分析了镍基粉末高温合金的成型、热处理等冶金工艺及夹杂缺陷的性质等与合金组织和性能的关系,描述了粉末高温合金的热处理工艺,提出了今后我们粉末高温合金组织性能研究工作的重点.
参考文献
[1] | ASM Metals Handbook Vol 7 Powder Metallurgy[M].Aerospace Applications,1984:646. |
[2] | Decker R F.Strengthening Mechanisms in Nickel-Base Superalloys[J].Climax Molybdenum Company Symposium Zurich |
[3] | 李力.粉冶高温合金近况[J].国外金属材料,1985(08):48. |
[4] | 孙兼,邹金文,刘培英.盘件用粉末高温合金的研究与发展[J].航空工程与维修,2001(1):29-30. |
[5] | Davidson J H;AubinC .High Temp Alloys for Gas Turbines[Z].,1982. |
[6] | 汪武祥;周瑞发.Rene95粉末高温合金的缺陷与粉末盘的可靠性[A].北京:航空材料研究所,1990:16. |
[7] | Eric S Huron;Paul G Roth.The in fluence of inclusion on low cycle fatigue life in a P/M Nickel-base disk superalloy Superalloys[M].The MineralsMetals & Materials Society USA,1996:359. |
[8] | Shamblen C E;Chang D R .Effect of Inclusiion on LCF Life of HIP Plus Heat Treated Powder Metal Rene95[J].Metallurgical and Materials Transactions B:Process Metallurgy and Materials Processing Science,1985,16:775. |
[9] | Mark G Benz et al.Eleceroslag Refining Beam Meting and Refining State of the Art[Z].USA,1992. |
[10] | Crison J;Ppemy L .Fatigue failure probability in a powder metallurgy Ni-base superalloy[J].Engineering Fracture Mechanics,1997,57(01):41. |
[11] | General Electric CompanyAircrafe Engine Group .Development of Hot Isoseatically Pressed ReneW95 Turbine Parts[R].AD A043688 |
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