The invention provides an aircraft capable of vertically taking off and landing. The aircraft comprises an aircraft body and wings, the aircraft body comprises a front aircraft body and a rear aircraft body, the wings are symmetrically arranged on the two sides of the front aircraft body, the plane where the two wings are located passes through the axis of the aircraft body and divides the rear aircraft body into an upper aircraft body and a lower aircraft body which are symmetrical, the tail of the front aircraft body is hinged to the head of the upper aircraft body and the head of the loweraircraft body, and the upper aircraft body and the lower aircraft body are connected with a folding mechanism for driving the same to unfold or fold; the tails of the upper aircraft body and the loweraircraft body are each provided with a first propeller and a first steering nozzle, each first steering nozzle is arranged at the tail of the corresponding first propeller and connected with a firstrotating mechanism capable of driving the first steering nozzle to rotate, and the rotating axis of each first steering nozzle is perpendicular to the axis of the corresponding aircraft body; the upper aircraft body and the lower aircraft body are linear when completely unfolded, and the bottoms of the upper aircraft body and the lower aircraft body and the tails of the two wings are located on the same plane. The space occupied by taking off and landing of the aircraft is reduced, and the flight power of the aircraft after vertical rising is increased.
本申请涉及一种可垂直起降的飞行器,包括机身和机翼,机身包括前机身和后机身,机翼对称设置在前机身的两侧,两机翼所在平面经过机身的轴线,并将后机身分为对称的上机身和下机身,前机身的尾部分别与上机身和下机身的头部铰接,上机身和下机身连接有驱动其展开或闭合的折叠机构;上机身和下机身的尾部分别设有一组第一推进器和第一转向喷嘴,每组第一转向喷嘴设置在第一推进器尾部,第一转向喷嘴连接可驱动其转动的第一旋转机构,第一转向喷嘴的旋转轴线与机身的轴线垂直;上机身与下机身完全展开时呈一字型,且上机身和下机身的底部与两个机翼的尾部位于同一平面。本申请减小了飞行器起落所占用的空间,增大了飞行器垂直升起后的飞行动力。
Aircraft capable of vertically taking off and landing
一种可垂直起降的飞行器
2021-02-12
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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