The present invention relates to a prefabricated airframe according to flight management, including: a main wing portion fixed to a fuselage; and an additional wing portion including a first wing portion and a second wing portion detachably coupled to left and right sides of the main wing portion, respectively, and configured to be additionally couplable between the main wing portion and the first wing portion and between the main wing portion and the second wing portion according to a flight environment of a prefabricated airframe.

    본 발명에 의한 비행 운용에 따른 조립식 기체에 있어서, 동체에 고정되는 주날개부, 상기 주날개부의 좌우 측면에 각각 착탈 가능하도록 결합되는 제1 날개부 및 제2 날개부를 포함하고, 상기 조립식 기체의 비행 환경에 따라 상기 주날개부와 상기 제1 날개부 사이 및 상기 주날개부와 상기 제2 날개부 사이에 추가적으로 결합될 수 있는 추가 날개부를 포함하는 것을 특징으로 한다.


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    Titel :

    Self-assembly aircraft of flight environment


    Weitere Titelangaben:

    비행 환경에 따른 조립식 기체


    Beteiligte:
    KIM JIN SUB (Autor:in) / CHANG BYUNG WOOK (Autor:in)

    Erscheinungsdatum :

    15.12.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

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



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