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2000 h高温时效对DD6合金组织的影响

Influence of 2000 h High Temperature Aging on Microstructures of DD6 Alloy
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摘要 研究了第二代单晶高温合金DD6在980℃无应变时效2000 h处理后的显微组织。结果表明:时效时间在1000 h以内时,γ'相呈立方形态分布,平均尺寸长大到1.0μm左右。在时效时间从1000 h增加到2000 h过程中,枝晶干与枝晶间的显微组织变化出现差异,枝晶干处γ'相明显粗化,但仍基本保持立方状;枝晶间γ'相连接、合并,时效2000 h时基本形成筏状组织。DD6合金980℃时效后组织基本稳定,2000 h时效后仅发现少量TCP相析出。 The microstructures of the second generation single crystal superalloy DD6 were investigated after aging at 980 ℃ for 2000 h without sWain. The results show that when the aging time is less than 1000 h, the γ' phase presents a cubic form distribution, and the average size is about 1.0 μm. During the aging time increasing from 1000 h to 2000 h, the difference of microstructure change between dendrite stem and interdendritic appears, the γ' phase at dendrite stem obviouly coarsens, but still basically maintains cube; the γ' phase in interdendritic connects and amalgamates, and the raft microstructure is formed at the aging for 2000 h. The microstructure of DD6 alloy is basically stable after aging at 980℃, and a small amount of TCP (topological closed packed) phase precipitates after aging for 2000 h.
出处 《热加工工艺》 CSCD 北大核心 2017年第14期197-199,共3页 Hot Working Technology
基金 航空科学基金项目(2014ZE21009)
关键词 长期时效 DD6合金 显微组织 TCP相 long term aging DD6 alloy microstructure TCP phase
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  • 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
  • 3西姆斯CT 赵杰(译).高温合金[M].大连:大连理工大学出版社,1991..
  • 4师昌绪.中国高温合金四十年[M].北京:中国科学技术出版社,1996..
  • 5张祖谦 刘志中.涡轮叶片用高温合金发展中的几个问题[J].国际航空,1978,(4):43-48.
  • 6Cetel 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.
  • 7Blavette 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.
  • 8Erickson 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.
  • 9Erickson 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.
  • 10Walston 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.

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