先进聚合物基复合材料疲劳性能测试与分析方法的研究现状
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摘要
随着复合材料在航空航天等重要领域的广泛使用,复合材料的疲劳性能备受人们关注。环境损伤效应作为材料在服役过程中不可避免的问题,使深入研究环境因素对复合材料疲劳行为的影响具有重要的理论与工程价值。对多种疲劳模拟试验方法和疲劳性能的分析研究手段进行了归纳分析,总结了材料性能和高低温、湿热、热循环等多种环境因素对复合材料疲劳性能的影响,以期为今后复合材料疲劳性能的研究提供有益的参考。
Great attention has been paid to the fatigue performance of composite materials due to the increasing applications in the aerospace and other important areas. It is of great scientific and engineering significance to thoroughly investigate the impact of environmental factors on the fatigue performance of composites in service. In this paper,A variety of fatigue simulation test methods and fatigue performance analyses were reviewed. The effects of material properties and different environmental factors such as high temperature,hygrothermal and vacuum thermo-cycling on their fatigue properties were summarized. The aim of this work is to provide a useful reference for the future research on fatigue performance of composites.
Great attention has been paid to the fatigue performance of composite materials due to the increasing applications in the aerospace and other important areas. It is of great scientific and engineering significance to thoroughly investigate the impact of environmental factors on the fatigue performance of composites in service. In this paper,A variety of fatigue simulation test methods and fatigue performance analyses were reviewed. The effects of material properties and different environmental factors such as high temperature,hygrothermal and vacuum thermo-cycling on their fatigue properties were summarized. The aim of this work is to provide a useful reference for the future research on fatigue performance of composites.
引文
[1]HUSTION R J.Fatigue Life Prediction in Composites[J].International Journal of Pressure Vessels and Piping,1994,9(4):131-140.
[2]TOLDY A,SZOLNOKI B,MAROSI G.Flame retardancy of fibre-reinforced epoxy resin composites for aerospace applications[J].Polymer Degradation and Stability,2011,96(3):371-376.
[3]SUN P,ZHAO Y,LUO Y F,et al.Effect of temperature and cyclic hygrothermal aging on the interlaminar shear strength of carbon fiber/bismaleimide(BM I)composite[J].M aterials and Design,2011,32(8-9):4341-4347.
[4]AWAJA F,MOON J B,GILBERT M,et al.Surface molecular degradation of selected high performance polymer composites under low earth orbit environmental conditions[J].Polymer Degradation and Stability,2011,96(7):1301-1309.
[5]SHINDO Y,INAMOTO A,NARITA F.Characterization of M ode I fatigue crack grow th in GFRP w oven laminates at low temperatures[J].Acta M aterialia,2005,53(5):1389-1396.
[6]SHINDO Y,MIURA M,TAKEDA T.Cryogenic delamination grow th in w oven glass/epoxy composite laminates under mixed-mode I/II fatigue loading[J].Composites Science and Technology,2011,(71):647-652.
[7]王军,程小全,张纪奎,等.T700复合材料层合板拉-拉疲劳性能[J].航空材料学报,2012,32(03):85-90.
[8]顾怡.FRP疲劳累积损伤理论研究进展[J].力学进展,2001(2):193-202.
[9]潘利剑,靳交通,彭超义,等.玻璃钢复合材料拉-拉疲劳性能试验方法及其改进[J].玻璃钢/复合材料,2009,(05):46-48+52.
[10]CAPRINO G,D'AMORE A.Flexural fatigue behaviour of random continuous fibre-reinforced thermoplastic composites[J].Composites Science and Technology,1998,58:957-965.
[11]梅端.玻璃纤维增强树脂基复合材料力学疲劳性能研究[D].武汉:武汉理工大学,2010.
[12]TANABE Y,YOSHIMURA T,WATANABE T,et al.Fatigue of C/C composites in bending and shear modes[J].Carbon,2004,42:1665-1670.
[13]杨乃宾,付惠民,高镇同.单向碳/环氧复合材料拉-拉疲劳性能研究[J].复合材料学报,1985,(3):54-60+119-120.
[14]周骏,乔生儒,席守谋,等.碳纤维/双马来酰亚胺复合材料的拉-拉疲劳性能[J].航空学报,1990,(5):305-308.
[15]王丹勇,温卫东.复合材料单向层合板损伤失效试验研究[J].复合材料学报,2007,(05):142-148.
