高性能S_2/Eps复合材料性能研究
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- 英文论文题名：RESEARCH ON HIGH-PERFORMANCE S_2/Eps COMPOSITE
- 论文作者：贾雪 ; 李晓光 ; 孙立娜 ; 韩明轩 ; 贾丽霞
- 英文论文作者：JIA Xue ; LI Xiao-guang ; SUN Li-na ; HAN Ming-xuan ; Harbin FRP Institute ; Johns Hopkins University ; school of medicine
- 年：2016
- 作者机构：哈尔滨玻璃钢研究院;Johns Hopkins University,school of medicine;
- 论文关键词：高性能 ; 层间剪切强度
- 英文论文关键词：high-performance ; ILSS(interlaminar shear strength)
- 会议召开时间：2016-09-22
- 会议录名称：第二十一届全国玻璃钢/复合材料学术年会论文集（《玻璃钢/复合材料》2016增刊）
- 语种：中文
- 分类号：TB332
- 学会代码：EUGQ
- 会议名称：第二十一届全国玻璃钢/复合材料学术年会
- 会议地点：中国黑龙江哈尔滨
- 主办单位：中国硅酸盐学会玻璃钢分会
- 学会名称：中国硅酸盐学会
- 页数：3
- 文件大小：302k
- 原文格式：O
- 会议级别：全国
摘要
采用自制环氧配方(记为Eps),以研制低成本、高性能高强玻纤环氧树脂基复合材料为目标,研究了1200Tex高强玻纤/环氧树脂复合材料(记为1200Tex/Eps)和240Tex高强玻纤/环氧树脂复合材料(记为240Tex/Eps)的界面性能和力学性能。研究结果表明,以自制环氧配方以及相同的缠绕工艺和固化工艺制备的1200Tex/Eps复合材料与240Tex/Eps复合材料的界面性能和力学性能良好。1200Tex/Eps复合材料单向板和240Tex/Eps复合材料单向板层间剪切强度分别为86.73MPa和76.68MPa;弯曲强度分别为1621.50MPa和1718.50MPa;弯曲模量分别为50.88GPa和46.70GPa。1200Tex/Eps和240Tex/Eps都能制作高性能环氧基复合材料,1200Tex高强玻纤有助于提高生产效率,降低成本。
Aiming at developing the low-cost and high-performance epoxy resin matrix composite,we used selfmade epoxy/anhydride formulation(denoted by Eps),and studied the inteifacial and mechanical properties of 1200 Tex high strength glass fiber /epoxy resin matrix composite(denoted 1200 Tex/Eps),and 240 Tex high strength glass fiber /epoxy resin matrix composite(240 Tex/Eps).The results showed that the 1200 Tex/Eps and 240Tex/Eps composite which were prepared by Eps and the same filament winding and curing process,performed good interfacial and mechanical properties.The interlaminar shear strength(ILSS) of the composite unidirectional laminates of the 1200 Tex/Eps and 240 Tex/Eps are 86.73 MPa and 76.68 MPa respectively:the flexural strength of them are 1621.50 MPa and 1718.50 MPa,and the flexural modulus of them are 50.88 GPa and 46.70 GPa respectively.In conclusion,both the 1200 Tex/Eps and 240 Tex/Eps matrix composites could be used to make highperformance epoxy resin matrix composite,and 1200 Tex high strength glass fiber increases productivity and lowers the cost.
Aiming at developing the low-cost and high-performance epoxy resin matrix composite,we used selfmade epoxy/anhydride formulation(denoted by Eps),and studied the inteifacial and mechanical properties of 1200 Tex high strength glass fiber /epoxy resin matrix composite(denoted 1200 Tex/Eps),and 240 Tex high strength glass fiber /epoxy resin matrix composite(240 Tex/Eps).The results showed that the 1200 Tex/Eps and 240Tex/Eps composite which were prepared by Eps and the same filament winding and curing process,performed good interfacial and mechanical properties.The interlaminar shear strength(ILSS) of the composite unidirectional laminates of the 1200 Tex/Eps and 240 Tex/Eps are 86.73 MPa and 76.68 MPa respectively:the flexural strength of them are 1621.50 MPa and 1718.50 MPa,and the flexural modulus of them are 50.88 GPa and 46.70 GPa respectively.In conclusion,both the 1200 Tex/Eps and 240 Tex/Eps matrix composites could be used to make highperformance epoxy resin matrix composite,and 1200 Tex high strength glass fiber increases productivity and lowers the cost.
引文
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[15]田谷稔."The future and Problem of heat resistant Composite Materials"FRP Symposium,1990.
[2]贾丽霞,王春雨,丁新静,等.复合材料耐低温耐腐蚀性能研究(I)[J].纤维复合材料,2011,28(1):24-26.
[3]张大厚.防腐蚀复合材料及其应用[M].北京:化学工业出版社.2006.
[4]中国航空研究院编著.复合材料结构设计手册[M].北京:航空工业出版社,2001:482-505.
[5]翁祖祺,陈博,张长发.中国玻璃钢大全[M].北京:国防工业出版社,1992.
[6]JIA Lixia.Research on the Process and Perfonnance of Heat Resistant Composites of Carbon Fiber/Polyimide[C]//ACCM-1Proceeding.Osaka Japan,1998:218-1-10.
[7]乔海霞,曾竟成,杜刚.混杂纤维增强环氧树脂复合材料电缆芯湿热老化性能研究[J].玻璃钢/复合材料,2007(1):42-45.
[8]#12
[9]褚兵强.低能量冲击对含孔隙CFRP层合板力学性能的影响研究[C].哈尔滨工业大学硕士论文,2011.
[10]蒋海平,彭如恕,毛杰勇,等.树脂基复合材料耐腐蚀性能的研究进展[J].机械研究与应用,2014.
[11]潘利剑.粘弹阻尼层共固化复合材料的性能研究与优化设计[D].《哈尔滨工业大学博士论文,2009.
[12]杨国腾,王巍.复合材料弯曲性能测试的研究[c].2012航空试验测试技术学术交流会论文集,2012.
[13]李典森,卢子兴,李嘉禄,等.三维编织T300/环氧复合材料的弯曲性能及破坏机理[N/OL].航空材料学报,2009.
[14]赵伟栋,张宗强,耿东兵,等.低温聚合物基复合材料研究进展[J].宇航材料工艺,2003,(5):21-25.
[15]田谷稔."The future and Problem of heat resistant Composite Materials"FRP Symposium,1990.