The invention relates to a rotorcraft. The center (C) of a connecting part (16) coincides with the center (U) of the lift force generated in the body of the rotorcraft (10). The center (C) of the connecting part (16) refers to the action point of the gravity on the supporting rod (21) of the connecting part (16) and the first carrying part. The center (U) of the lift force is the point of action of the lift force on the rotorcraft (10) and is the center of rotation in the connection part (16). Thus, since the center U of the lift force generated in the rotorcraft (10) is located at the center C of the connecting part, even if the body of the rotorcraft (10) is inclined, the support rod (21) and the first mounting part rotate about the center C of the connecting part, and therefore, no rotational moment caused by a weight such as a camera (28) is generated around the center U of the lift force. Accordingly, when the rotorcraft having a plurality of rotors advances in the horizontal direction, the difference between the number of rotations of each of the rotors forward and rearward in the advancing direction can be made smaller than in the prior art.

    本发明涉及旋翼机。连接部(16)的中心(C)与产生于旋翼机(10)的机体的升力的中心(U)一致。连接部(16)的中心(C)是指对连接部(16)的支撑棒(21)以及第一搭载部的重力的作用点。升力的中心(U)是指对旋翼机(10)的升力的作用点,并且是连接部(16)中的旋转中心。如此,由于产生于旋翼机(10)的升力的中心U位于连接部的中心(C),即使是旋翼机(10)的机体倾斜的情况下,支撑棒(21)以及第一搭载部以连接部的中心(C)为中心进行旋转,因此升力的中心(U)的周围不会产生因摄像机(28)等重物而引起的旋转力矩。据此,在具有多个旋翼的旋翼机沿着水平方向前进的情况下,可以使得前进方向前方以及后方的各旋翼的旋转数的差值比现有技术小。


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    Title :

    Rotorcraft


    Additional title:

    旋翼机


    Contributors:

    Publication date :

    2021-07-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

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



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