[16]杨忠清.玻璃纤维增强树脂基层合板疲劳行为研究[D].南京:南京航空航天大学,2008.
[17]CAO S H,WU Z S,WANG X.Tensile properties of CFRP and hybrid FRP composites at elevated temperatures[J].Journal of Composite M aterials,2009,43(4):315-330.
[18]高禹,刘佳琦,王绍权,等.高温老化对T700/HT280双马来酰亚胺复合材料疲劳性能的影响[J].复合材料学报,2017,34(2):240-246.
[19]刘佳琦.环境因素对T700/HT280复合材料力学性能的影响[D].沈阳:沈阳航空航天大学,2017.
[20]史汉桥,唐占文,孙建波,等.低温用碳/环氧复合材料性能[J].宇航材料工艺,2016,46(04):25-28.
[21]S.Sa'NCHEZ-SA'EZ,T.GO'MEZ-DEL R'O,E.BARBERO,et al.Static behavior of CFRPs at low temperatures[J].Composites,Part B,2002,33:383-390.
[22]王绍权.液氮浸渍对C/BMI复合材料性能的影响[D].哈尔滨:哈尔滨工业大学,2012.
[23]刘新,武湛君,蔡永超,等.超低温处理对T700碳纤维/环氧复合材料拉-压疲劳性能的影响[J].宇航学报,2014,35(07):850-856.
[24]RAY B C.Temperature effect during humid ageing on interfaces of glass and carbon fibers reinforced epoxy composites[J].Journal of Colloid and Interface Science,2006,298(1):111-117.
[25]KUMAR S B,SRIDHAR I,SIVASHANKER S.Influence of humid environment on the performance of high strength structural carbon fiber composites[J].M aterials Science and Engineering A,2008,498:174-178.
[26]PATEI S R,CASE S W.Durability of hygrothermally aged graphite/epoxy w oven composite under combined hygrothermal conditions[J].International Journal of Fatigue,2002,24:1295-1301.
[27]KAWAI M,YAGIHASHI Y,HOSHI H,et al.Anisomorphic constant fatigue life diagrams for quasi-isotropic w oven fabric carbon/epoxy laminates under different hygro-thermal environments[J].Advanced Composite M aterials,2013,22(2):79-98.
[28]刘鑫娴,曾建江,陈智.碳纤维/环氧复合材料湿热环境疲劳剩余强度试验[J].环境技术,2012,30(06):6-9.
[29]PARK S Y,CHOI W J,CHOI H S.The effects of void contents on the long-term hygrothermal behaviors of glass/epoxy and glare laminates[J].Composite Structures,2010,92(1):18-24.
[30]GAO Y,HE S,YANG D,et al.Effect of vacuum thermo-cycling on physical properties of unidirectional M40J/AG-80 composites[J].Composites Part B Engineering,2005,36:351-358.
[31]高禹,刘佳琦,王柏臣,等.真空热循环对T700/3234复合材料疲劳性能的影响[J].航空制造技术,2015,(14):26-29.
[32]ROTEM A,HASHIN Z.Fatigue failure of angle ply laminates[J].AIAA Journal,1976,14(7):868-872.
[33]HAN K S.Fatigue life prediction and failure mechanisms of composite materials[J].Advanced Composite M aterials,1992,2(1):29-50.
[34]BROUTMAN L J,SAHU S.A new theory to predict cumulative fatigue damage in fiberglass reinforced plastics[J].Composite materials:testing and design,1972,497:170-188.
[35]YANG J N.Fatigue and residual strength degradation for graphite/epoxy composites under tension-compression cyclic loadings[J].Journal of Composite M aterials,1978,12(1):19-39.
[36]刘英芝.复合材料层合板疲劳行为研究[D].哈尔滨:哈尔滨工业大学,2015.
[37]TSERPES K I,PAPANIKOS P,LABEAS G,et al.Fatigue damage accumulation and residual strength assessment of CFRP laminates[J].Composite Structures,2004,63(2):219-230.
[38]VAN PAEPEGEM W,DEGRIECK J.A new coupled approach of residual stiffness and strength for fatigue of fibre-reinforced composites[J].International Journal of Fatigue,2002,24(7):747-762.
[39]LV X Y,WANG R G,LIU W B,et al.Surface and interface properties of carbon fiber composites under cyclical aging[J].Applied Surface Science,2011,257:10459-10464.
