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Joining of hybrid AA6063-6SiCp-3Grp composite and AISI1030 steel by friction welding

Joining of hybrid AA6063-6SiC_p-3Gr_p composite and AISI 1030 steel by friction welding
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摘要 Joining of metals and aluminium hybrid metal matrix composites has significant applications in aviation,ship building and automotive industries. In the present work, investigation is carried out on Friction Welding of AISI 1030 steel and hybrid AA6063-6 SiC_p-3 Gr_pcomposite, that are difficult to weld by fusion welding technique. Silicon carbide and graphite particle reinforced AA6063 matrix hybrid composite was developed successfully using stir casting method and the joining feasibility of AISI1030 steel with AA6063-6 SiC_p-3 Gr_p hybrid composite was tried out by friction stud welding technique. During friction stage of welding process, the particulates(SiC & Graphite) used for reinforcement, tend to increase the viscosity and lead to improper mixing of matrix and reinforcement. This eventually results in lower strength in dissimilar joints. To overcome this difficulty AA1100 interlayer is used while joining hybrid composite to AISI 1030 steel. Experimentation was carried out using Taguchi based design of experiments(DOE) technique. Multiple regression methods were applied to understand the relationship between process parameters of the friction stud welding process. Micro structural examination reveals three separate zones namely fully plasticized zone, partially deformed zone and unaffected base material zone. Ultra fine dynamically recrystallized grains of about 341 nm were observed at the fully plasticized zone. EDX analysis confirms the presence of intermetallic compound Fe_2 Al_5 at the joint interface. According to the experimental analysis using DOE, rotational speed and interlayer sheet thickness contribute about 39% and 36% respectively in determining the impact strength of the welded joints. It is found that joining with 0.5 mm interlayer sheet provides efficient joints. Developed regression model could be used to predict the axial shortening distance and impact strength of the welded joint with reasonable accuracy. Joining of metals and aluminium hybrid metal matrix composites has significant applications in aviation,ship building and automotive industries. In the present work, investigation is carried out on Friction Welding of AISI 1030 steel and hybrid AA6063-6 SiC_p-3 Gr_pcomposite, that are difficult to weld by fusion welding technique. Silicon carbide and graphite particle reinforced AA6063 matrix hybrid composite was developed successfully using stir casting method and the joining feasibility of AISI1030 steel with AA6063-6 SiC_p-3 Gr_p hybrid composite was tried out by friction stud welding technique. During friction stage of welding process, the particulates(SiC & Graphite) used for reinforcement, tend to increase the viscosity and lead to improper mixing of matrix and reinforcement. This eventually results in lower strength in dissimilar joints. To overcome this difficulty AA1100 interlayer is used while joining hybrid composite to AISI 1030 steel. Experimentation was carried out using Taguchi based design of experiments(DOE) technique. Multiple regression methods were applied to understand the relationship between process parameters of the friction stud welding process. Micro structural examination reveals three separate zones namely fully plasticized zone, partially deformed zone and unaffected base material zone. Ultra fine dynamically recrystallized grains of about 341 nm were observed at the fully plasticized zone. EDX analysis confirms the presence of intermetallic compound Fe_2 Al_5 at the joint interface. According to the experimental analysis using DOE, rotational speed and interlayer sheet thickness contribute about 39% and 36% respectively in determining the impact strength of the welded joints. It is found that joining with 0.5 mm interlayer sheet provides efficient joints. Developed regression model could be used to predict the axial shortening distance and impact strength of the welded joint with reasonable accuracy.
出处 《Defence Technology(防务技术)》 SCIE EI CAS CSCD 2017年第5期338-345,共8页 Defence Technology
基金 financial support of this work by SERB of Department of Science&Technology,New Delhi.(Vide Letter No.:SERB/F/1452/2013-2014 dated 10.06.2013)
关键词 Metal MATRIX COMPOSITE WELDING Mechanical properties SCANNING ELECTRON MICROSCOPY Metal matrix composite Welding Mechanical properties Scanning Electron Microscopy
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