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.


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    Title :

    EMERGENCY PARK BRAKE SYSTEM


    Additional title:

    NOTFESTSTELLBREMSSYSTEM
    SYSTÈME DE FREIN DE STATIONNEMENT D'URGENCE


    Contributors:
    CAHILL ERIC (author) / STEIN DAVID B (author) / BURTE PAUL R (author)

    Publication date :

    2023-11-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B60T Bremsanlagen für Fahrzeuge oder Teile davon , VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF



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