A leading edge of the flow body is arranged between the bottom section and the top section. The spar extends from the bottom section to the top section. The front skin, the back skin and the spar enclose at least one air chamber that is in fluid communication with the air inlet. An outlet portion is arranged at least directly adjacent to the bottom section of the front skin. The outlet portion comprises a plurality of air outlets for letting air from the at least one air chamber exhaust through the air outlets.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    LEADING-EDGE DEVICE FOR AN AIRCRAFT


    Beteiligte:
    ERBAN MARCUS (Autor:in) / FEES MARTIN (Autor:in) / BENSMANN STEFAN (Autor:in)

    Erscheinungsdatum :

    2020-11-05


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    LEADING-EDGE DEVICE FOR AN AIRCRAFT

    BENSMANN STEFAN / ERBAN MARCUS / FEES MARTIN | Europäisches Patentamt | 2023

    Freier Zugriff

    AIRCRAFT LEADING EDGE ASSEMBLY

    GAO JUN / WU ZHIBIN / KONG LINGYONG et al. | Europäisches Patentamt | 2022

    Freier Zugriff

    Aircraft leading edge structure

    LIU CHUANJUN / JIA JIALE / FANG ZHIYANG et al. | Europäisches Patentamt | 2024

    Freier Zugriff

    Leading-edge device for an aircraft

    ERBAN MARCUS / FEES MARTIN / BENSMANN STEFAN | Europäisches Patentamt | 2022

    Freier Zugriff

    Aircraft leading edge sealing structure

    WANG ZHIGANG / FU SHUO / WANG LIPING et al. | Europäisches Patentamt | 2024

    Freier Zugriff