期刊文献+

抽拉速率对DD6单晶高温合金组织的影响 被引量:5

Effect of Withdrawing Rate on Microstructure of Single Crystal Superalloy DD6
下载PDF
导出
摘要 采用不同的抽拉工艺制备DD6单晶合金,分析了DD6单晶合金的显微组织,研究了不同抽拉工艺对DD6合金组织的影响。结果表明,随着抽拉速率的降低,DD6合金一次枝晶间距增加,枝晶干和枝晶间γ′相尺寸变大,共晶组织呈粗化趋势,γ-γ′共晶组织含量减少,合金中主要元素偏析程度减轻。 The effect of withdrawing rate on microstructure of single crystal superalloy DD6 was investigated.The results show that,with the decreasing of withdrawing rate,the primary dendrite arm spacing increases,the size of γ′ phase in the dendrite core and in the interdendrite increases slightly,the volume fraction of γ-γ′eutetic decreases,and the segregation of main elements decreases.
出处 《材料工程》 EI CAS CSCD 北大核心 2010年第11期8-10,16,共4页 Journal of Materials Engineering
关键词 单晶高温合金 抽拉速率 组织 single crystal superalloy withdrawing rate microstructure
  • 相关文献

参考文献9

  • 1GELL M, DUHL D N, GIAMEI A F. The Development of single crystal superalloy turbine blades[A]. TIEN J K, GEL L M MAURER G, et al. Superalloy 1980[C]. Warrendale, PA TMS, 1980. 205-214.
  • 2CNTEL A D, DUHL D N. Second Generation nickel base single crystal superalloy[A]. RECICHMAN S, DUHL D N, MAUR ERG, et al. Superalloy 1988 [C]. Warrendale, PA: TMS, 1988. 235 244.
  • 3SETH B B. Superalloys the utility gas turbine perspective[A]. POLLOCK T M, KISSINGER R D, BOWMAN R R, et al. Superalloys2000 [C]. Warrendale, PA: TMS, 2003. 3-16.
  • 4LI J R, ZHONG Z G, TANG D Z, et al. Alow-cost second generation single crystal superalloy DD6[A]. POLLOCK T M, KISSINGER R D, BOWMAN R R. et al. Superalloys 2000[C]. Warrendale, PA: TMS, 2000. 777-783.
  • 5李嘉荣 钟振刚 等.低成本第二代镍基单晶高温合金DD6[J].第九届全国高温合金年会学术论文集,金属学报,1999,:266-266.
  • 6胡壮麒,刘丽荣,金涛,孙晓峰.镍基单晶高温合金的发展[J].航空发动机,2005,31(3):1-7. 被引量:231
  • 7CALDWELL E C, FELA F J, FUCHS G E. Segregation of elements in high refractory content single crystal Nickel based superalloys[A]. GREEN K A, POLLOCK T M, HARADA H, et al.Superalloy2004[C]. Warrendale, PA: TMS, 2004. 811-818.
  • 8ZHANG X, HARADA H, ROY. Thermomeehanical fatigue mechanism in a modern single crystal nickel base superalloy TMS- 82[J]. Aeta Materialia, 2008, 56(13): 2975-2987.
  • 9KIM S H,KIM J M,LEE H J,et al. Effect of thermai gradient on solidification microstructure in the Ni-base single crystal superalloy CMSX10[J]. Diffusion and Defect Data:Part A, Solid State Data, Defect and Diffusion Forum, 2008, 273:361-366.

二级参考文献14

  • 1孔祥鑫.第四代战斗机及其动力装置[J].航空科学技术,1994(5):21-23. 被引量:9
  • 2陈荣章.单晶高温合金发展现状[J].材料工程,1995,23(8):3-12. 被引量:110
  • 3Cetel A D, Duhl D N. Second -generation nickel -base single crystal superalloy, Proc. 6th Int. Symp on Superalloys, Eds. D.N. Duhl et al. , 1988: 235.
  • 4Blavette D, Caron P and Khan T. An atom - probe study of some fine - scale microstructural features in Ni - based single crystal superalloys, Superalloys 1988, Reichman S, et al. eds. , The Metallurgical Society, 1988: 305.
  • 5Erickson G L. The development and application of CMSX -10, Superalloys 1996, Kissinger R D, Deye D J, Cetel A D,et al. eds. , TMS 1996: 35.
  • 6Erickson G L. The development of the CMSX - 11B and CMSX - 1lCalloys for industrial gas turbine application, Superalloys 1996, Kissinger R D, Deye D J, Cetel A D,et al.eds. , TMS 1996: 45.
  • 7Walston W S, O' Hara K S and Rose E W. ReneN6: Third generation single crystalsuperalloy, Superalloys 1996, Kissinger R D, Deye D J, Cetel A D,et al. eds. , TMS 1996: 27.
  • 8Erickson G L. USP 5366695, Single crystal nickel - based superalloy, 1994, 11.
  • 9Walston W R, et al. Nickel- base superalloy and article with high temperature strength and improved stability, USP 5270123, 1993, 12.
  • 10Didier A, Cyril V, Yves D, et al. Dominique. MC - NG:A 4th generation single - crystal superalloy for future aeronautical turbine blades and vanes, Superalloys 2000, Pollock T M, Kissinger R D, Bowman R R, et al. eds. ,TMS, 2000: 829.

共引文献231

同被引文献66

引证文献5

二级引证文献6

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部