The present invention relates to a drone equipped with a variable propulsion unit that can take off and land vertically and can improve propulsion by reducing air resistance during flight. According to the present invention, provided is a drone equipped with a variable propulsion unit, which comprises: a flying fuselage with fixed wings; and a variable propulsion unit removably coupled to the flying fuselage. The variable propulsion unit includes: a first variable propulsion portion which rotates to narrow the distance between each other to reduce air resistance in flight mode; and a second variable propulsion portion which rotates to exert lift and thrust.

    본 발명은 가변 추진 유니트가 장착된 드론에 관한 것이다. 본 발명은 고정익을 가지는 비행 동체; 상기 비행 동체에 착탈 가능하게 결합되는 가변 추진 유니트를 포함하고, 상기 가변 추진 유니트는, 비행 모드시 공기 저항을 줄일 수 있도록 서로 간의 간격이 좁혀지도록 회동하는 제1 가변 추진부, 양력과 추력을 발휘하도록 회동하는 제2 가변 추진부로 이루어지는 것을 특징으로 하는 가변 추진 유니트가 장착된 드론이 제공될 수 있다.


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    Title :

    Drone with Variable Propulsion Units


    Additional title:

    가변 추진 유니트가 장착된 드론


    Contributors:
    KO KUK WON (author) / BAE JEONG HWAN (author) / SHIN JAE HWAN (author) / YUM SEUNG YONG (author) / LIM DO YUN (author)

    Publication date :

    2021-03-10


    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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