A leading-edge slat (6) for an aircraft (62) is proposed, which comprises a front skin (10), a back skin (12), a spar (14) and an air inlet (16) for receiving air at an elevated temperature for de-icing or anti-icing. In the slat, at least one air chamber is created, which is supplied with said air. A first portion (28) of the back skin (12) is attached to the spar (14) at a distance to the bottom section (20), wherein a second portion (31) of the back skin (12) is attached to the top section (22). Thereby, a region in front of the fixed leading edge (2) is created, into which air from air outlets (48) integrated into the back skin (12) can be exhausted outside of the slat (6).


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    LEADING-EDGE SLAT FOR AN AIRCRAFT


    Weitere Titelangaben:

    VORDERKANTENLEISTE FÜR EIN FLUGZEUG
    BEC DE BORD D'ATTAQUE POUR AÉRONEF


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

    Erscheinungsdatum :

    06.10.2021


    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 Slat For An Aircraft

    BENSMANN STEFAN / ERBAN MARCUS / FEES MARTIN | Europäisches Patentamt | 2020

    Freier Zugriff

    LEADING-EDGE SLAT FOR AN AIRCRAFT

    BENSMANN STEFAN / FEES MARTIN / ERBAN MARCUS | Europäisches Patentamt | 2020

    Freier Zugriff

    Leading-edge slat for an aircraft

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

    Freier Zugriff

    Leading edge slat and wing of aircraft

    LI YAN / CHEN MENGYING / WANG BO | Europäisches Patentamt | 2024

    Freier Zugriff

    Leading edge slat

    COMMIS BEN / LYONS NEIL / KAY EDMUND | Europäisches Patentamt | 2024

    Freier Zugriff