大型铸锻件2024,Issue(4) :33-37,54.

超超临界汽轮机转子用IN706合金均匀化处理工艺研究

Research on Homogenization Treatment Process of IN706 Alloy for Ultra-supercritical Steam Turbine Rotor

张冰冰 白亚冠 聂义宏 张鑫 寇金凤
大型铸锻件2024,Issue(4) :33-37,54.

超超临界汽轮机转子用IN706合金均匀化处理工艺研究

Research on Homogenization Treatment Process of IN706 Alloy for Ultra-supercritical Steam Turbine Rotor

张冰冰 1白亚冠 2聂义宏 2张鑫 1寇金凤1
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作者信息

  • 1. 天津重型装备工程研究有限公司,天津300457
  • 2. 天津重型装备工程研究有限公司,天津300457;黑龙江省高端核电装备智能制造重点实验室,黑龙江 齐齐哈尔161042
  • 折叠

摘要

针对传统IN706和改进型IN706m合金开展了铸态显微组织观察分析并研究了其析出相回溶规律.经过研究发现,合金铸态组织中存在大量的γ+γ′共晶组织、η相、Laves相和M(C,N).γ+γ′共晶组织、针状η相可在高于1100℃的保温过程中完全回溶到基体中.IN706合金中Laves相的初熔点在1160~1180℃之间,IN706m合金Laves相的初熔点在1140~1160℃之间.在实际生产中,选择1140℃保温8 h以上,即可使得Laves相完全回溶到基体中而不发生初熔,元素微观偏析也能得到有效地消除.

Abstract

The as-cast microstructure of traditional IN706 and modified IN706 alloy was observed and analyzed,and the law of precipitated phase re-dissolution was studied. The results show that there are plenty of γ+γ′eutectic structure,η phases,Laves phases and M(C,N) in alloy as-cast structure. γ+γ′eutectic structure and needle-like η phase could be completely re-dissolved into the matrix when the holding temperature is above 1100℃. For IN706 alloy,the incipient melting point of the Laves phase is 1160~1180℃. For the IN706m alloy,the incipient melting point of the Laves phase is 1140~1160℃. In actual production,choose 1140℃ and hold for 8h,Laves phases could be completely re-dissolved into the matrix without incipient melting,and the element microsegregation can be eliminated effectively.

关键词

IN706合金/均匀化处理/Laves相

Key words

IN706 alloy/homogenization treatment/Laves phase

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基金项目

黑龙江省自然科学基金杰出青年项目(JQ2021E007)

出版年

2024
大型铸锻件
中国重型机械大型铸锻件行业协会 中国第二重型机械集团公司大型特锻件研究所

大型铸锻件

影响因子:0.098
ISSN:1004-5635
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