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微量元素Al及热处理工艺对GH3030高温合金性能的影响 被引量:7

Effect of Trace Al Element and Heat Treatment Process on Performance of Refractory Alloy GH3030
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摘要 研究了微量合金元素Al、固溶温度和固溶时间对GH3030高温合金室温综合力学性能的影响,结果表明,微量Al的添加极大地提高了合金的室温拉伸性能,但其添加量必须适中;当Al含量为0.15%时,合金可获得较好的综合性能。合金的综合力学性能对固溶温度和固溶时间较为敏感,最佳的固溶温度和固溶时间相应为1010℃和10min。 The effect of trace alloying element Al, temperature and time of solution treatment on the comprehensive mechanical properties of refractory alloy GH3030 was studied at room temperature. The results show that the addition of a moderate amount of aluminum greatly elevates tensile properties of the alloy at room temperature. The alloy with 0.15% Al will provide good comprehensive mechanical properties, which is sensitive to temperature and time of the solution treatment. The preferable solution treatment process for the alloy lies in heating at 1010 ℃for 10 min.
出处 《热处理》 CAS 2007年第5期43-46,共4页 Heat Treatment
关键词 GH3030高温合金 固溶温度 固溶时间 综合力学性能 GH3030 refractory alloy aluminum solution treatment temperature solution treatment time comprehensive mechanical properties
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参考文献13

  • 1Merrick H F. Precipitation within gamma prime particles in Nickel-base superalloys [ J]. Metallurgical Transactions, 1973, 4( 3 ) : 885-887.
  • 2国为民,冯涤,吴剑涛,张凤戈,张莹,张义文.镍基粉末高温合金冶金工艺的研究与发展[J].材料工程,2002,30(3):44-48. 被引量:17
  • 3邓波,韩光炜,冯涤.低膨胀高温合金的发展及在航空航天业的应用[J].航空材料学报,2003,23(z1):244-249. 被引量:40
  • 4Fleischer R. L. Production and properities of directionally solidified composites [J]. Metals and Materials, 1963, ( 11 ) :203.
  • 5Grosdidier T, Hazotte A, Simon A. Precipitation and dissolution processes in γ/γ' single crystal nickel-based supperalloy [J]. Materials Science and Engineering, 1998, 256(1-2) : 186-196.
  • 6Hazotte A, Grosdidier T, Denis S. γ' precipitate splitting in nickel-based superalloys [J]. A 3-D finite element analysis, 1996, 34 (4) :601-608.
  • 7胡壮麒,彭平,刘轶,金涛,孙晓峰,管恒荣.镍基合金中γ’相界面的强化设计[J].金属学报,2002,38(11):1121-1126. 被引量:21
  • 8《中国航空材料手册》编辑委员会.中国航空材料手册[M].北京:中国标准出版社,2002..
  • 9Douin J, Veyssiere P, Beauchamp P. Dislocation Line Stability in Ni3Al[J]. Metals and Materials, 1986(54) : 375-393.
  • 10黄乾尧,李汉康.高温合金[M].北京:冶金工业出版社,2004:23-25.

二级参考文献52

  • 1张绍维.低膨胀高温合金的发展与应用[J].航空制造工程,1994(9):5-8. 被引量:12
  • 2周兰章,郭建亭.微量硫对K4169合金组织与性能的影响[J].金属学报,1995,31(6). 被引量:8
  • 3李力 杨士仲 等.热等静压及其加锻造和热挤压粉末高温合金FGH95的组织和性能[J].钢铁研究总院学报,1985,5(4):411-415.
  • 4[1]SMITH D F,SMITH J S.A history of controlled low thermal expansion superalloys[A].RUSSELL K C,SMITH D F. Physical Metallurgy of Controlled Expansion Invar-Type Alloys[M]. 1990, 253-272.
  • 5[2]SCOTT Howard .Expansion properties of low-expansion Fe-Co-Ni Alloys[J]. Trans Am Inst of Mining and Metallurgical Engineers,1930, 89 , 506-537.
  • 6[3]HUNSICKER H Y,STUMPF H C.History of precipitation hardening[A].SMITH C S. The Sorby Centennial Symposium on the History of Metallurgy[M].New York: Gordon and Breach Science Publishers, 1965. 271-311.
  • 7[4]PILLING N B,TALBOT A M.Age Hardenable, Nickel - Iron - Chromium - Titanium Alloy Possessing Controlled Thermoelastic Properties[P].U. S. Patent:2266482,1941-12-16.
  • 8[5]EISELSTEIN H L,BELL J K.Alloy Characterized by Controlled Thermoelasticity at Elevated Temperatures[P]. U. S. Patent:3157495, 1964-11-17.
  • 9[6]Huntington Alloys.INCOLOY alloy 903[R]. 5M 7-78 s-51.
  • 10[7]SMITH D F,WENSCHHOF D E.A Survey of Progress in Controlled-Expansion[A]. Age-Hardenable Nickel- Iron- Cobalt Alloys [R]. The TMS-AIME Fall Meeting. Detroit. Michigan. Oct. 18~21,1971.

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