期刊文献+

氧含量对Ni-30Cr-1Cu镍基合金热加工性能的影响 被引量:1

Effect of Oxygen on Hot-working Properties of Ni-30Cr-lCu Superalloy
下载PDF
导出
摘要 采用小锭试验研究了氧含量对Ni-30Cr-1Cu镍基合金热加工性能的影响以及Cu在 合金相中的分布。结果表明,氧含量为0.0077%和0.015 8%的试验合金,其热加工性能显 著恶化,在1050℃和1 200℃加热后,变形量小于10%时,即在晶界普遍萌生裂纹,并沿晶界 迅速扩展。氧含量为0.003 3%的试验合金,在1 050℃和1 200℃的加热温度和900℃左右的 终锻条件下,均具有良好的热加工性能,一火变形量高达80%以上,仍未出现热加工缺陷。Cu 只明显富集于热加工完毕空冷过程中在晶内晶界析出的M23C6中,未观察到其对热加工性能 有明显的恶化作用。在正常工业生产中,采取措施把该合金氧含量控制在较低的范围内,解决 了该合金热加工成形问题,取得了良好效果。 The effect of oxygen content on hot-working properties and distribution of copper in Ni-30Cr-1Cu,a kind of superalloy,has been investigated with small ingots. The hot-working properties of alloys with 0. 007 7% and 0. 015 8% oxygen content respectively were obviously worsened. When they were heated up to 1 050℃ and 1 200℃ and the deformation is less than 10% , many cracks formed and spread quickly along grain boundaries. The alloy with 0. 003 3% oxygen content has good hot-working properties when it is heated up to 1 050℃ and 1 200℃ with finish forging temperature 900℃. No hot-working defects appear when the deformation in one heat reaches more than 80%. Experimental results show that copper is only concentrated in M23 C6 phase at grain boundaries and in grains. No obvious deterioration of its hot-working properties has been observed. In the normal production, measures are taken to control the alloy ' s oxygen content within lower limits so as to solve its formation problem during the heat treatment.
机构地区 特殊钢分公司
出处 《宝钢技术》 CAS 2005年第5期38-41,46,共5页 Baosteel Technology
关键词 镍基高温合金 热加工性能 oxygen, nickel-based superalloy, hot-working property
  • 相关文献

参考文献10

  • 1Mineura K, Tanaka K. Effect of calcium treatment on hot workability of Cr - Ni - 0. 7N stainlesssteel. Materials Science and Technology, 1990,6:743.
  • 2Krishna V G,Prasad YVRK,Birla N C,et al. Hot deformation mechanisms in near - alphatitanium alloy 685. JOM, 1996,48 (10) :56.
  • 3Rao A S,Prasad V V S, Baligidad R G,et al. Influence of hot working onelectro slag remelted low alloy steel. Transactions of the Indian Institute of Metals ( India), 1999,52 (2 ~ 3 ): 139.
  • 4Wu E,Li S, Qian C,et al. Development of material used for aviation apparatus axle journals. Transactions of the Nonferrous MetalsSociety of China, 1998,8 ( 2 ): 194.
  • 5Mitter W, Bauer R, Leitner H. Influence of trace elements on the hot ductility of nickel - base alloys - Calculation of strain fields and of the recrystallization behaviour after primarydeformation of some nickel - base alloys. High Temperature Alloys for Gas Turbines and Other Applications, 1986. Ⅱ, Liege, Belgium, 1986:855.
  • 6Li Y Q, Chen G S,Zhang J F,et al. Effects of trace elements on grain boundaries in some superalloys. Progress in Natural Science,2000,10:33.
  • 7Li Y Q,Liu J Y. Interaction of carbon boron and supture in superalloy.High Temperature Technology,1990,8:278.
  • 8Liu L R,Jin T,Zhao N R,et al. Formation of carbides and their effects on stress rupture of a Ni - base single crystal superalloy.Materials Science and Engineering,2003 ,A361:191.
  • 9《高温合金金相图谱》编写组.高温合金金相图谱[M].北京:冶金工业出版社,1977.7-10.
  • 10Fast J D. Gase in Metals. The Macmillan Press Ltd. , 1976:1 ~ 2.

共引文献1

同被引文献6

引证文献1

二级引证文献3

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