树脂基层合结构复合材料层间增韧研究
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摘要
综述近年来国内外对复合材料层间增韧的研究现状,重点介绍层间胶膜增韧、层间颗粒增韧、层间纳米纤维增韧和Z-pin增韧技术等4种层间增韧方法,总结树脂基层合结构复合材料在纺织领域的应用。文章表明,复合材料层合板由于易发生分层破坏,使得其在强度和刚度等性能上明显下降,最终使得整个复合材料发生破坏,严重限制了它的应用,全面对复合材料的层间断裂韧性问题进行研究,加强各种增韧方法增韧效果的系统研究,保证树脂基复合材料在提高其韧性的同时具有良好的综合性能,进一步开展适用多种成形工艺的层间增韧技术,对复合材料在各个领域的应用具有十分重要的意义。
The research status of interlaminar toughening of composite materials at home and abroad in recent years was reviewed. Four interlaminar toughening methods, including interlaminar adhesive film toughening,interlaminar particle toughening, interlaminar nanofibers toughening and Z-pin toughening technology, were introduced.The application of resin-based composite materials in textile field was summarized. The paper shows that the laminated composite plate is prone to delamination failure, which makes its strength and stiffness decrease obviously,and ultimately makes the whole composite material destroyed, which severely limits its application. The interlaminar fracture toughness of composite material is studied comprehensively, and the toughening efficiency of various toughening methods is strengthened. Systematic study of resin matrix composites can ensure that they have good comprehensive properties while improving their toughness. Further development of interlaminar toughening technology suitable for various forming processes will be of great significance to the application of composite materials in various fields.
The research status of interlaminar toughening of composite materials at home and abroad in recent years was reviewed. Four interlaminar toughening methods, including interlaminar adhesive film toughening,interlaminar particle toughening, interlaminar nanofibers toughening and Z-pin toughening technology, were introduced.The application of resin-based composite materials in textile field was summarized. The paper shows that the laminated composite plate is prone to delamination failure, which makes its strength and stiffness decrease obviously,and ultimately makes the whole composite material destroyed, which severely limits its application. The interlaminar fracture toughness of composite material is studied comprehensively, and the toughening efficiency of various toughening methods is strengthened. Systematic study of resin matrix composites can ensure that they have good comprehensive properties while improving their toughness. Further development of interlaminar toughening technology suitable for various forming processes will be of great significance to the application of composite materials in various fields.
引文
[1]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.
[2]姚辽军.复合材料层间I型静态及疲劳断裂机理研究[D].西安:西北工业大学,2016.
[3]沈登雄,李志生,刘金刚,等.碳/环氧复合材料层间增韧研究进展[J].宇航材料工艺,2013,43(4):1-7.
[4]MASTERS J E.Improved impaet and delamination resistanee through in terleaving[J].Key Engineering Materi als,1989(37):317.
[5]MASTERS J E,COURTER J L,E-VANS R R.Impact fracture and failure suppression using interleafed composite[J].31st International SAMPE SymPosium,1986(1):16.
[6]ISHAI O,SELA N.Interlaminar fracture toughness and toughening of laminated composite materials:a review[J].Composites,1989,20(5):423-435.
[7]ISHAI O,SELA N,BANKS L.The effete of adhesive thickness on interlarninar farcture toughness of interleaved CFRP speeimens[J].Composites,1989,20(3):257-264.
[8]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(4):36-39.
[9]刘玲,黄争鸣,周烨欣,等.超细纤维增强复合材料Ⅰ型层间断裂韧性分析[J].复合材料学报,2007(4):166-171.
[10]傅宏俊,崔雪娇,赵亚娣,等.玻纤表面毡改善层合复合材料层间断裂韧性[J].天津工业大学学报,2016,35(2):13-17.
[11]WOO E M,MAO K L.Interlaminar morphology effects on fracture resistance of amorphous polymer-modiifed epoxy/carbon fibre composites[J].Composites,1996(27):625-631.
[12]WOO E M,MAO K L.Evaluation of interlarnina-rtoughened poly(ether-imide)-modiifed epoxy/carbon fibre composites[J].Polymer Composites,1996,17(6):79-805.
