5
Modeling of Welding Heat Source for Laser Spot Welding Process Dr. Amit Trivedi Department of Production Engineering, B.V.M. Engineering College Vallabh Vidhyanagar-388120, Gujarat, India [email protected] Prof. Purvi Chauhan Department of Production Engineering, B.V.M. Engineering College Vallabh Vidhyanagar-388120, Gujarat, India [email protected] Prof. K. D. Bhatt Department of Production Engineering, B.V.M. Engineering College Vallabh Vidhyanagar-388120, Gujarat, India [email protected] Prof. Hardik S. Berawala Prof. N.J.Manek Department of Production Engineering, Department of Production Engineering, B.V.M. Engineering College B.V.M. Engineering College Vallabh Vidhyanagar-388120, Gujarat, India Vallabh Vidhyanagar-388120, Gujarat, India Abstract: The laser spot welding results in a controlled energy input, narrow heat affected zone and minimum thermal distortion. The representation of laser beam as the heat source is critical in numerical modeling as it governs the distribution of energy in and around the weld. The models to represent laser as point, line, surface or volume heat source has been reported. The volumetric heat source models can widely be used if the weld pool dimensions are known a priori. The present study aims at using an adaptive heat source model which progressively changes its nature from surface to volumetric heat source as the welding advances with time. The dimensions of the adaptive heat source dynamically changes as the weld pool starts growing and this eliminates the need for knowing the weld dimensions a priori. The present numerical model can thus be used for predicting thermal stresses with great reliability. Key Words: Laser Spot Welding, Heat Source Modeling, Finite Element Method and Transient Heat Transfer I. INTRODUCTION The heating source, which melts the metal in fusion welding processes, can be either arc, plasma, laser beam, electron beam or the combination of them. The transient temperature in and around the weld pool is greatly governed by the distribution of the energy from this heat source. It is thereby necessary to properly represent such a heat source. As the physics to represent arc, laser beam, electron beam or plasma beam is often complex, thermal modeling of welding heat sources has been developed. Rosenthal [1] and Rykalin [2] represented the welding arc as either a point, plane or line heat source depending on the dimensionality of the problem. However, assumption of point heat source resulted in a singularity of the temperature field. Furthermore, the thermal energy supplied by a welding arc or laser/plasma/electron beam is distributed over a finite area rather than at a single point. Pavelic et al. [6] thus considered welding arc as a distributed heat source with Gaussian distribution that could avoid singularities in the solution of transient temperature field. The heat flux distribution was represented in the form of a Gaussian form as ) cr exp( ) 0 ( q ) r ( q 2 (1) Where ) 0 ( q is the maximum heat flux; c is the concentration co-efficient, and r is termed as the radial distance of a point from the symmetric heat source axis. The heat distribution by laser beam is typical as its heat source has to account for the laser energy reaching inside the weld pool volume [7]. The numerical modeling needs sufficient trial–and–error exercises to obtain suitable parameters to represent the parameters to represent the heat source. Goldak et al. [7] initiated the concept of volumetric heat source in the context of moving arc welding that permitted the energy to reach inside the weld pool volume and defining a pseudo weld pool in the form of a double ellipsoid (Fig. 1). The double ellipsoid heat source was defined by parameters a, b, c1 for representing front of ellipsoid whereas the rear ellipsoid was defined by parameter a, b and c2. The power density distribution in the front and rear quadrant of weld pool was given as [7]. 13-14 May 2011 B.V.M. Engineering College, V.V.Nagar,Gujarat,India National Conference on Recent Trends in Engineering & Technology

Modeling of Welding Heat Source for Laser Spot Welding Process · 2001. 1. 2. · beam is often complex, thermal modeling of welding heat sources has been developed. Rosenthal [1]

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  • Modeling of Welding Heat Source for Laser Spot Welding Process

    Dr. Amit TrivediDepartment of Production Engineering,

    B.V.M. Engineering CollegeVallabh Vidhyanagar-388120, Gujarat, India

    [email protected]

    Prof. Purvi ChauhanDepartment of Production Engineering,

    B.V.M. Engineering CollegeVallabh Vidhyanagar-388120, Gujarat, India

    [email protected]

