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超温处理对GH4169合金显微组织及拉伸性能影响规律研究 被引量:2

Study on Effect of Overheat Treatment on Microstructure and Tensile Properties of GH4169
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摘要 采用不同热处理参数模拟超温服役工况,研究了超温工况下温度和时间对GH4169合金显微组织形貌和力学性能的影响。结果表明:合金内δ相的含量随温度的升高呈先升高后下降的趋势,900℃时δ相的析出量最大。在800~950℃时,δ相随超温时间的增加而增加,在1000~1050℃时,δ 相随超温时间的增加而减少。合金的显微维氏硬度随超温处理温度的升高而不断下降。800~900℃和950~1000℃时,GH4169合金的抗拉强度随超温处理温度的升高大致呈下降的趋势,900~950℃时,合金的抗拉强度变化不明显。合金的塑性随温度的升高而持续增大。 The effects of temperature and time on the microstructure and mechanical properties of GH4169 alloy were studied by using different heat treatment parameters to simulate the superheating service condition. The results show that, the content amount of δ phase in the alloy increases first and then decreases with the increase of temperature, and the precipitation of δ phase is the largest at 900 ℃. In 800-950 ℃, the δ phase increases with the increase of superheating time, while in 1000-1050 ℃, the δ phase decreases with the increase of superheating time. The micro-Vickers hardness of the alloy decreases with the increase of superheating treatment temperature. In 800-900 ℃ and 950-1000 ℃, the tensile strength of GH4169 alloy decreases with the increase of superheating treatment temperature. In 900-950 ℃, the tensile strength of the alloy does not change significantly. The plasticity of the alloy continues to increase with the increase of temperature.
作者 宋肖肖 杨文瑾 齐硕 张汛涛 陈昇 李宝轩 陈佳艺 SONG Xiaoxiao;YNAG Wenjin;QI Shuo;ZHANG Xuntao;CHEN Sheng;LI Baoxuan;CHEN Jiayi(Sino-European Institute of Aviation,Civil Aviation University of China,Tianjin 300300,China)
出处 《热加工工艺》 CSCD 北大核心 2018年第22期185-190,共6页 Hot Working Technology
基金 国家自然科学基金项目(11502285) 中央高校基本科研业务费项目中国民航大学专项项目(3122017113)
关键词 GH4169合金 超温热处理 显微维氏硬度 Δ相 拉伸性能 GH4169 alloy overheat treatment Vickers hardness δ phase tensile properties
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  • 1介红恩,谢蓉,黄钟岳.汽轮机末级动叶片断裂级性能数值研究[J].燃气轮机技术,2006,19(4):51-54. 被引量:2
  • 2彭泽琰 刘刚.航空燃气轮机原理[M].北京:国防工业出版社,2000..
  • 3鲁风鸣,金槿秀.GH169合金涡轮盘件长期时效组织稳定性的研究[J].金属学报,1995,(31增刊):14.
  • 4Muzyka D B. Physical metallurgy and effects d process variables on the microstructure of wrought superalloys [A]. Donachie M J, Jr. Superalloys [C]. American Society fox Metals, 1984.248.
  • 5Cremisio R S, Butter H M, Radavich J F. The effect of thermomechanical history on the stability of alloy 718 [J]. J. d Metal,1969, (11): 55.
  • 6航空工业总公司第621研究所.GH4169合金(Inconel 718)合金国内外标准选编[M].北京:《材料工程》印刷厂,1995.48.
  • 7Barker J F, Ross E W, Radavich J F. Long time stability d incond718 [J]. J. of Metals, 1970, (1): 31.
  • 8Muller J F, Donachie M J. The effects of solution and intermediate heat treatments on notch-rupture behavior of Ineond 718 [J].Metallurgical Trans., 1975, 6A(12): 2221.
  • 9Muzyka D K. Controlling microstructures and properties of superalloys via use of pn~cipitated phases [J]. Metals Eng. Quart.,1971, (11): 12.
  • 10WillWJ.热处理对GH4169合金的室温和高温断裂韧性的影响[J].国外金属材料,1980,(12):22-22.

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