Prediction of Load-Displacement Curve for Weld-Bonded Stainless Steel Using Finite Element Method Essam Al-Bahkali Jonny Herwan Department of Mechanical Engineering King Saud University, P.O.Box 800, Riyadh 11421, Saudi Arabia Multiphysics Dec 09-11, 2009 Lille, France Background • It is one of the oldest cost effective, less labor and readily automated electric welding techniques that is used to join similar and dissimilar metals. • Introducing an adhesive layer in conjunction with a spot weld nugget helps strengthening welded joints and balancing stresses in the weld nugget area. • Optimum welding quality of a spot welded or a weldbonded joints, Required optimum welding parameters, i.e. welding current, electrode force, and welding time. MULTIPHYSICS 2009 2 • The advantages of resistance welding process include – short process times – heat focused at the material interfaces. – easily be automated • While experimental work provides the necessary physical insight about the behavior of spot-welded joints, predictive tasks such as design; analysis and evaluation of spot-welded structures are often carried out by computational methods • In predicting stress distribution, stress concentration and failure modes of a weld-bonded or a spot welded nugget, a finite element modeling can do an excellent job in this 3 MULTIPHYSICS 2009 regard. • Engineers use the process of adhesive bonding to join materials • Adhesive bonding can be used to adhere a wide range of materials such as metal to metal, metal to ceramic, metal to polymer, … etc. • Some advantages of adhesive bonding – – – – Reducing weight Uniform stress distribution Fatigue resistance Ability to join thick with thin materials as well as the ability to join dissimilar materials. – No stress concentration MULTIPHYSICS 2009 4 • There are two types of Bonded structure – Purely Adhesive – Adhesive/Mechanical Connection. • Bonded-Welded • Bonded-Riveted • Bonded Screwed connections • The combined connections ensure high fatigue strength of the structures. • Single lap welded joint is one of the important method used to join two plates together. MULTIPHYSICS 2009 5 Objective • In present work – Manufacturing point of view • To develop a finite element model of weld-bonded that can represent a complete load-displacement curve • Minimize the experimental or trial in industrial application – Design point of view • To obtain the representative weld-bonded model which has reasonable deformation shape and fracture initiation. • To design the position and the effective number of these joints in the mechanical structures MULTIPHYSICS 2009 6 The scope of research Process Parameters : • welding current • welding time • electrode force • etc Size, Properties of Nugget, and HAZ Already done by some researchers: - A. De, et al [2003] - E. Feulvarch, et al [2004] - J. Z. Chen, et al [2006] - There was Sorpass Software that can analyze the temperature distribution, size of nugget and Heat Affected zone (HAZ) MULTIPHYSICS 2009 Deformation and Fracture of the Joints Our research ! 7 Experimental Analysis Material Verifications - Base Metal Tensile Test - Ductile Fracture Limit of AISI 304 steel - Mechanical Properties of Adhesive Adhesive Bonding Spot Weld Micro-hardness & Spherical Indentation Lap Shear Tensile Test Weld-Bonding Finite Element Analysis Modeling of Material Tensile Test Modeling of Lap Shear Tensile Test of Spot Welding Modeling of Lap Shear Tensile Test of Adhesive Bonding Modeling of Lap Shear Tensile Test of Weld-Bonding MULTIPHYSICS 2009 9 FE Modeling and Boundary Conditions 100 mm 30 mm x z 25 mm F Bonded Model (T.V) Strip - A Adhesive F Strip - B y 100 mm x Bonded Model (F.V) Nugget F 5 mm y x Weld-Bonded Model (F.V) MULTIPHYSICS 2009 10 Assumptions • 3-D FE model • Half of the model was considered to save computation time • Isotropic adhesive layer • The elastic-plastic FE model was considered in current analysis for verifying the model with the experimental test • There is no adhesive layer in a zone 1 mm around the circumference of the welds • The damage evolutions were chosen arbitrary in term of displacement because the failure propagation is not considered MULTIPHYSICS 2009 11 Finite Element Meshes • The FE mesh was modeled using eightnode linear brick reduced integration elements for strips and nugget Transverse direction Longitudinal direction Bonded Model Strip - A The FE mesh for adhesive layer was modeled using eight-node 3-D cohesive element Strip - B Adhesive Part MULTIPHYSICS 2009 Partial of the Bonded Model 12 • Fine mesh was used in strips around the nugget, nugget, and adhesive layers Partial of the Weld-Bonded Model Nugget Part Partial of the Adhesive Model MULTIPHYSICS 2009 13 Stress Triaxiality • In Abaqus, the ductile fracture limits are in term of stress triaxiality • The stress triaxiality equation can be written as: • Where • Stress triaxiality can be obtained through equivalent fracture strain. • This can be done by conducting standard tensile test to record the true strains at the fracture limit. • The value of the stress triaxiality were calculated numerically using finite element modeling of the notch tensile test MULTIPHYSICS 2009 14 Hardness Measurement and Indentation • Micro-hardness test was usedTest to define the location of the weld nugget and heat affected zone (HAZ) • The hardness measurement started from the center of the nugget and move a way from the center to the heat affected zone with a step of 0.25mm. • To obtain the plastic properties of each region, spherical indentation ( 2mm diameter) was carried out at several loads. • Spherical indentation data can be transferred to true stress-true strain curve using Ahn-Equation: • Where σ is the true stress, ε is the true strain, φ is the plastic constrain factor =3.6, P is the load, Pm is the mean pressure, α is the adjustment constant = 0.14, ac is the contact radius between the indenter and 15 MULTIPHYSICS 2009 Micro-hardness and Spherical Indentation Results 250 230 HV 210 190 170 Nugget HAZ HAZ 150 -8 -6 -4 -2 0 2 4 6 8 Position from center of nugget (mm) MULTIPHYSICS 2009 16 Tensile Test Comparison between Experimental and Finite Element Model 10 Experiment FE Model Load (kN) 8 6 4 2 0 0 10 20 30 40 50 Displacement (mm) MULTIPHYSICS 2009 17 Load- Displacement Curve of Spot Welding 10 Experiment-1 9 Experiment-2 8 Experiment-3 Experiment-4 Load (kN) 7 FE Model 6 5 4 3 2 1 0 0 0.5 1 1.5 2 2.5 3 3.5 4 4.5 5 Displacement (mm) MULTIPHYSICS 2009 18 Initial Failure Comparison between Experimental and Finite Element Model Failure Initiation from Experimental and Finite Element Model at HAZ MULTIPHYSICS 2009 19 Load- Displacement Curve of Adhesive Bonded 12 Experiment-1 Experiment-2 Experiment-3 Experiment-4 FE Model 10 Load (kN) 8 6 4 2 0 0 0.5 1 1.5 2 2.5 3 Displacement (mm) MULTIPHYSICS 2009 20 Load- Displacement Curve of WeldBonded 12 Experiment-1 Experiment-2 Experiment-3 Experiment-4 FE Model 10 Load (kN) 8 6 4 2 0 0 0.5 1 1.5 2 2.5 3 Displacement (mm) MULTIPHYSICS 2009 21 Conclusions • The ductile fracture limit criteria were developed to predict the deformation and fracture initiation of the model. • Detailed material properties of each zone of resistance spot welding (nugget, heat affected zone, and base metal) are essential to accurately simulate the model. • Reverse engineering analysis is introduced to get those material properties by modeling the indentation process using finite element software, and conduct some iteration of models until the load-displacement curve of indentation agree with the experimental curve. • The results in general for the load-displacements curve from finite element model shows a good agreement with 22 the experimental data.MULTIPHYSICS 2009
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