    Prof. K. D. BhattDepartment of Production Engineering,

    B.V.M. Engineering CollegeVallabh Vidhyanagar-388120, Gujarat, India

    [email protected]

    Prof. Hardik S. Berawala Prof. N.J.Manek Department of Production Engineering, Department of Production Engineering, B.V.M. Engineering College B.V.M. Engineering College Vallabh Vidhyanagar-388120, Gujarat, India Vallabh Vidhyanagar-388120, Gujarat, India

    Abstract: The laser spot welding results in a controlled energy input, narrow heat affected zone and minimum thermal distortion. The representation of laser beam as the heat source is critical in numerical modeling as it governs the distribution of energy in and around the weld. The models to represent laser as point, line, surface or volume heat source has been reported. The volumetric heat source models can widely be used if the weld pool dimensions are known a priori. The present study aims at using an adaptive heat source model which progressively changes its nature from surface to volumetric heat source as the welding advances with time. The dimensions of the adaptive heat source dynamically changes as the weld pool starts growing and this eliminates the need for knowing the weld dimensions a priori. The present numerical model can thus be used for predicting thermal stresses with great reliability.

    Key Words: Laser Spot Welding, Heat Source Modeling, Finite Element Method and Transient Heat Transfer

    I. INTRODUCTION

    The heating source, which melts the metal in fusion welding processes, can be either arc, plasma, laser beam,electron beam or the combination of them. The transient temperature in and around the weld pool is greatly governed by the distribution of the energy from this heat source. It is thereby necessary to properly represent such a heat source. As the physics to represent arc, laser beam, electron beam or plasma beam is often complex, thermal modeling of welding heat sources has been developed.

    Rosenthal [1] and Rykalin [2] represented the welding arc as either a point, plane or line heat source depending on the dimensionality of the problem. However, assumption of point heat source resulted in a singularity of the temperature field.

    Furthermore, the thermal energy supplied by a welding arc or laser/plasma/electron beam is distributed over a finite area rather than at a single point. Pavelic et al. [6] thus considered welding arc as a distributed heat source with Gaussian distribution that could avoid singularities in the solution of transient temperature field. The heat flux distribution was represented in the form of a Gaussian form as

    )crexp()0(q)r(q 2 (1)

    Where )0(q is the maximum heat flux; c is the concentration co-efficient, and r is termed as the radial distance of a point from the symmetric heat source axis. The heat distribution by laser beam is typical as its heat source has to account for the laser energy reaching inside the weld pool volume [7]. The numerical modeling needs sufficient trial–and–error exercises to obtain suitable parameters to represent the parameters to represent the heat source.

    Goldak et al. [7] initiated the concept of volumetric heat source in the context of moving arc welding that permitted the energy to reach inside the weld pool volume and defining a pseudo weld pool in the form of a double ellipsoid (Fig. 1). The double ellipsoid heat source was defined by parameters a, b, c1for representing front of ellipsoid whereas the rear ellipsoid was defined by parameter a, b and c2. The power density distribution in the front and rear quadrant of weld pool was given as [7].

    13-14 May 2011 B.V.M. Engineering College, V.V.Nagar,Gujarat,India

    National Conference on Recent Trends in Engineering & Technology

  • )c

    z

    b

    y

    a

    x(3

    s

    2

    2

    2

    2

    2

    2e

    )1c(ab

    Q)1f(36)z,y,x(q

    (2)

    (For Frontal Ellipsoid)

    )c

    z

    b

    y

    a

    x(3

    s

    2

    2

    2

    2

    2

    2e

    )2c(ab

    Q)2f(36)z,y,x(q

    (3)

    (For Rear Ellipsoid)

    Figure -1 Representation of double-ellipsoidalheat source [8].

