International Journal of Engineering Trends and Technology (IJETT) – Volume 17 Number 5 – Nov 2014 An Investigation of Mechanical Properties of Aluminium 6063-T6 after Friction Welding Process Al Faizal .B#1, Amarnath T S*2 ,Roshan T Ninan#3 # PG Scholar, Assistant Professors, Mechanical Department Musaliar College Of Engineering and Technology, Pathanamthitta, Kerala, India Abstract— A study of the friction welding process is carried out for Al 6063-T6. 3D model of the rotary friction welding is made. Thermo transient analysis and static structural analysis is carried out and steps were made to modify a conventional lathe to rotary friction welding set up to obtain friction welding with four different (250, 500, 775, and 1200) rpm and to find out its mechanical properties The simulation process are carried out with ANSYS workbench. Keywords— Rotary friction welding, ANSYS workbench comma. I. INTRODUCTION Rotary friction welding, in which one component is rotated against the other, is the most commonly used among the processes, and many carbon steel vehicle axles and subaxles are assembled in this way. The process is also used to fabricate suspension rods, steering columns, gear box forks and drive shafts, as well as engine valves, in which the ability to join dissimilar materials means that the valve stem and head can be made of materials suited to their different duty cycles in service. Traditionally, friction welding is carried out by moving one component relative to the other along a common interface, while applying a compressive force across the joint. The friction heating generated at the interface softens both components, and when they become plasticised the interface material is extruded out of the edges of the joint so that clean material from each component is left along the original interface. The relative motion is then stopped, and a higher final compressive force may be applied before the joint is allowed to cool. The key to friction welding is that no molten material is generated, the weld being formed in the solid state. The principle of this process is the changing of mechanical energy into heat energy. One component is gripped and rotated about its axis while the other component to be welded to it is gripped and does not rotate but can be moved axially to make contact with the rotating component. At a point fusion temperature is reached, then rotation is stopped and forging pressure is applied. Then heat is generated due to friction and is concentrated and localized at the interface, grain structure is refined by hot work. Then welding is done, but there will not occur the melting of parent metal. Briefly the friction-welding process consists in bringing into contact two elements to be welded while one of the two is static and the other is rotated rapidly on its axis. As the soon as the heat generated by attrition at the interface is sufficient for solid state welding without melting, the rotation is stopped and the elements are forced together under pressure producing ISSN: 2231-5381 local forging which concludes the intimate joining and also expels at the joint all surface contamination and some of the upset material called flash. II. OBJECTIVE A detailed study of the friction welding process is to be carried out, 3D model of the rotary friction welding is to be made. Thermo transient analysis and static structural analysis is to be carried out and FW joints are to be produced from specimen with different rpm (250, 500, 775, and 1200) and their tensile and hardness characteristics are assessed. Numerical simulation of welding process is to be modelled using solid works and is converted to ANSYS to gain the temperature field and finding strong friction welded joints for different rpm are to be obtained within the given parameters. The same parameters are to be used to make an experimental welded joint. The tensile strength is analysed using UTM and hardness is measured using hardness testing machine. III. LITERATURE REVIEW Ranjitsinh D. Jadeja et al [1] 2012. Develop a finite element simulation of friction stir welding of AA6063-T6 Aluminium alloy. Dr.K.P.Narayanan et al [2] 2013. Study on aluminium alloys. Strong friction welded joints for different surface interfaces were obtained and mechanical characteristic studies of the same were carried out. Biswajit Parida et al [3] 2012. Study of Mechanical properties and study of microstructural properties of Al-Alloy. Wichai Pumchan [4] 2011. The experimental application of a friction stir welding of the butt joints between aluminium AA6063 and AA7075 by changing the parameter. Ali. Moarrefzadeh [5] 2011. Numerical simulation of welding process in SIMPELC method and by ANSYS software for gaining the temperature field of carbon steel, the effect of parameter variation on temperature field and process optimization for different cases of electrode done. Pasquale Cavaliere [6] 2013. The fatigue life and crack behaviour of several aluminium alloys FSW joints have been presented. V. Balasubramanian et al [7] 2012. The FSW process parameters such as, the tool rotational speed, the welding speed and the axial force play a major role in deciding the weld quality. Vivekanandan. P et al [8] 2012. The influence of friction stir welding on the microstructure and hardness of aluminium 6035 and 8011. P.John Maclins [9] studied the effect of corrosion and low impact damage on aluminium alloy 6063- T6. http://www.ijettjournal.org Page 203 