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
2017-09-13
Patent
Electronic Resource
Korean
IPC: | B64C AEROPLANES , Flugzeuge |
Backward movement possible flight vehicle equipped fixed wing
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