Zhang J, Yang T, Lin T, et al. Phase morphology of nanofibre interlayers: critical factor for toughening carbon/epoxy composites[J]. Composites Science and Technology, 2012, 72(2): 256-262.
[2]
邹 科, 龙云泽, 吴佑实. 静电纺丝制备纳米纤维的进展及应用[J]. 合成纤维工业, 2007, 30(3): 54-57. Zou Ke, Long Yunze, Wu Youshi. Progress and application of electrospun nanofibers[J]. China Synthetic Fiber Industry, 2007, 30(3): 54-57.
Hamer S, Leibovich H, Green A, et al. Mode I interlaminar fracture toughness of Nylon 66 nanofibrilmat interleaved carbon/epoxy laminates[J]. Polymer Composites, 2011, 32(11): 1781-1789.
[5]
Faro C L, Carter J T, Maskell R K, et al. Flexible polymer element as toughening agent in prepregs: WIPO Patent, 2002016481[P]. 2002-03-01.
[6]
Hogg P J. Toughening of thermoset composites with thermoplastic fibres[J]. Materials Science and Engineering: A, 2005, 412(1): 97-103.
[7]
Yun N G, Won Y G, Kim S C. Toughening of carbon fiber/epoxy composite by inserting polysulfone film to form morphology spectrum[J]. Polymer, 2004, 45(20): 6953-6958.
[8]
Singh S, Partridge I K. Mixed-mode fracture in an interleaved carbon-fibre/epoxy composite[J]. Composites Science and Technology, 1995, 55(4): 319-327.
[9]
Todo M, Jar P Y B, Takahashi K. Initiation of a mode-Ⅱ interlaminar crack from an insert film in the end-notched flexure composite specimen[J]. Composites Science and Technology, 2000, 60(2): 263-272.
[10]
Masters J E, Courter J L, Evans R E. Impact fracture and failure suppression using interleaved composites[C]//The 31st International SAMPE Symposium and Exhibition. Covina, California: The Society for the Advancement of Material and Process Engineering, 1986: 844-858.
[11]
Masters J E. Characterization of impact damage development in graphite/epoxy laminates[M]//Masters J E, Au J J. Fractography of Modern Engineering Materials: Composites and Metals, ASTM STP 948. Houston: ASTM Interna-tional, 1987: 238-258.
[12]
Sela N, Ishai O, Banks-Sills L. The effect of adhesive thickness on interlaminar fracture toughness of interleaved CFRP specimens[J]. Composites, 1989, 20(3): 257-264.
[13]
Ozdil F, Carlsson L A. Mode I interlaminar fracture of interleaved graphite/epoxy[J]. Journal of Composite Materials, 1992, 26(3): 432-459.
[14]
Aksoy A, Carlsson L A. Interlaminar shear fracture of interleaved graphite/epoxy composites[J]. Composites Science and Technology, 1992, 43(1): 55-69.
[15]
Mai Y W, Castino F. Fracture toughness of Kevlar-epoxy composites with controlled interfacial bonding[J]. Journal of Materials Science, 1984, 19(5): 1638-1655.
[16]
Pegoretti A, Cristelli I, Migliaresi C. Experimental optimization of the impact energy absorption of epoxy-carbon laminates through controlled delamination[J]. Composites Science and Technology, 2008, 68(13): 2653-2662.
[17]
Tsotsis T K. Interlayer toughening of composite materials[J]. Polymer Composites, 2009, 30(1): 70-86.
[18]
Yasaee M, Bond I P, Trask R S, et al. Damage control using discrete thermoplastic film inserts[J]. Composites Part A: Applied Science and Manufacturing, 2012, 43(6): 978-989.
[19]
Hojo M, Ando T, Tanaka M, et al. Modes I and Ⅱ interlaminar fracture toughness and fatigue delamination of CF/epoxy laminates with self-same epoxy interleaf[J]. International Journal of Fatigue, 2006, 28(10): 1154-1165.
[20]
程群峰. 双马来酰亚胺树脂基复合材料的离位增韧研究[D]. 杭州: 浙江大学, 2007. Cheng Qunfeng. Studies on toughening composites based on BMI resin by ex-situ concept[D]. Hangzhou:Zhejiang University, 2007.
[21]
益小苏, 安学锋, 唐邦铭, 等. 一种提高层状复合材料韧性的方法: 中国, 01100981.0[P]. 2001-03-26. Yi Xiaosu, An Xuefeng, Tang Bangmin, et al. A method to increase the toughness of laminated composites: China, 01100981.0[P]. 2001-03-26.
[22]
益小苏, 许亚洪, 唐邦铭."离位"树脂转移模塑成型加工方法: 中国, 02101216.4[P]. 2002-09-18. Yi Xiaosu, Xu Yahong, Tang Bangmin. An ex-situ process-ing method for resin transfer molding: China, 02101216.4[P]. 2002-09-18.