    The heat input is represented as sq whereas the fractions f1 and

    f2 take into consideration asymmetry in magnitude of heat input at the front and the rear of the volumetric heat source. As this heat source considers the existence of pseudo weld pool from the beginning of the process, only the equation of conservation of energy needs to be solved to model the transient temperature field. The only limitation of this approach is that it considers the existence of pseudo weld pool a prioriand hence the nature of fluid flow in a weld pool driven by various convective forces cannot be predicted. The power density distribution from the laser beam was observed to be conical. Ranatowski and Pocwiardowski [18] had suggested a cylindrical-involution-normal representation corresponding to a laser beam as

    ))sz(u1(e)sKexp(1QKK

    )y,x(q dK)yx(K

    dz

    zc Z22

    C

    (4)

    where Q is the heat input, zK involution factor of heat source,

    cK the factor designating the heat source concentration, ds the

    heat source penetration depth, and )sz(u d the Heaveside’s

    function. The authors hypothesized that by changing the values of ds , zK and cK , equation (4) could account for point, line,

    plane, paraboloid, conical, or Gaussian presentation of heat source. The value of the depth of heat source ds was taken as hat a point where the power at the said depth was 5% of the total input power. The values of ds , cK and zK are rarely available

    and that has restricted the use of this present model. The recourse is to either calibrate a heat source expression against experimental data sets or evolve a route to determine optimized value of such uncertain parameters for varying weld conditions.

    The numerical process models that had undertaken detailed convection heat transfer analysis in weld pool preferred to use surface heat flux input following a Gaussian distribution. The numerical models that considered conduction heat transfer analysis alone preferred to use a combination of Gaussian surface heat flux distribution in association with a volumetric heat source expression or only the later. In cases like laser spot welding where weld pool size is small or the process involves rapid melting and solidification offering very less time for convective flows to develop fully, heat conduction based model with a volumetric heat source representation can provide a fairly reliable estimation of weld pool dimensions. In the present work, the energy input due to the laser beam is considered as a surface heat flux with Gaussian energy distribution and subsequently, an adaptive volumetric heat source is introduced as the weld pool grows with elapse of time. The experimental results of weld dimensions shows close agreement with the model developed.

    II. HEAT TRANSFER SIMULATION

    The axial symmetry of the laser beam permits us to apply the two-dimensional axisymmetric heat conduction equation

    t

    TCQ

    z

    Tkr

    zr

    1

    r

    Tkr

    rr

    1p

    (5)

    where r and z refer to radial and axial directions; k, ρ, and

    pC respectively refer to thermal conductivity, density, and

    specific heat of material; T and t refer to temperature and time

    variable respectively, and Q depicts internal heat generation per unit time and unit volume. The associated boundary condition can be stated as

    0TTTThqn

    Tk 40

    40s

    (6)

    where k refers to thermal conductivity normal to surface; h and depict surface heat transfer co-efficient and emissivity respectively; is Stefan- Boltzmann constant, and T0 is the ambient temperature. A lumped heat transfer co-efficient is used combining the convective and radiative heat loss by considering h, as [2]

    61.13 T104.2h (7)

    13-14 May 2011 B.V.M. Engineering College, V.V.Nagar,Gujarat,India

    National Conference on Recent Trends in Engineering & Technology

  • III. ADAPTIVE HEAT SOURCE

    In the present work, the energy input due to the laser beam is considered as a surface heat flux with Gaussian energy distribution and subsequently, as an adaptive volumetric heat source. The surface heat flux is considered till the top surface under the laser beam has reached melting point temperature. Once a melt pool of finite dimensions is formed, an adaptively defined volumetric heat source is considered that corresponds to the size and the shape of the growing weld pool. The mathematical expression of surface heat flux distribution considering Gaussian energy distribution is given as

    2eff

    2lb

    2eff

    lbgaus

    r

    r.dexp

    r

    d)(Pq

    (8)

    Where P refers to the beam power, gau the absorption

    coefficient of the laser beam at the work-piece surface, effr the

    effective radius of the focussed laser beam, and lbd the beam

    distribution parameter of the laser beam profile. The mathematical expression of adaptive volumetric heat source is given as

    p

    wb

    2

    2

    2b

    2

    2b

    vol

    wp2

    wl

    where p

    z3

    l

    r3exp

    pl

    )(P36q

    (9)

