A nose landing gear system is disclosed. In various embodiments, the nose landing gear system includes an electro-hydraulic actuator configured to raise and lower a nose shock strut assembly; a first electro-mechanical actuator configured to steer the nose shock strut assembly; and a second electro-mechanical actuator configured to open and close a fairing door.


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    Titel :

    ELECTRIC NOSE LANDING GEAR ARCHITECTURE


    Weitere Titelangaben:

    ARCHITECTURE DE TRAIN AVANT ELECTRIQUE


    Beteiligte:
    FAZELI AMIR (Autor:in) / CEPIC ADNAN (Autor:in)

    Erscheinungsdatum :

    2021-03-20


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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