超声波喷丸对7B04-T651铝合金应力腐蚀行为影响

孙强

装备环境工程 ›› 2026, Vol. 23 ›› Issue (5) : 64-72.

PDF(6375 KB)
PDF(6375 KB)
装备环境工程 ›› 2026, Vol. 23 ›› Issue (5) : 64-72. DOI: 10.7643/ issn.1672-9242.2026.05.008
航空航天装备

超声波喷丸对7B04-T651铝合金应力腐蚀行为影响

  • 孙强
作者信息 +

Effect of Ultrasonic Peening on Stress Corrosion Behavior of 7B04-T651 Aluminum Alloy

  • SUN Qiang
Author information +
文章历史 +

摘要

目的 解决以7B04铝合金为主要结构材料的某型航空装备主体结构应力腐蚀开裂风险高,影响装备结构完整性与服役可靠性的典型失效问题。方法 采用超声喷丸的方式对7B04-T651铝合金在装配前进行残余应力释放,通过监测应力腐蚀开裂裂纹扩展规律、处理前后金相组织、电化学耐蚀性能、微区电化学行为等表征,结合基于COMSOL多物理场的数值仿真结果,研究超声喷丸对铝合金应力腐蚀行为的影响。结果 基准试件的裂纹最早从第3循环开始萌生,到第7循环后裂纹扩展速率趋于平缓,约为2.81 mm/循环。超声喷丸试件的裂纹最早萌生在第6循环,裂纹长度呈现线性增大,平均裂纹扩展速率为2.01 mm/循环。结论 超声喷丸的方式有助于缓解7B04-T651铝合金应力腐蚀行为,超声波喷丸与基准件对比,对应力腐蚀的缓解效率约为11%,能够使得裂纹萌生周期推迟2个周期以上,同时也使得基体材料耐蚀性能提高36%。

Abstract

The work aims to address the typical failure of high stress corrosion cracking risks in the main structure of a certain type of aviation equipment with 7B04 aluminum alloy as the main structural material, which affects the structural integrity and service reliability of the equipment. Ultrasonic shot peening was adopted to release the residual stress of 7B04-T651 aluminum alloy before assembly. By monitoring the crack propagation law of stress corrosion cracking, metallographic structure before and after treatment, electrochemical corrosion resistance, micro-area electrochemical behavior and other characterizations, combined with the numerical simulation results based on COMSOL multi-physical field, the effect of ultrasonic shot peening on the stress corrosion behavior of aluminum alloy was studied. The crack of the reference specimen initiated at the 3rd cycle at the earliest, and the crack propagation rate tended to be gentle after the 7th cycle, about 2.81 mm/cycle. The crack of the ultrasonic shot peening specimen initiated at the 6th cycle at the earliest, and the crack length increased linearly, with an average crack propagation rate of 2.01 mm/cycle. In conclusion, ultrasonic shot peening is helpful to alleviate the stress corrosion behavior of 7B04-T651 aluminum alloy. Compared with the reference specimen, the mitigation efficiency of ultrasonic shot peening on stress corrosion is about 11%, which can delay the crack initiation cycle by more than 2 cycles, and also improve the corrosion resistance of the matrix material by 36%.

关键词

7B04铝合金 / 超声波喷丸 / 周期浸润 / 电化学分析 / 腐蚀仿真 / 应力腐蚀

Key words

7B04 aluminum alloy / ultrasonic shot peening / periodic immersion / electrochemical analysis / corrosion simulation / stress corrosion

引用本文

导出引用
孙强. 超声波喷丸对7B04-T651铝合金应力腐蚀行为影响[J]. 装备环境工程. 2026, 23(5): 64-72 https://doi.org/10.7643/ issn.1672-9242.2026.05.008
SUN Qiang. Effect of Ultrasonic Peening on Stress Corrosion Behavior of 7B04-T651 Aluminum Alloy[J]. Equipment Environmental Engineering. 2026, 23(5): 64-72 https://doi.org/10.7643/ issn.1672-9242.2026.05.008
中图分类号: TG172   