[23]
唐邦铭, 益小苏, 许亚洪, 等. "离位"树脂膜渗透成型加工方法: 中国, 03105536.2[P]. 2003-01-24. Tang Bangmin, Yi Xiaosu, Xu Yahong, et al. An ex-situ proce-ssing method for resin film infusion: China, 03105536. 2[P]. 2003-01-24.
[24]
Yi X S, An X F. Developments of high-performance composites by innovative ex-situ concept for aerospace appli-cation[J]. Journal of Thermoplastic Composite Materials, 2009, 22(1): 29-49.
[25]
许亚洪. RTM工艺用树脂及"离位"RTM技术研究[D]. 北京: 北京航空材料研究院, 2003. Xu Yahong. Study on RTMable resins and the ex-situ RTM technology[D]. Beijing: Beijing Institute of Aeronautical Materials, 2003.
[26]
李小刚. PMR型聚酰亚胺树脂及其复合材料性能研究[D]. 北京: 北京航空材料研究院, 2005. Li Xiaogang. Study on PMR-type polyimide resin system and the composites[D]. Beijing: Beijing Institute of Aeronautical Materials, 2005.
[27]
益小苏, 安学锋, 张 明, 等. 一种液态成型复合材料用预 制织物及其制备方法: 中国, 200810000135.2[P]. 2008-01-04. Yi Xiaosu, An Xuefeng, Zhang Ming, et al. A method to manufacturing of composite prefabricated reinforced fabric for liquid molding: China, 200810000135.2[P]. 2008-01-04.
[28]
益小苏, 刘 刚, 张尧州, 等. 一种促进树脂流动的高性能预制增强织物及制备方法: 中国, 201010581859.8[P]. 2010-12-13. Yi Xiaosu, Liu Gang, Zhang Yaozhou, et al. A promoter resin flow performance preparation of prefabricated reinforced fabric: China, 201010581859.8[P]. 2010-12-13.
[29]
Yun N G, Won Y G, Kim S C. Toughening of carbon fiber/epoxy composite by inserting polysulfone film to form morphology spectrum[J]. Polymer, 2004, 45(20): 6953-6958.
[30]
益小苏, 许亚洪, 程群峰, 等. 航空树脂基复合材料的高韧性化研究进展[J]. 科技导报, 2008, 26(6): 84-92. Yi Xiaosu, Xu Yahong, Cheng Qunfeng, et al. Development of studies on polymer matrix aircraft composite materials highly toughened[J]. Science & Technology Review, 2008, 26(6): 84-92.
[31]
矫桂琼, 宁荣昌, 卢智先, 等. 层间增韧复合材料研究[J]. 宇航材料工艺, 2001, 31(4): 36-39. Jiao Guiqiong, Ning Rongchang, Lu Zhixian, et al. A study on interleaved composites[J].Aerospace Materials & Technology, 2001, 31(4): 36-39.
[32]
Kim J K, Mackay D B, Mai Y W. Drop-weight impact damage tolerance of CFRP with rubber-modified epoxy matrix[J]. Composites, 1993, 24(6): 485-494.
[33]
Jang K, Cho W J, Ha C S. Influence of processing method on the fracture toughness of thermoplastic-modified, carbon-fiber-reinforced epoxy composites[J]. Composites Science and Technology, 1999, 59(7): 995-1001.
[34]
Sj？gren B A, Berglund L A. Toughening mechanisms in rubber-modified glass fiber/unsaturated polyester composites[J]. Polymer Composites, 1999, 20(5): 705-712.
[35]
Verrey J, Winkler Y, Michaud V, et al. Interlaminar fracture toughness improvement in composites with hyperbranched polymer modified resin[J]. Composites Science and Technology, 2005, 65(10): 1527-1536.
[36]
Pagano N J, Pipes R B. The influence of stacking sequence on laminate strength[J]. Journal of Composite Materials, 1971, 5(1): 50-57.
[37]
Jain L K, Mai Y W. On the effect of stitching on mode I delamination toughness of laminated composites[J]. Composites Science and Technology, 1994, 51(3): 331-345.
[38]
Jain L K, Mai Y W. Determination of mode Ⅱ delamination toughness of stitched laminated composites[J]. Composites Science and Technology, 1995, 55(3): 241-253.
[39]
Dransfield K A, Jain L K, Mai Y W. On the effects of stitching in CFRPs-I. Mode I delamination toughness[J]. Composites Science and Technology, 1998, 58(6): 815-827.
