A landing gear door system (20) for a landing gear compartment includes a door (22) pivotable about a pivot pin (44) configured for disposition in a longitudinal direction (21) on an airframe (10), and a mechanism (50) configured to rotate the door (22) about the pivot pin (44) between a closed position, in which an outer surface of the door panel (24) is configured to provide aerodynamic continuity with an outer aircraft skin of the airframe (10), and an open position, in which the door is rotated into the landing gear compartment and an opening is exposed. The door (22) has a door panel rigidly connected with an arm (30) such that the door panel (24) and arm (30) generally form a V-shape as viewed in the longitudinal direction (21).


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    Title :

    LANDING GEAR DOOR SYSTEM FOR A LANDING GEAR COMPARTMENT


    Additional title:

    FAHRWERKSTÜRSYSTEM FÜR EINEN FAHRWERKSRAUM
    SYSTÈME DE PORTE DE TRAIN D'ATTERRISSAGE POUR UN COMPARTIMENT DE TRAIN D'ATTERRISSAGE


    Contributors:
    WEBB SEAN C (author)

    Publication date :

    2024-03-20


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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