    In equation (9), wp and ww represent the instantaneous values of weld penetration (or depth) and weld width respectively that are computed from the numerical model. The parameters, vol , q , lb, and p refer to absorption coefficient of laser beam within weld pool, volumetric heat input, and the extent of heat source in longitudinal and axial directions respectively. At time t = 0, the numerical calculations for heat transfer analysis considers the irradiated laser beam as a surface heat flux on the top surface. Once a weld pool of finite size is formed in a subsequent time-step, the volumetric heat source term is activated within the melt volume. The calculated values of weld width (ww) and weld penetration (wp) are assigned respectively to bl and p as indicated in equation (9). The values

    of ww and wp change as the weld pool grows in size in subsequent time-steps for the total laser on-time. Thus, equation (9) does not need a-priori knowledge of the final weld pool shape that is otherwise required in similar expressions used earlier [7-8, 18-19].

    The symmetry of a stationary laser beam, permits a symmetric boundary condition to be applied along z-axis as

    0r

    T

    (10)

    (6)As, the process is transient in nature, an additional boundary condition is defined at time t = 0 as

    0T0,z,rT (11) (7)

    The details of finite element discretization followed in this present study is as per the formulation details given by Amit et al. [21].

    IV. RESULTS & DISCUSSION

    Figures 2(a) – (d) show the comparison of computed and the corresponding measured weld dimensions for 1.0 mm low carbon steel at a laser power of 1.0 kW and at on times 6, 10, 14, and 20 ms. The isotherms are zoomed in a domain of 1.0 mm x 1.0 mm near the laser beam axis, being an area of interest as regards to prediction of fusion and heat affected zone. Figures 2(a) – (d) depict that the computed dimensions of weld depth and width and they agree well with the corresponding measured results at all the four on-times.

    The legends of the temperature isotherms plotted are given in Figures 2(a)-(d) and hence, the intercepts of the 1773 K isotherm (referred to A) in the radial and in the axial directions confirm to half of the weld width and weld depth respectively. The fair agreement between the calculated and the corresponding measured shapes and sizes of the weld pool for all the on-times also indicate the robustness of the model that has considered adaptive heat source. However, such a procedure can be considered to be more effective and practical when uncertain parameters like absorption coefficient for the given laser power and laser on-time is predicted. For example, Pantsar et al. [22] has showed that at a constant value of powerdensity, increase in laser on-time, causes increase in absorption coefficient in laser welding process. Although an increase in the value of the absorption coefficient is a reality at higher laser on-time, the present model has considered a time-averaged value of absorption coefficient and thermal conductivity. The zone encompassed between the temperature isotherms 1773 K (referred to A) and 993 K (referred to D) is presumed extent of heat affected zone. The slight discrepancies between the calculated and measured extent of heat affected zone dimensions possibly indicate a greater value of lower critical temperature than 993 K that is considered here. A greater value of lower critical temperature indicates the need of superheating for transformation from α-ferrite to γ-austenite. The non-equilibrium cooling conditions prevailing due to rapid rate of heating and cooling during laser spot welding process might have led to higher value of lower critical temperature.

    V. CONCLUSION

    The present study has attempted to bring out the prediction of weld dimension by the numerical heat transfer model that has considered adaptive heat source. The computed values of the weld dimensions from the two-dimensional axisymmetric heat transfer analysis are validated with the corresponding measured results from experimental studies. It is also shown that the geometric dimensions of the adaptive volumetric heat source, as adapted in this work, closely follow the shape and size of the instantaneous weld pool. It is thus conceived that the approach, presented in this work, will alleviate the restricted use of volumetric heat source in the context of modeling of laser welding, in particular, and fusion welding, in general.

    13-14 May 2011 B.V.M. Engineering College, V.V.Nagar,Gujarat,India

    National Conference on Recent Trends in Engineering & Technology

  • Figure -2 Comparison between calculated weld dimensions and the corresponding experimentally obtained weld macrographs.Laser power: 1.0 kW; Sheet thickness: 1.0 mm;On–times (a) 6 ms (b) 10 ms (c) 14 ms (d) 20 ms[Isotherm legends: A – 1773 K, B – 1473 K, C – 1203 K, D –993 K, E – 623 K]

    VI. REFERENCES

    [1]D. Rosenthal: Mathematical theory of heat distribution during welding and cutting, Welding Journal, 20(5), 1941, 220s-234s.

