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GH864合金组织特征对裂纹扩展速率的影响 被引量:4

Effect of microstructure characteristics on the fatigue crack propagation rate of GH864 alloy
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摘要 利用光学显微镜、场发射扫描电镜等手段,研究了GH864合金三种轧制态组织经热处理后的演变过程,分析了热处理后不同组织对室温冲击韧性及高温650℃裂纹扩展速率的影响.结果表明,GH864合金由初始轧制态组织经标准热处理后(1020℃,4h/空冷→845℃,4h/空冷→760℃,16h/空冷)获得的晶粒组织,其晶粒组织演变具有明显的一致性,而合金的晶界碳化物分布及基体γ'强化相没有明显差别,其分布状态及尺寸大小基本一致.热处理后的晶粒尺寸越大,抗裂纹扩展能力越好,合金的室温冲击韧性越低;热处理后形成的项链状组织,对合金冲击韧性及裂纹扩展速率有较好的影响. The evolution of three different initial microstructures of GH864 alloy after heat treatment was studied by optical microscopy(OM) and field emission scanning electron microscopy(FESEM).The impact toughness at room temperature and crack propagation rate at 650℃ were analyzed after heat treatment.The results indicate that the grain microstructural evolution of GH864 alloy is hereditary between initial forging state and heat treatment state after 1020℃,4h/air cooling→845℃,4h/air cooling→760℃,16h/air cooling,while carbides in grain boundaries and γ′ phases are not significantly different.The larger the grain size,the better crack propagation behavior the alloy has,and the worse the impact toughness is.It is highlighting that the necklace microstructure has a better effect to improve the impact toughness and crack propagation behavior of GH864 alloy.
出处 《北京科技大学学报》 EI CAS CSCD 北大核心 2011年第12期1501-1507,共7页 Journal of University of Science and Technology Beijing
基金 国家自然科学基金资助项目(51071017)
关键词 高温合金 镍基合金 组织转变 析出相 裂纹扩展 superalloys nickel base alloys microstructural evolution precipitates crack propagation
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参考文献11

  • 1Whelchel R L, Kelekanjeri V S K G, Gerhardt R A, et al. Effect of aging treatment on the microstructure and resistivity of a nickel- base superanoy. Metall Mater Trans A, 2011, 42(5) :1362.
  • 2Chang K M, Liu X B. Effect of γ content on the mechanical behavior of the WASPALOY alloy system. Mater Sci Eng A, 2001, 308(1/2) : 1.
  • 3Semiatin S L, Fagin P N, Glavicic M G, et al. Deformation behavior of Waspaloy at hot-working temperatures. Scripta Muter, 2004, 50(5) : 625.
  • 4姚志浩,董建新,张麦仓,郑磊.GH864合金显微组织与力学性能的关联性[J].稀有金属材料与工程,2010,39(9):1565-1570. 被引量:24
  • 5Penkalla H J, Wosik J, Czyrska-Filemonowicz A. Quantitative mi- crostructural characterisation of Ni-base superalloys. Mater Chem Phys, 2003, 81(2/3): 417.
  • 6姚志浩,洪成淼,董建新,张麦仓,郑磊.烟气轮机动叶片断裂原因分析[J].失效分析与预防,2008,3(4):23-27. 被引量:8
  • 7Liu X B, Kang B, Chang K M. The effect ofhold-tlme on fatigue crack growth behaviors of Waspaloy alloy at elevated temperature. Mater Sci Eng A, 2003, 340(1/2): 8.
  • 8Sadananda K, Vasudevan A K. Analysis of high temperature fa- tigue crack growth behavior, lnt J Fatigue, 1997, 19 ( Suppl 1 ) : S183.
  • 9Mao J, Chang K M, Yang W H,et al. Cooling precipitation and strengthening study in powder metallurgy superalloy Rene88DT. Mater Sci Eng A, 2002, 332(1/2): 318.
  • 10Osinkolu G A, Onofrio G, Marchinni M. Fatigue crack growth in polycrystalline IN 718 superalloy. Mater Sci Eng A, 2003, 356 ( 1/2) : 425.

