A landing gear for a flight vehicle is used during landing. The landing gear for a flight vehicle includes a first cylinder structure configured to have an upper end which is coupled to be able to roll with respect to the flight vehicle; and a second cylinder structure configured to have a lower end which is able to come into contact with the ground, configured to be able to relatively move in an axial direction along a reference axis with respect to the first cylinder structure, and configured to be able to relatively rotate about the reference axis with respect to the first cylinder structure. The first cylinder structure and the second cylinder structure switch the landing gear between a stowed state and a released state by means of the relative movement and the relative rotation.


    Access

    Download


    Export, share and cite



    Title :

    Landing gear for flight vehicle


    Contributors:

    Publication date :

    2024-07-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    LANDING GEAR FOR FLIGHT VEHICLE

    ECHIZENYA TSUYOSHI | European Patent Office | 2023

    Free access

    LANDING GEAR FOR FLIGHT VEHICLE

    ECHIZENYA TAKESHI | European Patent Office | 2023

    Free access

    LANDING GEAR OF FLIGHT ROBOT

    INAGAKI HIROSHI | European Patent Office | 2023

    Free access

    Landing of flight vehicles without the landing gear

    Afanas’ev, V. A. / Degtyarev, G. L. / Meshchanov, A. S. et al. | Online Contents | 2014


    Landing of flight vehicles without the landing gear

    Afanas’ev, V. A. / Degtyarev, G. L. / Meshchanov, A. S. et al. | Springer Verlag | 2014