A multirotor aircraft that comprises a body, at least three motors and at least one wing that is connected to the body. The wing is designed to be folded and unfolded during flight of the multirotor aircraft and designed to change during the flight a low-drag creation position to a lift creation position, and vice versa. At least one motor has a greater motor power than another motor and the distance from the strong motor to the center of gravity of the multirotor aircraft is shorter than the distance from the another motor to the center of gravity. The wing is positioned in the geometric area between the motors.

    一种多旋翼飞机,包括:一机身、至少三个马达以及被连接至所述机身的至少一个机翼。所述机翼被设计成在所述多旋翼飞机的飞行期间折叠及伸展,并且被设计成在所述飞行期间将一低阻力创造位置转变为一升力创造位置,反之亦然。相较于另一个马达,至少一个马达具有一更大的马达功率,以及从所述强马达到所述多旋翼飞机的重心的距离短于从所述至少另一个马达到所述重心的距离。所述机翼被定位在所述至少马达之间的一几何区域。


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    Title :

    ASYMMETRIC MULTIROTOR


    Additional title:

    非对称多旋翼机


    Contributors:
    REGEV AMIT (author)

    Publication date :

    2022-01-11


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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