Effect of Laser Shock Peening Process Without Coating Parameters on Mechanical Properties and Surface Integrity of 12Cr2Ni4A Steel

XIE Cenchao, YU Shuiyou, WANG Ke, ZHANG Shaohua, WANG Rongping, CHEN Chao

Surface Technology ›› 2025, Vol. 54 ›› Issue (23) : 188-196.

PDF(10940 KB)
PDF(10940 KB)
Surface Technology ›› 2025, Vol. 54 ›› Issue (23) : 188-196. DOI: 10.16490/j.cnki.issn.1001-3660.2025.23.014
Laser Surface Modification Technology

Effect of Laser Shock Peening Process Without Coating Parameters on Mechanical Properties and Surface Integrity of 12Cr2Ni4A Steel

  • XIE Cenchao1,2, YU Shuiyou2, WANG Ke2, ZHANG Shaohua2, WANG Rongping1, CHEN Chao3,*
Author information +
History +

Abstract

This study investigates the effects of laser shock peening without coating (LSPwc) on the mechanical properties and surface integrity of 12Cr2Ni4A steel, with a focus on optimizing laser energy and impact counts to enhance its performance for aerospace applications. Experiments are conducted using an Nd:YAG laser system (wavelength: 532 nm, pulse width: 8 ns, spot diameter: 0.6 mm) under a coaxial water-jet configuration. The process parameters include laser energies of 70, 100, and 130 mJ, an overlap rate of 50%, a repetition frequency of 50 Hz, and impact counts of 1, 2, and 3 at 130 mJ. The microhardness, microstructure, residual stress, surface roughness, and surface morphology of both untreated and LSPwc-treated samples were systematically characterized and compared.
The results indicate that LSPwc induces plastic deformation in the near-surface region of 12Cr2Ni4A steel, forming a high-density dislocation structure and promoting the transformation of residual austenite to martensite, thereby enhancing microhardness and residual compressive stress. In terms of microhardness, with the increase of laser energy, the hardness of the treated samples reaches 574.78HV0.5, 605.52HV0.5, and 591.85HV0.5, representing increases of 4.1%, 9.7%, and 7.2%, respectively, compared with the untreated sample. Under the same laser energy (130 mJ), as the impact counts increase, the microhardness improvements are 6.7% and 3.7%. Residual stress analysis demonstrates that the maximum compressive residual stress occurs at a subsurface depth of about 50 µm, with values of 520.71, 611.66, and 666.2 MPa for energies of 70, 100, and 130 mJ, respectively. The affected layer depth increases with energy, reaching 400 µm at 130 mJ. Multiple impacts at 130 mJ further enhance the peak residual stress to 722.8 MPa (2 impacts) and 776.2 MPa (3 impacts), with corresponding depths extending to 500 and 550 µm. Kernel Average Misorientation (KAM) maps confirm intensified plastic deformation and increased dislocation density in the treated samples, consistent with the residual stress profiles. Surface roughness (Surface Arithmetic Average Height, Sa: The arithmetic mean of the absolute values of the height differences between all points in the sampling area and the reference plane.) exhibits a non-monotonic trend with increasing laser energy: it increases at 70 mJ due to localized plastic deformation and micro-cracking, decreases at 100 mJ as uniform plastic flow smoothed surface asperities, and rises again at 130 mJ owing to dominant thermal effects such as micro-melting and resolidification. Similarly, increasing the number of impacts leads to progressive roughness deterioration, attributing to cumulative plastic deformation and thermal damage. AFM topography further illustrates the evolution of surface morphology, with maximum peak-to-valley heights increasing significantly under high-energy and multi-impact conditions.
Overall, a single impact at 130 mJ achieves the optimal balance between the hardness gradient and residual stress distribution. Furthermore, the evolution of surface roughness and morphology in the treated samples is governed by the combined mechanical-thermal effects of laser shock peening. The trends of these changes with variations in laser energy and impact count are non-monotonic.
This investigation reveals that the influence of laser energy and impact counts on the mechanical properties and surface integrity of 12Cr2Ni4A steel is nonlinear. While increasing laser energy and impact count enhances the residual compressive stress, the improvement in microhardness does not follow a monotonic trend. This behavior is attributed to dislocation saturation and thermal damage effects induced by high energy levels and multiple impacts. To achieve high-performance laser shock peening for critical components such as aircraft gears and splines, it is essential to consider the combined effects of laser energy and impact counts and identify the optimal strengthening parameters.

