Corrosion mechanism and machinability of 7075-T6 aluminum alloy in high-speed cutting: With and without cryogenic treatment

被引:4
|
作者
Zhang, Ping [1 ,2 ,4 ]
Wang, Shunxiang [1 ]
Lin, Zhenyong [1 ]
Liu, Zehua [1 ,2 ]
Liu, Junling [3 ]
Mai, Qingqun [1 ]
Yue, Xiujie [5 ]
机构
[1] Guangdong Ocean Univ, Coll Mech & Power Engn, Zhanjiang, Peoples R China
[2] Qingdao Huanghai Univ, Coll Intelligent Mfg, Qingdao, Peoples R China
[3] Yantai Univ, Coll Intelligent Mfg, Qingdao, Peoples R China
[4] Guangdong Ocean Univ, Qingdao Huanghai Univ, 1 Haida Rd, Zhanjiang 524088, Peoples R China
[5] Qingdao Huanghai Univ, Qingdao 266033, Peoples R China
来源
MATERIALS AND CORROSION-WERKSTOFFE UND KORROSION | 2023年 / 74卷 / 06期
基金
中国国家自然科学基金;
关键词
7075-T6 aluminum alloy; corrosion resistance; cryogenic treatment; curface quality; cutting force; BEHAVIOR; MICROSTRUCTURE; COATINGS; STEEL; PEO;
D O I
10.1002/maco.202213515
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
This work aims to explore the effect of cutting parameters on the cutting force, surface quality, and corrosion resistance of 7075-T6 aluminum alloy after and without cryogenic treatment. Cryogenically treated (T6-C) and noncryogenically treated (T6) 7075-T6 aluminum alloy samples are experimentally cut and electrochemically corroded in a 3.5% NaCl solution. SEM, EDS, and electrochemical analysis are carried out to examine how cutting parameters affect the cutting force, surface quality, and corrosion resistance of cryogenically treated 7075-T6 aluminum alloy. The results show that after cryogenic treatment, under different cutting speeds, the cutting force is up to 39.8% smaller than without cryogenic treatment; under different cutting depths and feed rates, the cutting force is up to 136% and 21.54% smaller, respectively. Cryogenic treatment dramatically reduces the cutting force in the cutting process. As cutting speed increases, machined surface quality becomes better; fewer corrosion products and cracks are induced. When the cutting depth is 1.5 mm, there are fewer plows and micro-cracks on the machined surface than under other parameters, but cutting depth does not affect corrosion morphology significantly. The size of corrosion products is up to 55 mu m smaller. The electrochemical analysis finds that at the cutting speed of 1500 m/min, after cryogenic treatment, the current density is 59.4% smaller than without cryogenic treatment; polarization resistance is 1.68 x 10(5)omega center dot cm(2) larger. At the cutting depth of 1.5 mm, after cryogenic treatment, the current density is 66.16% smaller; self-corrosion potential shifts 0.19 V toward the positive pole. At the feed rate of 0.06 mm/z, after cryogenic treatment, self-corrosion potential shifts 0.18 V toward the positive pole; polarization resistance is 10.7% larger. These parameters correspond to the best corrosion resistance.
引用
收藏
页码:872 / 886
页数:15
相关论文
共 50 条
  • [21] Effect of Load on the Corrosion Behavior of Friction Stir Welded AA 7075-T6 Aluminum Alloy
    Cabrini, Marina
    Bocchi, Sara
    D'Urso, Gianluca
    Giardini, Claudio
    Lorenzi, Sergio
    Testa, Cristian
    Pastore, Tommaso
    MATERIALS, 2020, 13 (11)
  • [22] Piecewise Modeling of Flow Stress of 7075-T6 Aluminum Alloy in Hot Deformation
    Mei, Ruibin
    Bao, Li
    Cai, Ban
    Li, Changsheng
    Liu, Xianghua
    MATERIALS TRANSACTIONS, 2016, 57 (07) : 1147 - 1155
  • [23] Effect of T6I4 and T616 on the machinability of 7075 aluminum alloy and tool wear mechanism
    Zhang, Ping
    Gao, Yeran
    Wang, Shunxiang
    Liu, Zehua
    Lin, Zhenyong
    Zhang, Songting
    Yue, Xiujie
    INTERNATIONAL JOURNAL OF ADVANCED MANUFACTURING TECHNOLOGY, 2023, 127 (9-10) : 4453 - 4471
  • [24] Effect of surface mechanical attrition treatment on high cycle and very high cycle fatigue of a 7075-T6 aluminium alloy
    Gao, Tao
    Sun, Zhidan
    Xue, Hongqian
    Retraint, Delphine
    INTERNATIONAL JOURNAL OF FATIGUE, 2020, 139
  • [25] Mechanical Properties of 7075-T6 Aluminum Alloy in Electrically Assisted Forming
    Dou, Shasha
    Liu, Zhuang
    Li, Zhijun
    Shi, Haojie
    Zhou, Kang
    Xia, Jiansheng
    METALS, 2025, 15 (02)
  • [26] CRACK INVESTIGATION IN A FRAME OF A PASSENGER AIRPLANE STRUCTURE MADE OF ALUMINUM ALLOY 7075-T6
    Nikouee, A. R.
    Adibnazari, S.
    JOURNAL OF THE BALKAN TRIBOLOGICAL ASSOCIATION, 2016, 22 (03): : 2186 - 2197
  • [27] Mechanical properties and microstructure of aluminum alloy 7075-T6 spot-welding joint
    Zhang, Yue
    Jiang, Jiachuan
    Peng, Ruitao
    Zhu, Linwei
    Lu, Yan
    Lei, Bei
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART E-JOURNAL OF PROCESS MECHANICAL ENGINEERING, 2023,
  • [28] Investigation of the friction and wear properties of nitrided 7075-T6 aluminum alloy under vacuum and ambient air
    Ghahramanzadeh Asl, Hojjat
    Sert, Yasar
    Bayrak, Ozgu
    Kucukomeroglu, Tevfik
    PAMUKKALE UNIVERSITY JOURNAL OF ENGINEERING SCIENCES-PAMUKKALE UNIVERSITESI MUHENDISLIK BILIMLERI DERGISI, 2022, 28 (01): : 63 - 71
  • [29] Preparation and properties of a novel nano Ni-B-Sn by electroless deposition on 7075-T6 aluminum alloy for aerospace application
    Abdel-Gawad, Soha A.
    Sadik, Mervat A.
    Shoeib, Madiha A.
    JOURNAL OF ALLOYS AND COMPOUNDS, 2019, 785 : 1284 - 1292
  • [30] Study on the mechanical properties and fatigue failure mechanism of 7075-T6 aluminum alloy joints under different joining processes
    Zhang, Yue
    Zhu, Linwei
    Peng, Ruitao
    Xu, Honghe
    Lu, Yan
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART E-JOURNAL OF PROCESS MECHANICAL ENGINEERING, 2023, 237 (06) : 2466 - 2474