Please wait a minute...
中国腐蚀与防护学报  2018, Vol. 38 Issue (6): 579-586    DOI: 10.11902/1005.4537.2017.205
  本期目录 | 过刊浏览 |
硫酸阳极化对2E12铝合金力学性能的影响
陈高红1(),胡远森2,于美2,刘建华2,李国爱1
1. 北京航空材料研究院 北京市先进铝合金材料及应用工程技术研究中心 北京 100095
2. 北京航空航天大学材料科学与工程学院 北京 100191
Effect of Sulfuric Acid Anodizing on Mechanical Properties of 2E12 Al-alloy
Gaohong CHEN1(),Yuansen HU2,Mei YU2,Jianhua LIU2,Guoai LI1
1. Beijing Engineering Research Center of Advanced Aluminum Alloys and Applications, Beijing Institute of Aeronautical Materials, Beijing 100095, China
2. School of Materials Science and Engineering, Beihang University, Beijing 100191, China
全文: PDF(12575 KB)   HTML
摘要: 

采用传统的硫酸阳极氧化工艺对2E12航空铝合金进行处理,在铝合金表面制备了一层阳极氧化膜。研究了表面包铝层和阳极氧化时间对铝合金氧化膜表面形貌和硬度的影响,并探讨了硫酸阳极氧化处理对铝合金拉伸性能和疲劳性能的影响规律及机制。结果表明,2E12铝合金基体中的第二相在阳极氧化过程中会发生溶解,使得氧化膜表面出现孔洞。随着氧化时间的延长,氧化膜的厚度逐渐增加,孔洞数量也增多且尺寸变大。2E12铝合金经硫酸阳极氧化处理后,拉伸性能基本保持不变,但疲劳寿命出现明显下降。其中,去除包铝层的2E12铝合金经阳极氧化后,疲劳寿命最高下降到阳极氧化前的30%。硫酸阳极氧化处理后,疲劳裂纹起源于氧化膜表面的缺陷处,疲劳断口呈现多个裂纹源的特征。

关键词 航空铝合金硫酸阳极氧化疲劳寿命包铝层    
Abstract

2E12 Al-alloys without and with an Al-clad layer were treated via the traditional sulfuric acid anodizing process, so that an anodic oxide film was prepared on their surface. The effect of the Al-clad layer and anodic oxidation time on the surface morphology and mechanical properties of the anodic oxide films was investigated by means of morphological characterization, tensile property test and fatigue life test. The results showed that the dissolution of the second phase in the matrix of 2E12 Al-alloys can result in the formation of voids on the surface oxide film during the anodic oxidation process. With the increasing oxidation time, the thickness of the oxide film gradually increases, whilst the number and size of voids also increase. After sulfuric acid anodizing, the tensile property of 2E12 Al-alloy keeps basically unchanged, but the fatigue life decreases obviously. For the sulfuric acid anodized 2E12 Al-alloy without Al-clad layer, the fatigue life decreases to 30% of that for the counterpart . After the anodic oxidation treatment, the fatigue cracks originate from the defects of the oxide film surface, and the fatigue fracture shows multiple crack characteristics.

Key wordsaerospace aluminum alloy    sulfuric acid anodic oxidation    fatigue life    Al-clad layer
收稿日期: 2017-11-29     
ZTFLH:  TG174.451  
通讯作者: 陈高红     E-mail: 18611641263@163.com
Corresponding author: Gaohong CHEN     E-mail: 18611641263@163.com
作者简介: 陈高红,男,1986年生,硕士,工程师

引用本文:

陈高红,胡远森,于美,刘建华,李国爱. 硫酸阳极化对2E12铝合金力学性能的影响[J]. 中国腐蚀与防护学报, 2018, 38(6): 579-586.
Gaohong CHEN, Yuansen HU, Mei YU, Jianhua LIU, Guoai LI. Effect of Sulfuric Acid Anodizing on Mechanical Properties of 2E12 Al-alloy. Journal of Chinese Society for Corrosion and protection, 2018, 38(6): 579-586.

链接本文:

https://www.jcscp.org/CN/10.11902/1005.4537.2017.205      或      https://www.jcscp.org/CN/Y2018/V38/I6/579

