The invention relates to a telescopic folding wing, which is connected with an aircraft through a main bracket, and is characterized by comprising a telescopic central sleeve group which is arranged in the middle, is used for supporting and bearing and is telescopic, and an outer side sleeve group which is sleeved on the periphery of the central sleeve group, is used for generating lift force and is capable of synchronously stretching and retracting with the central sleeve group, the folding mechanism is used for connecting the central sleeve group and the outer side sleeve group with the main bracket together; the propeller is arranged on the outer end of the wing main body; the center sleeve set and the outer side sleeve set are connected in a sleeved mode to form a telescopic whole, and the telescopic whole is connected with the folding mechanism through a variable-diameter deformation pipe. A telescopic driving mechanism is installed in the center sleeve set. The structural design is compact, and synchronous stretching and retracting of the center sleeve set and the outer side sleeve sets are achieved through the stretching and retracting driving mechanism arranged in the center sleeve set. The defects that a fixed wing structure cannot be stretched and folded, and the area and the size cannot be changed are overcome, and technical support is provided for a transformable aircraft.
本发明涉及一种伸缩折叠机翼,该机翼通过主支架与飞行器连接,其特征在于:包括设置安装在中间、用于支撑承重、能够伸缩的中心套管组,套装在中心套管组外周、用于产生升力、能够与中心套管组同步伸缩的外侧套管组,用于将中心套管组和外侧套管组一起与主支架连接的折叠机构,设置在机翼主体外端上面的螺旋桨;所述中心套管组和外侧套管组套接组成伸缩整体,该伸缩整体通过变径变形管与折叠机构连接;所述中心套管组内部设置安装有伸缩驱动机构。结构设计紧凑,通过设在中心套管组内的伸缩驱动机构,实现中心套管组与外侧套管组的同步伸缩。解决了固定机翼结构不能够伸缩、折叠,面积、体积无法变化的缺点,为变形飞行器提供了技术支持。
Telescopic folding wing
一种伸缩折叠机翼
2024-09-06
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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