Aircraft brakes in an aircraft that includes a brake pedal and an electric brake actuator are controlled by at least determining an aircraft operational state and determining an application force that is supplied to the brake pedal. 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
Elektrisches Flugzeugbremsenbetätigungssystem und -verfahren
Système électrique d'actionnement du frein d'un avion et procédé
2016-02-24
Patent
Electronic Resource
English
IPC: | B60T Bremsanlagen für Fahrzeuge oder Teile davon , VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF |
Electric Motor Powered Brake Actuation System
SAE Technical Papers | 1984
|Electric Motor Powered Brake Actuation System
Automotive engineering | 1984
|