An emergency park brake system of an aircraft may include a user input interface (205) configured to receive actuation input from a user. The emergency park brake system may also include a first displacement sensor (210) and a second displacement sensor (212) that are both coupled to the user input interface. The first displacement sensor may be configured to detect displacement of the user input interface and generate a first status of the user input interface and the second displacement sensor may be configured to also detect displacement of the user input interface and generate a second status of the user input interface. The emergency park brake system may also include a controller (220) having a processor and memory. The controller may be configured to determine an emergency park brake condition.
EMERGENCY PARK BRAKE SYSTEM
NOTFESTSTELLBREMSSYSTEM
SYSTÈME DE FREIN DE STATIONNEMENT D'URGENCE
01.11.2023
Patent
Elektronische Ressource
Englisch