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Glare层板基本成形性能研究与实验验证
引用本文:田精明,李华冠,刘成,陶刚,张丽清,郑兴伟,刘红兵,陶杰.Glare层板基本成形性能研究与实验验证[J].航空材料学报,2017,37(1).
作者姓名:田精明  李华冠  刘成  陶刚  张丽清  郑兴伟  刘红兵  陶杰
作者单位:1. 南京航空航天大学 材料科学与技术学院,南京,211106;2. 上海飞机制造有限公司,上海,200436
基金项目:国家商用飞机制造工程技术研究中心创新基金资助项目,江苏省普通高校研究生科研创新计划资助项目,江苏省先进结构材料与应用技术重点实验室开放基金资助项目,国家级大学生创新创业训练计划资助项目,江苏高校优势学科建设工程资助项目
摘    要:为了探索Glare层板的成形性能特点,采用单向拉伸实验和三点弯曲实验,分析研究了Glare 2A,Glare 2B和Glare 3层板的基本成形性能,并借助扫描电子显微镜分析了Glare层板的失效特征。结果表明:纤维铺层方向对材料的成形性能存在显著影响,Glare 2A层板抵抗塑性变形的能力强,且难以发生厚向变形:采用σ=σy+Kεn硬化模型拟合真实应力-应变曲线,其相关系数最大,拟合结果最好:Glare 2A的弯曲回弹量最大,其弯曲破坏时,内表层受压应力,以皱缩和压缩断裂为主,外表层受拉应力,以纤维拉伸断裂和分层为主;对于Glare 2B层板,其弯曲回弹量最小,主要以基体破坏为主:通过滚弯成形验证了实验所得结果的准确性。

关 键 词:复合材料  Glare层板  基本成形性能  硬化模型  回弹

Basic Formability Research and Experimental Test of Glass Fiber Reinforced Aluminium Laminates
TIAN Jingming,LI Huaguan,LIU Cheng,TAO Gang,ZHANG Liqing,ZHENG Xingwei,LIU Hongbing,TAO Jie.Basic Formability Research and Experimental Test of Glass Fiber Reinforced Aluminium Laminates[J].Journal of Aeronautical Materials,2017,37(1).
Authors:TIAN Jingming  LI Huaguan  LIU Cheng  TAO Gang  ZHANG Liqing  ZHENG Xingwei  LIU Hongbing  TAO Jie
Abstract:The basic formability of Glare 2A, Glare 2B and Glare 3 laminates was investigated by unidirectional tensile and three-point bending tests to explore the formability characteristics of Glare. Meanwhile, the failure characteristic of Glare was studied by scanning electron microscopy ( SEM) . The results indicate that the direction of the fiber has strong effects on the formability of Glare. The Glare 2A laminates exhibit the strongest resistance to plastic deformation. Meanwhile, it is also hard to deform in thickness direction. σ = σy+Kεn is used to fit the real stress-strain curves of three variants and proves the most suitable model, presenting the maximum correla-tion coefficient. Furthermore, Glare 2A laminates exhibit the most serious bending springback. Shrinkage and compression fracture are visible in the inner layer which bears compressive stress, and fiber fracture and delamination are found in the outer layer which bears tensile stress. On the contrary, Glare 2B laminates show the minimum springback, following with the observed fiber-matrix cracks. Fi-nally, the accuracy of test results is verified by roll bending.
Keywords:composite  Glare laminates  basic formability  hardening model  springback
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