International Journal of Engineering Trends and Technology (IJETT) – Volume 17 Number 5 – Nov 2014 IV. MODELLING A. Model Creation As the rotary welding process can be modelled with solidworks 2014, an Axisymmetric 3D model of Al 6063-t6 rods of dimensions 20 mm radius and 120 mm length was made with symmetry about the Y axis. The model was meshed with 3830 nodes and elements 1956 and two displacement degrees of freedom in the X and Y directions respectively. The thermal effect of friction welding process depends on the friction type and melting point of the work piece. Numerical simulation of welding process by ANSYS software for gaining the temperature field of Al 6063 alloy and find out the weld strength and quality of the weld with different rpm of rotating specimen. At contact surface of two parts make an axial movement by giving free movement along y- axis and also arresting movement along x and y axis. A pressure of 10MPa is applied at the constrained end of the stationary specimen (i.e. at position “E” marked on fig 2). C. Transient Thermal Analysis A temperature load of 600°C (position “A” marked on fig 3.7) was given at the contact nodes since heat generation takes place during welding process which is equal to 600°C and the ends of two rods are given a temperature of 22°C (position “B” marked on fig 3.7) assuming to be the atmospheric temperature. Fig. 3 Boundary condition for thermal analysis for 1200,775,500, 250 rpm Fig. 1 Meshing of model, model is designed using solidworks and import it to the ansys workbench. Tetrahedral element was used for meshing. B. Static Structural for 1200, 775, 500 and 250 RPM V. EXPERIMENTAL STUDY Experimental studies included production of friction welded joints from Aluminium Alloy rods with 20mm diameters and 120mm lengths and with different rpm. (250, 500, 775 and 1200 rpm). After that the same were subjected to tensile test and hardness test characteristic studies. A. Friction Welding Setup Used The basic frame work of the friction welding setup is a medium duty lathe. The tail stock of the same was replaced with chuck with adequate hydraulic system as per the requirement of the friction welding process The RFW set up is suitable to hold work pieces whose diameter ranges from 0.75mm to 25 mm. Hydraulic system can provide a pressure up to 25 MPa B. Tension Test Fig. 2 Boundary condition for static structural analysis for 1200, 775,500 and 250 rpm. A 1200,775,500 and 250 rpm is being applied to the part connected with the head stock (i.e. at position “A” marked on fig 2). The model is constrained by arresting rotation of stationary specimen and axial movement of rotating specimen. This is done by arresting X direction motion at the end nodes of stationary specimen and Y direction motion at the end node ISSN: 2231-5381 Fig 4 ASTM Standard tensile specimen (All dimensions are in mm) All the welded joints were then subjected to tensile characteristic studies. Fig 4. Represents the tensile specimen prepared from these combinations as per ASTM standards (B557M) [9]. The value obtained for Maximum load, breaking http://www.ijettjournal.org Page 204 International Journal of Engineering Trends and Technology (IJETT) – Volume 17 Number 5 – Nov 2014 load and percentage elongations were then tabulated and hardness is measured using Brinell hardness testing machine VI. RESULTS AND DISCUSSION A. Equivalent Stress The Von Mises stress values at the initial stage seemed to be maximum on areas away from the constrained end regions with a value of 8.6654 MPa. Towards the end of the process the Von Mises stress was found to be maximum on end of rotating work piece with a value of 13.8 MPa. At the initial stage as well as in the final stage the minimum value of Von Mises stress was obtained at the heat affected zone of specimen with a value of 5.22 MPa for weld at 775,500,250 rpm and 9.66 MPa for 1200 rpm At the welding interface (the contact region) the value of von-Mises stress is less than the stress obtained at other regions. material flowing. Figure 6 shows the strain rate distributions for friction welding of Al6063-T6 alloy with different 1200,775, 500 and 250 rpm. Fig. 7 Directional deformation at welded joint C. Directional Deformation Directional deformation along y-axis is shown in fig 7 the job is symmetric along y-axis. From the obtained result shows maximum deformation is occurred at weld joint 250 rpm with 8.7mm this is due to the increases in contact pressure and time consuming for reaching its weld temperature at contact surface. TABLE I PERCENTAGE SHRINKAGE AFTER WELDING PROCESS BY USING SOFTWARE Fig. 5 Equivalent stress at welded joint B. Elastic Strain Test series Original Change in % description length (mm) length (mm) shrinkage 240 2.19 0.9125 240 3.83 1.59 240 7.66 3.19 240 8.75 3.65 Welded with 1200 rpm Welded with 775 rpm Welded with 500 rpm Welded with 250 rpm Fig. 6 Elastic strain at welded joints The strain rate is an important physical parameter during welding process. Therefore, the analysis was carried out to consider the strain rate distributions in the friction welding process. The most deformation that occurred in the interface was as a result of high transient temperature and subsequent ISSN: 2231-5381 D. Contact Pressure Distribution Flash formation is mainly depend on contact pressure at weld zone from fig 8 shows contact pressure distribution at weld zone. With Increases in rotational velocity of job results decrease in contact pressure. If