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复合材料带曲率C型梁热隔膜预成型试验与仿真分析

Experiment and Simulation Analysis of Hot Diaphragm Forming about Composite C-Beam with Curvature
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摘要 随着复合材料自动铺带和铺丝技术的成熟,并且广泛应用于复合材料结构的生产与制造。通过与铺带或铺丝技术相结合使得复合材料热隔膜预成型技术成为制作L型、C型,Z型等细长零件的重要手段,此种方式可以减少大量的人工操作,并且能够用于实现自动化工业生产。复合材料热隔膜预成型是一个使预浸料叠层变形的复杂过程,本文对带曲率C型梁的预成型过程进行仿真分析,首先通过试验得到预浸料铺层间摩擦系数,然后对湿态预浸料的力学性能进行测试。利用测试得到参数,采用有限元方法对C型梁预成型过程中铺层间的滑移进行模拟得到了铺层变形后的褶皱缺陷。通过专用的热隔膜成型设备对C型梁预成型进行试验研究,将试验结果与仿真结果进行对比分析,验证了预成型仿真手段的可行性,为后续热隔膜预成型过程中的参数优化提供指导。 With the maturity of composite material automatic tape laying(ATL)and automatic fiber placement(AFP),it is widely used in the production and manufacture of composite structure.Combining with ATL or AFP method,hot diaphragm forming(HDF)has become an important means of making L,C,Z and other slender structures.This method can reduce lots of manual operations and can be used for automatic industrial production.The HDF is a complex deformation process.In this paper,the simulation of the forming process of the C-beam with curvature is carried out.Firstly,the friction coefficient between the plies is obtained through the test,and then the mechanical properties of the wet prepreg are tested.The interlayer slipping during the forming process is simulated to obtain the wrinkle defects after the deformation of the composite plies.Experimental research on C-beam preforming is carried out with special thermal diaphragm forming equipment,and the experiment results were compared with simulation results to verify the feasibility of the preforming simulation method and provide guidance for parameter optimization in the subsequent HDF process.
作者 亚纪轩 叶亮 丁惢 刘传军 YA Jixuan;YE Liang;DING Suo;LIU Chuanjun(CNBM(Shanghai)Aviation Technology Co.,Ltd.,Shanghai 200126)
出处 《纤维复合材料》 CAS 2023年第2期42-48,共7页 Fiber Composites
关键词 复合材料 热隔膜预成型 有限元仿真分析 褶皱 层间滑移 composite material hot diaphragm forming finite element simulation wrinkle interlayer slipping
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  • 1元振毅,王永军,张跃,杨选宏,王俊彪,魏生民.基于材料性能时变特性的复合材料固化过程多场耦合数值模拟[J].复合材料学报,2015,32(1):167-175. 被引量:29
  • 2陈绍杰.复合材料与B7E7"梦想"飞机[J].航空制造技术,2005,48(1):34-37. 被引量:22
  • 3张卫红,吴琼,高彤.周期性金属桁架夹芯板的力学性能研究进展[J].昆明理工大学学报(理工版),2005,30(6):24-28. 被引量:7
  • 4章继峰,张博明,杜善义.平板型复合材料格栅结构的增强改进与参数设计[J].复合材料学报,2006,23(3):153-157. 被引量:13
  • 5师昌绪.材料大词典[M].北京:化学工业出版社,1994..
  • 6EDAS Deutschland GmbH, Corporate Research Center. The research requirements of the transport sectors to facilitate an increased usage of composite materials I: The composite material research requirements of the aerospace industry [EB/OL]. [2006- 12- 27] http:// gcep. stanford, edu/pdfs/as-sessment s/adv_t ransportation_assessment, pdf.
  • 7Darrel T, Byron R P. Advanced composites development for aerospace applications [EB/OL]. [2006-12-27]. http://cite-seer. ist. psu. edu/cache/papers/cs/29702/ftp: zSzzSztechreports, larc. nasa. govzSzpubzSztlzSzmtgzS zNASA-2001 - 7sampe- drt. pdf/advanced - composites - developme nt- for. pdf.
  • 8Rehfield W R, Cheung R H. SOme basic strategies for aeroelastic tailoring o{ wings with bend-twist coupling [C] //44^th AIAA/ASME/ASCE/AHS Structures, Structural Dynamics and Materials Conference. Norfolk, Virginia: American Institute of Aeronautics and Astronautics, lnc, 2003 : 7-10.
  • 9National Aerospace Laboratory NLR. Aerospace structures and materials status report 2003 [EB/OL]. www. nrel. gov/ncpv/t hin_film/docs/world_pv_st at us_rpt_2003, pdf.
  • 10Robinson M J. A qualitative analysis of some of the issues affecting the cost of composites structures [C]// Proc. 23^th International SAMPE Technical Conf. Covina CA: Society for the Advancement of Material and Process Engineering, 1991: 445-458.

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