The invention relates to an air-drop aircraft, comprising: an aircraft body comprising a detachable top cover; the front lifting airfoil is movably connected to the top cover; the rear lift airfoil is movably connected to the top cover; the rectification front cover is detachably connected to one side of the machine body; and the rectification caudal vertebra is detachably connected to one side of the machine body. According to the air-drop aircraft, the design of the top cover which is detachable relative to the aircraft body is adopted, after the top cover is opened, other parts can be stored in the inner space of the aircraft body, and when the air-drop aircraft needs to be used, the air-drop aircraft can be simply assembled. The assembled aircraft is similar to a glider, and is low in manufacturing cost, stable in flight and small in wind influence. And an engine is not used, so that the manufacturing cost is very low. In combination with an unmanned aerial vehicle control technology, a high-precision drop point target can be realized.
本发明涉及空投飞行器,包括:机体,包括可拆卸的顶盖;前升力翼面,活动连接在所述顶盖上;后升力翼面,活动连接在所述顶盖上;整流前罩,可拆卸连接在所述机体一侧;整流尾椎,可拆卸连接在所述机体一侧。本发明的空投飞行器,采用相对于机体可拆卸的顶盖设计,将顶盖打开后,便可以将其他部件收纳于机体内部空间中,当需要使用时,经过简单的组装即可。组装后的飞行器类似于滑翔机,其造价低廉,飞行稳定,受风力影响小。而且由于没有使用发动机,所以造价也非常便宜。结合无人机控制技术,便可以实现高精度落点的目标。
Air-drop aircraft
空投飞行器
2024-05-17
Patent
Electronic Resource
Chinese
Drop Tower and Aircraft Capabilities
NTRS | 2015
|Drop Tower and Aircraft Capabilities
NTIS | 2015
|"Drop-testing" aircraft electrical apparatus
Engineering Index Backfile | 1940