The aircraft comprises a front rotor 10 arranged on the front portion of an aircraft body. The rear rotor wing 12 is arranged at the rear part of the aircraft body; a front deflection mechanism that changes the angle of the front rotor 10 with respect to the fuselage within a first range; a rear deflection mechanism that changes the angle of the rear rotor 12 with respect to the fuselage within a second range; and a main body module (2) provided on the machine body and accommodating a conveyance object. The first range is provided such that a plane including the rotation surface of the front rotor 10 does not intersect the main body module 2. The second range is provided such that a plane including the rotation surface of the rear rotor 12 does not intersect the main body module 2.

    飞行器包括设置在机体前部的前旋翼10;设置在机体后部的后旋翼12;在第一范围内改变前旋翼10相对于机体的角度的前偏转机构;在第二范围内改变后旋翼12相对于机体的角度的后偏转机构;以及设置在机体上容纳输送对象的主体模块2。第一范围被设置为使包含前旋翼10的旋转面的平面不与主体模块2相交。第二范围被设置为使包含后旋翼12的旋转面的平面不与主体模块2相交。


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    Titel :

    Aircraft


    Weitere Titelangaben:

    飞行器


    Beteiligte:
    KITAMA SHOJI (Autor:in)

    Erscheinungsdatum :

    2023-08-01


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64U



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