GH4169D高温合金喷丸强化残余应力场仿真与参数化建模

罗健鑫 ,  张伟 ,  雷力明 ,  谭靓 ,  姚倡锋

航空材料学报 ›› 2026, Vol. 46 ›› Issue (8) : 84 -92.

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航空材料学报 ›› 2026, Vol. 46 ›› Issue (8) : 84 -92. DOI: 10.11868/j.issn.1005-5053.2026.000122

GH4169D高温合金喷丸强化残余应力场仿真与参数化建模

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Simulation and parametric modeling of residual stress field in shot peening of GH4169D superalloy

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摘要

残余压应力是影响零部件性能和寿命的关键因素,主动引入并精确控制残余压应力已成为提高零部件可靠性、延长使用寿命的核心技术手段之一。本工作针对GH4169D高温合金喷丸工艺参数优化困难、残余应力场预测精度不足等问题,采用仿真与实验相结合的方法开展研究。建立考虑弹丸随机分布特性的多弹丸喷丸过程仿真模型,分析不同工艺条件下材料应变率及残余应力与塑性应变的关系,并验证随机喷丸残余应力模型的准确性。基于响应曲面法开展喷丸强化工艺实验,对比不同喷丸强度和覆盖率对残余应力影响层深度分布的影响规律,并对残余应力影响层深度分布情况进行参数化建模。结果表明,使用余弦衰减函数可对GH4169D高温合金在不同喷丸工艺下的残余应力场进行参数化建模,拟合后R2大于0.95,这些结果为GH4169D高温合金喷丸强化工艺的快速优化和残余应力场的准确建模提供有效方法。

Abstract

Residual compressive stress is a critical factor affecting the performance and service life of components. The active introduction and precise control of residual compressive stress have become one of the core technical approaches to improve component reliability and extend service life. Aiming at the difficulties in optimizing shot peening process parameters and insufficient prediction accuracy of residual stress fields for GH4169D superalloy,this work adopts a combined simulation and experimental method for investigation. A multi-shot peening simulation model considering the random distribution characteristics of shot particles is established to analyze the material strain rate as well as the correlation between residual stress and plastic strain under various process conditions,and the accuracy of the random shot peening residual stress model is verified. Shot peening strengthening experiments are carried out based on the response surface methodology. The influence laws of different shot peening intensities and coverage rates on the depth distribution of the residual stress-affected layer are compared,and parametric modeling is performed for the depth distribution of the residual stress-affected layer. The results reveal that the cosine attenuation function can realize parametric modeling of residual stress fields of GH4169D superalloy under diverse shot peening processes,with the fitted determination coefficientR 2 greater than 0.95. These findings provide an effective method for rapid optimization of shot peening strengthening processes and accurate modeling of residual stress fields of GH4169D superalloy.

关键词

高温合金 / 喷丸强化 / 残余应力 / 有限元模拟 / 参数化建模

Key words

superalloy / shot peening / residual stress / finite element simulation / parametric modeling

引用本文

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罗健鑫,张伟,雷力明,谭靓,姚倡锋. GH4169D高温合金喷丸强化残余应力场仿真与参数化建模[J]. 航空材料学报, 2026, 46(8): 84-92 DOI:10.11868/j.issn.1005-5053.2026.000122

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参考文献

[1]

Liu L,Hu Z,Sun S,et al. Achieving superior fretting fatigue resistance of nickel-based single crystal superalloy tenon by shot peening[J].Materials & Design,2026:116114.

[2]

Bu X Y,Wang Z,Deng W W,et al. Gradient microstructural evolution and mechanical property enhancement mechanisms in laser shock peened IN718 superalloy[J].Materials Science and Engineering:A,2025,944:148905.

[3]

白昭若,黄康华,汤明军,等 . 承力孔孔边倒角高速超声冲击强化方法及表面完整性研究[J].机械工程学报,2026,62(5):434-442.

[4]

Bai Z R,Huang K H,Tang M J,et al. A controllable high-precision high-speed ultrasonic peening method for hole chamfer and the analysis of surface integrity[J].Journal of Mechanical Engineering,2026,62(5):434-442.

[5]

于焱,王优强,张平,等 . 水射流强化技术对表面完整性及疲劳性能的影响研究进展[J].表面技术,2026,55(3):196-218.

[6]

Yu Y,Wang Y Q,Zhang P,et al. Research progress on influences of water jet strengthening technology on surface integrity and fatigue performance[J].Surface Technology,2026,55(3):196-218.

[7]

许春玲,何家琦,罗学昆,等 . 航空发动机用表面强化技术的发展与建议[J].航空材料学报,2026,46(5/6):226-240.

[8]

Xu C L,He J Q,Luo X K,et al. Development and suggestions of surface mechanical treatments for aero-engines[J].Journal of Aeronautical Materials,2026,46(5/6):226-240.

[9]

孟宪凯,林珂,韦帅,等 . 能场辅助激光冲击强化在航空构件上的应用[J].航空制造技术,2026,69(4):14-34.

[10]

Meng X K,Lin K,Wei S,et al. Applications of energy field assisted laser shock peening in aerospace components[J].Aeronautical Manufacturing Technology,2026,69(4):14-34.

[11]

田伟,伏宇,张少平,等 . 喷丸强化对GH4096合金表面状态和疲劳性能的影响[J].稀有金属材料与工程,2024,53(6):1726-1734.

[12]

Tian W,Fu Y,Zhang S P,et al. Effect of shot peening on surface state and fatigue performance of GH4096 alloy[J].Rare Metal Materials and Engineering,2024,53(6):1726-1734.

