预浸料-真空固化复合材料工艺特点与应用
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摘要
文摘从树脂工艺性、预浸料结构及成型工艺等方面介绍了预浸料-真空固化复合材料工艺特点,简要总结了预浸料-真空固化技术在航空航天领域复合材料制造中的应用现状,并对预浸料-真空固化技术发展进行展望。
The process characteristics of prepregs-based vacuum-bag-only consolidation are reviewed,including resin manufacturability,prepreg architecture and moulding process. Its application in aeronautics and astronautics areas has been briefly introduced,meanwhile its current state and trends are discussed at the end of this article.
The process characteristics of prepregs-based vacuum-bag-only consolidation are reviewed,including resin manufacturability,prepreg architecture and moulding process. Its application in aeronautics and astronautics areas has been briefly introduced,meanwhile its current state and trends are discussed at the end of this article.
引文
[1]杜善义.先进复合材料与航空航天[J].复合材料学报,2007,24(1):1-12.
[2]益小苏.先进复合材料技术的挑战与创新[J].航空制造技术,2004,25(7):24-30.
[3]吴志恩.飞机复合材料构件成本问题的技术分析及改进措施[J].航空制造技术,2009,15:50-52.
[4]罗益锋,罗晰旻.高性能和多功能轻质材料在国防装备的应用进展[J].高科技纤维与应用,2015,40(6):1-11.
[5]赵云峰,孙宏杰,李仲平.航天先进树脂基复合材料制造技术及其应用[J].宇航材料工艺,2016,46(4):1-7.
[6]罗云烽,彭公秋,曹正华,等.航空用热压罐外固化预浸料复合材料的应用[J].航空制造技术,2012,18:26-31.
[7]唐见茂.航空航天复合材料非热压罐成型研究进展[J].航天器环境工程,2014,31(6):577-583.
[8]CENTEA T,GRUNENFELDER L K,NUTT S R.A review of out-of-autoclave prepregs:Material properties,process phenomena,and manufacturing considerations[J].Composites:Part A,2015,70:132-154.
[9]KRATZ J,HSIAO K,FERNLUND G,et al.Thermal models for MTM45-1 and Cycom 5320 out-of-autoclave prepreg resins[J].J.Compos.Mater.,2012,47:341-352.
[10]张宝艳,陈祥宝,周正刚.消泡剂对真空压力成型复合材料质量与性能的影响[J].材料工程,2007(12):3-7.
[11]THORFINNSON B,BIERMANN T.Production of void free composite parts without debulking[C]//Proc.31stint SAMPE symp.,Las Vegas,NV:Society for the Advancement of Material and Process Engineering,1986.
[12]THORFINNSON B,BIERMANN T.Degree of impregnation of prepregs-effects on porosity[C]//Proc.32ndint SAMPE symp.,Anaheim,CA:Society for the Advancement of Material and Process Engineering,1987.
[13]REPECKA L,BOYD J.Vacuum-bag-only-curable prepregs that produce void-free parts[C]//Proc.SAMPE 2002conf.,Long Beach,CA:Society for the Advancement of Material and Process Engineering,2002.
[14]GRUNENFELDER L K,CENTEA T,HUBERT P,et al.Effect of room-temperature out-time on tow impregnation in an out-of-autoclave prepreg[J].Compos.Part A Appl.Sci.Manuf.,2013,45:119-126.
[15]周宇,樊孟金,尚呈元,等.Oo A成型T800/607复合材料制备及性能[J].宇航材料工艺,2017,47(3):57-60.
[16]GRUNENFELDER L K,NUTT S R.Prepreg age monitoring via differential scanning calorimetry[J].J.Reinf.Plast.Compos.,2012,31:295-302.
[17]ANANDAN S,DHALIWAL G S,SAMARANAYAKE V A,et al.Influence of cure conditions on out-of-autoclave bismaleimide composite laminates[J].J.Appl.Polym.Sci.,2016,DOI:10.1002/APP.43984.
[18]VO T,VORA K,MINAIE B.Effects of postcure temperature variation on hygrothermal-mechanical properties of an out-of-autoclave polymer composite[J].J.Appl.Polym.Sci.,2013,3090-3097.
[19]张宝艳,陈祥宝.低温固化树脂及复合材料的研究与应用[J].材料工程,2002(增刊):248-252.
[20]张宝艳,陈祥宝,刘天舒,等.低温真空压力成型树脂体系研制[J].航空材料学报,2003,23:10-12.
[21]陈文.从两会看低成本有机复合材料制造技术的发展[J].航空制造工程,1997(10):10-12.
[22]陈亚莉.低成本复合材料技术的新进展(一)[J].航空工程与维修,2001(1):17-19.
[23]RUSSELL J D,SHENK B,HOLZWARTH R,et al.Advanced composite cargo aircraft[C]//Proc 41stint SAMPE tech conf.Witchita,KA:Society for the Advancement of Material and Process Engineering,2009.
[24]廉伟.低成本非热压罐工艺在飞机复材结构上的应用[C]//梦想成真的推动力-2011年商用飞机复合材料应用国际论坛,上海,2011.
[25]RIDGARD C.Advances in low temperature curing prepregs for aerospace structures[C]//Proc SAMPE 2000 conf.Long Beach,CA:Society for the Advancement of Material and Process Engineering,2000.
[26]RIDGARD C.Out of autoclave composite technology for aerospace,defense and space structures[C]//Proc.SAMPE2009 conf.Baltimore,MD:Society for the Advancement of Material and Process Engineering,2009.