二级参考文献10

  • 1董建新,丁利生,王振德.烟气轮机涡轮盘和叶片用WASPALOY合金研究[J].中国材料科技与设备,2006,3(2):68-73. 被引量:18
  • 2郝传龙,董建新,张麦仓,洪成淼.某烟气轮机动叶片榫齿断裂原因分析[J].失效分析与预防,2006,1(4):34-37. 被引量:9
  • 3[4]N.Vardar,A.Ekerim.Failure analysis of gas turbine blades in a thermal powder plant[J].Engineering Failure Analysis,2007,14:743-749.
  • 4[5]P.J.Golden,J.R.Calcaterra.A fracture mechanics life prediction methodology applied to dovetail fretting[J].Tribology International,2006,39(10):1172-1180.
  • 5[6]M.Veigh,P.Alison.Analysis of fretting fatigue in aircraft structure:Stresses,stress intensity factors and life predictions[D].Indiana:Puridue University,1999.1-3.
  • 6[7]M.R.Khajavi,M.H.Shariat.Failure of first stage gas turbine blades[J].Engineering Failure Analysis,2004,1:589-597.
  • 7[10]E.Poursaeidi,M.Salavatian.Failure analysis of generator rotor fan blades[J].Engineering Failure Analysis,2007,14:851-860.
  • 8洪成淼 董建新 张麦仓 等.国产超大型烟气轮机动叶片组织特征[J].北京科技大学学报,2006,28(1):541-541.
  • 9T. J. Garosshen,G. P. McCarthy. Low temperature carbide precipitation in a nickel base superalloy[J] 1985,Metallurgical Transactions A(7):1213~1223
  • 10方文.YL型烟气轮机的开发和应用[J].石油化工设备技术,2000,21(2):30-33. 被引量:14

共引文献29

同被引文献56

  • 1邹金文,汪武祥.粉末高温合金研究进展与应用[J].航空材料学报,2006,26(3):244-250. 被引量:111
  • 2姚志浩,董建新,张麦仓,郑磊.GH864合金显微组织与力学性能的关联性[J].稀有金属材料与工程,2010,39(9):1565-1570. 被引量:24
  • 3董建新,丁利生,王振德.烟气轮机涡轮盘和叶片用WASPALOY合金研究[J].中国材料科技与设备,2006,3(2):68-73. 被引量:18
  • 4赵钺,盖秀颖,宋贵宏.GH864合金在超温条件下的组织性能变化[J].理化检验(物理分册),2007,43(10):498-501. 被引量:6
  • 5Liu X B,Kang B, Chang K M. The effect of hold-time on fatigue crack growth behaviors of Waspaloy alloy at elevated temperature [ J]. Materials Science and Engineering A ,2003,340 : 8 - 14.
  • 6Tokoro K,Wikstrom N P, Ojo O A, et al. Variation in diffusion-induced solidification rate of liquated Ni-Cr-B insert during TLP bonding of Waspaloy superalloy[J]. Materials Science and Engineering,2008,477 : 311 - 318.
  • 7Chang K M,Liu X B. Effect of γ' content on the mechanical behavior of the Waspaloy alloy system [ J]. Materials Science and Engineering A,2001, 308:1-8.
  • 8Mandy L B, Andrew H R. Evaluation of the influence of grain structure on the fatigue variablity of Waspaloy[ C ]//Superalloys 2008, In: Reed R C, Green K A, Caron P, et al. Editors, Superalloys 2008, TMS, Warrendale (PA) ,2008 : 583 - 588.
  • 9Kelekanjeri V,Siva K G, Gerhardt R A. Characterization of mirostructure fluctuations in Waspaloy exposed to 760℃ for times up to 2500h [ J ]. Electrochimica Acta,2006,51 : 1873 - 1880.
  • 10Yao Z H, Zhang M C, Dong J X. Stress rupture fracture model and microstructure evolution for waspaloy [ J ]. Metallurgical and Materials Transactions A ,2013,44 (7) :3084 - 3098.

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