Research Progresses of Surface Integrity and Fatigue Performance for High-temperature Alloy Shot Peening Processes

doi:10.3969/j.issn.1004-132X.2026.02.007

China Mechanical Engineering ›› 2026, Vol. 37 ›› Issue (2): 315-331.DOI: 10.3969/j.issn.1004-132X.2026.02.007

Research Progresses of Surface Integrity and Fatigue Performance for High-temperature Alloy Shot Peening Processes

SUN Yunqi¹^,²(), YAO Changfeng¹^,²^,³(), SUN Huanfeng⁴, TAN Liang¹^,²^,³

^1.Key Laboratory of High Performance Manufacturing for Aero Engine，Ministry of Industry and Information Technology，Northwestern Polytechnical University，Xi'an，710072
^2.Engineering Research Center of Advanced Manufacturing Technology for Aero Engine，Ministry of Education，Northwestern Polytechnical University，Xi'an，710072
^3.State Key Laboratory of Cemented Carbide，Northwestern Polytechnical University，Xi'an，710072
^4.AECC Aviation Power Co. ，Ltd. ，Xi'an，710072

Received:2025-03-03 Online:2026-02-25 Published:2026-03-13
Contact: YAO Changfeng

高温合金喷丸工艺表面完整性及其疲劳性能研究进展

孙蕴齐¹^,²(), 姚倡锋¹^,²^,³(), 孙换凤⁴, 谭靓¹^,²^,³

^1.西北工业大学航空发动机高性能制造工业和信息化部重点实验室, 西安, 710072
^2.西北工业大学航空发动机先进制造技术教育部工程研究中心, 西安, 710072
^3.硬质合金全国重点实验室(西北工业大学), 西安, 710072
^4.中国航发动力股份有限公司, 西安, 710072

通讯作者: 姚倡锋
作者简介:孙蕴齐，男，1994年生，博士研究生。研究方向为整体叶盘多工艺复合加工表面完整性控制。E-mail：yqsun@mail.nwpu.edu.cn
姚倡锋^*（通信作者），男，1975年生，教授、博士研究生导师。研究方向为航空发动机关键零部件表面完整性控制及抗疲劳制造。E-mail：chfyao@nwpu.edu.cn。
第一联系人：张晨晨^*（通信作者），女， 1996 年生，讲师、博士。研究方向为流体传动与控制。E-mail： zhangchenchen@nbut.edu.cn。
基金资助:
国家自然科学基金(92360309);国家自然科学基金(92160301);陕西省重点研发计划(2024PT-ZCK-63)

Abstract

Abstract:

High temperature alloys were important materials for key components of aircraft engines， and shot peening was a critical step in the manufacturing process of blade parts. Through the high-speed impact of the projectile on the surfaces of the workpieces， residual compressive stress might be introduced to the surfaces， thereby offsetting some working loads and improving the fatigue performance of the components. Therefore， studying the shot peening processes of high-temperature alloys was of great significance for improving the service performance and reliability of key components in aircraft engines. This paper introduced the research status of high-temperature alloy shot peening processes in terms of simulation methods， surface integrity of high-temperature alloy shot peening， and fatigue performance of high-temperature alloy shot peening. Finally， the shortcomings of existing research and future research directions were analyzed.

Key words: high temperature alloy, shot peening, surface integrity, fatigue performance

摘要：

高温合金是航空发动机关键构件的重要材料，喷丸加工是叶片类零件工艺过程的关键环节，通过弹丸在工件表面的高速撞击，能够在表层引入残余压应力，从而抵消部分工作载荷，提高构件的疲劳性能，因此，研究高温合金喷丸工艺对改善航空发动机关键构件的使役性能与可靠性有重要意义。针对喷丸工艺模拟方法、高温合金喷丸表面完整性和高温合金喷丸疲劳性能三方面的研究成果，介绍了高温合金喷丸工艺的研究现状，分析了现有研究存在的一些不足，并指出了未来的研究方向。

关键词: 高温合金, 喷丸工艺, 表面完整性, 疲劳性能

CLC Number:

TG506

SUN Yunqi, YAO Changfeng, SUN Huanfeng, TAN Liang. Research Progresses of Surface Integrity and Fatigue Performance for High-temperature Alloy Shot Peening Processes[J]. China Mechanical Engineering, 2026, 37(2): 315-331.

孙蕴齐, 姚倡锋, 孙换凤, 谭靓. 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.

Figures/Tables 17

Fig.1 Schematic of shot peening strengthening［3］

Fig.2 The influence of shot peening coverage on surface deformation condition［5］

Fig.3 Finite element simulation of multiple shot peening［6］

Fig.4 Finite element simulation of shot peening with different coverage rates［13］

Fig.5 Finite element model of shot peening based on Abaqus-Python secondary development［17］

Fig.6 The influence of different coverage rates on surface quality［19］

Fig.7 FEM-DEM coupled shot blasting simulation method［20］

Fig.8 Scanning electron microscopy images of the sample surface after shot peening［27］

Fig.9 Surface morphology after the single shot peening and multiple shot peening

Fig.10 Comparison of surface roughness between the single shot peening and multiple shot peening

Fig.11 Pre-stress shot peening of Inconel625 alloy［33］

Fig.12 Surface microstructure of shot-peened specimens［38］

Fig.13 Metallographic structure of sub surface layer of FGH4113A high-temperature alloy under different shot peening intensities［43］

Fig.14 Fatigue fracture morphology of GH4169 high-temperature alloy treated with shot peening and vibration finishing decoration composite［46］

Fig.15 Fatigue strength of FGH96 alloy notch specimen in grinding/shot peening state［50］

Fig.16 Fracture characterization of IN718 fatigue specimens

Fig.17 High cycle fatigue life and fracture morphology of specimens under different shot peening pressures［60］

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Research Progresses of Surface Integrity and Fatigue Performance for High-temperature Alloy Shot Peening Processes

高温合金喷丸工艺表面完整性及其疲劳性能研究进展

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