Investigation of high-temperature homogenization of a single crystal nickel-based superalloy of the 3rd generation

A. Epishin
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Abstract

High-alloyed nickel-based superalloys used for casting of single crystal blades of aircraft gas-turbine engines have to be subjected to a long-term high-temperature homogenization annealing for dissolution of nonequilibrium γ′-eutectics and smoothing of dendritic segregation of alloying elements. Single crystal nickel-based superalloy of the 3-rd generation CMSX-10 developed by Cannon-Muskegon corporation for casting highly loaded uncooled single crystal blades of the first stage of a high pressure turbine of an aviation gas turbine engine Trent 800 belongs to such alloys. In the present work, the processes occurring during high-temperature homogenization annealing of this alloy have been investigated. It is shown that the kinetics of dissolution of nonequilibrium γ′-eutectics strongly depends on temperature: in the range of 1340 – 1360 °C the dissolution rate increases by about an order of magnitude with increasing temperature by 10 °C. Two types of homogenization annealing with a stepwise increase of temperature proposed for CMSX-10 by Cannon-Muskegon have been investigated: a long 45-hour annealing with 10 steps of temperature increase and a shortened 20-hour annealing with 6 temperature steps. The change in the solidus temperature of the alloy during the homogenization was studied by the method of measurement of the specific electrical resistance. It is shown, that during homogenization annealing of the both types the nonequilibrium eutectics is completely dissolved, and a longer 45-hour annealing provides a deeper chemical homogenization of the alloy. This is especially important for such alloying element as rhenium, which has a high segregation coefficient and very slow diffusion mobility in nickel. Deeper homogenization provides better thermal stability of the alloy microstructure and consequently higher long-term creep strength. A negative effect of high-temperature homogenization is increased porosity resulting from the dissolution of γ′-eutectics. Homogenization porosity can be reduced by optimizing the alloy composition and reducing the fraction of nonequilibrium γ′-eutectics.
第三代镍基单晶高温合金的高温均匀化研究
用于铸造航空燃气涡轮发动机单晶叶片的高合金镍基高温合金必须经过长期的高温均匀退火,以溶解非平衡γ′共晶和平滑合金元素的枝晶偏析。美国Cannon-Muskegon公司为铸造航空燃气涡轮发动机Trent 800高压涡轮一级高负荷非冷却单晶叶片而开发的第三代CMSX-10单晶镍基高温合金就属于这类合金。本文对该合金在高温均匀退火过程中发生的过程进行了研究。结果表明,非平衡态γ′-共晶的溶解动力学与温度密切相关:在1340 ~ 1360℃范围内,温度每升高10℃,溶解速率增加约一个数量级。本文研究了Cannon-Muskegon提出的CMSX-10的两种逐级升温均化退火方法:10步升温45小时的长退火和6步升温20小时的短退火。采用测量比电阻的方法,研究了均匀化过程中合金固相温度的变化。结果表明,在两种合金的均质退火过程中,非平衡共晶完全溶解,而45小时的退火使合金的化学均质化程度加深。这对于像铼这样的合金元素尤其重要,因为铼在镍中的偏析系数很高,扩散迁移率非常慢。均匀化程度越深,合金组织的热稳定性越好,长期蠕变强度也越高。高温均质化的负面影响是γ′共晶的溶解导致孔隙度增加。通过优化合金成分,减少非平衡γ′-共晶的含量,可以降低均匀化孔隙率。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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