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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    Title :

    ELECTRIC NOSE LANDING GEAR ARCHITECTURE


    Additional title:

    ELEKTRISCHE BUGFAHRWERKSARCHITEKTUR
    ARCHITECTURE ÉLECTRIQUE DE TRAIN D'ATTERRISSAGE AVANT


    Contributors:
    FAZELI AMIR M (author) / CEPIC ADNAN (author)

    Publication date :

    2023-08-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / F16D COUPLINGS FOR TRANSMITTING ROTATION , Nicht schaltbare Kupplungen



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