길이방향 띠형 창영역부를 가진 동체는 상부 및 하부 복합 스킨 섹션을 포함하는 복합 외부 스킨을 갖는다. 스킨은 띠형 창영역부에 위치되는 적어도 하나의 창 개구부를 포함한다. 상부 및 하부 스킨 섹션은 띠형 창영역부에 위치된 길이방향 이음 조인트부에 의해 함께 결합된다.

    A fuselage having a longitudinal window belt (58) has a composite outer skin including upper and lower composite skin sections (52, 54). The skin includes at least one window opening (70) located at the window belt (58). The upper and lower skin sections are joined together by a longitudinal splice joint (56) located at the window belt (58).


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    Titel :

    JOINING COMPOSITE FUSELAGE SECTIONS ALONG WINDOW BELTS


    Weitere Titelangaben:

    복합 동체 섹션들을 띠형 창영역부들을 따라 결합한 동체 및 이의 제작방법


    Erscheinungsdatum :

    2019-11-13


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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