Disclosed is a fuselage damage preventing vertical landing fixed wing flight vehicle, which allows a main wing coupled to a fuselage in a coupling manner of a protrusion and a groove so that impact more than or equal to certain pressure of the fuselage and the main wing is not transferred when the fuselage is hit by the land so that impact is applied thereto when an unmanned flight vehicle lands, thereby preventing the damage to the fuselage and the main wing.
무인비행체가 착륙 할 때 지면에 동체가 닿아 충격이 가해졌을 경우 주익이 동체에서 분리되어 동체 및 주익의 파손을 방지할 수 있게 구성되는 동체파손 방지형 수직착륙 고정익 비행체가 개시된다.
UNMANNED AERIAL VEHICLE FOR EASILY LANDING
동체파손 방지형 수직착륙 고정익 비행체
2019-12-09
Patent
Electronic Resource
Korean
IPC: | B64C AEROPLANES , Flugzeuge |
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