| 摘要 |
An aircraft comprising a landing gear, having at least one wheel rotatably driven by an electric motor, and a motor control system. The control system comprises a control panel, presenting a first control configured to deliver a torque or power value to the motor along a direction of forward travel of the aircraft and second control configured to deliver a taxiing speed value along a direction of reverse travel, a control unit connected to the control panel and to the electric motor, presenting a first arrangement configured to control, in torque or power, the motor according to the value delivered by the first control, and a second arrangement configured to control, in speed, the motor according to the taxiing speed value delivered by the second control, and a speed sensor configured to measure the taxiing speed of the aircraft, and to transmit this speed information to the control unit. |
| 主权项 |
1. An aircraft comprising:
a landing gear, having at least one wheel provided with an electric motor, configured to drive said wheel in rotation, a control system for said electric motor, said control system comprising: a control panel, presenting a first control apparatus configured to deliver a torque or power value to be applied to said motor according to a direction of forward travel of the aircraft and a second control apparatus configured to deliver a taxiing speed value of the aircraft according to a direction of reverse travel of the aircraft, a control unit connected to the control panel and to the electric motor, presenting a first arrangement configured to control, in torque or in power, the electric motor according to the value delivered by the first control apparatus, and a second arrangement configured to control, in speed, the electric motor according to the taxiing speed value delivered by the second control apparatus, and a speed sensor configured to measure the taxiing speed of the aircraft, and to transmit this speed information to the control unit, the first control apparatus and the second control apparatus comprising a single rotary button presenting a zero position, where a rotation, from the zero position to a first maximum angle, in a first direction of rotation, is representative of the control torque, or power, of the electric motor, and where a rotation, from the zero position to a second maximum angle, in a second direction of rotation is representative of the control speed of the electric motor. |
