A landing gear for an aircraft comprising a truck support strut, a landing gear retract mechanism coupling the truck support strut to a frame of the aircraft, so that the truck support strut is suspended from the frame by the landing gear retract mechanism, at least one wheel support arm rotatably coupled to the truck support strut, a carrier member coupled to the landing gear retract mechanism and to the truck support strut so that the landing gear retract mechanism drives the carrier member along the truck support strut, and at least one shock absorber, each of the at least one shock absorber being coupled to both a respective one of the at least one wheel support arm and the carrier member so that movement of the carrier member effects rotation of the at least one wheel support arm relative to the truck support strut.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Body mounted shrinking landing gear


    Beteiligte:
    TSAI KEVIN (Autor:in) / SAKURAI SEIYA (Autor:in)

    Erscheinungsdatum :

    2021-05-18


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    BODY MOUNTED SHRINKING LANDING GEAR

    TSAI KEVIN / SAKURAI SEIYA | Europäisches Patentamt | 2019

    Freier Zugriff

    Shrinking System for Landing Gear

    LUCE WILLIAM E | Europäisches Patentamt | 2015

    Freier Zugriff

    Shrinking system for landing gear

    LUCE WILLIAM E | Europäisches Patentamt | 2016

    Freier Zugriff

    HYDRAULIC SYSTEMS FOR SHRINKING LANDING GEAR

    PLUDE LEO W / BRYANT MALCOLM S / LINDAHL GARY M | Europäisches Patentamt | 2019

    Freier Zugriff

    Hydraulic systems for shrinking landing gear

    PLUDE LEO W / BRYANT MALCOLM S / LINDAHL GARY M | Europäisches Patentamt | 2020

    Freier Zugriff