随着飞行器结构中碳纤维增强树脂基复合材料用量的迅速增加,其应用范围从非主承力构件逐渐扩展到主承力构件,复合材料结构中的疲劳、低速冲击和高速撞击等动态力学问题已经引起了国内外研究者的广泛关注.本文综述了典型空天环境因素与碳纤维增强树脂基复合材料的交互作用,重点探讨了其在疲劳、低速冲击和高速撞击载荷作用下的行为,简述了环境损伤与动态载荷耦合对碳纤维增强树脂基复合材料动态力学性能的影响,以期为聚合物基复合材料在空天飞行器上的应用提供有益的参考.
参考文献
[1] | 张小达,吕维鉴.国外运载器、航天器从地面到空间自然环境标准综述[J].航天标准化,2001(01):29-33. |
[2] | 都亨,叶宗海.中国空间环境研究发展-空间物理前沿进展[M].北京:气象出版社,1998.1-15.DU H,YE Z H.Chinese Space Environment Research and Development-advances in Space Physics Frontier[M].Beijing:China Meteorological Press,1998.1-15.,1998. |
[3] | 谭立忠,朱风云.美国X-37B轫道试验飞行器发展研究[J].飞航导弹,2011(06):33-36. |
[4] | 邱惠中.美国空天飞机用先进材料最新进展[J].宇航材料工艺,1994,(6):5-9.QU H Z.The latest progress in advanced materials used in the United States for aerospace plane[J].Aerospace Materials & Technology,1994,(6):5-9.,1994. |
[5] | YANN G,GREGORY A,CATHERINE M,et al .Flaking of black anodic films in space environment:Ageing and numerical simulation[J].Mechanics of Materials,2012,45 |
[6] | 曹东,张晓云,陆峰,等.先进复合材料T300/5405综合环境实验谱的研究[J].材料工程,2014,(7):73-78.CAO Dong,ZHANG Xiao-yun,LU Feng,et al.Synthetical environmental spectrum aging of T300/5405 advanced composite material[J].Journal of Materials Engineering,2014,(7):73-78.,2014. |
[7] | 陈旭,尹鹏,咸贵军,刘燕峰,刘青曼,益小苏.苎麻纤维增强酚醛树脂基复合材料的湿热性能研究[J].航空材料学报,2013(02):58-65. |
[8] | ADAMCZAK A D,SPRIGGS A A,FITCH D M,et al .Blistering in carbon fiber filled fluorinated polyimide composites[J].Polymer Composites,2011,32(2):185-192.,2011. |
[9] | 臧振群,古士芬,师立勤,等 .航天器异常与空间环境[J].空间科学学报,1998,18(4):342-347.ZANG Z Q,GU S F,SHI LQ,et al.Study on spacecraft anomaly caused by space environment[J].Chinese Journal of Space Science,1998,18(4):342-347.,1998. |
[10] | 李成功,傅恒志,于翘.航空航天材料[M].北京:国防工业出版社,2002.123-185.LI C G,FU H Z,YU Q.Aerospace Materials[M].Beijing:National Defence Industry Press,2002.123-185.,2002. |
[11] | 王浚,黄本诚,万大才.环境模拟技术[M].北京:国防工业出版社,1996.195-200.WANG J,HUANG B C,WAN D C.Environment Simulation Technology[M].Beijing:National Defence Industry Press,1996.195-200.,1996. |
[12] | AWAJA F,JIN B M,ZHANG S N,et al .Surface molecular degradation of 3D glass polymer composite under low earth orbit simulated space environment[J].Polymer Degradation and Stability,2010,95(6):987-996.,2010. |
[13] | GAO Y,YANG D Z,XIAO J D,et al .Effect of proton irradiation on mechanical properties of carbon/epoxy composites[J].Journal of Spacecraft and Rockets,2006,43(3):505-508.,2006. |
[14] | PETERSON C E,PATIL R R,KALLMEYER A R,et al .A micromechanical damage model for carbon fiber composites at reduced temperatures[J].Journal of Composite Materials,2008,42 |
[15] | 高禹,代小杰,董尚利,陆春,包建文.热循环作用下单向炭纤维/环氧树脂复合材料的热应力[J].高分子材料科学与工程,2012(09):178-181. |
[16] | KWANG B S,CHUN G K,CHANG S H,et al .Prediction of failure thermal cycles in graphite/epoxy composite materials under simulated low earth orbit environments[J].Composites Part B,2000,31 |
[17] | ZHANG C,BINIENDA W K,MORSCHER G N,et al .Experimental and FEM study of thermal cycling induced microcracking in carbon/epoxy triaxial braided composites[J].Composites:Part A,2013,46 |
