The present embodiments relate to an aircraft door 104, and, more particularly, to an electromechanical door system 200 for operating an aircraft door 104 that closes an opening in the outer hull 102 of an aircraft 100, as well as to a method of operating an electromechanical door system 200 of an aircraft door 104 that closes an opening in the outer hull 102 of an aircraft 100. The electromechanical door system 200 may be adapted for operating in a normal opening mode, an emergency opening mode, and a closing mode. If desired, the electromechanical door system 200 may include a lifting and lowering lever 210, a lifting and lowering electric motor 215, and a gearbox 218 that transmits a force from the lifting and lowering electric motor 215 to the lifting and lowering lever 210.


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    Title :

    AIRCRAFT WITH AN ELECTROMECHANICAL DOOR SYSTEM


    Additional title:

    FLUGZEUG MIT EINEM ELEKTROMECHANISCHES TÜRSYSTEM
    AÉRONEF AVEC UN SYSTÈME DE PORTE ÉLECTROMÉCANIQUE


    Contributors:

    Publication date :

    2023-06-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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