The present invention relates to a drone with folding propellers, the drone comprising: a main body; first propeller parts in which a plurality of first driving arms are rotatably coupled to the upper surface of the main body and are inserted into the upper surface of the main body or withdrawn to the outside; and a cover part, which is coupled to the upper surface of the main body so as to be movable in the vertical direction, has a space part formed at the lower end thereof so that the inserted first propeller parts can be covered when the cover part is positioned at the lower side, and moves upward so that the first propeller parts can be withdrawn. Therefore, the first propeller parts are rotatably coupled to the upper surface of the main body and are inserted into and withdrawn from same, and the cover part is coupled to the upper surface of the main body so as to be movable in the vertical direction, and thus the first propeller parts are inserted into the cover part according to the rotation of the first propeller parts and the movement of the cover part so that the effects of enabling volume to be minimized when the drone is parked or stored and enabling damage to propellers to be prevented can be obtained.

    La présente invention se rapporte à un drone ayant des hélices pliantes, le drone comprenant : un fuselage principal ; des premières parties d'hélice dans lesquelles une pluralité de premiers bras d'entraînement sont couplés en rotation à la surface supérieure du fuselage principal et sont insérés dans la surface supérieure du fuselage principal ou retirés vers l'extérieur ; et une partie de couvercle, qui est couplée à la surface supérieure du fuselage principal de façon à être mobile dans la direction verticale, qui comporte une partie d'espace formée au niveau de l'extrémité inférieure de celui-ci de telle sorte que les premières parties d'hélice insérées puissent être recouvertes lorsque la partie de couvercle est positionnée au niveau du côté inférieur, et qui se déplace vers le haut de telle sorte que les premières parties d'hélice puissent être retirées. Par conséquent, les premières parties d'hélice sont couplées en rotation à la surface supérieure du fuselage principal et sont insérées dans celles-ci et retirées de celle-ci, et la partie de couvercle est couplée à la surface supérieure du fuselage principal de façon à être mobile dans la direction verticale, et ainsi les premières parties d'hélice sont insérées dans la partie de couvercle en fonction de la rotation des premières parties d'hélice et du mouvement de la partie de couvercle de telle sorte que les effets d'activation du volume puissent être réduits à un minimum lorsque le drone est stationné ou stocké et permettant d'empêcher un endommagement des hélices.

    본 발명은 날개 접이식 드론에 관한 것으로, 드론에 있어서, 본체; 상기 본체의 상면에 복수의 제1 구동암이 각각 회전 가능하게 결합되어 상기 본체의 상면에 인입되거나 외부로 인출되는 제1 날개부; 및 상기 본체의 상면에 상하 방향으로 이동 가능하게 결합되고, 하방에 위치 시 인입된 상기 제1 날개부의 덮을 수 있도록 하단에 공간부가 형성되며, 상기 제1 날개부가 인출 가능하도록 상방에 이동되는 커버부;를 포함한다. 이러한 구성으로, 본체의 상면에 제1 날개부가 회전 가능하게 결합되어 인입출되고, 본체의 상면에 상하 방향으로 이동 가능하도록 커버부가 결합됨으로써, 제1 날개부의 회전 및 커버부의 이동에 따라 제1 날개부가 커버부 내에 인입됨에 따라 주차하거나 보관 시 부피를 최소화할 수 있을 뿐만 아니라, 날개의 손상을 방지할 수 있는 효과를 얻을 수 있다.


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    Title :

    DRONE WITH FOLDING PROPELLERS


    Additional title:

    DRONE AYANT DES HÉLICES PLIANTES
    날개 접이식 드론


    Contributors:

    Publication date :

    2024-10-31


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Korean


    Classification :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge



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