An electric braking system (1) for braking an aircraft, the system comprising:a brake (3) comprising an electromechanical actuator (5) designed so that when it applies a force 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; andconfiguration 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.
AIRCRAFT WHEEL BRAKING SYSTEM, CONFIGURABLE TO OCCUPY A NORMAL MODE OR AN RTO MODE
2020-10-01
Patent
Elektronische Ressource
Englisch
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