    [2] Rykalin R R , Energy Source for Welding, Welding in the World, Vol 12, No. 9/10, p 227-248, 1974.

    [3] A. Paul and T. Debroy: Free surface flow and heat transfer in conduction mode laser welding, Metallurgical Transactions B, 19, 1998, 851-857.

    [4] S. Basu and T. Debroy: Liquid metal expulsion during laser irradiation, Journal of Applied Physics, 72(8), 2003, 3317-3322.

    [5] T. Zacharia, S. A. David, J. M. Vitek and T. Debroy: Heat transfer during Nd: YAG pulsed laser welding and its effect on solidification structure of austenitic stainless steels, Metallurgical Transactions A, 20, 1989, 957-967.

    [6] V. Pavelic, R. Tanabakuchi, O. Uyehara and P. Myers: Experimental and computed temperature histories in gas tungsten arc welding of thin plates, Welding Journal, 48(7), 1969, 295s-305s.

    [7] J. A. Goldak, B. Chakravarti and M. J. Bibby: A new finite element model for welding heat sources, Metallurgical Transactions B, 15, 1984, 229-305.

    [8] V. Kamla and J. A Goldak: Error due to two dimensional approximations in heat transfer analysis of welds, Welding Journal, 72(9), 1993, 440s-446s.

    [9] D. Grey, H. Long and P. Maropoulos: Effects of welding speed, energy input and heat source distribution on temperature variations in butt welding, Journal of Materials Processing Technology, 167, 2005, 393-401.

    [10] R. Akhter, M. Davis, J. Dowden, P. Kapadia, M. Ley and W. M. Steen: A method for calculating the fused zone profile of laser keyhole welds, Journal of Physics D: Applied Physics, 21, 1989, 23-28.

    [11] N. Sonti and M. F. Amateau: Finite element modeling of heat flow in deep penetration laser welds in aluminum alloys, Journal of Numerical Heat Transfer A, 16, 1989, 351-370.

    [12] R. Mueller: A study on heat source equations for prediction of weld shape, Proc. ICALEO’94, Orlando, USA, October 1994, 509-518.[13] J. Song, J. Y. Shanghvi and P. Michaleris: Sensitivity analysis and optimization of thermo-elasto-plastic processes with application to welding side heater design, Computer methods in applied mechanics and engineering, 193, 2004, 4541-4566.

    13-14 May 2011 B.V.M. Engineering College, V.V.Nagar,Gujarat,India

    National Conference on Recent Trends in Engineering & Technology

  • [14] R. G. Theissen, I. M. Richardson and J. Sietsma: Physically based modeling of phase transformations during welding of low carbon steel, Materials Science and Engineering A, 427, 2006, 223-231.

    [15] D. Deng and H. Murakawa: Numerical simulation of temperature field and residual stress in multi-pass weld in stainless steel pipe and comparison with experimental measurements, Computational Materials Science, 37, 2006, 269-277.

    [16] M. A. Wahab and M. J. Painter: Numerical models of gas metal arc welds using experimentally determined weld pool shapes as the representation of the welding heat source, International Journal of Pressure Vessels and Piping, 73, 1997, 153-159.

    [17] W. S. Chang and S. J. Na: A study on the prediction of the laser weld shape with varying heat source equations and thermal distortion of a small structure in micro-joining, Journal of Materials Processing Technology, 120, 2002, 208-214.

    [18] E. Ranatowski and A. Pocwiardowski: An analytic-numerical evaluation of the thermal cycle in the HAZ during welding, Proc. of Fourth International Seminar on Numerical Analysis of Weldability at Graz- Seggau, Austria- 4-5 September, 1997, 379-395.

    [19] W. Sudnik, D. Radaj and E. Erofeew: Computerized simulation of laser beam weld formation comprising joint gaps, Journal of Physics D: Applied Physics, 31, 1998, 3475-3480.

    [20] M. R. Frewin and D. A. Scott: Finite element model of pulsed laser welding, Welding Research Supplement, 78(1), 1999, 15s-22s.

