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固溶时效对热等静压制得的TC4钛合金组织与性能的影响 被引量：5

Effect of Solution Aging on Microstructure and Property of TC4 Titanium Alloy Prepared by Hot Isosmtatic Pressing
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摘要 采用热等静压工艺对Ti-6A1-4V雾化预合金粉的粉末冶金技术进行了研究,采用不同的固溶温度、时效温度以及时效时间,研究了热处理工艺对TC4钛合金组织和性能的影响。结果表明,采用预合金粉工艺制备的Ti-6A1-4V粉末钛合金材料性能良好,于965℃固溶并采用水冷,然后在470℃时效,试样的强度较好。 Powder metallurgy technology for pre-alloyed Ti-6Al-4V titanium alloy was studied by hot isosmtatic pressing （HIP）. By using different solution and aging temperature as well as aging time, the effects of heat treatment process on microstructure and properties of TC4 titanium alloy were more syetematically studied. The results show that solution treating at 965℃,cooling to room temperature by water cooling ,and then aging at 470℃ will help to obtain the optimum strength of the alloy.
作者 黎俊初 王晗 张国光 陈同彩
机构地区 南昌航空工业学院材料学院
出处 《热加工工艺》 CSCD 北大核心 2007年第10期65-67,共3页 Hot Working Technology
关键词 TI-6AL-4V 粉末冶金 热等静压 固溶处理 时效 Ti-6Al-4V powder metallurgy hot isosmtatic pressing solution treatment aging
分类号 TG156.9 [金属学及工艺—热处理] TG146.23 [金属学及工艺—金属材料]
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  • 1张秋平,张永寿.Be-Al合金的机械性能[J].飞航导弹,2002(12):57-61. 被引量：8
  • 2孙本双,宋兴海.等静压技术正在促进铍的应用和发展[J].稀有金属与硬质合金,1995,23(1):34-39. 被引量：1
  • 3Eylon D, Froes F H, Parsom L D. Titanium PM components for advanced aerospace applications. Met. Powder Rep., 1983; 38(10) :567 - 571.
  • 4Froes F H. Prealloyed titanium powder metallurgy-barriers to use. Int.J. Powder Metall., 1987;23(4) :267 - 269.
  • 5Froes F H, Hebeisen J. Emerging and furture applications for HIP of titanium based materials. In:Li Chenggong,Chen Hongxi-a,Ma Fukang eds. Hot isostatic pressing conference proceedings,HIP'99, Beijing: International academic publishers, 1999:1 - 24.
  • 6Rachuk V S, Goncharov N S, Martynyenko Y A et al. Design, development, and history of the oxygen/hydrogen engine RD-0 120,AIAA 95-2540.
  • 7Froes F H, Eylon D. Developments in titanium powder metallurgy. J. Met., 1980; (4) :47 - 54.
  • 8Sheinker A A, Chananic G R, Bohlen J W. Evaluation and application of prealloyed titanium P/M parts for airframe structures.Int. J. Powder Metall., 1987 ;23(3) : 171 - 179.
  • 9Parsonage T. Beryllium metal matrix composites for aerospace and commercial applications. Materials Science and Technology, 2000,16:733 - 734
  • 10Murray J L, Kahan D J. The Al-Be System ,Phase Diagrams of Binary Beryllium Alloys. ASM International, metals Park, 1987:109

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热加工工艺
2007年 第10期

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