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,致动器的退化不发生,而当它向摩擦构件(4)施加大于第一最大阈值的力时,退化有可能发生;控制装置(7),该控制装置(7)可配置为占用第一模式,在该第一模式下受控的制动力无法超过第一最大阈值,并且占用第二模式,在该第二模式下受控的制动力可以达到第二最大阈值;以及配置装置(10),该配置装置(10)被布置成将控制装置(7)配置为当处于飞行器的起飞的潜在中断(RTO)之前的境况中时占用第二模式,否则占用第一模式。
aircraft wheel brake system, configurable according to normal mode or RTO mode
可配置为占用正常模式或RTO模式的飞行器机轮制动系统
2020-10-20
Patent
Elektronische Ressource
Chinesisch
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