A leading-edge high-lift device according to an embodiment of the present invention is a leading-edge high-lift device that is deployable and retractable from/into a fixed leading edge of a main wing of an aircraft and includes: a leading edge portion; a trailing edge portion that forms a gap between a trailing edge portion and the main wing during deployment; a cusp portion formed at a lower edge of the leading edge portion; a lower surface portion formed between the cusp portion and the trailing edge portion; and a curved hump portion that is locally provided on a surface of the lower surface portion and protrudes toward the main wing in a cross-sectional shape perpendicular to a wing span direction of the main wing.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    LEADING-EDGE HIGH-LIFT DEVICE, WING, AND AIRCRAFT


    Beteiligte:
    YAMAMOTO KAZUOMI (Autor:in) / MURAYAMA MITSUHIRO (Autor:in) / YOKOKAWA YUZURU (Autor:in) / KOHZAI MASATAKA (Autor:in) / ISOTANI KAZUHIDE (Autor:in) / UENO YOSUKE (Autor:in) / HAYAMA KENJI (Autor:in) / HAYASHI KENSUKE (Autor:in)

    Erscheinungsdatum :

    2024-07-25


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    LEADING EDGE HIGH-LIFT DEVICE, WING, AND AIRCRAFT

    YAMAMOTO KAZUOMI / MURAYAMA MITSUHIRO / YOKOKAWA YUZURU et al. | Europäisches Patentamt | 2022

    Freier Zugriff

    LEADING EDGE HIGH-LIFT DEVICE, WING AND AIRCRAFT

    YAMAMOTO KAZUOMI / MURAYAMA MITSUHIRO / YOKOGAWA YUZURU et al. | Europäisches Patentamt | 2022

    Freier Zugriff

    LEADING-EDGE HIGH-LIFT DEVICE, WING, AIRCRAFT, AND BUFFERING MEMBER

    MURAYAMA MITSUHIRO / HIRAI TOHRU / YAMAMOTO KAZUOMI et al. | Europäisches Patentamt | 2024

    Freier Zugriff

    LEADING EDGE HIGH-LIFT DEVICE, WING AND AIRCRAFT, AND BUFFER MEMBER

    MURAYAMA MITSUHIRO / HIRAI TORU / YAMAMOTO KAZUOMI et al. | Europäisches Patentamt | 2022

    Freier Zugriff

    Wing for an aircraft with a deployable leading edge high lift assembly

    GARTELMANN RAINER | Europäisches Patentamt | 2023

    Freier Zugriff