[13]

Sadallah A,Miao H Y,Changeux B,et al. Effect of shot peening and high-temperature shot peening on the high cycle fatigue of 7010-T7452 aluminum alloy[C]//Light Metals 2024. Cham:Springer,2024:169-176.

[14]

Luo J X,Yao C F,Lei L M,et al. Effect of shot peening on surface integrity and elevated temperature fatigue behavior of ATI 718plus alloy[J].International Journal of Fatigue,2026,208:109527.

[15]

Chen X,Chen W,Li W,et al. Finite-element analysis of random shot peening in Inconel 718:effects of shot size,coverage,and impact sequence[J].Journal of Materials Research and Technology,2026,41:6483-6497.

[16]

Chaieb I,Ben M N,Ben F N,et al. An innovative contactless finite element simulation of the shot peening process[J].The International Journal of Advanced Manufacturing Technology,2021,114(9):2767-2784.

[17]

周文龙,王淼,孙一帆,等 . 大量弹丸随机分布的薄壁件喷丸强化形变仿真[J].航空制造技术,2022,65(15):14-22.

[18]

Zhou W L,Wang M,Sun Y F,et al. Simulation for shot peening strengthening deformation of thin-walled parts with multiple random shots[J].Aeronautical Manufacturing Technology,2022,65(15):14-22.

[19]

Lin Q J,Wei P T,Liu H J,et al. A CFD-FEM numerical study on shot peening[J].International Journal of Mechanical Sciences,2022,223:107259.

[20]

He W L,Yan C,Gorbachev S,et al. Numerical simulation of shot peening process for AISI 4340 steel using random balls method[J].Transactions of the Indian Institute of Metals,2023,76(10):2601-2614.

[21]

孙蕴齐,姚倡锋,孙换凤,等 . 高温合金喷丸工艺表面完整性及其疲劳性能研究进展[J].中国机械工程,2026,37(2):315-331.

[22]

Sun Y Q,Yao C F,Sun H F,et al. Research progresses of surface integrity and fatigue performance for high-temperature alloy shot peening processes[J].China Mechanical Engineering,2026,37(2):315-331.

[23]

Tan L,Yao C F,Zhang D H,et al. Empirical modeling of compressive residual stress profile in shot peening TC17 alloy using characteristic parameters and sinusoidal decay function[J].Proceedings of the Institution of Mechanical Engineers,Part B:Journal of Engineering Manufacture,2018,232(5):855-866.

[24]

梁巧云,蔺治强,张吉银,等 . 叶片铣削及喷丸加工残余应力测试与三维表征[J].机械科学与技术,2022,41(11):1794-1804.

[25]

Liang Q Y,Lin Z Q,Zhang J Y,et al. Measurement and three-dimensional characterization of residual stress after milling and shot peening of blade[J].Mechanical Science and Technology for Aerospace Engineering,2022,41(11):1794-1804.

[26]

Han K P,Zhang D H,Yao C F,et al. Studies and optimization of surface roughness and residual stress in ball burnishing of Ti60 alloy[J].Journal of Materials Engineering and Performance,2022,31(5):3457-3470.

[27]

Cao Y L,Yao C F,Tan L,et al. A novel methodology of surface integrity anisotropy in ATI718 plus alloy by oblique laser shock peening[J].Journal of Manufacturing Processes,2025,152:346-363.

[28]

汪帆星,汪舟,曾思明,等 . 基于FEM-DEM耦合模型喷丸铝合金薄壁件尺寸稳定性仿真研究[J].表面技术,2025,54(3):171-181.

[29]

Wang F X,Wang Z,Zeng S M,et al. Simulation research on dimensional stability of peened aluminum alloy thin-walled parts based on coupled FEM-DEM model[J].Surface Technology,2025,54(3):171-181.

[30]

Klemenz M,Schulze V,Vöhringer O,et al. Finite element simulation of the residual stress states after shot peening[J].Materials Science Forum,2006,524-525:349-354.

[31]

卓伟伟,张吉银,孙晓明,等 . 基于有限元仿真的喷丸强化控制参数对残余应力的影响规律研究[J].航空维修与工程,2024(4):56-65.

[32]

Zhuo W W,Zhang J Y,Sun X M,et al. Study on the influence of shot peening control parameters on residual stress based on finite element simulation[J].Aviation Maintenance & Engineering,2024(4):56-65.

[33]

任旭东,汪舟,卢伟,等 . 基于FEM-DEM的空心稳定杆内壁喷丸仿真分析[J].表面技术,2023,52(1):410-420.

[34]

Ren X D,Wang Z,Lu W,et al. FEM-DEM simulation on inner wall shot peening of hollow stabilizer bar[J].Surface Technology,2023,52(1):410-420.

[35]

田凯,吴小燕,李伟,等 . 激光喷丸-机械喷丸复合强化对GH4169合金表面完整性和振动疲劳性能的影响[J].材料工程,2025,53(8):147-156.

[36]

Tian K,Wu X Y,Li W,et al. Effect of co-strengthening of laser shock peening and mechanical shot peening on surface integrity and vibration fatigue properties of GH4169 alloy[J].Journal of Materials Engineering,2025,53(8):147-156.

[37]

Lu T W,Chiu C C,Tseng S C,et al. Mechanisms of surface strengthening in shot-peened 316L stainless steel:experimental and numerical insights[J].Materials Chemistry and Physics,2026,360:132622.

基金资助

太行国家实验室自主立项项目(BK133)

国家自然科学基金项目(92360309)

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