The present invention relates to an unmanned aerial vehicle with foldable wings, in which both side wings are folded, thereby being simply carried, and more specifically, to an unmanned aerial vehicle with foldable wings, in which the wings can be used by being taken out only in case of use while a plurality of rotors providing thrust to the unmanned aerial vehicle are rotated and the wings provided on both sides of the aerial vehicle are folded to be fixed to a main body, thereby being easily carried.
본 발명은 양측 날개를 접어 휴대가 간편해질 수 있는 접이식 날개를 구비한 무인항공기에 관한 것으로서, 보다 상세하게는 무인항공기의 추진력을 제공하는 복수개의 로터가 회전하면서 사용시에만 꺼내어 사용할 수 있고, 항공기의 양측에 구비된 날개를 접어 본체에 고정하여 휴대성이 용이해진 접이식 날개를 구비한 무인항공기에 관한 것이다.
Unmanned aerial vehicle of folding wing-type
접이식 날개를 구비한 무인항공기
2020-05-14
Patent
Electronic Resource
Korean
IPC: | B64C AEROPLANES , Flugzeuge |
Wing folding mechanism, unmanned aerial vehicle and wing folding method of unmanned aerial vehicle
European Patent Office | 2023
|Unmanned aerial vehicle wing folding mechanism and unmanned aerial vehicle
European Patent Office | 2022
|