| 缝合碳纤维缎纹织物复合材料研究 |
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| 引用本文： | 郭扬,宫少波,邢福军.缝合碳纤维缎纹织物复合材料研究[J].航空材料学报,2006,26(3):343-344. |
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| 作者姓名： | 郭扬 宫少波 邢福军 |
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| 作者单位： | 1. 北京航空材料研究院,北京,100095
2. 哈尔滨航空工业集团公司,哈尔滨,150006 |
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| 摘 要： | 使用高强度玻璃纤维缝合G803-T300-40B五枚缎纹碳纤维织物预制体,并用树脂膜熔融渗透(RFI)工艺成型复合材料.测试了改性环氧树脂胶膜熔体粘度对固化温度和时间的依赖性,将缝合与未缝合复合材料层合板试样的基本力学性能进行了试验对比.
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| 关 键 词： | 缝合复合材料 RFI 碳纤维预制体 |
| 文章编号： | 1005-5053(2006)03-0343-02 |
| 修稿时间： | 2006年1月20日 |
Study on Stitched Carbon Fabric Satin Weave Composites |
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| GUO Yang,GONG Shao-bo,XING Fu-jun.Study on Stitched Carbon Fabric Satin Weave Composites[J].Journal of Aeronautical Materials,2006,26(3):343-344. |
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| Authors: | GUO Yang GONG Shao-bo XING Fu-jun |
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| Abstract: | Layers of dry carbon fabric satin weave G803-T300-40B were stacked and stitched through the thickness with high strength glass threads.RFI of perform with modified epoxy resin followed by autoclave curing process.Viscosity of the RFI resin film as a function of curing temperature and time were tested respectively.The mechanical properties of stitched and unstitched composite laminates were evaluated. |
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| Keywords: | stitching composites RFI carbon fabric perform |
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