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金属学报  2023, Vol. 59 Issue (9): 1173-1189    DOI: 10.11900/0412.1961.2023.00134
  综述 本期目录 | 过刊浏览 |
镍基高温合金表面冲击强化机制及应用研究进展
王磊1(), 刘梦雅1, 刘杨1(), 宋秀1, 孟凡强2
1东北大学 材料各向异性与织构教育部重点实验室 沈阳 110819
2中山大学 中法核工程与技术学院 珠海 519000
Research Progress on Surface Impact Strengthening Mechanisms and Application of Nickel-Based Superalloys
WANG Lei1(), LIU Mengya1, LIU Yang1(), SONG Xiu1, MENG Fanqiang2
1Key Laboratory for Anisotropy and Texture of Materials, Ministry of Education, Northeastern University, Shenyang 110819, China
2Sino-French Institute of Nuclear Engineering and Technology, Sun Yat-Sen University, Zhuhai 519000, China
引用本文:

王磊, 刘梦雅, 刘杨, 宋秀, 孟凡强. 镍基高温合金表面冲击强化机制及应用研究进展[J]. 金属学报, 2023, 59(9): 1173-1189.
Lei WANG, Mengya LIU, Yang LIU, Xiu SONG, Fanqiang MENG. Research Progress on Surface Impact Strengthening Mechanisms and Application of Nickel-Based Superalloys[J]. Acta Metall Sin, 2023, 59(9): 1173-1189.

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摘要: 

为满足不断攀升的两机涡轮动力系统的快速发展,表面冲击强化技术在涡轮转子用高温合金表面强化的应用及相应机制的研究受到了广泛关注。然而,高温合金表面硬化层在高温服役环境下的回复、再结晶行为难以避免,由此引起的表面强韧化、抗疲劳效果的退化,成为制约表面冲击强化技术在先进高温合金关键部件深入应用的瓶颈。本文总结了近年来镍基高温合金表面冲击强化机制及应用研究进展,分析了表面冲击强化对镍基高温合金表面强韧性及抗疲劳的作用规律,探究了高温合金表面冲击硬化层在高温及长期时效过程中的显微组织、微结构演化及其对高温稳定性的作用机理。以期为发展镍基高温合金表面冲击强化、提高两机涡轮转子疲劳抗力提供基础。

关键词 镍基高温合金表面强化处理抗疲劳制造硬化层组织和性能高温稳定性    
Abstract

There has been rapid development in the turbine power systems of aeroengines and gas turbines. Consequently, the application of surface impact strengthening technology for the surface strengthening of superalloys used in turbine rotors and its corresponding mechanisms have attracted wide attention. However, it is difficult to prevent the recovery and recrystallization of the surface hardened layer of superalloys serviced at high temperatures. This leads to the degradation of both the surface strengthening/toughening and fatigue resistance. This is the main hurdle restricting the wide application of surface impact strengthening technology for key components of advanced superalloys. In this paper, the progress made in surface impact strengthening mechanisms and the applications of nickel-based superalloys in recent years are summarized. The effect of surface impact strengthening on the surface strength, toughness, and fatigue resistance of nickel-based superalloys is analyzed. The evolution of the microstructure of the hardened surface of the alloys during long-term aging at high temperatures, and its effect on high-temperature stability are explored. The paper aims to provide essential and important information for developing surface impact strengthening mechanisms of nickel-based superalloys and improving the fatigue resistance of turbine rotors of aeroengines and gas turbines.

Key wordsnickel-based superalloy    surface strengthening technology    anti-fatigue manufacturing    hardened layer    high temperature stability of microstructure and property
收稿日期: 2023-03-29     
ZTFLH:  TG132.2  
基金资助:国家重点研发计划项目(2022YFB3705102);国家重点研发计划项目(2022YFB3705101);国家科技重大专项项目(J2019-VI-0020-0136);国家自然科学基金项目(U1708253);国家自然科学基金项目(51571052)
作者简介: 王 磊,男,1961年生,教授,博士
图1  喷丸处理对FGH96合金表面硬化层残余压应力分布的影响[30]
图2  GH4169合金喷丸处理获得的表面硬化层截面梯度分布的纳米晶和形变孪晶层[33]
图3  喷丸处理前后GH4169合金的表面形貌[13]
图4  喷丸处理对Udimet 720Li合金相同载荷幅条件下疲劳裂纹萌生位置的影响[35]
图5  不同强度的表面喷丸处理对GH4169合金疲劳应力幅-循环周次(S-N)曲线的影响[13]
图6  不同孔挤压处理的IN718合金孔壁硬化层的残余压应力分布[43]
图7  FGH96高温合金经不同表面处理后的表面形貌[48]
图8  IN718合金LSP、温度辅助耦合激光冲击强化技术(WLSP)硬化层中的γ″相及位错形态[52]
图9  单激光脉冲LSP处理后GH4586合金残余压应力的分布[50]
图10  LSP处理对GH4586合金表面晶粒尺寸及孪晶数量的影响[50]
图11  LSP处理对某镍基单晶高温合金表面硬化层基体位错密度及γ′相内部微结构的影响[65]
图12  LSP和WLSP处理对IN718合金表面硬度分布的影响[19]
图13  WLSP处理后IN718合金表面硬化层γ″相/高密度位错复合体形态及强冲击作用下γ″相中出现的微孪晶[19]
图14  经WLSP处理后IN718合金表面硬化层中γ″/γ界面细节的HRTEM像[52]
图15  650℃时效200 h对LSP和WLSP处理IN718合金表面硬化层硬度分布的影响[52]
图16  喷丸处理与LSP处理后IN100合金表面硬化层在650℃、100 h时效后的残余应力分布对比[82]
图17  不同温度长期时效后IN718合金LSP和WLSP硬化层硬度分布及硬化层深度变化[81]
图18  长期时效对LSP和WLSP处理的IN718合金表面硬化层强化机制贡献增量的影响[81]
图19  650℃长期时效后LSP和WLSP处理IN718合金表面硬化层的几何必需位错(GND)密度分布图及正态分布统计图[52]
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