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热处理对变形高铝Ni_3Al基合金组织及性能的影响

Effect of Heat Treatment on Structure and Properties of Deformed Ni_3Al-based Alloy with High Al Content
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摘要 对热变形量56%的高铝Ni3Al基合金在热处理过程中的组织转变进行了研究。结果表明:热处理过程中随β-NiAl相的增大,γ+γ'相区不断向β+γ'相区扩展,借此消除锻后形成的γ'脆性晶界,提高锻后合金的塑性。在γ+γ'两相区,γ'相不断发生回溶;而在β+γ'两相区,随着M23C6向MCⅡ碳化物逆转变的进行,γ相以MCⅡ为形核质点发生再结晶长大。此外于扩大的γ相内有呈方形的粒状γ'相析出,与γ相保持完全共格,可提高合金高温强度。 The microstructure transformation was investigated for Ni3Al-based alloy containing high Al content under 56% hot deformation.The results show that: during the heat treatment,with the increase of the β-NiAl phase,the γ+γ’ phase area has a continuous enlarging towards the β+γ’ phase area,then the γ’ brittle grain boundary can get eliminated depend on that,which can improve the alloy plastic property.On the area of γ+γ’ phase,the γ’ phase has a continuous solid-solution,while on the β+γ’ phase area,with the inverse reaction for the M23C6 carbides changing into MCⅡ carbides happened,the MCⅡ carbides become to the nucleation sites for the γ phase.And some second γ’ phase about 1 μm can also be precipitated on the γ phase grain.Due to the second γ’ phase keeps coherence with the γ phase,the high temperature strength can be improved for the alloy.
出处 《热加工工艺》 CSCD 北大核心 2012年第16期160-164,共5页 Hot Working Technology
基金 "十一五"军品配套项目(保密)
关键词 变形高铝Ni3Al基合金 热处理 组织 性能 deformed Ni3Al-based alloy with high A1 content heat treament microstructure properties
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参考文献8

  • 1Decvi S C, Sikka V K. Nickel and iron aluminides:an over view on properties processing and applications [J]. Intermetallics, 1996, (4) : 357-375.
  • 2田世藩,张国庆,李周,颜鸣皋.先进航空发动机涡轮盘合金及涡轮盘制造[J].航空材料学报,2003,23(z1):233-238. 被引量:49
  • 3张永刚,韩雅芳,陈国良,等.金属问化合物结构材料[M].北京,国防工业出版社,2001.
  • 4Sikka V K, Deevi S C, Viswanathan S, et al. Advances in processing of Ni3Al-based intermetallics and applications [J]. lntermetallics, 2000, (8): 1329-1337.
  • 5Yvrk Prasadi, Sasidhara I S, Sikka V K. Characterization of mechanisms of hot deformation of as-cast nickel aluminide alloy [J]. lntermetallics, 2000, (8) : 987-995.
  • 6李玉清.NiCrWTi铸造高温合金中MC和M23C6的可逆反应.金属学报,1982,18(5):577-580.
  • 7仲增墉 马培立 陈淦生.高合金化镍基变形高温合金中弯曲晶界的初步研究.金属学报,1983,19(3):214-214.
  • 8葛占英,于文秀,杨莲隐,等.奥氏体高温合金弯曲晶界普遍性的研究[J].北京钢铁学院学报,1986,6(专辑1):51-60.

二级参考文献14

  • 1[1]ALLEN M M , et al. Nickel-base superalloy powder metallurgy:state of the art[C]. Progress in Powder Metallurgy,1975,31.
  • 2[2]EVANS D J,et al.Development of a high strength hot isostatically-processed disk alloy MERL-76 [C].Modern Developments in P/M,1980, 14:51-63.
  • 3[3]BARTOS J L,et al.Development of hot isostatically pressed (as-HIP) P/W Rene′ 95 turbine hardware[C].Superalloys: Metallurgy & Manufacture,1976.495-508.
  • 4[4]KRUEGER D D,et al.Development and introduction of a damage tolerant high temperature Ni-base disk alloy Rene-88DT[C].Superalloys 1992,277-286.
  • 5[5]DUEROCQ C,et al.N18 a new damage tolerant P/M superalloy for high temperature[C].Superalloys 1988,63-72.
  • 6[6]HOPPIN G S,et al.Manufacturing processes for long-life gas turbine [J].J of Metals 1986(7):20-23.
  • 7[7]Gabb T P,et al.γ′formation in a Ni-base disk superalloy[C].Superalloys 2000,405-414.
  • 8[8]LACQ D,et al.Microstructure stability and crack growth behaviour of a polycrystalline Ni-base superalloy[C].Superalloys 2000,795-802.
  • 9[9]HUNT D W,et al.Microstructure stability and crack growth behaviour of a polycrystalline Ni-base superalloy [C]. Superalloys 2000,795-802.
  • 10[10]GENEREUX P D,et al.Characterization of freckles in a high strength wrought nickel superalloy[C].Superalloys 2000,19-27.

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