The invention discloses a quickly-assembled unmanned aerial vehicle, relates to the technical field of aircrafts and aims to solve the problem that time and labor are wasted when an unmanned aerial vehicle is assembled and disassembled. The quickly-assembled unmanned aerial vehicle comprises a fuselage body, a central wing, rotary wing connecting rods, outer wings, an empennage, a first undercarriage, a second undercarriage, rotary wings and a rear propeller; the central wing is detachably arranged on the fuselage body; the outer wings are detachably arranged on the two sides of the central wing; the rotary wing connecting rods are arranged on the central wing or the outer wings; the empennage is detachably arranged at the tail end of the fuselage body; the first undercarriage is arrangedat the tail end of the fuselage body; the second undercarriage is arranged at the front end of the fuselage body; the rotary wings are detachably arranged at the two ends of each rotary wing connecting rod; the rear propeller is arranged at the tail end of the fuselage body; the rotary wing connecting rods and the rotary wings are fixed through second locking devices; all the components are connected in a quick detachable mode, so that the assembling and disassembling efficiency is remarkably improved; and in search and rescue, topographic survey and other occasions, the improvement of efficiency is very important.
本发明公开了一种快速组装的无人机,涉及飞行器技术领域。能够解决无人机组装与拆卸的费时费力的问题。一种快速组装的无人机包括机身主体、中央翼、旋翼连杆、外翼、尾翼、第一起落架、第二起落架、旋转翼及后置螺旋桨。中央翼可拆卸地设置在机身主体上。外翼可拆卸地设置在中央翼两侧。旋翼连杆设置在中央翼或外翼上。尾翼可拆卸地设置在机身主体末端。第一起落架设置在机身主体末端。第二起落架设置在机身主体前端。旋转翼可拆卸地设置在旋翼连杆两端。后置螺旋桨设置在机身主体末端。旋翼连杆与旋转翼通过第二锁紧装置固定。各部件均采用可快速拆卸式连接,组装与拆卸的效率得到显著提升。在搜救、地形勘察等场合,这样的效率提升至关重要。
Quickly-assembled unmanned aerial vehicle
一种快速组装的无人机
2020-09-15
Patent
Electronic Resource
Chinese
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