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国内先进树脂基复合材料制造技术经过30多年的发展,已初步形成以热熔预浸料制造、热压罐和树脂传递模塑(RTM)成型技术为代表的先进树脂基复合材料制造技术体系,所制备的先进树脂基复合材料已在航空领域得到大量应用.本文中主要介绍国内先进树脂基复合材料热压罐成型技术、RTM成型技术和自动铺放技术的最新进展以及先进树脂基复合材料制造过程模拟与优化技术,讨论了国内先进树脂基复合材料制造技术的主要发展方向.

参考文献

[1] 陈祥宝.聚合物基复合材料手册[M].北京:化学工业出版社,2004:4-5.Chen Xiangbao.Handbook of polymer matrix composites[M].Beijing:Chemical Industry Press,2004:4-5.
[2] 陈绍杰.复合材料技术与大飞机[J].航空学报,2008,29(3):605-610.Chen Shaojie.Composite technology and large aircraft[J].Acta Aeronautics et Astronautica Sinica,2008,29(3):605-610.
[3] 刘代军,陈亚莉.先进树脂基复合材料在航空工业中的应用[J].材料工程,2008,z1:194-198.Liu Daijun,Chen Yali.Application of advanced polymer matrix composites in aviation industry[J].Journal of Materials Enginnering,2008,z1:194-198.
[4] 杜善义.先进复合材料和航空航天[J].复合材料学报,2007,24(1):1-12.Du Shanyi.Advanced composite materials and aerospace engineering[J].Acta Matriae Compositae Sinica,2007,24(1):1-12.
[5] Wilkinsin S P.Reactive blends of amorphous functionalized engineering thermoplastics and bismaleimide/diallyl bisphenol--A resins for high performance composite matrices[C]//International SAMPE Symposium.San Diego:SAMPE,1991,36:482-495.
[6] Steiner P A,Browne J M.Development of failure resistant bismaleimide/carbon composite[J].SAMPE J,1987(3/4):8-14.
[7] Cheng Qunfeng,Fang Zhengping,Yi Xiaosu.Ex-situ concept for toughening the RTMable BMI matrix composite.Part Ⅰ.Improving the interlaminar fracture toughenss[J].Joural of Applied Polymer Science,2008,109:1625-1634.
[8] Cheng Qunfeng,Fang Zhengping,Yi Xiaosu.Ex-situ concept for toughening the RTMable BMI matrix composite.Ⅱ.Improving the compression after impact[J].Journal of Applied Polymer Science,2008,108:2211-2217.
[9] 邢丽英,李斌太.一种树脂基复合材料层间增韧方法:中国,200810075870.X[P].2008-06-27.Xing Liying,Li Bintai.A interlaminar toughenss technology of polymer matrix composites:China,200810075870.X[P].2008-06-27.
[10] Ruud N.Rapid tooling for Resin Transfer Moulding,RTM[C]//Proceedings of the Sixth International Conference on Rapid Prototyping.Dayton,OH:Rapid Prototyping Journal,1995:205-215.
[11] Brouwer W D,Herpt van E,Labordus M.Vacuum injection moulding for large structural applications[J].Composites Part A:Applied Sdence and Manufacturing,2003,34(6):551-558.
[12] Suh J D,Lee D G.Manufacture of composite screw rotors for air compressors by RTM process[J].Journal of Materials Processing Technology,2001,113(1-3):196-201.
[13] 益小苏.先进复合材料技术研究与进展[M].北京:国防工业出版社,2006.Yi Xiaosu.Research and development of advanced composites[M].Beijing:National Defence Industry Press,2006.
[14] 陈祥宝.先进树脂基复合材料制造模拟与优化技术[M].北京:化学工业出版社,2006:7-15.Chen Xiangbao.The simulation and optimization technology of advanced polymer composites[M].Beijing:Chemical Industry Press,2006:7-15.
[15] 肖 军,李 勇,李建龙.自动铺放技术在大型航空复合材料结构中的应用[J].航空制造技术,2008(1):50-53.Xiao Jun,Li Yong,Li Jianlong.The application of automatic laying technique on manufacturing of large scale aeronautical composite structures[J].Aeronautical Manufacturing Technology,2008(1):50-53.
[16] Grimshaw M.Tape laying large composite structures[M].Cincinnati:Cincinnati Machine,2004.
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