The problem addressed by the present invention is that of enhancing the functionality and efficiency of a lightweight aircraft designed for use on short-haul routes. The technical effect to be achieved by the use of the invention is that of allowing the loading and unloading and the transport of different freight having maximum possible dimensions for this aircraft class. At the same time, maximum stiffness and strength of the fuselage and good aerodynamic properties of the aircraft are achieved.


    Access

    Download


    Export, share and cite



    Title :

    RUMPF EINES LEICHTEN TRANSPORTFLUGZEUGS


    Additional title:

    FUSELAGE OF A LIGHTWEIGHT TRANSPORT AIRCRAFT
    FUSELAGE D'UN AÉRONEF DE TRANSPORT LÉGER


    Contributors:

    Publication date :

    2021-12-22


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    German


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    RUMPF EINES LEICHTEN TRANSPORTFLUGZEUGS

    KORNEEV ALEXANDR N / SOLOVYOV VIKTOR K | European Patent Office | 2021

    Free access


    SCHALENANORDNUNG FÜR EINEN RUMPF EINES LUFTFAHRZEUGS UND RUMPF FÜR EIN LUFTFAHRZEUG

    EILKEN WOLFGANG / SCHULZE WOLFGANG / SCHWEIM CHRISTOPH et al. | European Patent Office | 2020

    Free access

    Druckschott für einen druckbeaufschlagten Rumpf eines Fahrzeugs

    WESSELOH MARC / MERTEN ANNALENA | European Patent Office | 2021

    Free access