An aircraft (10) with no vertical tail is provided with: a fuselage (20) extending in the aircraft axis direction; primary wings (30) provided to lateral surfaces (55) of the fuselage (20); and a negative pressure generating section (40) for generating negative pressure over the lateral surfaces (55) at the rear of the fuselage (20) with respect to sideslip.

    L'invention concerne un aéronef (10) sans empennage vertical, comportant : un fuselage (20) s'étendant dans la direction de l'axe de l'aéronef ; des ailes principales (30) disposées sur des surfaces latérales (55) du fuselage (20) ; et une section de génération de pression négative (40) pour générer une pression négative sur les surfaces latérales (55) à l'arrière du fuselage (20) par rapport à la glissade.

    無垂直尾翼機(10)は、機軸方向に延びる胴体(20)と、前記胴体(20)の側面(55)に設けられた主翼(30)と、横滑りに対して前記胴体(20)の後部における側面(55)上に負圧を発生させる負圧発生部(40)と、を備えている。


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    Title :

    AIRCRAFT WITH NO VERTICAL TAIL


    Additional title:

    AÉRONEF SANS EMPANNAGE VERTICAL
    無垂直尾翼機


    Contributors:

    Publication date :

    2019-11-14


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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