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材料研究学报  2026, Vol. 40 Issue (2): 143-151    DOI: 10.11901/1005.3093.2025.126
  研究论文 本期目录 | 过刊浏览 |
高温时效对GH4169镍基高温合金性能的影响
郑建军(), 张涛, 陈浩, 吕磊
内蒙古电力(集团)有限责任公司内蒙古电力科学研究院分公司 呼和浩特 010020
Effect of High-temperature Aging on Microstructure and Mechanical Properties of GH4169 Nickel-based Superalloy
ZHENG Jianjun(), ZHANG Tao, CHEN Hao, LV Lei
Inner Mongolia Power Research Institute Branch, Inner Mongolia Power (Group) Co., Ltd., Hohhot 010020, China
引用本文:

郑建军, 张涛, 陈浩, 吕磊. 高温时效对GH4169镍基高温合金性能的影响[J]. 材料研究学报, 2026, 40(2): 143-151.
Jianjun ZHENG, Tao ZHANG, Hao CHEN, Lei LV. Effect of High-temperature Aging on Microstructure and Mechanical Properties of GH4169 Nickel-based Superalloy[J]. Chinese Journal of Materials Research, 2026, 40(2): 143-151.

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摘要: 

对GH4169镍基高温合金分别进行标准热处理后、和在900 ℃进行不同时间的时效处理,研究了其对这种合金的组织和性能的影响。结果表明:标准热处理后合金的基体是γ相,在晶界存在微量短棒状δ相(含量为0.139% (体积分数),相尺寸0.32 μm),合金的强度最优(屈服强度1330 MPa、抗拉强度1385 MPa、硬度为497HV),但是塑性较低(断面收缩率19.75%)。在900 ℃时效不同时间后δ相的尺寸由2.65 μm增大到2.86 μm,呈现晶界短棒状裂解与晶内定向针状分布特征。时效500 h后亚稳γ''相向δ相(Ni3Nb)持续转变,δ相含量提高到14.2%;时效1134 h后δ相的含量提高到15.1%。力学性能呈现显著时效效应:硬度下降57%,屈服强度降低34%,冲击韧性同步降低19%,而塑性提高80%。在时效初期晶界δ相通过钉扎作用产生细晶强化,但是随着时效时间的延长晶界δ相粗化消耗γ''强化相并诱发基体弱化,高温促进晶内δ相直接析出削弱沉淀强化效果。断口形貌从标准态的等轴韧窝的韧性断裂转变为时效后的柳叶状韧窝与解理面共存的韧-脆混合模式,δ相界面成为裂纹优先扩展路径。

关键词 金属材料高温合金高温时效δ断裂机制    
Abstract

The influence of prolonged high-temperature aging on the microstructural evolution and mechanical properties of GH4169 nickel-based superalloy was investigated. The results demonstrate that the standard heat-treated alloy primarily consists of a γ-phase matrix with trace amounts of short rod-shaped δ-phase (0.139% volume fraction, 0.32 μm in size) distributed along grain boundaries, achieving optimal mechanical properties: yield strength 1330 MPa, ultimate tensile strength 1385 MPa, and hardness 497HV, albeit with limited ductility 19.75% reduction of area. During aging at 900 °C for 500-1134 h, the metastable γ'' phase progressively transforms into δ-phase (Ni3Nb), accompanied by a substantial increase in δ-phase content (14.2% at 500 h and 15.1% at 1134 h) and coarsening from 2.65 μm to 2.86 μm. The δ-phase evolves distinct microstructural characteristics: intergranular short-rod fragmentation and intragranular oriented needle-like precipitation. Significant aging effects are observed, manifesting as a 57% hardness reduction, 34% yield strength decline, 19% decrease in impact toughness, and an 80% ductility improvement. Mechanistic analysis reveals that initial grain-boundary δ-phase enhances the strength via grain refinement through Zener pinning. However, prolonged aging induces δ-phase coarsening at grain boundaries, which consumes γ'' strengthening precipitates and weakens the matrix. Concurrently, high-temperature aging promotes direct intragranular δ-phase precipitation, deteriorating the precipitation strengthening efficacy. Fractography transitions from equiaxed dimples (ductile fracture) in the standard condition to a ductile-brittle mixed mode featuring willow-leaf-shaped dimples and cleavage planes in the aged alloys, with δ-phase interfaces acting as preferential pathways for crack propagation. These findings elucidate the critical role of δ-phase evolution in governing the strength-ductility trade-off during high-temperature aging.

Key wordsmetallic materials    superalloy    high-temperature aging    δ-phase    fracture mechanism
收稿日期: 2025-03-31     
ZTFLH:  TG156.1  
基金资助:内蒙古电力科学研究院2023年自筹科技项目(2023-ZC-1-12)
通讯作者: 郑建军,高级工程师,dkyzjj@163.com,研究方向为电力设备材料理化检验及失效分析
Corresponding author: ZHENG Jianjun, Tel: (0471) 6223747, E-mail: dkyzjj@163.com
作者简介: 郑建军,男,1987年生,博士
图1  热处理工艺
图2  在不同条件热处理后GH4169镍基高温合金的金相组织
图3  在不同条件热处理后GH4169镍基高温合金的XRD谱
图4  在不同条件热处理后GH4169镍基高温合金的SEM照片
图5  在不同条件热处理后GH4169镍基高温合金的TEM照片
Sampleδ-phase content / %Averageδ-phase size / μm
Standard heat treatment0.139 ± 0.0020.320 ± 0.010
Aging treatment 500 h14.2 ± 1.312.655 ± 0.014
Aging treatment 1134 h15.1 ± 1.202.861 ± 0.018
表1  在不同条件热处理后试样中δ相的含量和尺寸
图6  在不同条件热处理后GH4169镍基高温合金中析出相的特征
PositionAlSiTiCrFeNiNbMo
10.850.551.278.427.3120.215.530.9
21.50.530.9615.4113.9138.692.541.29
31.630.123.164.95.2863.4816.430.99
41.690.371.0617.615.6940.411.691.13
52.150.591.8315.4814.1155.918.191.66
61.930.560.7919.1516.8741.851.331.98
表2  在不同条件热处理后,GH4169镍基高温合金中δ相的成分及其两侧无析出处的成分
图7  时效不同时间后GH4169镍基高温合金试样的显微组织
SampleMechanical property
Hardness(HV)Yield strength / MPaTensile strength / MPaElongation after fracture / %Impact absorbed energy / J
Standard heat treatment497.44 ± 8.521330 ± 01385 ± 7.0719.75 ± 1.0658.17 ± 12.04
Aging treatment 500 h270.21 ± 5.45870 ± 17.67932.5 ± 10.6135.5 ± 0.7046.83 ± 2.75
Aging treatment 1134 h267.28 ± 3.96840 ± 28.28932.5 ± 14.1434.5 ± 0.7046.83 ± 3.54
表3  在不同条件热处理后GH4169镍基高温合金的力学性能
图8  不同条件热处理后GH4169镍基高温合金的拉伸应力-应变曲线
图9  不同热处理状态试样的拉伸断口形貌
图10  时效处理1134 h试样的拉伸断口开裂位置的SEM照片
图11  在不同条件热处理后试样冲击断口的形貌
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