The present invention aims to provide an aerial vehicle of a multi-blade type to improved yaw maneuverability and a method for achieving the purpose. The aerial vehicle can modify the pitch angle (alpha) of its rotors blades, wherein the axis of movement of at least two pairs of the aerial vehicle's rotors are tilted in a symmetrical configuration in relation to the aerial vehicle's yaw plane, sothat each pair converges towards another point on the same level along a longitudinal axis plane of the aerial vehicle while creating an angle (gamma) between the rotation planes of the rotors of eachpair, which is less than 180 degrees and greater than 140 degrees.

    提供了提高偏航机动性的多桨叶类型的飞行器以及实现此目的的方法,该飞行器能够修改其旋翼桨叶的桨距角(α),其中飞行器旋翼中的至少两对旋翼的运动轴线相对于飞行器偏航平面以对称的构造倾斜,使得每对旋翼沿着飞行器的纵向轴线平面向同一水平上的不同点会聚,同时在每对旋翼的旋转平面之间产生小于180°且大于140°的角(γ)。


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    Titel :

    Aircraft with improved maneuverability and method for achieving purpose


    Weitere Titelangaben:

    提高机动性的飞行器和实现此目的的方法


    Beteiligte:
    AGRONOV AHARON (Autor:in)

    Erscheinungsdatum :

    2020-11-17


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge





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