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Aerodynamically efficient lightweight vertical take-off and landing aircraft with swirling rotor blades and contained rotor blades

机译:空气动力学效率高的轻型垂直起降飞机,具有旋转的旋翼桨叶和封闭式旋翼桨叶

摘要

An aerial vehicle adapted for vertical takeoff and landing using a set of wing mounted thrust producing elements and a set of tail mounted rotors for takeoff and landing. An aerial vehicle which is adapted to vertical takeoff with the rotors in a rotated, take-off attitude then transitions to a horizontal flight path, with the rotors rotated to a typical horizontal configuration. The aerial vehicle uses different configurations of its wing mounted rotors and propellers to reduce drag in all flight modes.
机译:一种适用于垂直起飞和降落的飞行器,其使用一组机翼安装的推力产生元件和一组用于起飞和降落的尾部安装的旋翼。然后,在转子以旋转的起飞姿势的情况下适于垂直起飞的飞行器过渡到水平飞行路径,其中转子旋转到典型的水平配置。飞机使用其机翼安装的旋翼和螺旋桨的不同配置来减少所有飞行模式中的阻力。

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