more contact pressure results more flush will be form that will reduce the length of job. Fig 7 shows change in length of job with different rpm. From the ansys result it is clear that more flush will form at job with 250 rpm because of http://www.ijettjournal.org Page 205 International Journal of Engineering Trends and Technology (IJETT) – Volume 17 Number 5 – Nov 2014 increases in contact pressure value of 28.42MPa as compared with other job with rpm of 1200,775 and 500. process. From the experimentally it is clear that the rpm of job is affect the weld quality and time for completing the job. Friction increases with speed because friction resistance depends on interface shear stress. If interface shear stress increases with speed, friction will increase with speed. Due to this heat developed at mating surface suddenly increases and joined TABLE III PERCENTAGE SHRINKAGE AFTER WELDING PROCESS BY EXPERIMENT Test series Original Change in % description length(mm length(mm) shrinkage ) 240 3.5 1.46 240 4 1.67 240 7 2.92 240 10 4.17 Welded with 1200 rpm Welded with 775 rpm Welded with Fig. 8 Contact pressure distribution at weld zone for 250 rpm welded joint 500 rpm E. Total Heat Flux Welded with The maximum total heat flux of the specimen is found to 7.829 W/〖mm〗^2 at one second is shown in figure 9 250 rpm When increases in rotational velocity of job, result reduce the deformation because of decreases in contact pressure and time consuming for reaching its weld temperature at contact surface. Table III shows percentage shrinkage after welding process by experiment. BHN VS LEN GTH 79 78 80 75 bhn 73 73 73 73 70 Fig. 9 Total heat flux for welded joints. F. Experimental Results TABLE II TIME TAKEN FOR COMPLETING DIFFERENT WELDING Speed of rotating Time taken for completing the chuck in rpm welding operation in minutes 250 7.4 500 6.2 775 5.1 1200 2.58 It was found that increases the speed of rotating component results reduce the time for finishing the welding ISSN: 2231-5381 60 67 66 65 67 66 65 63 63 -30 -20 -10 0 10 20 30 1200 rpm 73 73 67 79 67 73 73 775 rpm 73 73 66 79 66 73 73 500 rpm 73 73 65 78 65 73 73 250 rpm 73 73 63 75 63 distance from weld zone in mm 73 73 Fig 10 BHN distribution along welded specimen with 1200, 775,500 and 250 rpm. Hardness distribution along the weld was investigated by finding out Brinell hardness number (BHN) on both sides at equal distances from the welded joint formed at 1200,775, 500, and 250 rpm. The increase in hardness at the plasticized zone is attributed to the finer grain size of plasticized zone and strain hardening effect due to upsetting. Thermal softening led to reduction of hardness near the weld zone. Hence the weld zone becomes almost softened. Then hardness increases and http://www.ijettjournal.org Page 206 International Journal of Engineering Trends and Technology (IJETT) – Volume 17 Number 5 – Nov 2014 again decreases to reach a constant value. Hardness distribution along the weld specimen is obtained as shown in figures 10. TABLE IV TENSILE TEST RESULT FOR ALUMINIUM ALLOY 6063 WELDED JOINT Test Test series Maximum Breaking % series description load (KN) load elongation 26.5 24.8 14 26.2 24.5 13.4 25.8 23.8 12 25.6 23.1 11.88 6.8 6 2.66 1 Parent material [3]. [4]. [5]. [6]. 2 3 4 5 Welded material with 1200 rpm Welded material with 775 rpm Welded material with 500 rpm Welded material with 250 rpm VII. CONCLUSIONS The results of the tensile test shows that the weld zone is stronger than the base metals since the rupture occurred outside of the welding area. The quality of rotary friction welding is depend on rotating velocity of members. In this study it is clear that at high rpm material binds together due to high material penetration and hence length of the workpiece is reduced after welding. The weld zone was divided into three regions based on the microstructure (center of weld and two HAZ). The center of weld had fine grains due to dynamic recrystallization with higher tensile strength and hardness. The maximum hardness of 79 BHN is achieved at a weld speed of 1200 rpm that resulted in a high tensile strength compare with other welded joints (775,500 and 250 rpm). The study reveals that for Al 6063-T6 after friction welding at 1200, 775 and 500 rpm the mechanical properties are remains almost same as that of parent material. But at 250 rpm the mechanical properties are reduced. This shows that the speed of rotating member affect the quality of weld. Ranjitsinh D. Jadeja, Tausif M. Shaikh, A Review On Experimental And Numerical Investigation Of Friction Stir Welds Of Aluminium Alloy, , International Journal of Advanced Engineering Research and Studies, E-ISSN 2249–8974 Baiju Sasidharan, Dr.K.P.Narayanan, R.Arivazhakan, Influence of Interface Surface Geometries In The Tensile Characteristics Of Friction Welded Joints From Aluminium Alloys, Proceedings of ISSN: 2231-5381 [10]. [11]. [12]. [13]. [14]. [15]. [16]. [17]. [18]. [19]. [20]. [21]. REFERENCES [2]. [8]. [9]. From Table IV it is clear that the welded joint formed at 1200 rpm can take more load than that formed at 775 rpm, 500 rpm and 250 rpm. The breaking strength, ultimate strength and percentage elongation of welded joint formed at 1200rpm were found to be higher than that formed at other welded joints. The welded joints formed had almost the same strength as that of the parent material 6063-T6 Aluminium alloy. [1]. [7]. [22]. 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