aircraft wheel brake system, configurable according to normal mode or RTO mode

The present invention provides an electric braking system (1) for braking an aircraft. The system comprises a brake (3) comprising an electromechanical actuator (5) designed so that when it applies aforce to the friction members (4) that is less than or equal to a first maximum threshold, no degradation of the actuator occurs, and when it applies a force to the friction members (4) that is greater than the first maximum threshold, degradation is likely to occur; control means (7) configurable to occupy a first mode in which the controlled braking force cannot exceed the first maximum threshold, and to occupy a second mode in which the controlled braking force can reach the second maximum threshold; and configuration means (10) arranged to configure the control means (7) to occupy the second mode when in a situation preceding a potential interruption of takeoff (RTO) of the aircraft, and otherwise to occupy the first mode. 一种用于制动飞行器的电制动系统(1)，该系统包括：包括机电致动器(5)的制动器(3)，该机电致动器(5)被设计成使得当它向摩擦构件(4)施加小于或等于第一最大阈值的力时，致动器