본 발명은 멀티콥터에 관한 것으로, 본체부와, 일단부는 상기 본체부에 연결되고 타단부에는 프로펠러조립체가 연결되는 날개부와, 상기 날개부가 접어지도록 상기 날개부에 배치되는 접이부 및, 상기 본체부에 배치되고 지면에 안착되는 다리부를 포함하며, 본 발명에 따르면, 크기 축소, 분해/조립 및 운반/보관을 용이하게 할 수 있으며, 고중량 화물에 대한 페이로드값 향상, 장시간 비행 등이 가능하고, 전반적인 무게중심이 프로펠러의 하부에 위치하도록 하여 비행안정성을 높이는 효과가 있다.

    The present invention relates to a multicopter comprising: a main body portion; wing portions each having one end portion connected to the main body portion and the other end portion to which a propeller assembly is connected; a folding portion arranged on each wing portion so as to fold the wing portion; and a leg portion arranged on the main body portion and mounted on the ground. According to the present invention, size reduction, disassembly/assembly, and transport/storage can be easily executed, a payload value with respect to high weight cargo can be improved, a long-time flight is possible, and a general center of gravity is located at the lower part of the propeller to provide an effect of improving flying stability.


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    Title :

    MULTICOPTER


    Additional title:

    멀티콥터


    Publication date :

    2022-11-01


    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



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