing order when the aircraft is stationary;
in response to the taxiing order, powering the main taxiing motor and the auxiliary taxiing motor to cause the aircraft to taxi;
after the aircraft begins to taxi, controlling the auxiliary taxiing motor to reduce the torque delivered by the auxiliary taxiing motor to zero while controlling the main taxiing motor to deliver torque to continue taxiing the aircraft.
2. The method according to claim 1 , wherein after the aircraft begins to taxi, each auxiliary taxiing motor is controlled to reduce the torque delivered by the auxiliary taxiing motor member to zero while controlling the main taxiing motor to deliver torque to continue taxiing the aircraft.
3. The method according to claim 1 , wherein at least one of the main undercarriage carries wheels that are not braked and that are fitted with auxiliary taxiing motors.
4. The method according to claim 1 , wherein the taxiing motors are controlled in a differential manner in order to assist the aircraft in turning.
5. The method according to claim 1 , wherein each of the wheels of the nose undercarriage is fitted with a respective main taxiing motor.
6. The method according to claim 1 , wherein each of the wheels of the main undercarriages is fitted with a respective auxiliary taxiing motor.
7. The method according to claim 1 , wherein the auxiliary taxiing motor is powered when the aircraft is taxied on a taxiway that is sloping or that presents a low coefficient of friction such that the main taxiing motor alone is unable to deliver sufficient torque for taxiing the aircraft.