期刊文献+

稳定化处理对优质GH738合金组织及力学性能的影响 被引量:1

Effect of stabilizing treatment on microstructure and mechanical properties of high quality GH738 alloy
原文传递
导出
摘要 采用光学显微镜、扫描电镜和力学性能测试等研究了稳定化处理对优质GH738合金组织及力学性能的影响。结果表明,稳定化温度对优质GH738合金的组织和强度影响不显著,845℃及以下时,随稳定化温度的升高,优质GH738合金的强度和持久寿命略微升高,主要原因在于二次γ′相的尺寸随稳定化温度的升高逐渐长大,一次γ′相尺寸基本不变,二者含量随稳定化温度的升高变化不明显;与稳定化温度相比,稳定化处理时间对优质GH738合金组织和性能的影响作用更加显著,随稳定化时间延长,两种γ′相的尺寸均缓慢长大,而合金强度先升高后降低。不同稳定化处理条件下优质GH738合金的力学性能变化的本质是一次及二次γ′相的尺寸、分布及其与位错的交互作用所致。 Effect of stabilizing treatment on microstructure and mechanical properties of high quality GH738 alloy was studied by means of optical microscope, scanning electron microscopy and mechanical properties test. The results show that the effect of stabilizing temperature on the microstructure and strength of the GH738 alloy is not significant, and when the temperature is equal or lower than 845 ℃, the strength and rupture life of the high-quality GH738 alloy increase slightly with the increase of stabilizing temperature. The main reason is that with the increase of stabilizing temperature, the size of secondary γ′ phase grows up gradually, but the size of primary γ′phase is basically unchanged, and the content of both of them does not change obviously. Compared with stabilizing temperature, the effect of stabilizing time on the microstructure and mechanical properties of the high quality GH738 alloy is obvious, and with the increase of stabilizing time, the sizes of the two γ′ phases grow slowly, while the strength of the alloy increases first and then decreases. The change of mechanical properties of the high quality GH738 alloy under different stabilization conditions is essentially caused by the size and distribution of primary and secondary γ′ phases and their interaction with dislocations.
作者 李钢 荣义 杨成斌 曲敬龙 杜金辉 LI Gang;RONG Yi;YANG Cheng-bin;QU Jing-long;DU Jin-hui(AECC Hunan Aviation Powerplant Research Institute,Zhuzhou 412002,China;Gaona Aero Material Co Ltd,Beijing 100081,China;Beijing Key Laboratory of Advanced High Temperature Materials,Central Iron and Steel Research Institute,Beijing 100081,China)
出处 《材料热处理学报》 CAS CSCD 北大核心 2021年第7期65-71,共7页 Transactions of Materials and Heat Treatment
基金 某发动机用优质GH738合金涡轮盘锻件研制(XXXX-2016-076)。
关键词 优质GH738合金 稳定化处理 组织性能 high quality GH738 alloy stabilizing treatment microstructure and mechanical property
  • 相关文献

参考文献4

二级参考文献38

  • 1曹春晓.选材判据的变化与高损伤容限钛合金的发展[J].金属学报,2002,38(z1):4-11. 被引量:104
  • 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
  • 4Merrick H F, Floreen S. The effects of microstructure on elevated temperature crack growth in Nickel-base alloys. Metall Trans A, 1978,9(2) : 231.
  • 5Chen E Y,Sauer S, Meshii M,et al. Fatigue microcrack distributions and the reliability of a nickel base superalloy. Int J Fatigue, 1997,19(Suppl) :S75.
  • 6Remy L,Alam A, Haddar N, et al. Growth of small cracks and prediction of lifetime in high-temperature alloys. Mater Sci Eng A, 2007,468-470:40.
  • 7Liu X B,Kang B, Chang K M. The effect of hold-time on fatigue crack growth behaviors of WASPALOY alloy at elevated temperature. Mater Sci Eng A, 2003, 340 (1/2) :8.
  • 8He L Z,Zheng Q,Sun X F,et al. Effect of carbides on the creep properties of a Ni-base superalloy M963. Mater Sci Eng A, 2005,397(1/2) :297.
  • 9Pang H T,Reed P A S. Microstructure effects on high temperature fatigue crack initiation and short crack growth in turbine disc nickel-base superalloy Udimet 720Li. Mater Sci Eng A ,2007,448 (1/2) :67.
  • 10Liu 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.

共引文献20

同被引文献6

引证文献1

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