A propulsion system fastened to one side of an aircraft and having a longitudinal axis and a mid-plane and having a nacelle with two inner cowls, two outer cowls, two lower structural elements and two upper structural elements, wherein each outer cowl is articulated on a pylon by hinges with axes parallel to the longitudinal axis. The two outer cowls are contiguous at a separation plane containing the longitudinal axis and making, with the mid-plane, an acute angle. The axes are asymmetrical with respect to the mid-plane.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    PROPULSION SYSTEM OF AN AIRCRAFT, HAVING AN ASYMMETRICAL NACELLE


    Beteiligte:

    Erscheinungsdatum :

    30.05.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    Propulsion system of an aircraft, having an asymmetrical nacelle

    GOUGEON PASCAL / BELLANGER ALEXANDRE / VANDERBAUWEDE SIMON | Europäisches Patentamt | 2025

    Freier Zugriff

    Strake for aircraft propulsion system nacelle

    BINKS ALAN J | Europäisches Patentamt | 2020

    Freier Zugriff

    STRAKE FOR AIRCRAFT PROPULSION SYSTEM NACELLE

    BINKS ALAN J | Europäisches Patentamt | 2018

    Freier Zugriff

    Nacelle unit, distributed propulsion nacelle and new energy aircraft

    LYU GANLIN / WANG YILIN / YU HANG et al. | Europäisches Patentamt | 2025

    Freier Zugriff

    Aircraft nacelle section and aircraft having aircraft nacelle section

    WEN AMY / KIRSTEIN HENNING / TEICHMANN SIEGFRIED et al. | Europäisches Patentamt | 2022

    Freier Zugriff