The invention discloses a double-rotor aircraft. The aircraft comprises an aircraft body, a left engine, a right engine, a left rotor wing and a right rotor wing, the left engine and the right engineare fixedly connected to the left side and the right side of the machine body. A left rotor wing is fixedly connected to a rotating shaft of the left engine, a right rotor wing is fixedly connected toa rotating shaft of the right engine, a left rudder and a right rudder are further arranged on the left side and the right side of the vehicle body, and the left rudder and the right rudder are arranged below the left rotor wing and the right rotor wing respectively. The double-rotor aircraft has the advantages of higher aerodynamic efficiency, lower power consumption, longer flight time, simplerstructure and easiness in realizing automatic and intelligent control.

    本发明公开了一种双旋翼飞行器,包括机体、左发动机、右发动机、左旋翼、右旋翼,所述左发动机和右发动机固定连接在所述机体的左右两侧,所述左发动机的转轴上固定连接有左旋翼,所述右发动机的转轴上固定连接有右旋翼,所述机体的左右两侧还设置有左舵和右舵,所述左舵和右舵分别设置于所述左旋翼和右旋翼的下方。本发明具有更高的气动效率,耗电更少、飞行时间更长,结构较为简单,容易实现自动、智能的控制。


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    Title :

    Double-rotor aircraft


    Additional title:

    一种双旋翼飞行器


    Contributors:
    DAI JIN (author)

    Publication date :

    2020-06-05


    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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