参考文献

[1] 汝继刚, 伊琳娜. 不同时效处理对7B04铝合金腐蚀性能的影响[J]. 轻合金加工技术, 2004, 32(5): 45-47.
RU J G, YI L N.Effect of Different Ageing Treatment on Corrosion Properties of 7B04 Alloy[J]. Light Alloy Fabrication Technology, 2004, 32(5): 45-47.
[2] 耿志强, 李玉仙, 蔡云卿等. 不同表面处理对7050- T7451铝合金应力腐蚀性能影响的研究[J]. 材料工程, 2013, (12): 44-49.
GENG Z Q, LI Y X, CAI Y Q, et al.Study on the Effect of Different Surface Treatments on the Stress Corrosion Performance of 7050-T7451 Aluminum Alloy[J]. Journal of Materials Engineering, 2013, (12): 44-49.
[3] 胡国胜, 张硕, 赵玉盼, 等. 应力腐蚀裂纹形成扩展机理及影响因素研究进[J]. 稀有金属材料与工程, 2018, 47(10): 3008-3016.
HU G S, ZHANG S, ZHAO Y P, et al.Research Progress on the Formation and Propagation Mechanism of Stress Corrosion Cracks and Influencing Factors[J]. Rare Metal Materials and Engineering, 2018, 47(10): 3008-3016.
[4] 刘志远, 朱宏亮, 王磊, 等. 应力腐蚀行为对环境、材料、应力的敏感性研究[J]. 材料导报, 2017, 31(6): 12-15.
LIU Z Y, ZHU H L, WANG L, et al.Study on the Sensitivity of Stress Corrosion Behavior to Environment, Material and Stress[J]. Materials Reports, 2017, 31(6): 12-15.
[5] ZHANG X Y, LIU M, LU F, et al.Atmospheric Corrosion of 7B04 Aluminum Alloy in Marine Environments[J]. Corrosion Science and Technology, 2018, 17(1): 6-11.
[6] 陈跃良, 赵红君, 王晨光, 等. 7B04铝合金和30CrMnSiA钢短期腐蚀的电化学行为研究[J]. 装备环境工程, 2018, 15(1): 34-39.
CHEN Y L, ZHAO H J, WANG C G, et al.Short-Term Electrochemical Corrosion Behavior of 7B04 Aluminum Alloy and 30CrMnSiA Steel[J]. Equipment Environmental Engineering, 2018, 15(1): 34-39.
[7] 陈跃良, 赵红君, 卞贵学, 等. 电偶效应对与30CrMnSiA钢耦合的7B04铝合金当量折算系数的影响[J]. 航空学报, 2017, 38(12): 314-323.
CHEN Y L, ZHAO H J, BIAN G X, et al.Influence of Galvanic Action on Equivalent Conversion Coefficient of 7B04 Aluminum Alloy Coupled with 30CrMnSiA Steel[J]. Acta Aeronautica et Astronautica Sinica, 2017, 38(1 2): 314-323.
[8] 刘治国, 颜光耀, 吕航. 7B04铝合金服役环境下点蚀表面损伤特征研究[J]. 环境技术, 2017, 35(5): 46-49.
LIU Z G, YAN G Y, LYU H.Research on Pitting Corrosion Damage Characteristics of 7B04 Aluminum Alloys in Service Environment[J]. Environmental Technology, 2017, 35(5): 46-49.
[9] 刘治国, 韩玉, 朱武峰, 等. 基于点蚀试验的7B04铝合金材料点蚀密度研究[J]. 环境技术, 2017, 35(4): 8-11.
LIU Z G, HAN Y, ZHU W F, et al.Research of 7B04 Aluminum Alloys Pitting Corrosion Density Based on Pitting Corrosion Test[J]. Environmental Technology, 2017, 35(4): 8-11.
[10] 段娜, 刘兰华, 魏颖. 2000 MPa级高强度端接板钢的应力腐蚀性能影响的研究[J]. 金属学报, 2018, 54(12): 1710-1770.
DUAN N, LIU L H, WEI Y.Study on the Effect of Stress Corrosion Performance of 2000 MPa Grade High- Strength and Plate Steel[J]. Acta Metallurgica Sinica, 2018, 54(12): 1710-1770.
[11] 何小亮. 铜合金应力腐蚀研究进展[J]. 腐蚀与防护, 2018, 39(9), 951-956.
HE X L.Research Progress on Stress Corrosion of Copper Alloys[J]. Corrosion and Protection, 2018, 39(9): 951-956.
[12] 刘艳洁, 王振尧, 柯伟. 2024-T3铝合金在模拟海洋大气环境中的腐蚀行为[J]. 中国有色金属学报, 2013, 23(5): 1208-1216.
LIU Y J, WANG Z Y, KE W.Corrosion Behavior of 2024-T3 Aluminum Alloy in Simulated Marine Atmospheric Environment[J]. The Chinese Journal of Nonferrous Metals, 2013, 23(5): 1208-1216.
[13] 郑传波, 益帼, 高延敏. 高强铝合金应力腐蚀及氢渗透行为研究进展[J]. 腐蚀与防护, 2013, 34(7): 600-604.
ZHENG C B, YI G, GAO Y M.Research Progress of Stress Corrosion Cracking and Hydrogen Permeation Behavior of High Strength Aluminum Alloys[J]. Corrosion & Protection, 2013, 34(7): 600-604.
