To provide systems and methods for manufacturing wing panels for an aircraft wing.SOLUTION: An apparatus includes one or more panels. The one or more panels include an outer face sheet comprising a plurality of first composite materials, an inner face sheet comprising a plurality of second composite materials, and a plurality of foam pieces disposed between the outer face sheet and the inner face sheet, where the foam pieces reduce warping of the panels.SELECTED DRAWING: None

    【課題】航空機の主翼用の翼パネルを製造するためのシステム及び方法を提供する。【解決手段】1以上のパネルを含む装置であって、該1以上のパネルは、複数の第1の複合材料を含む外面シート、複数の第2の複合材料を含む内面シート、及び前記外面シートと前記内面シートとの間に配置された複数の発泡体片を含み、前記発泡体片は前記パネルの反りを低減させる、装置。【選択図】なし


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    Titel :

    COMPOSITE THIN WINGBOX ARCHITECTURE FOR SUPERSONIC BUSINESS JETS


    Weitere Titelangaben:

    超音速ビジネスジェット機用の複合材薄型主翼ボックスアーキテクチャ


    Beteiligte:

    Erscheinungsdatum :

    16.02.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Japanisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B29C Formen oder Verbinden von Kunststoffen , SHAPING OR JOINING OF PLASTICS



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