To provide a method for manufacturing a composite structure.SOLUTION: A first section (108) for a composite structure is formed. At this time, a first end (112) of the first section has a chevron shape (114), and a first composite layer (128) included in the first section configures a first step pattern (118) at the first end. A second section (110) for the composite structure is formed. At this time, a second end (120) of the second section has a counterpart shape (141) for the chevron shape, and a second composite layer (124) included in the second section configures a second step pattern (126) at the second end. The first and second ends are positioned so that the first composite layer included in the first step pattern overlaps the second composite layer included in the second step pattern in a splice position (132).SELECTED DRAWING: Figure 1

    【課題】複合構造体の作製方法の提供。【解決手段】複合構造体の第1セクション(108)を形成し、この際に、第1セクションの第1端部(112)がシェブロン形状(114)を有し、第1セクションに含まれる第1複合レイヤ(128)が、第1端部に第1階段状パターン(118)を構成する。複合構造体の第2セクション(110)を形成し、この際に、第2セクションの第2端部(120)が、シェブロン形状の相手側形状(141)を有し、第2セクションに含まれる第2複合レイヤ(124)が、第2端部に第2階段状パターン(126)を構成するようにする。第1階段状パターンに含まれる第1複合レイヤが、第2階段状パターンに含まれる第2複合レイヤと、スプライス位置(132)で重なり合うように、第1端部及び第2端部を配置する。【選択図】図1


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    Title :

    SPLICE FOR COMPOSITE STRUCTURE AND METHOD FOR MANUFACTURING COMPOSITE STRUCTURE


    Additional title:

    複合構造体のスプライス及びその方法


    Contributors:

    Publication date :

    2019-11-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B29C Formen oder Verbinden von Kunststoffen , SHAPING OR JOINING OF PLASTICS / B32B LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM , Schichtkörper, d.h. aus Ebenen oder gewölbten Schichten, z.B. mit zell- oder wabenförmiger Form, aufgebaute Erzeugnisse / B64C AEROPLANES , Flugzeuge




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