[14] 郑捷, 刘洋, 童明波. 腐蚀环境对飞机梁结构连接件疲劳寿命和裂纹扩展的影响[J]. 中国机械工程, 2019, 30(17): 2129-2134.
ZHENG J, LIU Y, TONG M B.Influences of Corrosion Environments on Fatigue Life and Crack Propagation of Aircraft Beam Structure Connectors[J]. China Mechanical Engineering, 2019, 30(17): 2129-2134.
[15] 罗开玉, 邢月华, 柴卿锋, 等. 激光冲击强化对2Cr13不锈钢腐蚀疲劳性能的影响[J]. 吉林大学学报(工学版), 2019, 49(3): 850-858.
LUO K Y, XING Y H, CHAI Q F, et al.Effects of Laser Shock Peening on Corrosion Fatigue Behaviour of 2Cr13 Stainless Steel[J]. Journal of Jilin University (Engineering and Technology Edition), 2019, 49(3): 850-858.
[16] SHENG J, XIA J W, MA R W.Experimental Study on the Coupling Effect of Sulfate Corrosion and Loading on the Mechanical Behavior of Steel and H-Section Beam[J]. Construction and Building Materials, 2018, 189: 711-718.
[17] 贺旺, 王燕礼, 王亚南, 等. 旋片喷丸对 7B04-T6 铝合金应力腐蚀抗性的影响[J]. 航空材料学报, 2020, 40(6): 75-82.
HE W, WANG Y L, WANG Y N, et al.Effect of Rotary Shot Peening on Stress Corrosion Resistance of 7B04-T6 Aluminum Alloy[J]. Journal of Aeronautical Materials, 2020, 40(6): 75-82.
[18] 张新明, 何道广, 刘胜胆, 等. 多级强化固溶处理对7050铝合金厚板强度和断裂韧性的影响[J]. 中国有色金属学报, 2012, 22(6): 1546-1554.
ZHANG X M, HE D G, LIU S D, et al.Effects of Multi-Stage Promotively-Solutionizing Treatment on Strength and Fracture Toughness of 7050 Aluminum Alloy Thick Plate[J]. The Chinese Journal of Nonferrous Metals, 2012, 22(6): 1546-1554.
[19] 李明, 朱金阳, 李刚, 等. 典型航空装备用金属材料在不同酸性盐雾环境下的腐蚀效应及机理[J]. 装备环境工程, 2019, 16(4): 38-45.
LI M, ZHU J Y, LI G, et al.Corrosion Performance and Mechanism of Typical Aviation Metal Materials under Different Acid Salt Spray Test Environments[J]. Equipment Environmental Engineering, 2019, 16(4): 38-45.
[20] 陈跃良, 黄海亮, 卞贵学, 等. 多电极偶接对金属大气腐蚀影响的试验与仿真[J]. 航空学报, 2018, 39(6): 205-215.
CHEN Y L, HUANG H L, BIAN G X, et al.Test and Simulation of Effects of Multi-Electrode Coupling on Atmospheric Corrosion of Metals[J]. Acta Aeronautica et Astronautica Sinica, 2018, 39(6): 205-215.
[21] 陶春虎, 刘昌奎. 舰载机的腐蚀失效及其预防[J]. 中国材料进展, 2014, 33(S1): 623-629.
TAO C H, LIU C K.Corrosion Failure and Prevention of Carrier-Based Aircraft[J]. Materials China, 2014, 33(S1): 623-629.
[22] 雷明华. 金属材料应力腐蚀分析[J]. 合成材料老化与应用, 2019, 48(1): 115-119.
LEI M H.Stress Corrosion Analysis of Metal Materials[J]. Synthetic Materials Aging and Application, 2019, 48(1): 115-119.
[23] 李春岭. 7075铝合金应力腐蚀开裂机理研究[D]. 镇江: 江苏科技大学, 2014.
LI C L.The Study of7075aluminum Alloy to Stress Corrosion Cracking Mechanism[D]. Zhenjiang: Jiangsu University of Science and Technology, 2014.
[24] 祁文娟, 宋仁国, 祁星, 等. 不同时效状态下7050铝合金氢致开裂行为[J]. 材料热处理学报, 2014, 35(11): 56-62.
QI W J, SONG R G, QI X, et al.Hydrogen-Induced Cracking Behavior of 7050 Aluminum Alloy under Various Aging States[J]. Transactions of Materials and Heat Treatment, 2014, 35(11): 56-62.
[25] 谭晓明, 张丹峰, 战贵盼, 等. 海洋环境与疲劳载荷联合作用下喷丸超高强度钢损伤机制[J]. 航空学报, 2020, 41(8): 255-263.
TAN X M, ZHANG D F, ZHAN G P, et al.Damage Mechanism of Shot Peened Ultra-High Strength Steel under Combined Action of Marine Environment and Fatigue Load[J]. Acta Aeronautica et Astronautica Sinica, 2020, 41(8): 255-263.

PDF(6375 KB)

Accesses

Citation

Detail

段落导航
相关文章

/