To provide a method for fabricating a composite wing structural component for an aircraft.SOLUTION: The method comprises extruding a filler material into each mold channel of a plurality of mold channels of a die to form a plurality of filler segments, removing the plurality of filler segments from the plurality of mold channels of the die, and arranging the plurality of filler segments in a space in the composite structural component, the space being defined by an R part of the composite structural component, such that the filler segments are in end-to-end contact. The method further comprises curing the plurality of filler segments in the space to fuse the plurality of filler segments.SELECTED DRAWING: None

    【課題】航空機用の複合翼構造用構成要素を製造するための方法を提供する。【解決手段】複数の充填材セグメントを形成するために、充填材をダイの複数の金型チャネルの各金型チャネルに押し出すこと、ダイの複数の金型チャネルから複数の充填材セグメントを取り除くこと、及び複数の充填材セグメントを複合材の構造用構成要素の空間に配置することであって、前記充填材セグメントがエンドツーエンドで接触するよう、空間が複合材の構造用構成要素のR部によって画定される、複数の充填材セグメントを複合材の構造用構成要素の空間に配置することを含む。本方法は、複数の充填材セグメントを融合するために、空間で複数の充填材セグメントを硬化することをさらに含む。【選択図】なし


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    Title :

    AIRCRAFT COMPRISING COMPOSITE STRUCTURAL COMPONENT, AND METHOD FOR FORMING COMPOSITE STRUCTURAL COMPONENT


    Additional title:

    複合材の構造用構成要素を備えた航空機、及び複合材の構造用構成要素を形成するための方法


    Contributors:

    Publication date :

    2021-04-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

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



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