Provided, in the present invention, is an aerial unmanned aircraft comprising: a main body including first to third frames arranged at predetermined intervals, a loading part formed through the first to third frames for loading an object, and an opening and closing part for opening and closing the loading part; an imaging part including a camera provided at a front, a lower, and a rear respectively, with respect to a flying direction of the main body for dropping the object placed on the loading part to a target point; a dropping control part for controlling an opening/closing part for dropping an object placed on the loading part in accordance with an image information of the imaging part; a moving part including a plurality of propellers; and a landing part for supporting the main body during take-off and landing, and the object is dropped from the loading part at the same time or at a different time by the dropping control part.

    본 발명은 소정간격 떨어져 배치된 제1 내지 제3 프레임, 물체를 적재하기 위해 제1 내지 제3 프레임을 관통하여 형성된 적재부, 적재부를 개폐하기 위한 개폐부를 포함하는 본체; 적재부에 적재된 물체를 목표지점에 투하하기 위해 본체의 비행방향에 대해 전방, 하방 및 후방에 각각 마련된 카메라를 포함하는 영상부; 영상부의 영상정보에 따라 적재부에 적재된 물체를 투하하기 위한 개폐부를 제어하는 투하 제어부; 복수 개의 프로펠러를 포함하는 이동부; 이착륙 시 본체를 지지하기 위한 랜딩부; 를 포함하며, 물체는 투하 제어부에 의해 적재부로부터 동시 또는 시간차를 두어 각각 투하되는 것을 포함하는 공중 투하 무인항공기를 제공하고자 한다.


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    Title :

    MULTI PURPOSE AIRDROP UNMANNED AERIAL VEHICLE


    Additional title:

    다목적 공중 투하 무인항공기


    Contributors:

    Publication date :

    2019-01-07


    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 / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen



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