According to one embodiment of the present invention, provided is a drone having a rotational inertia strengthening portion, which comprises: a drone main body; a rotational inertia strengthening unit installed in the drone main body; and a connecting unit connecting the drone main body to the rotational inertial strengthening unit. The rotational inertia strengthening unit can generate rotational inertia. Moreover, the moment of inertia of the drone can be increased by the rotational inertia so that flight stability of the drone can be increased.

    일 실시예에 따른 회전관성 증강부를 구비하는 드론은 드론 몸체, 상기 드론 몸체에 설치되는 회전관성 증강부, 및 상기 드론 몸체 및 상기 회전관성 증강부를 연결하는 연결부를 포함하고, 상기 회전관성 증강부는 회전관성을 생성하고, 상기 회전관성에 의해 상기 드론의 관성모멘트가 증가하는 효과를 통하여 상기 드론의 비행 안정성은 증대될 수 있다.


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    Titel :

    DRONE EQUIPPED WITH ROTATIONAL INERTIA REINFORCING STRUCTURE


    Weitere Titelangaben:

    회전관성 증강부를 구비하는 드론


    Beteiligte:
    KANG SUNG DUK (Autor:in) / JANG JONG TAI (Autor:in) / SEUNG MYEONG HUN (Autor:in) / GONG HYEON CHEOL (Autor:in)

    Erscheinungsdatum :

    2018-06-25


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / F16F SPRINGS , Federn



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