[40]何梅洪.基于超声的复合材料构件疲劳损伤检测与评价研究[D].天津:天津工业大学,2016.
[41]冯古雨,曹海建,钱坤.三维角联锁机织复合材料弯曲抗疲劳性能有限元分析[J].玻璃钢/复合材料,2017(2):5-9.
[42]刘亚沣.复合材料层合板疲劳累积损伤分析研究[D].大连:大连理工大学,2015.
[43]HASHIN Z.Failure criteria for unidirectional fiber composites[J].journal of applied mechanics,1980,47(2):329-334.
[44]徐颖,温卫东,崔海涛.复合材料层合板疲劳逐渐累积损伤寿命预测方法[J].航空动力学报,2007,(4):602-607.
[45]籍庆辉,朱平,卢家海,等.基于Kriging近似模型的碳纤维增强复合材料疲劳性能预测及其应用[J].上海交通大学学报,2017,51(2):129-135.
[2]TOLDY A,SZOLNOKI B,MAROSI G.Flame retardancy of fibre-reinforced epoxy resin composites for aerospace applications[J].Polymer Degradation and Stability,2011,96(3):371-376.
[3]SUN P,ZHAO Y,LUO Y F,et al.Effect of temperature and cyclic hygrothermal aging on the interlaminar shear strength of carbon fiber/bismaleimide(BM I)composite[J].M aterials and Design,2011,32(8-9):4341-4347.
[4]AWAJA F,MOON J B,GILBERT M,et al.Surface molecular degradation of selected high performance polymer composites under low earth orbit environmental conditions[J].Polymer Degradation and Stability,2011,96(7):1301-1309.
[5]SHINDO Y,INAMOTO A,NARITA F.Characterization of M ode I fatigue crack grow th in GFRP w oven laminates at low temperatures[J].Acta M aterialia,2005,53(5):1389-1396.
[6]SHINDO Y,MIURA M,TAKEDA T.Cryogenic delamination grow th in w oven glass/epoxy composite laminates under mixed-mode I/II fatigue loading[J].Composites Science and Technology,2011,(71):647-652.
[7]王军,程小全,张纪奎,等.T700复合材料层合板拉-拉疲劳性能[J].航空材料学报,2012,32(03):85-90.
[8]顾怡.FRP疲劳累积损伤理论研究进展[J].力学进展,2001(2):193-202.
[9]潘利剑,靳交通,彭超义,等.玻璃钢复合材料拉-拉疲劳性能试验方法及其改进[J].玻璃钢/复合材料,2009,(05):46-48+52.
[10]CAPRINO G,D'AMORE A.Flexural fatigue behaviour of random continuous fibre-reinforced thermoplastic composites[J].Composites Science and Technology,1998,58:957-965.
[11]梅端.玻璃纤维增强树脂基复合材料力学疲劳性能研究[D].武汉:武汉理工大学,2010.
[12]TANABE Y,YOSHIMURA T,WATANABE T,et al.Fatigue of C/C composites in bending and shear modes[J].Carbon,2004,42:1665-1670.
[13]杨乃宾,付惠民,高镇同.单向碳/环氧复合材料拉-拉疲劳性能研究[J].复合材料学报,1985,(3):54-60+119-120.
[14]周骏,乔生儒,席守谋,等.碳纤维/双马来酰亚胺复合材料的拉-拉疲劳性能[J].航空学报,1990,(5):305-308.
[15]王丹勇,温卫东.复合材料单向层合板损伤失效试验研究[J].复合材料学报,2007,(05):142-148.
[16]杨忠清.玻璃纤维增强树脂基层合板疲劳行为研究[D].南京:南京航空航天大学,2008.
[17]CAO S H,WU Z S,WANG X.Tensile properties of CFRP and hybrid FRP composites at elevated temperatures[J].Journal of Composite M aterials,2009,43(4):315-330.
[18]高禹,刘佳琦,王绍权,等.高温老化对T700/HT280双马来酰亚胺复合材料疲劳性能的影响[J].复合材料学报,2017,34(2):240-246.
[19]刘佳琦.环境因素对T700/HT280复合材料力学性能的影响[D].沈阳:沈阳航空航天大学,2017.
[20]史汉桥,唐占文,孙建波,等.低温用碳/环氧复合材料性能[J].宇航材料工艺,2016,46(04):25-28.