[13]JANG K,CHO W J,HAC S.Influenee of processing method on the fraeture toughness of thermoplastic-modiifed[J]Earbon-ifbe-rreinforced Epoxy Composites,1999(59):995-1001.
[14]张兴迪,刘刚,党国栋,等.含磷聚芳醚酮颗粒层间增韧碳纤维/双马树脂RTM复合材料[J].高分子学报,2016(9):1254-1262.
[15]安学锋,张晨乾.PES颗粒层间增韧碳纤维/双马树脂RTM复合材料[J]复合材料学报,2013,30(S1):65-69.
[16]SUE H J,JONES R E,GARCIA EI.Fracture behavior ofmodel toughened composites under modeⅠand modeⅡdelamination[J]Mater Sci,1993,28(23):6381-6391.
[17]刘刚,胡晓兰,张朋,等.碳纳米管膜层间改性碳纤维/环氧树脂复合材料[J].高分子学报,2013(10):1334-1340.
[18]AKANGAH P,LINGAIAH S,SHIV-AKUMAR K.Effect of Nylon-66 nano-fiber interleaving on impact damage resistance of epoxy/carbon fiber composite laminates[J].Composite Structures,2010,92(6):1432-1439.
[19]BRUGO T,PALAZZETTI R.The effect of thickness of nylon 6,6 nanofibrous mat on modes I-II fracture mechanics of UD and woven composite laminates[J].Composite Structures,2016(154):172-178.
[20]黄智彬,李刚,李鹏,等.聚砜纳米纤维增韧CFRP的制备及性能[J].复合材料学报,2008,25(5):25-32.
[21]MASAHIRO A,KAZUTOSHI M,S-ATOSHI H.Criterion for interlaminar strength of CFRP laminates toughened with carbon nanofiber interlayer[J].Composites Part A,2011,42(7):703.
[22]DZENIS Y A,RENEKER D H.Delamination resistant composites prepared by small diameter fiber reinforcement at ply interfaces:US,6265333[P].2001-07-24.
[23]PEGORIN F,PINGKARAWAT K,DAYNES S.Influence of Z-pin length on the delamination fracture toughness and fatigue resistance of pinned composites[J].Composites Part B,2015,78(1):298-307.
[24]DENIS D R C,MANOS T,IVANAK.Partridge delamination of Z-pinned carbon fibre reinforced laminates[J]Composites Science and Technology,2006,66(6):855-861.
[25]RUGG K L,COX B N,MASSABOR.Mixed mode delamination of polymer composite laminates reinforced through the thickness by z-fibers[J].Composites Part A:Applied Science and Manufacturing,2002,33(2):177-190.
[26]刘韡,矫桂琼.Z-pins增强C/SiC复合材料层间I型断裂韧性[J].固体力学学报,2013(5):466-471.
[27]杨帆,郑锡涛,李亚智,等.Z-pin增强复合材料I型断裂韧性数值分析[J]复合材料学报,2009,26(4):163-168.
[28]张涛涛,周洪,史文华,等.Z-pin植入对二维机织复合材料层合板力学性能影响的数值模拟[J].复合材料学报,2014,31(2):295-303.
[29]尚自杰,吴晓青,诸利明.二维编织在复合材料中的应用研究[J].天津纺织科技,2016(2):6-7.
[30]NEOGI D,DOUGLAS CD.Design and development of a self deployable structural element[J].Int Space Struct1995,10(2):77-87.
[2]姚辽军.复合材料层间I型静态及疲劳断裂机理研究[D].西安:西北工业大学,2016.
[3]沈登雄,李志生,刘金刚,等.碳/环氧复合材料层间增韧研究进展[J].宇航材料工艺,2013,43(4):1-7.
[4]MASTERS J E.Improved impaet and delamination resistanee through in terleaving[J].Key Engineering Materi als,1989(37):317.
[5]MASTERS J E,COURTER J L,E-VANS R R.Impact fracture and failure suppression using interleafed composite[J].31st International SAMPE SymPosium,1986(1):16.
[6]ISHAI O,SELA N.Interlaminar fracture toughness and toughening of laminated composite materials:a review[J].Composites,1989,20(5):423-435.
[7]ISHAI O,SELA N,BANKS L.The effete of adhesive thickness on interlarninar farcture toughness of interleaved CFRP speeimens[J].Composites,1989,20(3):257-264.