[18] | GAO Y,DONGS L,HE S,et al .Characterization on stress distribution and thermal expansion behavior for M40J/AG-80 composites experienced vacuum thermo-cycling[J].Journal of Reinforced Plastics and Composites,2006,25(16):1647-1657.,2006. |
[19] | GAO Y,HE S,YANG D Z,et al .Effect of vacuum thermo-cycling on physical properties of unidirectional M40J/AG-80 composites[J].Composites Part B:Engineering,2005,36(4):351-358.,2005. |
[20] | KOBAYASHI S,TAKEDA N .Experimental characterization of microscopic damage behavior in carbon/bismaleimide composite-effects of temperature and laminate configuration[J].Composites:Part A,2002,33 |
[21] | UPADHYAYA P,SINGH S,ROY S .A mechanism-based multi-scale model for predicting thermo-oxidative degradation in high temperature polymer matrix composites[J].Composites Science and Technology,2011,71 |
[22] | LAFARIE-FRENOT M C,GRANDIDIER J C,GIGLIOTTI M,et al .Thermo-oxidation behaviour of composite materials at high temperatures:a review of research activities carried out within the COMEDI program[J].Polymer Degradation and Stability,2010,95(6):965-974.,2010. |
[23] | DINH Q V,MARCO G,LAFARIE-FRENOT M C .Experimental characterization of thermo-oxidation-induced shrinkage and damage in polymer-matrix composites[J].Composites Part A,2012,43(4):577-586.,2012. |
[24] | JACQUES C,BRUNO M .Influence of laminate thickness on composite durability for long term utilization at intermediate temperature (100-150℃)[J].Composites Science and Technology,2009,69(9):1432-1436.,2009. |
[25] | UEKI T,NISHIJIMA S,IZUMI Y .Designing of epoxy resin systems for cryogenic use[J].Cryogenics,2005,45 |
[26] | KIM R Y,STEVE L D .Experimental and analytical studies on the damage initiation in composite laminates at cryogenic temperatures[J].Composite Structures,2006,76 |
[27] | 冯青,李敏,顾轶卓,刘洪新,张佐光.不同湿热条件下碳纤维/环氧复合材料湿热性能实验研究[J].复合材料学报,2010(06):16-20. |
[28] | 张立鹏,沈真.复合材料吸湿试验的若干问题[C].高性能复合材料结构制造与检测技术暨第五届全国复合材料性能测试与检测技术交流会论文集,2009:85-88. |
[29] | GUY .The relaxation behaviour of GFRP unidirectional laminates[J].Transactions of Nanjing University of Aeronautics and Astronautics,1999,16(2):148-153.,1999. |
[30] | WU F Q,YAO W X .A model of fatigue life distribution of composite laminates based on their static strength distribution[J].Chinese Journal of Aeronautics,2008,21(3):241-246.,2008. |
[31] | BROUTMAN L J,SAHU S.A new theory to predict cumulative fatigue damage in fiberglass reinforced plastics[A].Composite Materials:Testing and Design (Second conference)[C].ASTM STP 497,1972,170-188.,1972. |
[32] | CHOU P C,CROMAN R .Residual strength in fatigue based on the strength life equal rank assumption[J].Journal of Composite materials,1978,12(2):127-194.,1978. |
[33] | 顾怡,姚卫星.疲劳加载下纤维复合材料的剩余强度[J].复合材料学报,1999(03):98-102. |
[34] | CAPRINO G,TETI R,IORIO I D .Predicting residual strength of pre-fatigued glass fibre-reinforced plastic laminates through acoustic emission monitoring[J].Composites:Part B,2005,36 |
[35] | YAO W X,HIMMEL N .A new cumulative fatigue damage model for fiber reinforced plastics[J].Composites Science and Technology,2000,60(1):59-64.,2000. |
