Development of moldable CNT / polyimide composites having high heat-resistance and high strength
| Project/Area Number |
15K06610
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| Research Category |
Grant-in-Aid for Scientific Research (C)
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| Allocation Type | Multi-year Fund |
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| Section | 一般 |
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| Research Field |
Aerospace engineering
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| Research Institution | Japan Aerospace EXploration Agency |
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Principal Investigator |
Ishida Yuichi 国立研究開発法人宇宙航空研究開発機構, 航空技術部門, 主任研究開発員 (20371114)
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| Co-Investigator(Kenkyū-buntansha) |
小笠原 俊夫 東京農工大学, 工学(系)研究科(研究院), 教授 (20344244)
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| Project Period (FY) |
2015-04-01 – 2018-03-31
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| Project Status |
Completed (Fiscal Year 2017)
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| Budget Amount *help |
¥4,550,000 (Direct Cost: ¥3,500,000、Indirect Cost: ¥1,050,000)
Fiscal Year 2017: ¥1,430,000 (Direct Cost: ¥1,100,000、Indirect Cost: ¥330,000)
Fiscal Year 2016: ¥1,690,000 (Direct Cost: ¥1,300,000、Indirect Cost: ¥390,000)
Fiscal Year 2015: ¥1,430,000 (Direct Cost: ¥1,100,000、Indirect Cost: ¥330,000)
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| Keywords | ナノコンポジット / ポリイミド / カーボンナノチューブ / 耐熱複合材 / ナノ複合材 |
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| Outline of Final Research Achievements |
An aligned CNT composites based on thermosetting polyimide TriA-X, thermoplastic polyimide ISAS-TPI, and these blends were prepared and evaluated. In the resin film infusion method, it was impossible to sufficiently impregnate because of its high melt viscosity. In the polyimide solution prepreg route, an aligned CNT / polyimide composites having a thickness of 0.02 to 0.1 mm could be prepared. The aligned CNT / polyimide composites showed significant improvements in tensile strength and modulus compared with resin.
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Report
(4 results)
Research Products
(1 results)
