期刊文献+

Re对耐腐蚀镍基定向高温合金组织及持久寿命的影响 被引量:8

Effect of Re on Microstructure and Stress-Rupture Life of Corrosion Resistant DS Ni-Base Superalloy
原文传递
导出
摘要 优化设计了4种不同Re含量的耐腐蚀定向镍基高温合金,含Re分别为0%,1%,2%和3%(质量分数)。对比了不同Re含量合金的铸态枝晶、γ'相形貌及持久性能试样的断口筏排化组织,测试了不同Re含量合金热处理态的980℃/200 MPa持久寿命,研究了Re对耐腐蚀镍基定向合金组织及持久寿命的影响。研究表明:随着Re含量的增加,合金的一次枝晶间距减小;γ'相尺寸减小,立方化程度增加;蠕变试样的筏排组织更加细化、完善与稳定,因此,合金持久寿命提高。 Four Ni-based superalloys with varying rhenium contents (0%, 1%, 2% and 3% (mass fraction), respectively) were prepared to investigate the effects of Re content on the microstructure and the stress-rupture life of the superalloys. The as-cast primary dendritic arm spacing of the four alloys were compared, and the precipitates of as-cast and aged alloys were studied. The stress-rup- ture life at 980 ℃/200 MPa were tested and the rafting microstructure were analyzed with varying Re contents. The results showed that with the increase of Re contents, the primary dendritic arm spacing decreased; the size of the secondary y^1 precipitates decreased; and the morphology of y^1 precipitates became more cubic due to the enlargement of lattice misfit moreover, well rafting microstructure formed with larger driving force because of larger lattice misfit. As a result, the stress-rupture increased.
出处 《稀有金属》 EI CAS CSCD 北大核心 2012年第4期547-551,共5页 Chinese Journal of Rare Metals
基金 重点实验室基金项目(9140C4301050801) 国家自然科学基金项目(50801058) 国家航空基金项目(20085321009) 国家工信部科技专项基金项目(2009ZX04006-041)资助
关键词 耐腐蚀高温合金 RE 微观组织 持久寿命 corrosion resistant superalloy rhenium microstructure stress-rupture life
  • 相关文献

参考文献17

  • 1Cetel A D, Duhl D N. Second generation columnar grain nick- el-base superalloy [ A ]. Antolovich S D, Stusrud R W, et al. Superalloys [C]. 1992. 287.
  • 2Ross E W, O'Hara K S. Rene' 142: a high strength, oxidation resistance DS turbine airfoil alloy [ A ]. Antolovich S D, Stusrud R W. et al. Superallovs F C 1. 1992. 257.
  • 3Harris K, Erickson G L. Development of the rhenium contai- ning superalloys CMSX-4 & CM186 LC for single crystal blade and directional solidified vane application in advanced turbine en- gines [ A ]. Antolovich S D, Stusrud R W, et al. Superalloys [C]. 1992. 297.
  • 4Kobayashi T, Sato M, Harada H. Development of a third gener- ation DS superalloy [ A ]. Pollock T M, Kissinger R D, et al. Superaloy [ C ]. 2000. 323.
  • 5Toshiharu K, Yutaka K, Himshi H. Development of a 4th gen- eration DS superalloy [ J ]. Journal of Japan Institute Metals, 2002, 66 (9) : 897.
  • 6BIlrgel R, Grossmann J, Ltlsebrink O. Development of a new alloy for directional solidification of large industrial gas turbineblades [ J ]. Superalloys, 2004. 25.
  • 7骆宇时.Re在单晶高温合金中的强化机理[D].北京:北京航空材料研究院,2006.
  • 8骆宇时,李嘉荣,刘世忠,孙凤礼,韩梅,曹春晓.铼对单晶高温合金γ、γ′相的影响[J].钢铁研究学报,2007,19(6):61-64. 被引量:6
  • 9骆宇时,李嘉荣,刘世忠,曹春晓.Re对单晶高温合金蠕变过程中γ′相定向粗化的影响[J].材料工程,2006,34(7):43-46. 被引量:7
  • 10骆宇时,李嘉荣,刘世忠,孙凤礼,曹春晓.Re对单晶高温合金持久性能的强化作用[J].材料工程,2005,33(8):10-14. 被引量:14

二级参考文献26

共引文献38

同被引文献84

引证文献8

二级引证文献30

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