The invention relates to an aircraft landing gear, particularly a front landing gear with at least one EHDC unit, which has at least one electric motor and at least one hydraulic pump, whereby at least one adjusting device is provided for the adjustment of the position of the aircraft landing gear, whereby the adjusting device comprises at least one actuator for driving the adjusting device, whereby the steering angle and/or the steering speed and/or the retraction speed and/or the extension speed and/or the end position damping and/or the position of the adjusting device can be controlled or adjusted by means of the electric motor driving the at least one actuator of the adjusting device by means of the hydraulic pump.


    Access

    Download


    Export, share and cite



    Title :

    Aircraft landing gear


    Contributors:

    Publication date :

    2016-10-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    LANDING GEAR OF AIRCRAFT AND AIRCRAFT COMPRISING LANDING GEAR

    SAKAMOTO FUMINOBU / KUROSE TOYOTOSHI | European Patent Office | 2018

    Free access

    Landing gear of aircraft and aircraft comprising landing gear

    SAKAMOTO FUMINOBU / KUROSE TOYOTOSHI | European Patent Office | 2021

    Free access

    Aircraft landing gear

    BENJAMIN BISHOP | European Patent Office | 2023

    Free access

    Aircraft landing gear

    WOOLCOCK JOHN / HANCOCK NICHOLAS | European Patent Office | 2022

    Free access

    AIRCRAFT LANDING GEAR

    BENNETT IAN | European Patent Office | 2020

    Free access