A brake system for an aircraft is provided according to various embodiments. The system may include a left pedal arrangement comprising a left pedal, a first left sensor to generate a first left signal in response to translation of the left pedal. The system also includes a right pedal arrangement comprising a right pedal, a first right sensor to generate a first right signal in response to translation of the right pedal. Normal brake control logic controls the brake system in response to a normal condition being set. The normal brake control logic commands a left brake based on the left signal, and a right brake based on the first right signal. Emergency brake control logic controls the brake system in response to an emergency condition being set. The emergency brake control logic commands a same force to the left and right brakes based the left and right signals.
SYSTEMS AND METHODS FOR EMERGENCY AIRCRAFT BRAKE OPERATION
2018-04-19
Patent
Electronic Resource
English
Systems and methods for emergency aircraft brake operation
European Patent Office | 2019
|SYSTEMS AND METHODS FOR EMERGENCY AIRCRAFT BRAKE OPERATION
European Patent Office | 2021
|