A nacelle apparatus for a vertical take-off and landing (VTOL) aircraft includes a drive apparatus connected to a wing of the VTOL aircraft via a pylon apparatus and is configured to be pivoted relative to the pylon apparatus about a rotation axis between a propulsion position and a lift position. The nacelle apparatus further includes an air-conducting device having a first inlet opening on the pylon apparatus arranged in the region in which the first air flow strikes the pylon apparatus and a second inlet opening arranged on the nacelle apparatus and/or on the pylon apparatus so that a second air flow is configured to flow in through the second inlet opening in the propulsion position. The air-conducting device further includes an air distribution device with which the flowing air quantities from the first and second inlet openings are configured to be controlled inside the nacelle apparatus.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    NACELLE APPARATUS WITH AIR-CONDUCTING DEVICE AND VERTICAL TAKE-OFF AND LANDING AIRCRAFT


    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 / B64C AEROPLANES , Flugzeuge



    Vertical take-off and landing aircraft nacelle parameter testing device

    LIU MING / LI YUANTONG / TANG WEICHEN et al. | Europäisches Patentamt | 2022

    Freier Zugriff

    Electric motor nacelle for a vertical take-off and landing aircraft and aircraft comprising such a nacelle

    CASTELLI CHRISTOPHE / MESNIL VALENTIN ANTOINE MAXIME / THIAM ABDOULAHAD | Europäisches Patentamt | 2024

    Freier Zugriff

    ELECTRIC MOTOR NACELLE FOR A VERTICAL TAKE-OFF AND LANDING AIRCRAFT AND AIRCRAFT COMPRISING SUCH A NACELLE

    CASTELLI CHRISTOPHE / MESNIL VALENTIN ANTOINE MAXIME / THIAM ABDOULAHAD | Europäisches Patentamt | 2023

    Freier Zugriff