Disclosed is an aircraft brake control system for controlling a plurality of brakeable wheels of a landing gear. Each brakeable wheel comprises a brake actuator and a wheel speed sensor. The system comprises a controller configured to receive aircraft control parameters and provide brake commands to the brake actuator of each wheel. The controller being configured to activate pre-retraction braking in response to an aircraft control parameter indicating that landing gear retraction is required and execute a functional brake test during pre-retraction braking. A method of operating an aircraft braking system is also disclosed.
公开了一种用于控制起落架的多个可制动轮的飞行器制动控制系统。每个可制动轮包括制动致动器和轮速传感器。该系统包括控制器,该控制器被配置成接收飞行器控制参数并且向每个轮的制动致动器提供制动命令。该控制器被配置成响应于指示需要起落架收回的飞行器控制参数而激活预收回制动,并且在预收回制动期间执行功能制动测试。还公开了一种操作飞行器制动系统的方法。
AIRCRAFT BRAKE CONTROL SYSTEM
飞行器制动控制系统
2021-10-26
Patent
Elektronische Ressource
Chinesisch