    [21] Integrating Finite Element based Heat Transfer Analysis with Multivariate Optimization for Efficient Weld Pool Modeling By Amit Trivedi, Anand Suman, and Amitava De, ISIJ International, Vol. 46 (2006), No. 2, 267-275.

    [22] H. Pantsar and V. Kujanappa: Diode laser beam absorption in laser transformation hardening of low alloy steel, Journal of Laser Applications, 16(3), 2004, 147-153.

    [23] S. Katayama, S. Kohsaka, M. Mizutani, K. Nishizawa and A. Matsunawa: Pulse shape optimization for defect prevention in pulsed laser welding of stainless steels, ICALEO, Orlando, USA, 24-28 October 1993, 487-497.

    13-14 May 2011 B.V.M. Engineering College, V.V.Nagar,Gujarat,India

    National Conference on Recent Trends in Engineering & Technology

    Modeling of Welding Heat Source for Laser Spot Welding Process

    Dr. Amit Trivedi

    Department of Production Engineering,

    B.V.M. Engineering College

    Vallabh Vidhyanagar-388120, Gujarat, India

    [email protected]

    Prof. Purvi Chauhan

    Department of Production Engineering,

    B.V.M. Engineering College

    Vallabh Vidhyanagar-388120, Gujarat, India

    [email protected]

    Prof. K. D. Bhatt

    Department of Production Engineering,

    B.V.M. Engineering College

    Vallabh Vidhyanagar-388120, Gujarat, India

    [email protected]

    Prof. Hardik S. Berawala Prof. N.J.Manek

    Department of Production Engineering, Department of Production Engineering,

    B.V.M. Engineering College B.V.M. Engineering College

    Vallabh Vidhyanagar-388120, Gujarat, India Vallabh Vidhyanagar-388120, Gujarat, India

    Abstract: The laser spot welding results in a controlled energy input, narrow heat affected zone and minimum thermal distortion. The representation of laser beam as the heat source is critical in numerical modeling as it governs the distribution of energy in and around the weld. The models to represent laser as point, line, surface or volume heat source has been reported. The volumetric heat source models can widely be used if the weld pool dimensions are known a priori. The present study aims at using an adaptive heat source model which progressively changes its nature from surface to volumetric heat source as the welding advances with time. The dimensions of the adaptive heat source dynamically changes as the weld pool starts growing and this s as the weld pool starts growingically nates the wherein such dimensions are not to be known a priori.

    eliminates the need for knowing the weld dimensions a priori. The present numerical model can thus be used for predicting thermal stresses with great reliability.

    Key Words: Laser Spot Welding, Heat Source Modeling, Finite Element Method and Transient Heat Transfer

    I. Introduction

    The heating source, which melts the metal in fusion welding processes, can be either arc, plasma, laser beam, electron beam or the combination of them. The transient temperature in and around the weld pool is greatly governed by the distribution of the energy from this heat source. It is thereby necessary to properly represent such a heat source. As the physics to represent arc, laser beam, electron beam or plasma beam is often complex, thermal modeling of welding heat sources has been developed.

    Rosenthal [1] and Rykalin [2] represented the welding arc as either a point, plane or line heat source depending on the dimensionality of the problem. However, assumption of point heat source resulted in a singularity of the temperature field. Furthermore, the thermal energy supplied by a welding arc or laser/plasma/electron beam is distributed over a finite area rather than at a single point. Pavelic et al. [6] thus considered welding arc as a distributed heat source with Gaussian distribution that could avoid singularities in the solution of transient temperature field. The heat flux distribution was represented in the form of a Gaussian form as

    )

    cr

    exp(

    )

    0

    (

    q

    )

    r

    (

    q

    2

    -

    =

    (1)

    Where

    )

    0

    (

    q

    is the maximum heat flux; c is the concentration co-efficient, and r is termed as the radial distance of a point from the symmetric heat source axis. The heat distribution by laser beam is typical as its heat source has to account for the laser energy reaching inside the weld pool volume [7]. The numerical modeling needs sufficient trial–and–error exercises to obtain suitable parameters to represent the parameters to represent the heat source.