[27]黄诚,刘德博,吴会强,等.我国航天运载器复合材料贮箱应用展望[J].沈阳航空航天大学学报,2016,33(2):27-35.
[28]LANE S A,HIGGINS J,BISKNER A,et al.Out-ofautoclave composite fairing design,fabrication,and test[J].Journal of Manufacturing Science and Engineering,2011,133:031020-1-031020-10.
[2]益小苏.先进复合材料技术的挑战与创新[J].航空制造技术,2004,25(7):24-30.
[3]吴志恩.飞机复合材料构件成本问题的技术分析及改进措施[J].航空制造技术,2009,15:50-52.
[4]罗益锋,罗晰旻.高性能和多功能轻质材料在国防装备的应用进展[J].高科技纤维与应用,2015,40(6):1-11.
[5]赵云峰,孙宏杰,李仲平.航天先进树脂基复合材料制造技术及其应用[J].宇航材料工艺,2016,46(4):1-7.
[6]罗云烽,彭公秋,曹正华,等.航空用热压罐外固化预浸料复合材料的应用[J].航空制造技术,2012,18:26-31.
[7]唐见茂.航空航天复合材料非热压罐成型研究进展[J].航天器环境工程,2014,31(6):577-583.
[8]CENTEA T,GRUNENFELDER L K,NUTT S R.A review of out-of-autoclave prepregs:Material properties,process phenomena,and manufacturing considerations[J].Composites:Part A,2015,70:132-154.
[9]KRATZ J,HSIAO K,FERNLUND G,et al.Thermal models for MTM45-1 and Cycom 5320 out-of-autoclave prepreg resins[J].J.Compos.Mater.,2012,47:341-352.
[10]张宝艳,陈祥宝,周正刚.消泡剂对真空压力成型复合材料质量与性能的影响[J].材料工程,2007(12):3-7.
[11]THORFINNSON B,BIERMANN T.Production of void free composite parts without debulking[C]//Proc.31stint SAMPE symp.,Las Vegas,NV:Society for the Advancement of Material and Process Engineering,1986.
[12]THORFINNSON B,BIERMANN T.Degree of impregnation of prepregs-effects on porosity[C]//Proc.32ndint SAMPE symp.,Anaheim,CA:Society for the Advancement of Material and Process Engineering,1987.
[13]REPECKA L,BOYD J.Vacuum-bag-only-curable prepregs that produce void-free parts[C]//Proc.SAMPE 2002conf.,Long Beach,CA:Society for the Advancement of Material and Process Engineering,2002.
[14]GRUNENFELDER L K,CENTEA T,HUBERT P,et al.Effect of room-temperature out-time on tow impregnation in an out-of-autoclave prepreg[J].Compos.Part A Appl.Sci.Manuf.,2013,45:119-126.
[15]周宇,樊孟金,尚呈元,等.Oo A成型T800/607复合材料制备及性能[J].宇航材料工艺,2017,47(3):57-60.
[16]GRUNENFELDER L K,NUTT S R.Prepreg age monitoring via differential scanning calorimetry[J].J.Reinf.Plast.Compos.,2012,31:295-302.
[17]ANANDAN S,DHALIWAL G S,SAMARANAYAKE V A,et al.Influence of cure conditions on out-of-autoclave bismaleimide composite laminates[J].J.Appl.Polym.Sci.,2016,DOI:10.1002/APP.43984.
[18]VO T,VORA K,MINAIE B.Effects of postcure temperature variation on hygrothermal-mechanical properties of an out-of-autoclave polymer composite[J].J.Appl.Polym.Sci.,2013,3090-3097.
[19]张宝艳,陈祥宝.低温固化树脂及复合材料的研究与应用[J].材料工程,2002(增刊):248-252.
[20]张宝艳,陈祥宝,刘天舒,等.低温真空压力成型树脂体系研制[J].航空材料学报,2003,23:10-12.
[21]陈文.从两会看低成本有机复合材料制造技术的发展[J].航空制造工程,1997(10):10-12.
[22]陈亚莉.低成本复合材料技术的新进展(一)[J].航空工程与维修,2001(1):17-19.
[23]RUSSELL J D,SHENK B,HOLZWARTH R,et al.Advanced composite cargo aircraft[C]//Proc 41stint SAMPE tech conf.Witchita,KA:Society for the Advancement of Material and Process Engineering,2009.
[24]廉伟.低成本非热压罐工艺在飞机复材结构上的应用[C]//梦想成真的推动力-2011年商用飞机复合材料应用国际论坛,上海,2011.
[25]RIDGARD C.Advances in low temperature curing prepregs for aerospace structures[C]//Proc SAMPE 2000 conf.Long Beach,CA:Society for the Advancement of Material and Process Engineering,2000.
[26]RIDGARD C.Out of autoclave composite technology for aerospace,defense and space structures[C]//Proc.SAMPE2009 conf.Baltimore,MD:Society for the Advancement of Material and Process Engineering,2009.
[27]黄诚,刘德博,吴会强,等.我国航天运载器复合材料贮箱应用展望[J].沈阳航空航天大学学报,2016,33(2):27-35.
[28]LANE S A,HIGGINS J,BISKNER A,et al.Out-ofautoclave composite fairing design,fabrication,and test[J].Journal of Manufacturing Science and Engineering,2011,133:031020-1-031020-10.