Key words

laser shock peening without coating / 12Cr2Ni4A steel / surface integrity / process optimization

Cite this article

Download Citations
XIE Cenchao, YU Shuiyou, WANG Ke, ZHANG Shaohua, WANG Rongping, CHEN Chao. Effect of Laser Shock Peening Process Without Coating Parameters on Mechanical Properties and Surface Integrity of 12Cr2Ni4A Steel[J]. Surface Technology. 2025, 54(23): 188-196 https://doi.org/10.16490/j.cnki.issn.1001-3660.2025.23.014

References

[1] 焦锋, 兰帅领, 王毅, 等. 超声滚压12Cr2Ni4A齿轮钢残余压应力特性研究及参数优化[J]. 表面技术, 2020, 49(11): 334-341.
JIAO F, LAN S L, WANG Y, et al.Residual Stress Characteristics and Parameters Optimization of Ultrasonic Rolling 12Cr2Ni4A Gear Steel[J]. Surface Technology, 2020, 49(11): 334-341.
[2] 曹金华, 吕长生, 杨昊, 等. 直升机传动系统的设计与优化[J]. 中国机械, 2024(3): 13-16.
CAO J H, LYU C S, YANG H, et al.Design and Optimization of Helicopter Transmission System[J]. Machine China, 2024(3): 13-16.
[3] 丁琪, 金华, 黄艳松. 直升机战伤分析与评估[J]. 直升机技术, 2009(2): 64-67.
DING Q, JIN H, HUANG Y S.Analysis and Evaluation of Helicopter War Injury[J]. Helicopter Technique, 2009(2): 64-67.
[4] 吴吉展, 朱才朝, 魏沛堂, 等. 航空齿轮钢强化工艺与表面完整性关联规律研究[J]. 表面技术, 2024, 53(1): 153-168.
WU J Z, ZHU C C, WEI P T, et al.Correlation between Strengthening Process and Surface Integrity of Aviation Gear Steel[J]. Surface Technology, 2024, 53(1): 153-168.
[5] 沈铁宏, 贾德凯, 周永鑫, 等. 表面滚压强化工艺对FV520B钢表面完整性的影响及预测模型建立[J]. 精密成形工程, 2023, 15(7): 166-175.
SHEN T H, JIA D K, ZHOU Y X, et al.Effect of Surface Rolling Strengthening Process on Surface Integrity of FV520B Steel and Establishment of Prediction Model[J]. Journal of Netshape Forming Engineering, 2023, 15(7): 166-175.
[6] 杨园园. 喷丸强化工艺及对齿轮的影响[J]. 科技创新与应用, 2016, 6(34): 137-138.
YANG Y Y.Shot Peening Strengthening Technology and Its Influence on Gear[J]. Technology Innovation and Application, 2016, 6(34): 137-138.
[7] 潘伟, 刘广华, 王炫力, 等. 热障涂层材料与技术发展综述[J]. 热喷涂技术, 2025, 17(1): 1-17.
PAN W, LIU G H, WANG X L, et al.Review of the Development of Thermal Barrier Coating Materials and Technologies[J]. Thermal Spray Technology, 2025, 17(1): 1-17.
[8] 赵绪杰, 马永新, 张增焕, 等. 激光冲击强化技术研究与应用现状[J]. 应用激光, 2022, 42(10): 111-119.
ZHAO X J, MA Y X, ZHANG Z H, et al.Research and Application Status of Laser Shock Peening Technology[J]. Applied Laser, 2022, 42(10): 111-119.
[9] 曹晓蝶, 李莹华, 杨玉奇, 等. 激光冲击强化机理及其在航空构件上的应用[J]. 表面技术, 2025, 54(8): 1-15.
CAO X D, LI Y H, YANG Y Q, et al.Laser Shock Processing Mechanism and Its Applications in Aeronautical Components[J]. Surface Technology, 2025, 54(8): 1-15.
[10] 窦杨, 周王凡, 吴永胜, 等. 无保护层激光冲击强化的热效应研究[J]. 表面技术, 2023, 52(5): 347-355.
DOU Y, ZHOU W F, WU Y S, et al.Thermal Effect of Laser Shock Peening without Coating[J]. Surface Technology, 2023, 52(5): 347-355.
[11] 蔡振兵, 周龙龙, 俞延庆, 等. 激光冲击强化技术在核电领域的研究进展[J]. 中国表面工程, 2024, 37(1): 41-58.
CAI Z B, ZHOU L L, YU Y Q, et al.Research Progress of Laser Shock Peening Technology in Nuclear Power Equipment[J]. China Surface Engineering, 2024, 37(1): 41-58.
[12] CHEN H Q, YAO Y L, KYSAR J W.Spatially Resolved Characterization of Residual Stress Induced by Micro Scale Laser Shock Peening[J]. Journal of Manufacturing Science and Engineering, 2004, 126(2): 226-236.
[13] CHEN H Q, YAO Y L, KYSAR J W, et al.Fourier Analysis of X-Ray Micro-Diffraction Profiles to Characterize Laser Shock Peened Metals[J]. International Journal of Solids and Structures, 2005, 42(11/12): 3471-3485.
