航天推进技术研究院主办
XU Weichao,XUE Luping,YE Hui.Local hard anodizing technology of 2A14 aluminum alloy[J].Journal of Rocket Propulsion,2019,45(02):79-84.
2A14铝合金局部硬质阳极氧化工艺
- Title:
- Local hard anodizing technology of 2A14 aluminum alloy
- 文章编号:
- 1672-9374(2019)02-0079-06
- Keywords:
- 2A14 Aluminum Alloy; local hard anodizing; chromic acid anodizing film; double-sealed; corrosion resistance
- 分类号:
- V463
- 文献标志码:
- A
- 摘要:
- 针对2A14铝合金局部硬质阳极氧化工艺进行了深入研究,提出以双重封闭后的铬酸阳极氧化膜代替传统的涂漆保护,作为2A14铝合金局部硬质阳极氧化的遮蔽层。利用极化曲线、阻抗谱(EIS)和点滴试验等测试方法,研究了双重封闭后铬酸阳极氧化膜的腐蚀行为,并与重铬酸钾封闭、水封闭后氧化膜进行比较。与重铬酸钾封闭、水封闭相比,双重封闭后铬酸阳极氧化膜的腐蚀电流密度下降2个数量级,氧化膜多孔层电阻Rp值提高500倍以上,氧化膜点滴试验时间提高2倍~5倍。结果表明,双重封闭技术能有效提高铬酸阳极氧化膜的封孔质量,增强了耐腐蚀、耐电压性能,可作为2A14铝合金局部硬质阳极氧化遮蔽层。采用该工艺制备的局部硬质阳极氧化膜均匀致密,厚度可达60 μm,平均硬度可达360,满足设计要求(厚度≥40 μm,硬度≥329)。
- Abstract:
- The local hard anodizing process of 2A14 aluminum alloy has been studied and it was proposed that the double-sealed chromic acid anodizing film can be used as the shielding layer for the local hard anodizing of 2A14 aluminum alloy instead of the traditional painted protection.The corrosion behavior of the double-sealed chromic acid anodizing film was studied by means of polarization curve, electrochemical impedance spectroscopy(EIS)and dropping test, which was also compared with the oxidation film sealed by potassium dichromate and water.According to the comparison results, after double sealing, the corrosion current density of the chromic acid anodizing film decreases by two orders of magnitude, the resistance Rp value of porous oxide film is increased by more than 500 times, and the dropping test time is increased by 2 to 5 times.The results show that the double-sealed technology effectively improved the sealing quality of the chromic acid anodizing film so that it can be used as the local hard anodizing shielding layer of 2A14 aluminum alloy with good corrosion resistance and voltage resistance.The local hard anodizing film prepared by this process is uniform and dense, with the thickness up to 60 μm and the average hardness up to 360, which meets the design requirements(thickness≥40 μm and hardness≥329).
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备注/Memo
收稿日期:2017-10-18; 修回日期:2018-05-29 作者简介:许维超(1987—),男,硕士,工程师,研究领域为液体火箭发动机表面处理