The invention relates to an aircraft comprising a fuselage (32), a first wing (34.1) and a second wing (34.2) positioned on both sides of the fuselage (32), characterized in that each wing (34.1, 34.2) comprises an inner portion (48.1, 48.2) connected to the fuselage (32) and an outer portion (50.1, 50.2) extending the inner portion (48.1, 48.2), an end (56.2) of each inner portion (48.1, 48.2) being connected to the fuselage (32), the height of the end being greater than half of the height of the fuselage, and extends over a length greater than or equal to half the distance separating the front tip (42.1) and the rear tip (42.2) of the fuselage (32).

    本发明涉及一种飞行器,包括机身(32)、定位于机身(32)的两侧的第一机翼(34.1)和第二机翼(34.2),其特征在于,每个机翼(34.1、34.2)包括连接到机身(32)的内部部分(48.1、48.2)以及延伸内部部分(48.1、48.2)的外部部分(50.1、50.2),每个内部部分(48.1、48.2)的端部(56.2)连接到机身(32),端部的高度大于机身的高度的一半,并且在大于或等于将机身(32)的前尖部(42.1)和后尖部(42.2)分隔开的距离的一半的长度上延伸。


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    Titel :

    Aircraft comprising fuselage and wing having outer part and inner part


    Weitere Titelangaben:

    包括机身和具有外部部分和内部部分的机翼的飞行器


    Beteiligte:
    BOOS ANDREAS (Autor:in) / LAVIEN JEAN (Autor:in) / FORBES ANDREW (Autor:in)

    Erscheinungsdatum :

    2023-03-17


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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




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