The present invention relates to a take-off and landing apparatus for an unmanned aerial vehicle, which includes: a fixed support part; a rotational support part installed on the fixed support part to be rotatable around a first direction; and a horizontal maintaining rotation part installed on the rotational support part to be rotatable around a second direction perpendicular to the first direction, having an upper portion on which a take-off and landing surface capable of take-off and landing of the unmanned aerial vehicle is installed, and having a lower portion on which the center of weight is positioned. Therefore, the take-off and landing apparatus for an unmanned aerial vehicle can be easily maintained.

    본 발명은 무인비행체의 이착륙장치에 관한 것으로, 고정지지부와, 고정지지부에 제1방향을 중심으로 회전가능하게 설치되는 회전지지부와, 회전지지부에 제1방향과 직각되는 제2방향을 중심으로 회전가능하게 설치되고, 상부에 무인비행체의 이착륙이 가능한 이착륙면이 형성되며, 무게 중심이 하부에 위치되는 수평유지회전부를 포함하는 것을 특징으로 한다.


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    Title :

    TAKEOFF AND LANDING APPARATUS FOR UNMANNED AERIAL VEHICLE


    Additional title:

    무인비행체의 이착륙장치


    Contributors:
    YONGHO JEON (author) / MOON GU LEE (author) / LEE BYUNG HUN (author)

    Publication date :

    2020-10-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Korean


    Classification :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / F16M Rahmen, Gehäuse oder Grundplatten von Kraftmaschinen oder anderen Maschinen oder von Apparaten, nicht auf eine besondere Art von Maschine oder Apparat eingeschränkt, die anderweitig vorgesehen ist , FRAMES, CASINGS, OR BEDS, OF ENGINES OR OTHER MACHINES OR APPARATUS, NOT SPECIFIC TO AN ENGINE, MACHINE, OR APPARATUS PROVIDED FOR ELSEWHERE




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