An aircraft landing gear assembly has a longitudinally elongated frame coupled to a lower portion of a fuselage of an aircraft, the frame being capable of supporting at least a portion of the weight of the aircraft. A fairing encloses substantially all of the frame. An optional integrated step can be carried by the frame, and a longitudinally elongated aperture would be formed in the fairing adjacent the step. The step allows a user to place a foot into the aperture and onto the step. An optional door can cover the aperture, and an optional secondary step can be carried by the door.


    Access

    Download


    Export, share and cite



    Title :

    Fully faired landing gear with integrated step


    Contributors:

    Publication date :

    2022-06-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    FULLY FAIRED LANDING GEAR WITH INTEGRATED STEP

    LOVELAND STEVEN / GRIFFITHS PAUL CHARLES / BRITTAIN ALLEN | European Patent Office | 2020

    Free access

    Amphibious vehicle provided with a faired running gear

    DIVRY ERIC | European Patent Office | 2021

    Free access

    Amphibious vehicle provided with a faired running gear

    DIVRY ERIC | European Patent Office | 2023

    Free access

    AMPHIBIOUS VEHICLE PROVIDED WITH A FAIRED RUNNING GEAR

    DIVRY ERIC | European Patent Office | 2020

    Free access

    Faired Towline Hydrodynamics

    D. E. Calkins | AIAA | 1970