PROBLEM TO BE SOLVED: To provide a system and method for joining composite components which accommodates variations in contours of mating surfaces of the composite components while minimizing bondline thickness.SOLUTION: A method of forming a structural assembly may include providing a first component 300 and a second component 400 to be joined together. The method may additionally include scanning a contour of a first mating surface of the first component and scanning a contour of a second mating surface of the second component. The method may further include producing a thermoplastic element including a thermoplastic radius filler 512, having a first element surface 514 and a second element surface which oppose each other and substantially match the contour of the first mating surface and the contour the second mating surface.

    【課題】接着層厚さを最低限に抑えつつ複合材コンポーネントの合わせ面の外形におけるばらつきを調整する、複合材コンポーネントを接合するシステム及び方法を提供する。【解決手段】構造的アセンブリを形成する方法は、共接合させるために第1のコンポーネント300及び第2のコンポーネント400を提供することを含み得る。方法はさらに、第1のコンポーネント第1の合わせ面の外形をスキャンすること、及び、第2のコンポーネント第2の合わせ面の外形をスキャンすることを含み得る。方法はさらに、第1の合わせ面の外形と第2の合わせ面の外形とに実質的に一致する、対向する第1の素子表面514と第2の素子表面とを有する、熱可塑性半径充填材512を含む、熱可塑性素子を生産することを含み得る。【選択図】図22


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    Title :

    SYSTEM AND METHOD OF JOINING COMPONENTS


    Additional title:

    コンポーネントを接合するシステム及び方法


    Contributors:

    Publication date :

    2015-07-02


    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 / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / C09J ADHESIVES , Klebstoffe



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