[40]
Jain L K, Dransfield K A, Mai Y W. On the effects of stitching in CFRPs-Ⅱ. Mode Ⅱ delamination toughness[J]. Composites Science and Technology, 1998, 58(6): 829-837.
[41]
Watt A, Goodwin A A, Mouritz A P. Thermal degradation of the mode I interlaminar fracture properties of stitched glass fibre/vinyl ester composites[J]. Journal of Materials Science, 1998, 33(10): 2629-2638.
[42]
Yan W, Liu H Y, Mai Y W. Mode Ⅱ delamination toughness of Z-pinned laminates[J]. Composites Science and Techno-logy, 2004, 64(13): 1937-1945.
[43]
Cartié D D R, Troulis M, Partridge I K. Delamination of Z-pinned carbon fibre reinforced laminates[J]. Composites Science and Technology, 2006, 66(6): 855-861.
[44]
Naik R A. Failure analysis of woven and braided fabric reinforced composites[J]. Journal of Composite Materials, 1995, 29(17): 2334-2363.
[45]
Chan W S, Ochoa O O. Edge delamination resistance by a crictical ply termination[J]. Key Engineering Materials, 1991, 37: 285-304.
[46]
Howard W E, Jr T G, Jones R M. Composite laminate free-edge reinforcement with U-shaped caps part 11: theoretical-experimental correlation[J]. AIAA Journal, 1989, 27(5): 617-623.
[47]
Hillermeier R W, Seferis J C. Interlayer toughening of resin transfer molding composites[J]. Composites Part A: Applied Science and Manufacturing, 2001, 32(5): 721-729.
[48]
Odagiri N, Kishi H, Yamashita M. Development of TORAYCA prepreg P2302 carbon fiber reinforced plastic for aircraft primary structural materials[J]. Advanced Composite Materials, 1996, 5(3): 249-254.
[49]
Lee S H, Noguchi H, Kim Y B, et al. Effect of interleaved non-woven carbon tissue on interlaminar fracture toughness of laminated composites: Part I-Mode Ⅱ[J]. Journal of Composite Materials, 2002, 36(18): 2153-2168.
[50]
Lee S H, Noguchi H, Kim Y B, et al. Effect of interleaved non-woven carbon tissue on interlaminar fracture toughness of laminated composites: Part I-Mode Ⅱ[J]. Journal of Composite Materials, 2002, 36(18): 2153-2168.
[51]
Matsuda S, Hojo M, Ochiai S, et al. Effect of ionomer thickness on mode I interlaminar fracture toughness for ionomer toughened CFRP[J]. Composites Part A: Applied Science and Manufacturing, 1999, 30(11): 1311-1319.
[52]
Yun N G, Won Y G, Kim S C. Toughening of carbon fiber/epoxy composite by inserting polysulfone film to form morphology spectrum[J]. Polymer, 2004, 45(20): 6953-6958.
[53]
Gao F, Jiao G, Lu Z, et al. Mode Ⅱ delamination and damage resistance of carbon/epoxy composite laminates interleaved with thermoplastic particles[J]. Journal of Composite Materials, 2007, 41(1): 111-123.
[54]
Walker L, Sohn M S, Hu X Z. Improving impact resistance of carbon-fibre composites through interlaminar reinforcement[J]. Composites Part A: Applied Science and Manufacturing, 2002, 33(6): 893-902.
[55]
Shivakumar K, Panduranga R. Interleaved polymer matrix composites-a review[C]//54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. Boston: American Institute of Aeronautics and Astronautics, 2013:1-13.
[56]
益小苏. 先进树脂基复合材料高性能化理论与实践[M]. 北京: 国防工业出版社, 2011. Yi Xiaosu. Theory and application of high-performance polymer matrix composites[M]. Beijng: National Defense Industry Press, 2011.
[57]
Sela N, Ishai O. Interlaminar fracture toughness and toughening of laminated composite materials: a review[J]. Composites, 1989, 20(5): 423-435.
[58]
益小苏. 先进复合材料技术研究与发展[M]. 北京: 国防工业出版社, 2006. Yi Xiaosu. Research and development of advanced composites technology[M]. Beijng: National Defense Industry Press, 2006.
[59]
Hillermeier R W, Seferis J C. Interlayer toughening of resin transfer molding composites[J]. Composites Part A: Applied Science and Manufacturing, 2001, 32(5): 721-729.
[60]
Hunston D L, Moulton R J, Johnston N J, et al. Matrix resin effects in composite delamination: mode I fracture aspects[M]//Johnston N J. Toughened Composites: Symposium on Toughened Composites, ASTM STP 937. Houston: ASTM International, 1987: 74-94.
[61]
Dejan S. Delamination properties of a vinyl-ester/glass fibre composite toughened by particulate-modified interlayers[D]. Canberra: Department of Engineering, Austrlian National University, 2001.
