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Bupesh Raja, V. K.
- Formability of Heat Treated AA19000, AA5052 and Simulation Using ABAQUS/CAE
Abstract Views :258 |
PDF Views:174
Authors
Affiliations
1 Dept. of Mech. Engg., Sathyabama University, Chennai, Tamil Nadu, IN
2 Dept. of Automobile Engg., Sathyabama University, Chennai, Tamil Nadu, IN
3 Dept. of Mech. Engg., Vel Tech University, Chennai, Tamil Nadu, IN
1 Dept. of Mech. Engg., Sathyabama University, Chennai, Tamil Nadu, IN
2 Dept. of Automobile Engg., Sathyabama University, Chennai, Tamil Nadu, IN
3 Dept. of Mech. Engg., Vel Tech University, Chennai, Tamil Nadu, IN
Source
International Journal of Vehicle Structures and Systems, Vol 9, No 4 (2017), Pagination: 233-237Abstract
In this paper the formability of heat treated AA19000 and AA5052 aluminium alloys was studied through experimentation and finite element simulation. The aluminium alloys of 1mm thickness as received and annealed condition were subjected to tensile test and Erichsen cupping test. The experimental results showed that AA5052 possessed better formability than AA19000, due to its magnesium content. The material properties obtained from the tests were validated through simulation using ABAQUS/CAE.Keywords
Tensile Test, Annealing, Formability, Erichsen Cupping Test, ABAQUS/CAE.Full Text
References
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- K. Logesh and V.K.B. Raja. 2014. Investigation of mechanical properties of AA8011/PP/AA1100 sandwich materials, Int. J. Chem. Tech. Research, 6(3), 1749-1752.
- W. Xin-yun, H.E. Hu and X. Ju-chen. 2009. Effect of deformation condition on plastic anisotropy of as-rolled 7050 aluminum alloy plate, Mater. Sci. and Engg.: A, 515(1), 1-9. https://doi.org/10.1016/j.msea.2009.03.061.
- R. Esmaeilizadeh, K. Khalili1, B.Mh. Sadeghi and H. Arabi. 2014. Simulated and experimental investigation of stretch sheet forming of commercial aluminum alloy AA1200, Trans. Non Ferrous Metals Society of China, 24. https://doi.org/10.1016/s1003-6326(14)63086-7.
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- K. Logesh, V.K.B. Raja. 2015. Formability analysis for enhancing forming parameters in AA8011/PP/AA1100 sandwich materials, Int. J. Adv. Manuf. Tech., 81(1-4).
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- Mechanical Characterization of Dissimilar Alloys Joined Using Electron Beam Welding:Technical Note
Abstract Views :319 |
PDF Views:134
Authors
Affiliations
1 Dept. of Automobile Engg., Sathyabama University, Chennai, Tamil Nadu, IN
2 Dept. of Mech. Engg., Karpagam College of Engg., Coimbatore, Tamil Nadu, IN
3 Dept. of Mech. Engg., Veltech Dr. RR and Dr. SR University, Chennai, Tamil Nadu, IN
1 Dept. of Automobile Engg., Sathyabama University, Chennai, Tamil Nadu, IN
2 Dept. of Mech. Engg., Karpagam College of Engg., Coimbatore, Tamil Nadu, IN
3 Dept. of Mech. Engg., Veltech Dr. RR and Dr. SR University, Chennai, Tamil Nadu, IN
Source
International Journal of Vehicle Structures and Systems, Vol 10, No 2 (2018), Pagination: 89-92Abstract
Electron Beam Welding (EBW) is used in various industrial applications for joining dissimilar metals due to its accuracy and good quality joints. International Thermonuclear Experimental Reactor (ITER) is the first experimental fusion power generating reactor in India. It uses a host of metals and alloys like Ti-6Al-4V, Ni-Al bronze and a special copper alloy (CRZ). This investigation aims to study the metallurgical and mechanical aspects of CRZ alloy and its EBW joint with a dissimilar metal like Nickel and stainless steel. Characterization includes material composition and effect of heat-treatment. The CRZ alloys were solution annealed at the temperature of 980°C for 15 minutes and then aged at 460-480°C for 4.5 hrs. The EBW welded joints were fabricated with CRZ-CRZ, CRZ-Ni and Ni-SS combination. The microstructure and mechanical properties were analyzed.Keywords
Mechanical Properties, Electron Beam Welding, Microstructure, Annealing, Copper Alloy.Full Text
References
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- M. Lipa, A. Durocher, R. Tivey, Th. Huber, B. Schedler and J. Weigert. 2005. The use of copper alloy Cu-Cr-Zr as a structural material for actively cooled plasma facing and in vessel components, Fusion Engg. and Design, l75-79, 469-473.
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- O. Gillia, L. Briottet, I. Chu, P. Lemoine, E. Rigal and A. Peacock. 2009. Characterization of Cu-Cr-Zr and Cu-Cr-Zr/SS joint strength for different blanket components manufacturing conditions, J. Nuclear Materials, 386-388, 830-833. https://doi.org/10.1016/j.jnucmat.2008.12.244.
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- Stretch Formability Behaviour of Glass Fibre Reinforced Nanoclay on Fiber Metal Laminated Composites
Abstract Views :261 |
PDF Views:110
Authors
Affiliations
1 Dept. of Mech. Engg., Sathyabama University, Chennai, IN
2 Dept. of Automobile Engg., Sathyabama University, Chennai, IN
3 Dept. of Mech. Engg., Karpagam College of Engg., Coimbatore, IN
1 Dept. of Mech. Engg., Sathyabama University, Chennai, IN
2 Dept. of Automobile Engg., Sathyabama University, Chennai, IN
3 Dept. of Mech. Engg., Karpagam College of Engg., Coimbatore, IN
Source
International Journal of Vehicle Structures and Systems, Vol 10, No 2 (2018), Pagination: 115-121Abstract
Innovations and research in material processing have brought forward new and improvised materials that are applied in body panels of automobiles, aircraft cabins and railway wagons. These materials are used widely is because of their good mechanical properties and their high strength to weight ratio. In this paper Fibre Metal Laminates (FMLs) were added with organo modified montmorillonite (MMT) commonly known as nanoclay along with epoxy resin. The homogeneous dispersion of nanoclay in epoxy resin is accomplished by a hand stirrer dispersion method in ethanol. The FML material was processed by hand layup method. In this study the aluminium alloy 5052-H32 was used as a skin material and glass fibre (woven roving) used as core material which is bounded by epoxy with 5 wt.% nano clay (closet 30B). The fabricated sandwich material was cut by using water jet machine as per IS standards for testing. The fabricated material subjected to erichsen cupping test and was observed under Scanning Electron Microscope (SEM). The results from SEM image analysis indicated that the FML had fibre pull out and surface cracks were obtained in the skin material. Progressive loading resulted in ductile fracture which is absorbed in the specimen. Fibres came across brittle failure and the skin through ductile fracture. Non-uniform distribution of reinforcement is observed in the material, SEM micrographs revealed fibre cracks which were oriented in line to the direction of crack growth on the skin material. This study shows that these fibre metal laminates can be safely applied in automotive field.Keywords
Fibre Metal Laminates, Montmorillonite, Erichsen Cupping Test, Scanning Electron Microscope.Full Text
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