[8]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(4):36-39.
[9]刘玲,黄争鸣,周烨欣,等.超细纤维增强复合材料Ⅰ型层间断裂韧性分析[J].复合材料学报,2007(4):166-171.
[10]傅宏俊,崔雪娇,赵亚娣,等.玻纤表面毡改善层合复合材料层间断裂韧性[J].天津工业大学学报,2016,35(2):13-17.
[11]WOO E M,MAO K L.Interlaminar morphology effects on fracture resistance of amorphous polymer-modiifed epoxy/carbon fibre composites[J].Composites,1996(27):625-631.
[12]WOO E M,MAO K L.Evaluation of interlarnina-rtoughened poly(ether-imide)-modiifed epoxy/carbon fibre composites[J].Polymer Composites,1996,17(6):79-805.
[13]JANG K,CHO W J,HAC S.Influenee of processing method on the fraeture toughness of thermoplastic-modiifed[J]Earbon-ifbe-rreinforced Epoxy Composites,1999(59):995-1001.
[14]张兴迪,刘刚,党国栋,等.含磷聚芳醚酮颗粒层间增韧碳纤维/双马树脂RTM复合材料[J].高分子学报,2016(9):1254-1262.
[15]安学锋,张晨乾.PES颗粒层间增韧碳纤维/双马树脂RTM复合材料[J]复合材料学报,2013,30(S1):65-69.
[16]SUE H J,JONES R E,GARCIA EI.Fracture behavior ofmodel toughened composites under modeⅠand modeⅡdelamination[J]Mater Sci,1993,28(23):6381-6391.
[17]刘刚,胡晓兰,张朋,等.碳纳米管膜层间改性碳纤维/环氧树脂复合材料[J].高分子学报,2013(10):1334-1340.
[18]AKANGAH P,LINGAIAH S,SHIV-AKUMAR K.Effect of Nylon-66 nano-fiber interleaving on impact damage resistance of epoxy/carbon fiber composite laminates[J].Composite Structures,2010,92(6):1432-1439.
[19]BRUGO T,PALAZZETTI R.The effect of thickness of nylon 6,6 nanofibrous mat on modes I-II fracture mechanics of UD and woven composite laminates[J].Composite Structures,2016(154):172-178.
[20]黄智彬,李刚,李鹏,等.聚砜纳米纤维增韧CFRP的制备及性能[J].复合材料学报,2008,25(5):25-32.
[21]MASAHIRO A,KAZUTOSHI M,S-ATOSHI H.Criterion for interlaminar strength of CFRP laminates toughened with carbon nanofiber interlayer[J].Composites Part A,2011,42(7):703.
[22]DZENIS Y A,RENEKER D H.Delamination resistant composites prepared by small diameter fiber reinforcement at ply interfaces:US,6265333[P].2001-07-24.
[23]PEGORIN F,PINGKARAWAT K,DAYNES S.Influence of Z-pin length on the delamination fracture toughness and fatigue resistance of pinned composites[J].Composites Part B,2015,78(1):298-307.
[24]DENIS D R C,MANOS T,IVANAK.Partridge delamination of Z-pinned carbon fibre reinforced laminates[J]Composites Science and Technology,2006,66(6):855-861.
[25]RUGG K L,COX B N,MASSABOR.Mixed mode delamination of polymer composite laminates reinforced through the thickness by z-fibers[J].Composites Part A:Applied Science and Manufacturing,2002,33(2):177-190.
[26]刘韡,矫桂琼.Z-pins增强C/SiC复合材料层间I型断裂韧性[J].固体力学学报,2013(5):466-471.
[27]杨帆,郑锡涛,李亚智,等.Z-pin增强复合材料I型断裂韧性数值分析[J]复合材料学报,2009,26(4):163-168.
[28]张涛涛,周洪,史文华,等.Z-pin植入对二维机织复合材料层合板力学性能影响的数值模拟[J].复合材料学报,2014,31(2):295-303.
[29]尚自杰,吴晓青,诸利明.二维编织在复合材料中的应用研究[J].天津纺织科技,2016(2):6-7.
[30]NEOGI D,DOUGLAS CD.Design and development of a self deployable structural element[J].Int Space Struct1995,10(2):77-87.