[62]
Woo E M, Mao K L. Evaluation of interlaminar-toughened poly (etherlmide)-modified epoxy/carbon fiber composites[J]. Polymer Composites, 1996, 17(6): 799-805.
[63]
Hsiao H M, Ni C N, Wu M D, et al. A novel optical technique for observation of global particle distribution in toughened composites[J]. Composites Part A: Applied Science and Manufacturing, 2012, 43(9): 1523-1529.
[64]
Hsiao H M. Compression-after-impact strength and surface morphology in toughened composite materials[J]. Inter-national Journal of Fracture, 2012, 176(2): 229-236.
[65]
Pearson R A, Yee A F. Influence of particle size and particle size distribution on toughening mechanisms in rubber-modified epoxies[J]. Journal of Materials Science, 1991, 26 (14), 3828-3844.
[66]
Pearson R A, Yee A F. Toughening mechanisms in thermoplastic-modified epoxies: 1. Modification using poly(phenylene oxide)[J]. Polymer, 1993, 34(17): 3658-3670.
[67]
Scott J M, Phillips D C. Carbon fibre composites with rubber toughened matrices[J]. Journal of Materials Science, 1975, 10(4): 551-562.
[68]
Gilbert E N, Hayes B S, Seferis J C. Interlayer toughened unidirectional carbon prepreg systems: effect of preformed particle morphology[J]. Composites Part A: Applied Science and Manufacturing, 2003, 34(3): 245-252.
[69]
Gao F, Jiao G, Lu Z, et al. Mode Ⅱ delamination and damage resistance of carbon/epoxy composite laminates interleaved with thermoplastic particles[J]. Journal of Composite Materials, 2007, 41(1): 111-123.
[70]
Odagiri N, Kishi H, Nakae T. T800H/3900-2 toughened epoxy prepreg system: toughening concept and mechanism[C]//Proceedings of the American Society for Composites. Sixth Technical Conference. Composite Materials, Mechanics and Processing. New York: Technomic Publishing Company, 1991: 43-52.
[71]
Hojo M, Matsuda S, Tanaka M, et al. Mode I delamination fatigue properties of interlayer-toughened CF/epoxy lamin-ates[J]. Composites Science and Technology, 2006, 66(5): 665-675.
[72]
Kageyama K, Kimpara I, Ohsawa I, et al. Mode I and mode Ⅱ delamination growth of interlayer toughened carbon/epoxy (T800H/3900-2) composite system[M]//Martin R H. Composite Materials: Fatigue and Fracture (Fifth Volume), ASTM STP 1230. Houston: ASTM International, 1995: 19-37.
[73]
Matsuda S, Hojo M, Ochiai S, et al. Effect of ionomer thickness on mode I interlaminar fracture toughness for ionomer toughened CFRP[J]. Composites Part A: Applied Science and Manufacturing, 1999, 30(11): 1311-1319.
[74]
Sihn S, Kim R Y, Huh W, et al. Improvement of damage resistance in laminated composites with electrospun nano-interlayers[J]. Composites Science and Technology, 2008, 68(3): 673-683.
[75]
Li G, Li P, Yu Y, et al. Novel carbon fiber/epoxy composite toughened by electrospun polysulfone nanofibers[J]. Materials Letters, 2008, 62(3): 511-514.
[76]
Li G, Li P, Zhang C, et al. Inhomogeneous toughening of carbon fiber/epoxy composite using electrospun polysulfone nanofibrous membranes by in situ phase separation[J]. Composites Science and Technology, 2008, 68(3): 987-994.
[77]
Zhang J, Lin T, Wang X. Electrospun nanofibre toughened carbon/epoxy composites: effects of polyetherketone cardo (PEK-C) nanofibre diameter and interlayer thickness[J]. Composites Science and Technology, 2010, 70(11): 1660-1666.
[78]
Liu L, Liang Y M, Xu G Y, et al. Mode I interlaminar fracture of composite iaminates incorporating with ultrathin fibrous sheets[J]. Journal of Reinforced Plastics and Composites, 2008, 27(11): 1147-1162.
[79]
Sohn M S, Hu X Z. Comparative study of dynamic and static delamination behaviour of carbon fibre/epoxy composite laminates[J]. Composites, 1995, 26(12): 849-858.
[80]
Sohn M S, Hu X Z, Kim J K, et al. Impact damage characterisation of carbon fibre/epoxy composites with multi-layer reinforcement[J]. Composites Part B: Engineering, 2000, 31(8): 681-691.
[81]
Zucchelli A, Focarete M L, Gualandi C, et al. Electrospun nanofibers for enhancing structural performance of composite materials[J]. Polymers for Advanced Technologies, 2011, 22(3): 339-349.
