PROBLEM TO BE SOLVED: To provide a method for assembling a composite material structure particularly regarding the production of a composite material article.SOLUTION: A first laminated body 206 formed by first composite material layers 204 and further including a first hardened part 208 and a first un-hardened part 210; and a second laminated body 216 formed by a second composite material layer 214 and further including a second hardened part 218 and a second un-hardened part 220 are prepared. In the method for joining them, at first, at least one of the first composite material layers 204 in the first un-hardened part 210 is inserted into the second composite material layer 214 in the second un-hardened part 220 so as to form a joined region 256. Then, the joined region 256 is hardened, thus the first laminated body 206 and the second laminated body 216 are joined to form an integrated composite material assembly.SELECTED DRAWING: Figure 11
【課題】複合材品の製造に関し、特に、複合材料構造体を組み立てるための方法を提供する。【解決手段】第1複合材料層204によって形成されると共に第1硬化部分208及び第1未硬化部分210を有する第1積層体206と、第2複合材料層214によって形成されるとともに第2硬化部分218及び第2未硬化部分220を有する第2積層体216とを用意する。これらを接合する方法は、まず、接合領域256を形成すべく、第1未硬化部分210内の第1複合材料層204のうちの少なくとも1つを、第2未硬化部分220内の第2複合材料層214に挟み込み配置する。そして、接合領域256を硬化することによって、第1積層体206を第2積層体216と接合し、一体複合材料アセンブリを形成する。【選択図】図11
CO-HARDENING PROCESS FOR JOINING COMPOSITE MATERIAL STRUCTURE
複合材料構造体を接合するための共硬化プロセス
29.09.2016
Patent
Elektronische Ressource
Japanisch
IPC: | B29C Formen oder Verbinden von Kunststoffen , SHAPING OR JOINING OF PLASTICS / B64C AEROPLANES , Flugzeuge / 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 |
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