COMPOSITE MATERIAL

To provide composite materials with excellent heat resistance.SOLUTION: A composite with a plurality of stacked layers, a plurality of fibers arranged in parallel in the interior of the layers in a direction orthogonal to the thickness direction of the layers, the fibers arranged in the nth layer an...

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Bibliographische Detailangaben
Hauptverfasser:	OKUYAMA KEIICHI, IMAICHI CHIAKI, NAKANISHI TOMOAKI, MINAMIDATE JUN, TSUNODA JUNICHI
Format:	Patent
Sprache:	eng ; jpn
Schlagworte:	AEROPLANES AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F,C08G AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING AIRCRAFT AVIATION CHEMISTRY COMPOSITIONS BASED THEREON COSMONAUTICS GENERAL PROCESSES OF COMPOUNDING HELICOPTERS LAYERED PRODUCTS LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT ORNON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM METALLURGY ORGANIC MACROMOLECULAR COMPOUNDS PERFORMING OPERATIONS SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR SHAPING OR JOINING OF PLASTICS THEIR PREPARATION OR CHEMICAL WORKING-UP TRANSPORTING WORKING OF PLASTICS WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL WORKING-UP
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Beschreibung
Zusammenfassung:	To provide composite materials with excellent heat resistance.SOLUTION: A composite with a plurality of stacked layers, a plurality of fibers arranged in parallel in the interior of the layers in a direction orthogonal to the thickness direction of the layers, the fibers arranged in the nth layer and the fibers arranged in the n+1 layer cross each other, n is a positive integer, and the layers have a matrix resin including thermoplastic resin and a porosity of 3% to 20%.SELECTED DRAWING: Figure 1 【課題】耐熱性に優れる複合体を提供する。【解決手段】積層された複数の層と、上記層の内部に、上記層の厚さ方向と直交する方向に並列配置された複数本の繊維と、を備え、ｎ層目の上記層に配置された上記繊維と、ｎ＋１層目の上記層に配置された上記繊維とが交差しており、ただし、ｎは正の整数であり、上記層は、熱可塑性樹脂を含むマトリックス樹脂を有し、空隙率が３％以上２０％以下である、複合体。【選択図】図１