A lift-changing mechanism (1) is configured to change generated by a wing (2) of an aircraft and includes a slit (3) and an opening and closing member (4). The slit (3) extends in a wingspan direction inside the wing (2) and forms openings (3A, 3B) on the lower surface (2A) of the wing (2) and on the upper surface (2B) of the wing (2), respectively. A part of an airflow below the lower surface (2A) is allowed to flow toward the upper surface (2B) through the slit (3). The opening and closing member (4) is configured to open and close the slit (3). When the opening and closing member (4) opens the slit (3), lift generated on the wing (2) is decreased compared with the arrangement when the slit (3) is closed.


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    Titel :

    LIFT-CHANGING MECHANISM


    Weitere Titelangaben:

    AUFTRIEBSWECHSELMECHANISMUS
    MÉCANISME DE CHANGEMENT DE PORTANCE


    Beteiligte:
    KOBAYASHI WATARU (Autor:in) / HAYASHI HIROTAKA (Autor:in) / NAKAMURA MIZUKI (Autor:in) / SASAKI MASAFUMI (Autor:in)

    Erscheinungsdatum :

    13.11.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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