Disclosed is a landing gear system controller 120 for controlling a landing gear system 100 of an aircraft. The controller is configured to receive a request to operate a non-landing gear system element of the aircraft, and to cause operation of at least part of the landing gear system of the aircraft during a take-off or landing procedure on the basis of the request. The non-landing gear system may be a main lift control surface, an aileron, an elevator, a rudder, a flap, a slat, a spoiler, an automatic landing system or an automatic braking system. The deployment of the landing gear may also depend on a predetermined condition such as a predetermined speed, altitude or rate of climb. The landing gear system may comprise a landing gear actuator 112, landing gear lock 113, landing gear bay door, landing gear bay door actuator 116 or a landing gear bay door lock 117. There is also claimed a method of controlling landing gear comprising receiving a request to operate a non-landing gear system and causing the operation of at least part of the landing gear system.


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    Titel :

    Landing gear system control


    Beteiligte:
    SEAN KERR (Autor:in) / MARTIN DOWNEY (Autor:in)

    Erscheinungsdatum :

    11.09.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen / B64C AEROPLANES , Flugzeuge



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