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Repair of Impact Damage by Thermal Fusion Bonding and Recovery of Residual Compressive Strength on CF/PA6 Laminates

机译：CF / PA6层压板的热熔熔接和剩余抗压强度恢复的抗冲击损伤修复

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Manato KANESAKI; Chika UCHIJO; Mototsugu TANAKA; Hiroshi SAITO; Masaaki NISHIKAWA; Masaki HOJO; Isao KIMPARA;
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年度 2015
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1. Effects of Repair Temperature and Duration in Thermal Fusion Bonding on Interlaminar Shear Strength of Delaminated CF/PA6 Laminates [J] . Takatoshi UEDA, Takumi MATSUMOTO, Manato KANESAKI, Advanced Experimental Mechanics . 2018,第4期

机译：修复温度和热熔合时间对分层CF / PA6层合板层间剪切强度的影响
2. Simplified and Unified Approach to Characterization of Compressive Residual Strength of Impact-Damaged CFRP Laminates [J] . I. Kimpara, K. Kageyama, T. Suzuki Key Engineering Materials . 1998,第Part期

机译：冲击损伤的CFRP层压板抗压残余强度表征的简化统一方法
3. Residual strength of a damaged laminated CFRP under compressive fatigue stresses [J] . M. De Freitas, R. De Carvalho Composites Science and Technology . 2006,第3a4期

机译：压缩疲劳应力作用下受损的层压CFRP的残余强度
4. REPAIR OF CF/PA6 LAMINATES BELOW MELTING POINT WITH BARELY VISIBLE IMPACT DAMAGE [C] . M. Kanesaki, C. Uchijo, M. Tanaka, International Conference on Composite Materials . 2013

机译：使用几乎可见的影响损伤，修复熔点以下熔点以下的层压板
5. Residual compressive strength prediction of carbon/epoxy laminates subjected to low velocity impact damage. [D] . Hess, Christopher D. 2003

机译：碳/环氧层压板受到低速冲击破坏后的残余抗压强度预测。
6. Correlation between Drop Impact Energy and Residual Compressive Strength According to the Lamination of CFRP with EVA Sheets [O] . Sun-Ho Go, Min-Sang Lee, Chang-Gi Hong, 2020

机译：CFRP与EVA片材层压时液滴冲击能量与残余抗压强度的相关性
7. Residual Compressive Strength of CFRP Laminate Damaged by Impact Loading. Effects of stacking sequence and impact velocity. [O] . Haruo ISHIKAWA, Tadashi NATSUMURA, Yasuyuki TANAKA, 1992

机译：CFRP层压材料的残留抗压强度受冲击载荷损坏。堆叠序列和冲击速度的影响。
8. Relevance of impacter shape to nonvisible damage and residual tensile strength of a thick graphite/epoxy laminate [R] . Poe, C. C., Jr. 1990

机译：冲击器形状与厚石墨/环氧树脂层压板的非可见损伤和残余抗拉强度的相关性

Repair of Impact Damage by Thermal Fusion Bonding and Recovery of Residual Compressive Strength on CF/PA6 Laminates

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