The invention discloses a novel retractable tandem rotor composite wing aircraft layout which comprises a streamlined fuselage, wings are arranged on the two sides of the fuselage, a plurality of rotors are arranged at the upper end of the fuselage, and the plurality of rotors are uniformly distributed on the fuselage in series; two empennages are arranged at the lower end of the tail part of the fuselage and are distributed in a splayed shape, and auxiliary lift fans are arranged at the tip parts of the wings and are mounted in mounting holes formed in the wings; the upper end and the lower end of the mounting holes are each provided with an auxiliary lift fan opening cover capable of being opened and closed, a rotor wing mounting groove is formed in the fuselage, the rotor wing is mounted in the rotor wing mounting groove through a folding and unfolding mechanism, and a rotor wing opening cover capable of being opened and closed is arranged at the upper end of the rotor wing mounting groove. The vertical take-off and landing stability of the composite wing aircraft is enhanced, the paddle tension threshold value capable of being borne by the aircraft is increased, the flexibility of flight control is promoted, and the aircraft has more stable and reliable vertical take-off and landing capacity on the whole.
本发明公开了一种新型可收放串列旋翼复合翼飞行器布局,其包括流线型的机身,机身的两侧均设置有机翼,机身的上端设置有若干旋翼,若干旋翼均匀串列分布在机身上;机身尾部的下端设置有两片尾翼,两片尾翼成八字形分布,机翼的翼稍部设置有辅助升力风扇,辅助升力风扇安装在机翼上设置的安装孔内;安装孔的上端和下端均设置有可开合的辅助升力风扇口盖,机身上设置有旋翼安装槽,旋翼通过收放机构安装在旋翼安装槽内,旋翼安装槽的上端设置有可开合的旋翼口盖。本发明增强了复合翼飞行器垂直起降的稳定性,增大了飞行器可承受桨叶拉力阈值,促进了飞行控制的灵活度,飞行器整体上具备了更稳定可靠的垂直起降能力。
Novel retractable tandem rotor wing composite wing aircraft layout
一种新型可收放串列旋翼复合翼飞行器布局
2021-08-31
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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