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SiC_p/2024Al复合材料板材脉冲电流辅助拉深成形 被引量:15

Pulse current auxiliary deep drawing of SiC_p/2024Al composites sheet
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摘要 为解决颗粒增强铝基复合材料塑性加工困难的问题,采用脉冲电流辅助热拉深成形工艺。利用脉冲电流产生的焦耳热效应加热坯料,加热速度快、效率高,极大减少了坯料在加热过程中的热损耗。脉冲电流密度达到21.7A.mm-2时,坯料温度达到成形温度400℃。同时,铜电极和坯料之间安装的高电阻、低热传导率的不锈钢隔热片,有效地减小了坯料与电极间的热传导,提高了坯料的温度场分布均匀性。成形的工件表面质量光滑、形状精确、厚度均匀、无明显划伤和褶皱,圆角处无显微裂纹出现,尺寸精度达到±0.2mm。脉冲电流辅助热拉深成形工艺为SiCp/2024Al复合材料板材的塑性加工提供了一种高效、节能的绿色工艺方法。 The feasibility of pulse current auxiliary thermal deep drawing was designed and investigated to form the SiC particle reinforced Aluminum composites sheet.This technique set the sheet directly into the die and inputted high-intensity pulse current to heat sheet,which had many advantages,including high-speed heating,lower heat loss and reducing oxidation.The average pulse current density was achieved at 21.7 A·mm-2 with temperature of SiCp/2024Al composites reaching around 400 ℃.During electrification,the stainless steel was inserted between the sheet and the copper electrodes successfully prevented heat dissipation and promoted temperature uniformity.The workpiece shows good shape retention,surface quality and high geometry accuracy.The present investigation has successfully verified the feasibility of process procedure for PCATDD of SiCp/2024Al composites sheet.
出处 《锻压技术》 CAS CSCD 北大核心 2012年第5期22-26,共5页 Forging & Stamping Technology
基金 国家自然科学基金资助项目(51175112) 中央高校基本科研业务费专项资金资助项目(HIT.KLOF.2010039)
关键词 SiCp/2024Al基复合材料 脉冲电流 热拉深成形 温度场分布 SiCp/2024Al composites pulse current thermal deep drawing temperature distribution
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参考文献14

  • 1Mohan B, Rajadurai A, Satyanarayana K G. Electric dis-charge machining of Al-SiC metal matrix composites using ro-tary tube electrode [J]. Journal of Materials ProcessingTechnology, 2004,153- 154: 978- 985.
  • 2Sahin Y. Preparation and some properties of SiC particle rein-forced aluminium alloy composites [J]. Materials and De-sign, 2003,24: 671 - 679.
  • 3崔岩.碳化硅颗粒增强铝基复合材料的航空航天应用[J].材料工程,2002,30(6):3-6. 被引量:229
  • 4毕敬,肖伯律,马宗义.SiCp/2024铝基复合材料的超塑性变形行为研究[J].金属学报,2002,38(6):621-624. 被引量:4
  • 5胡代忠,陈礼清,赵明久,毕敬,徐永波.SiC颗粒增强铝基复合材料薄板的力学性能[J].中国有色金属学报,2000,10(6):827-831. 被引量:13
  • 6Mori K, Maki S, Tanaka Y. Warm and hot stamping of ultrahigh tensile strength steel sheets using resistance heating[J ]. CIRP Annals-Manufacturing Technology,2005, 54(1): 209- 212.
  • 7Yanagimoto J, Izumi R. Continuous electric resistance heat-ing-Hot forming system for high-alloy metals with poor work-ability [J]. Journal of Materials Processing Technology,2009’ 209: 3060-3068.
  • 8Maki S,Harada Y,MdH K. Application of resistance sinteringtechnique to fabrication of metal matrix composite [J]. Journal ofMaterials Processing Technology, 2001,119: 210 - 215.
  • 9Maki S, Mori K? Ishiguro M. Improvement of productstrength and formability in stamping of Al-Mg-Si alloy sheetshaving bake harden-ability by resistance heat and artificial ag-ing treatments [J]. International Journal of Machine Tools& Manufacture, 2006,46: 1996- 1971.
  • 10Xu Z H,Tang G Y,Tian S Q. Research of electroplastic roil-ing of AZ31 Mg alloy strip [J]. Journal of Materials Process-ing Technology, 2007, 182: 128- 133.

二级参考文献30

  • 1陈亚莉.美国F-22先进战斗机选材分析.航空信息研究报告,YH95016-00400[M].,1995..
  • 2H Liu B.Michel.-[J].材料研究学报,1995,9:561-571.
  • 3张迎久.-[J].材料导报,1997,11(3):52-56.
  • 4李义春.-[J].材料研究学报,1995,9:555-559.
  • 5中国航空信息中心.1996年世界国防科技与武器装备发展动态(三)[M].,1997.58.
  • 6丁立铭 饶勤 等.F-22战斗机选材与制造技术.航空信息研究报告[M].,1996,6.25-26.
  • 7崔岩 张少卿.2000年材料科学与工程进展[M].北京:冶金工业出版社,2001.1591-1594.
  • 8[1]Han B Q, Chan K C. Scr Mater, 1997; 36:593
  • 9[2]Jeong H G, Hiraga K, Cho H S, Kim M S. Mater Lett,2000, 45:86
  • 10[3]Chan K C, Tong G Q. Mater Lett, 2001; 51:389

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