PretreatmentSolutionTemperature / °CTime / s
Degreasing20 g/L Na3PO45080
10 g/L Na2CO3
5 g/L NaOH
Etching50 g/L NaOH5060
Pickling400 g/L HNO32510
表1  前处理溶液的化学组成,处理时间和温度
图1  拉伸试样示意图
图2  疲劳试样示意图
图3  氧化膜厚度与氧化时间的关系
图4  去除包铝层和保留包铝层的2E12铝合金经不同时间阳极氧化后的表面SEM像
SampleAnodizing time / minσb/ MPaδ10/ %σP0.2/ MPa
Unclad 2E12 Al-alloy047121.3329
1547120.4328
3046920.7325
4546120.2321
6046619.4325
Alclad 2E12 Al-alloy045321.4316
1545619.4316
3045319.2317
4545218.1316
6045518.9313
表2  去除包铝层和带包铝层的2E12铝合金阳极氧化处理前后的拉伸性能结果
Anodizing time / minNo.Fatigue lifeNi/ cyclelgN50Fatigue lifeN50/ cycleRelative life / %
011.63×1055.16001.45×105100%
21.49×105
31.57×105
41.19×105
51.39×105
1514.7×1044.67604.8×10433%
24.8×104
33.9×104
44.7×104
55.8×104
3015.7×1044.62214.3×10430%
24.3×104
34.7×104
44.0×104
52.8×104
4514.9×1044.64454.4×10430%
24.5×104
34.7×104
44.6×104
53.5×104
6015.1×1044.71645.2×10436%
24.9×104
35.2×104
46.0×104
54.9×104
表3  去除包铝层的2E12铝合金阳极氧化不同时间后疲劳性能结果
Anodizing time / minNo.Fatigue lifeNi/ cyclelgN50Fatigue lifeN50/ cycleRelative life / %
018.6×1044.97409.4×104100%
29.5×104
39.9×104
41.03×105
58.9×104
1517.6×1044.92978.5×10490%
28.5×104
38.9×104
47.9×104
59.8×104
3017.6×1044.86307.3×10478%
27.2×104
36.9×104
47.2×104
57.6×104
4516.0×1044.77406.0×10464%
25.4×104
36.5×104
46.4×104
55.5×104
6017.4×1044.84457.0×10474%
26.3×104
37.0×104
47.1×104
57.2×104
表4  保留包铝层的2E12铝合金阳极氧化不同时间后疲劳性能结果
图5  去除包铝层和带包铝层的2E12铝合金中值疲劳寿命相对值
图6  去除包铝层和带包铝层的2E12铝合金阳极氧化不同时间后的断口形貌
[1] Chen Z G,Ren J K,Zhang J S,et al.Regulation mechanism of novel thermomechanical treatment for microstructure and properties of 2E12 aluminum alloy[J].Rare Met. Mater. Eng.,2015,44:2341
[2] Liu X Y,Jiang J M,Chen Z T,et al.Research progress in anti-corrosive protection for aluminum alloy[J].Mod. Paint Finish.,2007,10(12):11
[2] 刘希燕,蒋健明,陈正涛等.铝合金防腐保护研究进展[J].现代涂料与涂装,2007,10(12):11
[3] Yin D Y,Liu H Q,Chen Y Q,et al.Effect of grain size on fatigue-crack growth in 2524 aluminium alloy[J].Int. J. Fatigue,2016,84:9
[4] Capelossi V R,Poelman M,Recloux I,et al.Corrosion protection of clad 2024 aluminum alloy anodized in tartaric-sulfuric acid bath and protected with hybrid sol-gel coating[J].Electrochim. Acta,2014,124:69
[5] Yoganandan G,Balaraju J N,Grips V K W.The surface and electrochemical analysis of permanganate based conversion coating on alclad and unclad 2024 alloy[J].Appl. Surf. Sci.,2012,258:8880
[6] Sieber M,Morgenstern R,Lampke T.Anodic oxidation of the AlCu4Mg1 aluminium alloy with dynamic current control[J].Surf. Coat. Technol.,2016,302:515
[7] Ma Y,Zhou X,Thompson G E,et al.Anodic film formation on AA 2099-T8 aluminum alloy in tartaric-sulfuric acid[J]. J. Electrochem. Soc.,2011,158:C17
[8] Mingo B,Němcová A,Hamad D,et al.Efficiency of anodising of Al-Cu alloy in sulphuric acid at low potentials[J].Trans. IMF,2015,93:18
[9] Zhang Y B,Zhang L M,Zhang J W,et al.Effect of anodizing treatment on bending fatigue properties of 2014-T6 aluminium alloy[J].Acta Metall. Sin.,2014,50:715
[9] 张艳斌,张立民,张继旺等.阳极氧化处理对2014-T6铝合金弯曲疲劳性能的影响[J].金属学报,2014,50:715
[10] Yu M,Chen G H,Liu J H,et al.Effect of adipic acid on fatigue performance of sulfuric anodizing for aluminum alloy[J].Heat Treat. Met.,2011,36(6):50
[10] 于美,陈高红,刘建华等.己二酸对铝合金硫酸阳极氧化疲劳性能的影响[J].金属热处理,2011,36(6):50
[11] China Iron and Steel Industry Association, CISA.GB/T 228.1-2010 Metallic materials-tensile testing-Part 1: Method of test at room temperature[S].Beijing:China Standard Press,2011
[11] 中国钢铁工业协会.GB/T 228.1-2010 金属材料 拉伸试验 第1部分: 室温试验方法[S].北京:中国标准出版社,2011
[12] HB 5287-96 Fatigue Test Method of Metal Material Under Axial Loading [S].Beijing:China Standard Press,1996
[12] HB 5287-96 金属材料轴向加载疲劳试验方法 [S].北京: 中国标准出版社,1996
[13] Veys-Renaux D,Chahboun N,Rocca E.Anodizing of multiphase aluminium alloys in sulfuric acid:In-situelectrochemical behaviour and oxide properties[J].Electrochim. Acta,2016,211:1056
[14] Yan J H,Peng C.Effect of sodium benzoate content on microstructure and properties of boric-sulfuric acid anodic film materials protection[J].Mater. Prot.,2013,46(10):18
[14] 颜杰红,彭超.苯甲酸钠含量对硼酸-硫酸阳极氧化膜形貌和性能的影响[J].材料保护,2013,46(10):18
[15] Huang Y S,Shih T S,Chou J H.Electrochemical behavior of anodized AA7075-T73 alloys as affected by the matrix structure[J].Appl. Surf. Sci.,2013,283:249
[1] 包俊成,赵捷,王志奇,马叙. 钛合金BT20焊接接头腐蚀疲劳性能的实验研究[J]. 中国腐蚀与防护学报, 2010, 30(4): 313-316.
[2] 张正; 宋诗哲; 陶蕾 . NaCl溶液中包覆铝层的LY12CZ铝合金阳极极化过程EIS特征[J]. 中国腐蚀与防护学报, 2008, 28(3): 135-140 .
[3] 常红; 韩恩厚; 王俭秋; 柯伟 . 飞机蒙皮涂层对LY12CZ铝合金腐蚀疲劳寿命的影响[J]. 中国腐蚀与防护学报, 2006, 26(1): 34-36 .