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Abstract
Aluminum alloy is the main structural material of aircraft, launch vehicle, spaceship, and space station and is processed by milling. However, tool wear and vibration are the bottlenecks in the milling process of aviation aluminum alloy. The machining accuracy and surface quality of aluminum alloy milling depend on the cutting parameters, material mechanical properties, machine tools, and other parameters. In particular, milling force is the crucial factor to determine material removal and workpiece surface integrity. However, establishing the prediction model of milling force is important and difficult because milling force is the result of multiparameter coupling of process system. The research progress of cutting force model is reviewed from three modeling methods: empirical model, finite element simulation, and instantaneous milling force model. The problems of cutting force modeling are also determined. In view of these problems, the future work direction is proposed in the following four aspects: (1) high-speed milling is adopted for the thin-walled structure of large aviation with large cutting depth, which easily produces high residual stress. The residual stress should be analyzed under this particular condition. (2) Multiple factors (e.g., eccentric swing milling parameters, lubrication conditions, tools, tool and workpiece deformation, and size effect) should be considered comprehensively when modeling instantaneous milling forces, especially for micro milling and complex surface machining. (3) The database of milling force model, including the corresponding workpiece materials, working condition, cutting tools (geometric figures and coatings), and other parameters, should be established. (4) The effect of chatter on the prediction accuracy of milling force cannot be ignored in thin-walled workpiece milling. (5) The cutting force of aviation aluminum alloy milling under the condition of minimum quantity lubrication (mql) and nanofluid mql should be predicted.
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Details
1 Qingdao University of Technology, School of Mechanical and Automotive Engineering, Qingdao, China (GRID:grid.412609.8) (ISNI:0000 0000 8977 2197)
2 Nanjing University of Aeronautics and Astronautics, College of Mechanical and Electrical Engineering, Nanjing, China (GRID:grid.64938.30) (ISNI:0000 0000 9558 9911)
3 Chongqing University, State Key Laboratory Mechanical Transmiss, Chongqing, China (GRID:grid.190737.b) (ISNI:0000 0001 0154 0904)
4 Zhejiang University of Technology, Key Laboratory of Special Purpose Equipment and Advanced Processing Technology, Ministry of Education & Zhejiang Province, Hangzhou, China (GRID:grid.469325.f) (ISNI:0000 0004 1761 325X)
5 Shanghai University of Engineering Science, School of Mechanical and Automotive Engineering, Shanghai, China (GRID:grid.412542.4) (ISNI:0000 0004 1772 8196)
6 Changsha University of Science and Technology, College of Automotive and Mechanical Engineering, Changsha, China (GRID:grid.440669.9) (ISNI:0000 0001 0703 2206)
7 University of Nottingham Ningbo China, School of Aerospace, Ningbo, China (GRID:grid.50971.3a) (ISNI:0000 0000 8947 0594)
8 Shandong University, Key Lab High Efficiency and Clean Mech Manufacture, Jinan, China (GRID:grid.27255.37) (ISNI:0000 0004 1761 1174)
9 University of Sharjah, College of Engineering, Sharjah, United Arab Emirates (GRID:grid.412789.1) (ISNI:0000 0004 4686 5317)
10 Curtin University, Mechanical Engineering Department, Miri, Malaysia (GRID:grid.412789.1)
11 King Fahd University of Petroleum and Minerals, Mechanical Engineering Department, Dhahran, Saudi Arabia (GRID:grid.412135.0) (ISNI:0000 0001 1091 0356)