[14] GUO Y B, CASLARU R.Fabrication and Characterization of Micro Dent Arrays Produced by Laser Shock Peening on Titanium Ti-6Al-4V Surfaces[J]. Journal of Materials Processing Technology, 2011, 211(4): 729-736.
[15] SANO Y, OBATA M, KUBO T, et al.Retardation of Crack Initiation and Growth in Austenitic Stainless Steels by Laser Peening without Protective Coating[J]. Materials Science and Engineering: A, 2006, 417(1/2): 334-340.
[16] KARTHIK D, DESHMUKH K, PRAVEENKUMAR K, et al.Laser Peening Induced Mitigation of Severe Pitting Corrosion in Titanium Stabilized 321 Steel[J]. Optics & Laser Technology, 2024, 172: 110537.
[17] DANG X F, LIANG X Q, LUO S H, et al.Surface Strengthening and Fatigue Life Improvement of Single Crystal Ni-Based Superalloys via Laser Shock Peening without Coating[J]. Materials & Design, 2023, 232: 112097.
[18] CHEN H T, DOU M, LI L, et al.Plastic Deformations of 42CrMo4 under LSPwC and Subsequent Cyclic Stresses[J]. International Journal of Mechanical Sciences, 2023, 259: 108623.
[19] 郭大浩, 吴鸿兴, 王声波, 等. 激光冲击强化机理研究[J]. 中国科学E辑: 技术科学, 1999, 29(3): 222-226.
GUO D H, WU H X, WANG S B, et al.Study on Mechanism of Laser Shock Strengthening[J]. Science in China, Ser E, 1999, 29(3): 222-226.
[20] 何兆儒, 沈一洲, 周晋, 等. 激光冲击强化的微观组织演变与性能研究进展[J]. 航空制造技术, 2021, 64(19): 48-58.
HE Z R, SHEN Y Z, ZHOU J, et al.Microstructure Evolution and Performance Enhancement of Laser Shock Peening[J]. Aeronautical Manufacturing Technology, 2021, 64(19): 48-58.
[21] ZHAO X Y, LI H J.Experimental Study on the Dynamic Behavior of a Cr-Ni-Mo-V Steel under Different Shock Stresses[J]. Metals, 2023, 13(4): 663.
[22] LEN E, GALSTIAN I, GUSTMANN T, et al.Effect of High Energy Laser Processing on Defect and Structural Phase State of Titanium Products Made by Additive Technologies[J]. Applied Physics A, 2025, 131(3): 187.
[23] 周建忠, 黄舒, 赵建飞, 等. 激光喷丸强化铝合金疲劳特性的数字化分析[J]. 中国激光, 2008, 35(11): 1735-1740.
ZHOU J Z, HUANG S, ZHAO J F, et al.Numerical Analysis on Fatigue Properties of Aluminum Alloy Induced by Laser Shock Peening[J]. Chinese Journal of Lasers, 2008, 35(11): 1735-1740.
[24] RUBIO-GONZÁLEZ C, OCAÑA J L, GOMEZ-ROSAS G, et al. Effect of Laser Shock Processing on Fatigue Crack Growth and Fracture Toughness of 6061-T6 Aluminum Alloy[J]. Materials Science and Engineering: A, 2004, 386(1/2): 291-295.
[25] LIU L M, WANG H Y.The Effect of the Adhesive on the Microcracks in the Laser Welded Bonding Mg to Al Joint[J]. Materials Science and Engineering: A, 2009, 507(1/2): 22-28.
[26] 段晓峰, 汪岳峰, 牛燕雄, 等. 激光辐照光学材料热力效应的解析计算和损伤评估[J]. 中国激光, 2004, 31(12): 1455-1459.
DUAN X F, WANG Y F, NIU Y X, et al.Analytic Calculation and Evaluation of Thermal and Mechanical Damage in Optical Materials Induced by Laser[J]. Chinese Journal of Lasers, 2004, 31(12): 1455-1459.
[27] 杨启, 付雪松, 周文龙. 激光喷丸表面强化技术的研究综述[J]. 航空制造技术, 2020, 63(12): 14-22.
YANG Q, FU X S, ZHOU W L.Research Status and Application Progress of Laser Shot Peening Surface Strengthening Technology[J]. Aeronautical Manufacturing Technology, 2020, 63(12): 14-22.

Funding

National Key Research and Development Program of China (2022YFB4601703)
PDF(10940 KB)

Accesses

Citation

Detail

Sections
Recommended

/