The invention relates to the technical field of aircrafts and discloses an aircraft with V-shaped tail wing and multi-rotor vertical take-off and landing layout. The aircraft comprises an aircraft body, fixed side wings, a V-shaped tail wing and a power mechanism for providing advancing tension for the aircraft. Wingtip rotor wings are symmetrically arranged at positions, close to a tip end, of the fixed side wings on the two sides, and rotating planes of the wingtip rotor wings and the side wings are located in the same plane; and V-shaped tail rotors are symmetrically arranged in the two wing sections of the V-shaped tail wing, and the rotating planes of the two V-shaped tail rotors and the wing sections of the V-shaped tail wing are located in the same plane. A layout form that the fourrotors are embedded into the wing tips of the wings on the two sides and the V-shaped tail wing is adopted, and the appearance layout of the aircraft can improve wind resistance of the multi-rotor aircraft, reduce resistance and improve a flight speed on the premise that structural strength of the aircraft body is ensured to be high and power is sufficient.
本发明涉及飞行器技术领域,公开了一种V型尾翼多旋翼垂直起降布局的飞行器,包括机身、固定侧翼、V型尾翼和提供飞行器前进拉力的动力机构,两侧固定侧翼靠近尖端的位置对称设置有翼尖旋翼,翼尖旋翼的旋转平面与所在的侧翼位于同一平面内;V型尾翼的两个翼段内对称设置有V尾旋翼,两个V尾旋翼的旋转平面与所在的V型尾翼翼段位于同一平面内。本发明采用四个旋翼分别内嵌于两侧机翼翼尖及V型尾翼的布局形式,该类飞行器的外形布局能在保证机体结构强度较高、动力充足前提下,提高多旋翼飞行器的抗风能力,减小阻力,并提高飞行速度。
Aircraft with V-shaped tail wing and multi-rotor vertical take-off and landing layout
一种V型尾翼多旋翼垂直起降布局的飞行器
2020-08-14
Patent
Electronic Resource
Chinese
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