Abstract
Deformation mechanism of low-rigidity thin part caused by clamping force is studied in this paper. A coupled thermo-mechanical simulation process of aluminum alloy 6061 is developed using the finite element method with Abaqus. The results of simulation are verified by experimental measurements of cutting force and surface residual stress. Then using the model investigates the effect on residual stresses along the thickness of aluminum alloy 6061 load and unloadthe clamping forces. The deformation condition is also studied after removing fixing.
Publisher
Trans Tech Publications, Ltd.
Reference7 articles.
1. Guo H, Zuo D, Yu W, et al. Simulation of Effect of Clamping On Residual Stress of Aero-Components by Means of Fem[C]. Suzhou, China: Aviation Industry Press, 2004: 730-734.
2. Kaya N. Machining Fixture Locating and Clamping Position Optimization Using Genetic Algorithms[J]. Computers in Industry. 2006, 57(2): 112-120.
3. Zhaoliang Jiang and X.X. Meng. Advanced Materials Research Vols. 102-104 (2010), pp.12-16.
4. Z.L. Jiang, Y. M Liu and W. Yi. Advanced Materials Research Vol. 426 (2012) , pp.265-269.
5. Mohammadpour M, Razfar M R, Jalili Saffar R. Numerical Investigating the Effect of Machining Parameters On Residual Stresses in Orthogonal Cutting[J]. Simulation Modelling Practice and Theory. 2010, 18(3): 378-389.
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