본 발명은 수직 이착륙 고정익 무인기에 관한 것으로 고정익을 가지는 기체, 상기 기체의 진행방향을 따라 상기 고정익을 가로질러 배치되고 상기 고정익의 양측에 평행하게 설치되는 회전익 지지부, 상기 회전익 지지부 상에 상호 대칭되게 배치되고 일부는 상기 기체의 최선단의 전방에 배치되는 복수의 회전익들, 및 상기 복수의 회전익들 각각에 결합되고 상기 복수의 회전익들을 특정 각도로 기울일 수 있는 틸트부를 포함한다. 따라서 수직 이착륙 고정익 무인기는 도약과 비행 메커니즘을 동시에 수행하여 장애물, 험지 등의 비정형 환경, 예를 들어 붕괴된 벽과 같은 재난 환경에서 신속하게 이동할 수 있다.

    The present invention relates to a vertical takeoff and landing unmanned aerial vehicle with fixed wings, which includes: a fuselage having the fixed wings; rotor support parts arranged across the fixed wings along a progress direction of the fuselage and installed on both sides of the fixed wings in parallel; a plurality of rotors which are arranged on the rotor support parts to be symmetrical to each other and of which a part is arranged at the front of the most front end of the fuselage; and a tilt part respectively coupled to the plurality of rotors and tilting the plurality of rotors at a specific angle. Accordingly, the vertical takeoff and landing unmanned aerial vehicle with the fixed wings performs leap and flight mechanism at the same time to be quickly moved in an atypical environment such as obstacles and rough places and a disaster environment such as a collapsed wall.


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    Title :

    VERYICAL TAKEOFF AND LANDING FIXED WING UNMANNED AERIAL VEHICLE


    Additional title:

    수직 이착륙 고정익 무인기


    Publication date :

    2020-07-17


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Korean


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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