[21]S.Sa'NCHEZ-SA'EZ,T.GO'MEZ-DEL R'O,E.BARBERO,et al.Static behavior of CFRPs at low temperatures[J].Composites,Part B,2002,33:383-390.
[22]王绍权.液氮浸渍对C/BMI复合材料性能的影响[D].哈尔滨:哈尔滨工业大学,2012.
[23]刘新,武湛君,蔡永超,等.超低温处理对T700碳纤维/环氧复合材料拉-压疲劳性能的影响[J].宇航学报,2014,35(07):850-856.
[24]RAY B C.Temperature effect during humid ageing on interfaces of glass and carbon fibers reinforced epoxy composites[J].Journal of Colloid and Interface Science,2006,298(1):111-117.
[25]KUMAR S B,SRIDHAR I,SIVASHANKER S.Influence of humid environment on the performance of high strength structural carbon fiber composites[J].M aterials Science and Engineering A,2008,498:174-178.
[26]PATEI S R,CASE S W.Durability of hygrothermally aged graphite/epoxy w oven composite under combined hygrothermal conditions[J].International Journal of Fatigue,2002,24:1295-1301.
[27]KAWAI M,YAGIHASHI Y,HOSHI H,et al.Anisomorphic constant fatigue life diagrams for quasi-isotropic w oven fabric carbon/epoxy laminates under different hygro-thermal environments[J].Advanced Composite M aterials,2013,22(2):79-98.
[28]刘鑫娴,曾建江,陈智.碳纤维/环氧复合材料湿热环境疲劳剩余强度试验[J].环境技术,2012,30(06):6-9.
[29]PARK S Y,CHOI W J,CHOI H S.The effects of void contents on the long-term hygrothermal behaviors of glass/epoxy and glare laminates[J].Composite Structures,2010,92(1):18-24.
[30]GAO Y,HE S,YANG D,et al.Effect of vacuum thermo-cycling on physical properties of unidirectional M40J/AG-80 composites[J].Composites Part B Engineering,2005,36:351-358.
[31]高禹,刘佳琦,王柏臣,等.真空热循环对T700/3234复合材料疲劳性能的影响[J].航空制造技术,2015,(14):26-29.
[32]ROTEM A,HASHIN Z.Fatigue failure of angle ply laminates[J].AIAA Journal,1976,14(7):868-872.
[33]HAN K S.Fatigue life prediction and failure mechanisms of composite materials[J].Advanced Composite M aterials,1992,2(1):29-50.
[34]BROUTMAN L J,SAHU S.A new theory to predict cumulative fatigue damage in fiberglass reinforced plastics[J].Composite materials:testing and design,1972,497:170-188.
[35]YANG J N.Fatigue and residual strength degradation for graphite/epoxy composites under tension-compression cyclic loadings[J].Journal of Composite M aterials,1978,12(1):19-39.
[36]刘英芝.复合材料层合板疲劳行为研究[D].哈尔滨:哈尔滨工业大学,2015.
[37]TSERPES K I,PAPANIKOS P,LABEAS G,et al.Fatigue damage accumulation and residual strength assessment of CFRP laminates[J].Composite Structures,2004,63(2):219-230.
[38]VAN PAEPEGEM W,DEGRIECK J.A new coupled approach of residual stiffness and strength for fatigue of fibre-reinforced composites[J].International Journal of Fatigue,2002,24(7):747-762.
[39]LV X Y,WANG R G,LIU W B,et al.Surface and interface properties of carbon fiber composites under cyclical aging[J].Applied Surface Science,2011,257:10459-10464.
[40]何梅洪.基于超声的复合材料构件疲劳损伤检测与评价研究[D].天津:天津工业大学,2016.
[41]冯古雨,曹海建,钱坤.三维角联锁机织复合材料弯曲抗疲劳性能有限元分析[J].玻璃钢/复合材料,2017(2):5-9.
[42]刘亚沣.复合材料层合板疲劳累积损伤分析研究[D].大连:大连理工大学,2015.
[43]HASHIN Z.Failure criteria for unidirectional fiber composites[J].journal of applied mechanics,1980,47(2):329-334.
[44]徐颖,温卫东,崔海涛.复合材料层合板疲劳逐渐累积损伤寿命预测方法[J].航空动力学报,2007,(4):602-607.
[45]籍庆辉,朱平,卢家海,等.基于Kriging近似模型的碳纤维增强复合材料疲劳性能预测及其应用[J].上海交通大学学报,2017,51(2):129-135.