A system and method of controlling aircraft brakes in an aircraft that includes a brake pedal and an electric brake actuator. An aircraft operational state is determined and an application force that is supplied to the brake pedal is determined. When the determined aircraft operational state is a ground-idle state and the determined application force is greater than a set force magnitude, an actuator brake is moved to engage the electric brake actuator and the electric brake actuator is de-energized.
Aircraft electric brake actuation system and method
2016-09-13
Patent
Electronic Resource
English
Electric Motor Powered Brake Actuation System
SAE Technical Papers | 1984
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