[36] | YANG J N .Fatigue and residual strength degradation for graphite/epoxy composites under tension-compression cyclic loading[J].Journal of Composite Materials,1978,12(1):19-39.,1978. |
[37] | YANG J N,JONES D L,YANG S H .A stiffness degradation model for graphite/epoxy laminates[J].Journal of Composite Materials,1987,24(7):753-796.,1987. |
[38] | 徐建新,冯振宇.常幅疲劳载荷下复合材料层合板刚度退化试验研究[J].机械科学与技术,2005(09):1069-1070,1102. |
[39] | 孙崇强,张建宇,费斌军.CFRP孔板拉伸疲劳环境效应的正交试验[J].北京航空航天大学学报,2012(10):1341-1345. |
[40] | PATEL S R,CASE S W .Durability of hygrothermally aged graphite/epoxy woven composite under combined hygrothermal conditions[J].International Journal of Fatigue,2002,24(12):1295-1301.,2002. |
[41] | ZHANGAY,LIDH,LUHB,etal .Qualitative separation of the effect of voids on the bending fatigue performance of hygrothermal conditioned carbon/epoxy composites[J].Materials & Design,2011,32(10):4803-4809.,2011. |
[42] | BELINGARDI G,VADORI R .Influence of the laminate thickness in low velocity impact behavior of composite material plate[J].Composite Structures,2003,61:27-38.,2003. |
[43] | 屈天骄,郑锡涛,范献银,郑晓霞.复合材料层合板低速冲击损伤影响因素分析[J].航空材料学报,2011(06):81-86. |
[44] | 沈真,杨胜春,陈普会.复合材料层压板抗冲击行为及表征方法的实验研究[J].复合材料学报,2008(05):125-133. |
[45] | 沈真,杨胜春,陈普会.复合材料抗冲击性能和结构压缩设计许用值[J].航空学报,2007(03):561-566. |
[46] | 徐颖,温卫东,崔海坡.含冲击损伤复合材料层合板疲劳试验研究[J].宇航材料工艺,2007(02):73-76,80. |
[47] | BAUCOM J N,ZIKRY M A .Low-velocity impact damage progression in woven E-glass composite systems[J].Composites Part A,2005,36(5):658-664.,2005. |
[48] | THOMA K,SCHAFER F,HIERMAIER S,et al .An approach to achieve progress in spacecraft shielding[J].Advances in Space Research,2004,34(5):1063-1075.,2004. |
[49] | 王洋 .碳纤维/环氧复合材料高速撞击损伤效应研究[D].哈尔滨工业大学,2009. |
[50] | 张子龙,程小全,益小苏.复合材料层合板准静态横压损伤及其压缩破坏研究[J].复合材料学报,2002(05):108-113. |
[51] | 沈真,张子龙,王进,杨胜春,叶林.复合材料损伤阻抗和损伤容限的性能表征[J].复合材料学报,2004(05):140-145. |
[52] | JACKSON W C,POE C C .The use of impact force as a scale parameter for the impact response of composite laminates[J].Journal of Composites Technology Research,1993,15(4):282-289.,1993. |
[53] | 罗靓,张佐光,李敏,沈真,杨胜春.复合材料层合板准静态压痕实验研究[J].复合材料学报,2007(03):154-159. |
[54] | 郑晓霞,郑锡涛,沈真,杨胜春.低速冲击与准静态压痕力下复合材料层合板的损伤等效性[J].航空学报,2010(05):928-933. |
[55] | QI B,HERSZBERG I .An engineering approach for predicting residual strength of carbon/epoxy laminates after impact and hygrothermal cycling[J].Composite Structures,1999,47:483-490.,1999. |
[56] | AOKI Y,YAMADA K,ISHIKAWA T .Effect of hygrothermal condition on compression after impact strength of CFRP laminates[J].Composites Science and Technology,2008,68(6):1376-1383.,2008. |
[57] | ZHANG A Y,LU H B,ZHANG D X .Effects of voids on residual tensile strength after impact of hygrothermal conditioned CFRP laminates[J].Composite Structures,2013,95 |
[58] | MOKHTAR H,SICOT O,ROUSSEAU J,et al .The influence of ageing on the impact damage of carbon epoxy composites[J].Procedia Engineering,2011,10 |
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