The invention refers to an asymmetric aircraft configuration having a first (3', 3") and a second wing (4), the first wing (3', 3") having a span larger than the second wing (4); a first engine (1) mounted on the first wing (3', 3"), and a second engine (2) mounted on the rear end of the aircraft with its centerline (12) aligned with the aircraft longitudinal axis, the rear end of the aircraft having a T tail (14), and the second engine (1) designed to ingest and consume air forming a boundary layer during the flight; and a main landing gear assembly comprising a first landing gear (8) attached to the first wing (3', 3"), and a second landing gear (9) attached to an area of the fuselage close to the second wing (4).

    本发明涉及一种非对称飞行器构型,所述非对称飞行器构型具有:第一机翼(3’,3”)和第二机翼(4),所述第一机翼(3’,3”)的翼展大于所述第二机翼(4)的翼展;安装在所述第一机翼(3’,3”)上的第一发动机(1),以及安装在所述飞行器的后端的第二发动机(2),其中,所述第二发动机的中心线(12)与所述飞行器纵向轴线对准,所述飞行器的后端具有T型尾翼(14),并且所述第二发动机(1)被设计成在飞行期间摄入并且消耗形成所述边界层的空气;以及主起落架组件,所述主起落架组件包括附接至所述第一机翼(3’,3”)的第一起落架(8),以及附接至所述机身的靠近所述第二机翼(4)的区域的第二起落架(9)。


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    Titel :

    ASYMMETRIC AIRCRAFT CONFIGURATION


    Weitere Titelangaben:

    非对称飞行器构型


    Beteiligte:

    Erscheinungsdatum :

    14.09.2021


    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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