The present invention relates to a flight vehicle equipped with a fixed wing, wherein a shape and a flight direction of the flight vehicle by rotating a wing after adjusting an angle of the wing during a flight to rapidly raise a fuselage. According to the present invention, a backward movable flight vehicle comprises: a body unit forming a body of the flight vehicle; a long wing unit rotationally coupled to a first rotating shaft individually protruding to one side and the other side of the body unit; and a short wing unit spaced from the first rotating shaft, and rotationally coupled to a second rotating shaft individually protruding to one side and the other side of the body unit.
본 발명은 비행 중 날개의 각도를 조절하여 동체를 급격하게 상승시킨 후 날개를 회전시킴으로써 비행체의 형상 및 비행 방향이 전환되는 고정익 비행체에 관한 것이다. 본 발명에 의한 후진 가능한 비행체는 비행체의 몸체를 구성하는 본체부와 본체부의 일측 및 타측 방향으로 각각 돌출되는 제1 회전축에 회전 가능하도록 체결되는 장익부와 제1 회전축과 이격되어, 본체부의 일측 및 타측 방향으로 각각 돌출되는 제2 회전축에 회전 가능하도록 체결되는 단익부를 포함하여 구성되는 것을 특징으로 한다.
Backward movement possible flight vehicle equipped fixed wing
후진 가능한 고정익 비행체
13.09.2017
Patent
Elektronische Ressource
Koreanisch
IPC: | B64C AEROPLANES , Flugzeuge |
Backward movement possible flight vehicle equipped fixed wing
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