본 발명은 비행 중 추락의 위험성이 감지되면 동체의 측방으로 전개된 후 추락하는 동체의 상측으로 위치가 변화되는 낙하산이 구비된 무인 비행체에 관한 것이다. 본 발명에 의한 낙하산이 구비된 무인 비행체는 복수 개의 회전익으로 구성되는 무인 비행체의 하부에 장착되고, 외부로 전개되는 낙하산이 내부에 구비되며, 일측이 개방된 통형의 본체 부재와 무인 비행체의 현재 상태를 감지하는 추락 감지 유닛과 본체 부재를 개방시키는 모터 부재를 포함하여 구성되는 것을 특징으로 한다.

    The present invention relates to an unmanned aerial vehicle equipped with a parachute. When a risk of falling during flying is detected, the unmanned aerial vehicle equipped with a parachute is stretched to a side direction of a fuselage and a position thereof is changed to the top of the fuselage. The unmanned aerial vehicle equipped with a parachute comprises: a cylindrical main body member installed in a lower portion of the unmanned aerial vehicle composed of a plurality of rotation blades, provided with a parachute stretched to the outside therein, and having one side thereof opened; a falling detection unit for detecting a current state of the unmanned aerial vehicle; and a motor member for opening the main body member.


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    Titel :

    Unmanned air vehicle equipped parachute


    Weitere Titelangaben:

    낙하산이 구비된 무인 비행체


    Erscheinungsdatum :

    29.03.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    F16H Getriebe , GEARING / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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