An unmanned aerial vehicle according to various embodiments of the present invention comprises: a main body; at least one connection frame connected to the main body; at least one propeller part connected to the connection frame; a driving part disposed in the connection frame; a heat dissipating structure coupled to the driving part and connected to the at least one propeller part; and an antenna module connected to the heat dissipating structure, wherein the driving part is disposed between the at least one propeller part and the antenna module to rotate the antenna module, and the heat dissipating structure covers at least a portion of the antenna module and uses air blown from the at least one propeller part to allow heat generated in the antenna module to be diffused into the air. Various other embodiments are also possible.

    La présente invention concerne un véhicule aérien sans pilote qui, selon divers modes de réalisation, comprend : un corps principal ; au moins un cadre de raccordement raccordé au corps principal ; au moins une partie hélice raccordée au cadre de raccordement ; une partie d'entraînement disposée dans le cadre de raccordement ; une structure de dissipation de chaleur accouplée à la partie d'entraînement et raccordée à la ou aux parties hélices ; et un module d'antenne raccordé à la structure de dissipation de chaleur, la partie d'entraînement étant disposée entre la ou les parties hélices et le module d'antenne pour mettre en rotation le module d'antenne, et la structure de dissipation de chaleur recouvre au moins une partie du module d'antenne et utilise l'air soufflé à partir de la ou des parties hélices pour permettre à la chaleur générée dans le module d'antenne d'être diffusée dans l'air. Divers autres modes de réalisation sont également possibles.

    본 발명의 다양한 실시예들은 무인 비행체에 있어서, 본체; 상기 본체에 연결된 하나 이상의 연결 프레임; 상기 연결 프레임에 연결된 하나 이상의 프로펠러부; 상기 연결 프레임에 배치된 구동부; 상기 구동부에 결합되고, 상기 하나 이상이 프로펠러부와 연결된 방열 구조체; 및 상기 방열 구조체에 연결된 안테나 모듈을 포함하고, 상기 구동부는 상기 하나 이상의 프로펠러부와 상기 안테나 모듈 사이에 배치되어서, 상기 안테나 모듈을 회전시키고, 상기 방열 구조체는 상기 안테나 모듈의 적어도 일부를 감싸며, 상기 하나 이상의 프로펠러부에서 송풍된 공기를 이용하여 상기 안테나 모듈에 발생한 열을 공중으로 확산시킬 수 있다. 그 밖에 다양한 실시예들이 가능하다.


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    Title :

    UNMANNED AERIAL VEHICLE INCLUDING ANTENNA MODULE


    Additional title:

    VÉHICULE AÉRIEN SANS PILOTE COMPRENANT UN MODULE D'ANTENNE
    안테나 모듈을 포함하는 무인 비행체


    Contributors:
    KIM YONGHWA (author) / YOON YEONGGYU (author) / LEE YONGSUK (author) / CHOI HEESEUNG (author) / NA HYOSEOK (author) / YOON BYOUNGUK (author)

    Publication date :

    2020-12-17


    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 / H01Q Antennen , ANTENNAS, i.e. RADIO AERIALS



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