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Mechanical Properties of Carbon Fiber Reinforced Thermoplastic Matrix Composites
https://jaxa.repo.nii.ac.jp/records/45193
https://jaxa.repo.nii.ac.jp/records/451934e42fb31-3293-40c4-83de-697baa7d0249
| 名前 / ファイル | ライセンス | アクション |
|---|---|---|
naltr00934.pdf (1.4 MB)
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| Item type | テクニカルレポート / Technical Report(1) | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|
| 公開日 | 2015-03-26 | |||||||||
| タイトル | ||||||||||
| タイトル | Mechanical Properties of Carbon Fiber Reinforced Thermoplastic Matrix Composites | |||||||||
| 言語 | en | |||||||||
| 言語 | ||||||||||
| 言語 | eng | |||||||||
| 資源タイプ | ||||||||||
| 資源タイプ識別子 | http://purl.org/coar/resource_type/c_18gh | |||||||||
| 資源タイプ | technical report | |||||||||
| その他のタイトル | ||||||||||
| その他のタイトル | 炭素繊維織物強化熱可塑性複合材料の力学的特性試験 | |||||||||
| 著者 |
野口, 義男
× 野口, 義男
× NOGUCHI, Yoshio
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| 著者所属 | ||||||||||
| 航空宇宙技術研究所機体第一部 | ||||||||||
| 著者所属（英） | ||||||||||
| en | ||||||||||
| First Airframe Division, National Aerospace Laboratory(NAL) | ||||||||||
| 出版者 | ||||||||||
| 出版者 | 航空宇宙技術研究所 | |||||||||
| 出版者（英） | ||||||||||
| 出版者 | National Aerospace Laboratory(NAL) | |||||||||
| 書誌情報 |
航空宇宙技術研究所報告 en : Technical Report of National Aerospace Laboratory TR-934 巻 934, p. 14, 発行日 1987-06 |
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| 抄録（英） | ||||||||||
| 内容記述タイプ | Other | |||||||||
| 内容記述 | Carbon fiber reinforced thermoplastic (CFRTP) composites have a great potential for use in aircraft structures especially where toughness is concerned. In this study, experiments are conducted on a fabric-CFRTP and fabric-CFRP composites subjected to the effect of elevated temperature on short beam shear strength and flexural fatigue strength. Composite were fabricated from carbon fiber 8-harness satin fabric reinforced with two thermoplastic matrices, polyethersulphon (PES) and polyetheretherketon (PEEK) and compared with those of an epoxy matrix system. The CFRTP laminates were prepared by the film stacking method, namely thermoplastic resin films and carbon fiber fabric were stacked altermately then consolidated into a laminate by heat and pressure. Short beam shear tests were performed under environmental conditions at temperatures of 25C to 180C. Flexural fatigue tests were performed at a room temperature of 25C and elevated temperatures of 80～90C and 130～140C. Short beam shear strength under elevated temperature conditions for fabric-CFRTP is comparable to that obtained with most fabric-CFRP. The fatigue failure specimens indicated that the tough thermoplastic matrix system shows an improved fatigue behavior compared to the brittle epoxy matrix system, mainly due to resistance to the initiation and growth of fatigue damage related to the matrix. | |||||||||
| ISSN | ||||||||||
| 収録物識別子タイプ | ISSN | |||||||||
| 収録物識別子 | 0389-4010 | |||||||||
| 資料番号 | ||||||||||
| 内容記述タイプ | Other | |||||||||
| 内容記述 | 資料番号: NALTR0934000 | |||||||||
| レポート番号 | ||||||||||
| 内容記述タイプ | Other | |||||||||
| 内容記述 | レポート番号: NAL TR-934 | |||||||||
