宋雨键,秦海勤,张德跃,吉鹏程,刘坤,秦敏.典型阳极氧化工艺对2A12-T4铝合金疲劳寿命的影响[J].装备环境工程,2025,22(3):26-32. SONG Yujian,QIN Haiqin,ZHANG Deyao,JI Pengcheng,LIU Kun,QIN Min.Influence of Typical Anodizing Process on Fatigue Life of 2A12-T4 Aluminum Alloy[J].Equipment Environmental Engineering,2025,22(3):26-32.
典型阳极氧化工艺对2A12-T4铝合金疲劳寿命的影响
Influence of Typical Anodizing Process on Fatigue Life of 2A12-T4 Aluminum Alloy
投稿时间:2024-11-21  修订日期:2025-02-12
DOI:10.7643/issn.1672-9242.2025.03.004
中文关键词:  2A12-T4铝合金  阳极氧化  疲劳试验  表面处理  疲劳寿命  分散系数中图分类号:V252.2 文献标志码:A 文章编号:1672-9242(2025)03-0026-07
英文关键词:2A12-T4 aluminum alloy  anodizing  fatigue test  surface treatment  fatigue life  dispersion coefficient
基金项目:山东省自然科学基金(ZR2021QE193)
作者单位
宋雨键 海军航空大学青岛校区,山东 青岛 266041;中国人民解放军95939部队,河北 沧州 061037 
秦海勤 海军航空大学青岛校区,山东 青岛 266041 
张德跃 中国人民解放军95939部队,河北 沧州 061037 
吉鹏程 海军航空大学青岛校区,山东 青岛 266041 
刘坤 海军航空大学青岛校区,山东 青岛 266041 
秦敏 海军航空大学青岛校区,山东 青岛 266041 
AuthorInstitution
SONG Yujian Qingdao Campus of Naval Aviation University, Shandong Qingdao 266041, China;Unit 95939, People's Liberation Army, Hebei Cangzhou 061037, China 
QIN Haiqin Qingdao Campus of Naval Aviation University, Shandong Qingdao 266041, China 
ZHANG Deyao Unit 95939, People's Liberation Army, Hebei Cangzhou 061037, China 
JI Pengcheng Qingdao Campus of Naval Aviation University, Shandong Qingdao 266041, China 
LIU Kun Qingdao Campus of Naval Aviation University, Shandong Qingdao 266041, China 
QIN Min Qingdao Campus of Naval Aviation University, Shandong Qingdao 266041, China 
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中文摘要:
      目的 研究4种典型阳极氧化工艺对2A12-T4铝合金疲劳寿命的影响。方法 分别采用硫酸阳极氧化、硬质阳极氧化、硫酸-硼酸阳极氧化和微弧氧化等4种典型阳极氧化工艺对2A12-T4铝合金试件进行表面处理,并开展150、200 MPa等2种最大应力下的疲劳试验,对未经表面阳极化处理和不同阳极化处理试验件的疲劳寿命进行统计分析,研究典型阳极氧化工艺对2A12-T4铝合金疲劳寿命的影响。结果 普通试件和4种阳极氧化试件疲劳寿命均服从对数正态分布。4种阳极氧化工艺均对2A12-T4铝合金试件的疲劳寿命产生不利影响,即分散系数变大,安全寿命减小。同时发现,应力水平增大时,同一阳极氧化工艺处理试件的分散系数也会变大,安全寿命相应减小。结论 经4种阳极氧化工艺处理后,2A12-T4铝合金的疲劳寿命仍服从对数正态分布,但除最大应力为150 MPa下的硫酸-硼酸阳极氧化试件的疲劳寿命增加0.4%外,其他试件的疲劳寿命均出现下降,且下降幅度与分散系数均和应力水平成正相关。
英文摘要:
      The work aims to study the effects of four typical anodizing processes on the fatigue life of 2A12-T4 aluminum alloy.The surface of 2A12-T4 aluminum alloy specimens was treated with four typical anodizing processes:sulfuric acid anodizing, hard anodizing, sulfuric-boric acid anodizing, and microarc oxidation. Fatigue tests were conducted at two maximum stress levels of 150 MPa and 200 MPa. The fatigue life of anodized specimens and ordinary specimens was statistically analyzed to investigate the effects of typical anodizing processes on the fatigue life of 2A12-T4 aluminum alloy.The result showed that the fatigue life of both ordinary and anodized specimens followed a lognormal distribution. All four anodizing processes had an adverse effect on the fatigue life of 2A12-T4 aluminum alloy specimens, resulting in an increased dispersion coefficient and a reduced safe life. It was also found that the dispersion coefficient of specimens treated with the same anodizing process increased, and the safe life correspondingly decreased, with the increase of stress level. In conclusion,the fatigue life of 2A12-T4 aluminum alloy treated with the four anodizing processes still follows a lognormal distribution. However, except for a 0.4% increase in fatigue life for sulfuric-boric acid anodized specimens under a maximum stress of 150 MPa, the fatigue life of other specimens decreased. There is a positive correlation between the decreasing amplitude and the dispersion coefficient.
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