The present invention relates to a drone, which may comprise: a frame; a plurality of rotor blades (100) which rotate to generate lift of the frame; a motor (110) for driving the rotor blade (100); and a battery (120) for supplying power to the motor (110). The motor (110) or the battery (120) may be installed below the rotor blade (100) with respect to the frame. The present invention can improve the resilience by lowering the center of gravity (C0) of the drone, improve flight stability, and reduce energy consumption required for posture control.

    본 발명의 드론은, 프레임; 상기 프레임의 양력을 발생하도록 회전하는 복수의 회전익(100); 상기 회전익(100)을 구동하는 모터(110); 상기 모터(110)에 전원을 공급하는 배터리(120);를 포함할 수 있다. 상기 모터(110) 또는 상기 배터리(120)는 상기 프레임에 대하여 상기 회전익(100)보다 하부에 설치될 수 있다.


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    Titel :

    HIGH EFFICIENCY DRONE WITH A LOW GRAVITY CENTER


    Weitere Titelangaben:

    저중심 고효율 드론


    Beteiligte:
    LEE DONG GU (Autor:in) / SEONG I CHANG (Autor:in) / HONG JONG MIN (Autor:in) / OH HYEON DO (Autor:in) / LEE HYEON HA (Autor:in) / MO SEONG RYEOL (Autor:in)

    Erscheinungsdatum :

    04.06.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

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



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