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可控燃烧合成高体积分数(Al3Ti+B4C)/Al复合材料

Controlled Combustion Synthesis of High Volume Fraction (Al3Ti+B4C)/Al Composite
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摘要 基于Al-Ti-B4C体系,采用原位反应工艺-燃烧反应法制备了高体积分数(Al_3Ti+B_4C)/Al复合材料,研究了燃烧环境对反应进程和致密化的影响。结果表明,850℃铝液的高速热源和控温介质作用,可使压块发生可控燃烧反应,在2 min内制备出致密度大于99%的(Al_3Ti+B_4C)/Al复合材料;燃烧反应的可控性在于仅Al-Ti被引燃,B_4C未参与反应,使燃烧波加热速率较低,所以Al-Ti液相能有效填补压块内部的残余孔隙。 Based on A1-Ti-B4C system, (A13Ti+B4C)/A1 composite with high volume fraction was fabricated by in-situreaction process-combustion reaction method. The effects of combustion environment on the reaction process anddensification process were studied. The results show that the the effect of heat source and the temperature control media of850 ℃ liquid aluminum contributes to the appearance of the controlled bum reaction of the compacts. (A13Ti+BaC)/A1composite with density greater than 99% can be prepared in less than 2 min. The controllability of the combustion reaction liesin the ignition of only A1-Ti, while B4C does not participate in the reaction, which can lead to the combustion wave with alower heating rate, so that the A1-Ti liquid phase can effectively fill the residual porosity in compacts.
作者 刘梦璐 张振亚 陈刚 孟明艾 张再磊 袁方今 LIU Menglu, ZHANG Zhenya, CHEN Gang, MENG Ming'ai, ZHANG Zailei, YUAN Fangjin(1. School of Materials Science and Engineering, Jiangsu University, Zhenjiang 212013, China; 2. Jiangsu Province Key Laboratory of High-end Structural Materials, Zhenjiang 212013, Chin)
出处 《热加工工艺》 CSCD 北大核心 2018年第4期129-133,共5页 Hot Working Technology
基金 江苏省自然基金(青年)项目(BK20140547) 国家自然科学基金资助项目(51174098) 江苏省科技支撑计划项目(BE2012135) 江苏省重点研发计划项目(BE2015148) 江苏高校优势学建设工程资助项目(2014) 江苏省重大科技成果转化项目(BA2014112、BA2015153)
关键词 燃烧反应 致密化 Al-Ti液相 复合材料 组织 combustion synthesis densification AI-Ti liquid phase composite microstructure
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  • 1王自东,李庆春,李春玉,张录山,于桂复.原位TiC粒子增强Al-Si合金的组织及性能[J].金属学报,1994,30(1). 被引量:19
  • 2董尚利,杨德庄.碳化硅晶须和颗粒增强铝基复合材料的时效行为[J].材料工程,1996,24(8):45-48. 被引量:4
  • 3Massardier V, Pelletier L, Merle P. Influence of the introduc-tion of ceramic particles in Al-Cu alloys on G.P. zone formation[J] . Mater Sci Eng, 1998, A 249: 121-133.
  • 4EI-Baradie Z M, EI-Shahat O A, Abd EI-Azim A N. Accele-rated aging process in SiC-7020 aluminum composite[J]. J Mat Proc Tech, 1998,79:1-8.
  • 5Ma Wenchuan, Gu Jialin. Effect of SiC particles on aging behavior of SiCP/7075 composites[J]. J Mater Sci Lett, 1997, 16: 1867-1869.
  • 6Suresh S, Christman T, Sugimure Y. Accelerated aging in a cast alloy-SiC particulate composite[J]. Scripta Metall,1989, 23:1599-1602.
  • 7Song Y, Baker T N. Accelerated aging process in ceramic re-inforced AA6061 composites[J]. Mater Sci Tech, 1994, 10: 406-413.
  • 8Lin J S, Li P X, Wu R J. Aging evaluation of cast particulate-reinforced SiC/Al (2024) composites[J]. Scripta Metall Mater, 1993, 28: 281-286.
  • 9Towle D J, Friend C M. The effect of particulate oxidation on the age-hardening characteristics of SiC/6061 MMC produced by the preform infiltration route[J]. Scripta Metall Trans, 1992, 26: 437-442.
  • 10Badini C, Marino F, Verne E. Calorimetric study on precipi-tation path in 2024 alloy and its SiC composite[J]. Mater Sci Eng, 1995, A 191: 185-191.

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