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DZ40M合金的热疲劳性能 被引量:14

Thermal Fatigue Properties of DZ40M Alloy
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摘要 采用扫描电子显微镜研究DZ40M定向凝固钴基高温合金的热疲劳性能。结果表明,随着上限温度的升高,裂纹扩展速率增加,热疲劳抗力降低。在上限温度相同时,随着保温时间的延长,热疲劳性能提高,在合金表面形成均匀致密的氧化物保护膜有利于热疲劳性能的提高。由于碳化物与基体的热膨胀系数不同,合金在受温度交替变化时,易在基体和碳化物界面处产生裂纹孔洞,从而萌生裂纹。热疲劳裂纹通过裂纹孔洞的相互连接向前扩展。 Thermal fatigue properties of DZ40M directionally solidified cobalt-base superalloy was investigated by scanning electric microscope. The results show that the crack propagation rate increases and the thermal fatigue resistance decreases with the rise of the upper temperature. Resistance of thermal fatigue is improved with the holding time prolonging at the same upper temperature, which is caused by the formation of uniform and compact film of oxide on the surface. Due to different thermal expanding coefficients of the matrix and the carbides, crack holes are easily formed in the boundary of the matrix and carbides at alternating temperatures during thermal fatigue; as a result, cracks of thermal fatigue initiate. The interconnection of crack holes makes thermal fatigue crack propagate.
出处 《稀有金属材料与工程》 SCIE EI CAS CSCD 北大核心 2011年第1期152-155,共4页 Rare Metal Materials and Engineering
关键词 DZ40M合金 热疲劳 裂纹萌生 裂纹扩展 DZ40M alloy thermal fatigue crack initiation crack propagation
作者简介 夏鹏成,男,1977年生,博士,讲师,山东科技大学材料学院,山东青岛266510,电话:0532—80691738,E-mal:xpc328@126.com
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参考文献10

  • 1Huang Qianyao(黄乾尧), Li Hankang(李汉康) et al. Superalloy(高温合金)[M]. Beijing: Metallurgy Industry Press,2000
  • 2Sims C T. Superalloys if[M]. New York: John Wiley & Sons, 1987:3.
  • 3Matthew J, Donachie J. Superalloy[M]. Ohio: American Society for Metals, 1984:3.
  • 4李友林,袁超,郭建亭.铸造镍基高温合金K445的热疲劳行为[J].金属学报,2006,42(10):1056-1060. 被引量:16
  • 5Woodfood D A, Mowbray D F. Mater Sci Eng[J], 1974, 16:5.
  • 6Frankli A W, Heslop J, Smith R A. J Inst Met[J], 1963-1964, 92:313.
  • 7夏鹏成,于金江,孙晓峰,管恒荣,胡壮麒.DZ951合金的热疲劳性能[J].稀有金属材料与工程,2008,37(1):50-53. 被引量:11
  • 8Yang J X, Zheng Q, Sun X F et al. Rare Metal [J], 2006, 25:202.
  • 9于金江,孙晓峰,侯贵臣,金涛,管恒荣,胡壮麒.M951合金的热疲劳行为[J].钢铁研究学报,2003,15(z1):179-182. 被引量:6
  • 10Blumm M, Mestral B D, Eggeler Get al. Scr Metall Mater[J], 1995, 33(5): 719.

二级参考文献34

  • 1于金江,孙晓峰,侯贵臣,金涛,管恒荣,胡壮麒.M951合金的热疲劳行为[J].钢铁研究学报,2003,15(z1):179-182. 被引量:6
  • 2李志军,周兰章,郭建亭,姚俊.返回料添加比例对K44合金热疲劳性能的影响[J].材料工程,2005,33(8):24-27. 被引量:8
  • 3夏鹏成,于金江,孙晓峰,赵乃仁,侯桂臣,管恒荣,胡壮麒.热处理对定向镍基高温合金DZ951γ′相的影响[J].稀有金属材料与工程,2006,35(5):779-782. 被引量:21
  • 4[1]Woodford D A, Mowbray D F. Materials Science and Engineering, 1974,16:5-43.
  • 5[2]Glenny E, Taylor T A. J Inst Metals, 1960,88:449.
  • 6[3]Glenny E. Proc Conf on Thermal and High Strain Fatigue. Metals and Metallurgy Trust, 1967. 346.
  • 7[4]Coffin H E. ASTM Symp on Fatigue at Elevated Temperature. 1972.
  • 8[5]Howes M A H. NASA Cr-72738. USA: NASA, 1970.
  • 9袁福河 孙晓峰 管恒荣.一种钴基高温全金的热疲劳行为[J].材料工程,2001,:22-24,28.
  • 10Varin J D. In: Sims C T, Hagel W C eds, The Superalloys,New York: John Wiley & Sons, 1972:242

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