The present invention relates to a lift generation increasing duct unit provided in a drone, comprising: a propeller provided in a turbo shaft of a motor in a plurality of supports installed in an extra circumference of a drone main body; and a lift generation increasing cylinder provided with the propeller, wherein communicating pipes of the lift generation increasing duct unit installed in an upper portion of the drone main body and having the propeller driven by a central motor therein are connectively installed with the lift generation increasing cylinder, such that the lift generation increasing cylinder and the lift generation increasing duct unit are effectively generating lift for lifting the drone main body, and the drone main body can be easily lifted off and is able to transport a cargo having a predetermined weight thereby.

    본 발명은 드론본체의 가외둘레에 다수개로 설치된 지지대에 모터의 터보샤프트에 구비된 프로펠러와, 이 프로펠러가 구비된 양력발생증가통체와, 드론본체의 상부에 설치되고 내부에 중앙모터로 구동되는 프로펠러를 갖는 양력발생증가덕트부의 연통관들이 양력발생증가통체와 연계되게 설치되어 드론본체의 이륙을 위한 양력을 양력발생증가통체와 양력발생증가덕트부로 보다 효과적으로 발생하여 드론본체가 보다 쉽게 이륙하게 되고 드론본체로 소정의 무게를 갖는 화물을 운발할 수 있도록 한 드론에 구비된 양력발생증가덕부에 관한 것이다.


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    Titel :

    Duct part of drone


    Weitere Titelangaben:

    드론에 구비된 양력발생증가덕트부


    Beteiligte:
    KIM DONG MIN (Autor:in)

    Erscheinungsdatum :

    2018-12-13


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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