期刊文献+

固溶及稳定化工艺对GH738合金碳化物和γ'相析出规律的影响 被引量:11

Influence of solution and stabilization heat treatment on carbide and gamma prime for super alloy GH738
原文传递
导出
摘要 实验研究固溶及稳定化处理工艺对GH738合金碳化物及γ'强化相析出规律的影响。以标准热处理:1020℃×4 h/AC(空冷)+845℃×4 h/AC+760℃×16 h/AC和1080℃×4 h/AC+845℃×24 h/AC+760℃×16 h/AC为基础,调整稳定化阶段保温时间。研究了该合金稳定化过程中碳化物及γ'强化相析出和回溶规律,绘制了γ'强化相长大曲线。结果表明,1020℃固溶后,稳定化时间的延长使晶界析出碳化物增多且呈现半连续分布;而经1080℃固溶后,碳化物析出沿着晶界呈连续状分布;同时,经两种固溶温度处理后,稳定化时间延长,γ'强化相长大符合Oswald熟化规律;经1020℃标准热处理后,合金具有较好强塑性配合,尤其在塑性指标方面有明显优势;而经1080℃标准热处理后,合金持久性能表现更佳。 Precipitation and dissolution behavior of carbides and gamma prime were studied for super alloy GH738 during solution and stabilization heat treatment. Based on two standard heat treatments: 1020 ℃ × 4 h/AC + 845 ℃ × 4 h/AC + 760 ℃ × 16 h/AC and 1080 ℃ ×4 h/AC + 845 ℃ x 24 h/AC + 760 ℃ × 16 h/AC, the stabilization holding time was adjusted to examine the evolution of carbides and gamma prime in the process of heat treatments. The results indicate that the solution and stabilization process have great influence on carbides and gamma prime. The carbides are precipitated discountinuously at grain boundaries for solution treatment at 1020 ℃ and the continuous distribution of the carbides at grain boundaries is observed for the alloy after solution treatment at 1080 ℃. The rate of growth for gamma prime is consistent with Ostwald rule during the stabilization treatment. The two standard heat treatments exhibit different effects on microstructure and mechanical properties for the alloy. The better tensile properties can be obtained after the standard treatment at 1020 ℃ , while better stress rupture properties can be acquired after standard treatment at 1080 ℃ for super alloy GH738.
出处 《材料热处理学报》 EI CAS CSCD 北大核心 2013年第10期43-49,共7页 Transactions of Materials and Heat Treatment
基金 国家自然科学基金(51071017)
关键词 GH738合金 碳化物 γ′强化相 热处理 力学性能 super alloy GH738 carbides gamma prime heat treatment mechanical properties
  • 相关文献

参考文献14

  • 1Liu 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.
  • 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姚志浩,董建新,张麦仓.GH864合金组织特征对裂纹扩展速率的影响[J].北京科技大学学报,2011,33(12):1501-1507. 被引量:4
  • 4Tokoro 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.
  • 5Chang 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.
  • 6Mandy 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.
  • 7姚志浩,董建新,张麦仓,于秋颖,郑磊.固溶温度对GH864合金组织性能的影响[J].材料热处理学报,2011,32(7):44-50. 被引量:11
  • 8Kelekanjeri 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.
  • 9姚志浩,董建新,张麦仓.GH738高温合金热变形过程显微组织控制与预测 Ⅰ.组织演化模型的构建[J].金属学报,2011,47(12):1581-1590. 被引量:30
  • 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.

二级参考文献16

  • 1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
  • 2沈丙振,方能炜,沈厚发,柳百成.低碳钢奥氏体再结晶模型的建立[J].材料科学与工艺,2005,13(5):516-520. 被引量:17
  • 3Whelchel 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.
  • 4Chang 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.
  • 5Semiatin S L, Fagin P N, Glavicic M G, et al. Deformation behavior of Waspaloy at hot-working temperatures. Scripta Muter, 2004, 50(5) : 625.
  • 6Penkalla H J, Wosik J, Czyrska-Filemonowicz A. Quantitative mi- crostructural characterisation of Ni-base superalloys. Mater Chem Phys, 2003, 81(2/3): 417.
  • 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.

共引文献55

同被引文献96

引证文献11

二级引证文献66

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