The invention discloses a double-fuselage tandem rotor wing composite wing aircraft layout which comprises two parallel fuselages, the side faces of the two fuselages are connected through a central wing, power devices are arranged at the tails of the fuselages, wings are arranged on the side faces of the two fuselages, the tails of the two fuselages are connected through an empennage, and the empennage is of an arch structure. A plurality of rotors are arranged above each fuselage and are uniformly distributed, the central wing is a rectangular wing, and the plane where the central wing is located is perpendicular to the symmetry plane of the two fuselages. The rigidity and strength of the double fuselages are fully utilized, the vertical take-off and landing stability of large and heavy composite wing aircrafts is enhanced, flight control of the aircrafts is facilitated, and compared with the design of traditional rotor wing supporting arms, the threshold value of lift force capable of being borne by the fuselages is increased.
本发明公开了一种双机身串列旋翼复合翼飞行器布局,其包括两个并列的机身,两个机身的侧面通过中央翼连接,机身的尾部设置有动力装置,两个机身的侧面设置有机翼,两个机身的尾部通过尾翼连接,尾翼为拱形结构,每个机身的上方均设置有若干旋翼,若干旋翼均匀分布,中央翼为矩形翼,中央翼所在平面与两个机身的对称面垂直。本发明充分利用双机身的刚度和强度,增强了大型和重型复合翼飞行器垂直起降的稳定性,有利于飞行器的飞行控制,相对于传统旋翼支臂的设计,机身可承受升力的阈值增大。
Double-fuselage tandem rotor wing composite wing aircraft layout
一种双机身串列旋翼复合翼飞行器布局
2021-09-03
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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