An unmanned aerial vehicle and an automatic charging device for the unmanned aerial vehicle are disclosed. In one embodiment, the unmanned aerial vehicle comprises a main body and a connection part. The main body includes: a battery; and a flight power providing part driven by power provided from the battery, thereby generating flight power. The connection part includes a first charging terminal and a second charging terminal arranged in the main body, and respectively and electrically connected to different polarities of the battery. The first charging terminal and the second charging terminal are arranged so as to be spaced from each other on the outer surface of the connection part, wherein at least a portion of the connection part, hereinafter, referred to as an insertion part, is inserted into a recessed part formed on a charging platform during a process in which the main body is loaded on the charging platform. During a process in which the insertion part is inserted into the recessed part, the first charging terminal and the second charging terminal are electrically connected to a first electrode and a second electrode arranged to be spaced from each other on the charging platform. Each of the first charging terminal and the second charging terminal is electrically connected to the first electrode and the second electrode such that the battery can be charged by receiving electrical energy from the charging platform.

    L'invention concerne un véhicule aérien sans pilote et un dispositif de charge automatique pour le véhicule aérien sans pilote. Dans un mode de réalisation, le véhicule aérien sans pilote comprend un corps principal et une partie de connexion. Le corps principal comprend : une pile ; une partie de fourniture d'énergie de vol entraînée par l'énergie fournie par la pile, générant ainsi une énergie de vol. La partie de connexion comprend une première borne de charge et une seconde borne de charge disposées dans le corps principal, respectivement et électriquement connectées à différentes polarités de la pile. La première borne de charge et la seconde borne de charge sont agencées de manière à être espacées l'une de l'autre sur la surface externe de la partie de connexion, au moins une partie de la partie de connexion, ci-après appelée partie d'insertion, est insérée dans une partie renfoncée, formée sur une plate-forme de charge pendant un processus dans lequel le corps principal est chargé sur la plate-forme de charge. Au cours d'un processus dans lequel la partie d'insertion est insérée dans la partie renfoncée, la première borne de charge et la seconde borne de charge sont électriquement connectées à une première électrode et à une seconde électrode agencées afin d'être espacées l'une de l'autre sur la plate-forme de charge. Chacune de la première borne de charge et de la seconde borne de charge est électriquement connectée à la première électrode et à la seconde électrode de telle sorte que la pile peut être chargée par réception d'énergie électrique provenant de la plate-forme de charge.

    무인항공기 및 무인항공기 자동충전장치가 개시된다. 일 실시 예에 있어서, 상기 무인항공기는 본체 및 접속부를 포함한다. 상기 본체는 배터리와 상기 배터리로부터 제공되는 전원에 의하여 구동되어 비행력을 발생시키는 비행력 제공부를 포함한다. 상기 접속부는 상기 본체에 배치되며, 상기 배터리의 서로 다른 극성과 각각 전기적으로 연결되는 제1충전단자 및 제2충전단자를 포함한다. 상기 제1충전단자 및 상기 제2충전단자는 상기 접속부의 외면에 서로 이격되어 배치된다. 이 경우, 상기 접속부의 적어도 일부-이하 삽입부라 함-는 상기 본체가 충전플랫폼에 안착되는 과정에서 상기 충전플랫폼에 형성되는 함몰부에 삽입된다. 상기 삽입부가 상기 함몰부에 삽입되는 과정에서 상기 제1충전단자 및 상기 제2충전단자는 상기 충전플랫폼에 서로 이격되어 배치되는 제1전극 및 제2전극과 전기적으로 연결된다. 상기 제1충전단자 및 상기 제2충전단자 각각이 상기 제1전극 및 상기 제2전극과 전기적으로 연결됨으로써 상기 배터리는 상기 충전플랫폼으로부터 전기에너지를 공급받아 충전될 수 있다.


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    Title :

    UNMANNED AERIAL VEHICLE AND AUTOMATIC CHARGING DEVICE FOR UNMANNED AERIAL VEHICLE


    Additional title:

    VÉHICULE AÉRIEN SANS PILOTE ET DISPOSITIF DE CHARGE AUTOMATIQUE POUR VÉHICULE AÉRIEN SANS PILOTE
    무인항공기 및 무인항공기 자동충전장치


    Contributors:
    KIM DAE NYEON (author) / KIM SANG SIK (author) / LEE DONG HYUK (author) / KIM HYO SU (author) / KIM JAE WOOK (author)

    Publication date :

    2018-04-12


    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 / H02J CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER , Schaltungsanordnungen oder Systeme für die Abgabe oder Verteilung elektrischer Leistung



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