    Goldak et al. [7] initiated the concept of volumetric heat source in the context of moving arc welding that permitted the energy to reach inside the weld pool volume and defining a pseudo weld pool in the form of a double ellipsoid (Fig. 1). The double ellipsoid heat source was defined by parameters a, b, c1 for representing front of ellipsoid whereas the rear ellipsoid was defined by parameter a, b and c2. The power density distribution in the front and rear quadrant of weld pool was given as [7].

    )

    c

    z

    b

    y

    a

    x

    (

    3

    s

    2

    2

    2

    2

    2

    2

    e

    )

    1

    c

    (

    ab

    Q

    )

    1

    f

    (

    3

    6

    )

    z

    ,

    y

    ,

    x

    (

    q

    +

    +

    -

    =

    p

    p

    (2)

    (For Frontal Ellipsoid)

    )

    c

    z

    b

    y

    a

    x

    (

    3

    s

    2

    2

    2

    2

    2

    2

    e

    )

    2

    c

    (

    ab

    Q

    )

    2

    f

    (

    3

    6

    )

    z

    ,

    y

    ,

    x

    (

    q

    +

    +

    -

    =

    p

    p

    (3)

    (For Rear Ellipsoid)

    Figure -1 Representation of double-ellipsoidal

    heat source [8].

    The heat input is represented as

    s

    q

    whereas the fractions f1 and f2 take into consideration asymmetry in magnitude of heat input at the front and the rear of the volumetric heat source. As this heat source considers the existence of pseudo weld pool from the beginning of the process, only the equation of conservation of energy needs to be solved to model the transient temperature field. The only limitation of this approach is that it considers the existence of pseudo weld pool a priori and hence the nature of fluid flow in a weld pool driven by various convective forces cannot be predicted. The power density distribution from the laser beam was observed to be conical. Ranatowski and Pocwiardowski [18] had suggested a cylindrical-involution-normal representation corresponding to a laser beam as

    (

    )

    ))

    s

    z

    (

    u

    1

    (

    e

    )

    s

    K

    exp(

    1

    Q

    K

    K

    )

    y

    ,

    x

    (

    q

    d

    K

    )

    y

    x

    (

    K

    d

    z

    z

    c

    Z

    2

    2

    C

    -

    -

    -

    -

    =

    -

    +

    -

    p

    (4)

    where

    Q

    is the heat input,

    z

    K

    involution factor of heat source,

    c

    K

    the factor designating the heat source concentration,

    d

    s

    the heat source penetration depth, and

    )

    s

    z

    (

    u

    d

    -

    the Heaveside’s function. The authors hypothesized that by changing the values of

    d

    s

    ,

    z

    K

    and

    c

    K

    , equation (4) could account for point, line, plane, paraboloid, conical, or Gaussian presentation of heat source. The value of the depth of heat source

    d

    s

    was taken as h at a point where the power at the said depth was 5% of the total input power. The values of

    d

    s

    ,

    c

    K

    and

    z

    K

    are rarely available and that has restricted the use of this present model. The recourse is to either calibrate a heat source expression against experimental data sets or evolve a route to determine optimized value of such uncertain parameters for varying weld conditions.

    The numerical process models that had undertaken detailed convection heat transfer analysis in weld pool preferred to use surface heat flux input following a Gaussian distribution. The numerical models that considered conduction heat transfer analysis alone preferred to use a combination of Gaussian surface heat flux distribution in association with a volumetric heat source expression or only the later. In cases like laser spot welding where weld pool size is small or the process involves rapid melting and solidification offering very less time for convective flows to develop fully, heat conduction based model with a volumetric heat source representation can provide a fairly reliable estimation of weld pool dimensions. In the present work, the energy input due to the laser beam is considered as a surface heat flux with Gaussian energy distribution and subsequently, an adaptive volumetric heat source is introduced as the weld pool grows with elapse of time. The experimental results of weld dimensions shows close agreement with the model developed.

    II. Heat transfer simulation

    The axial symmetry of the laser beam permits us to apply the two-dimensional axisymmetric heat conduction equation

    t

    T

    C

    Q

    z

    T

    kr

    z

    r

    1

    r

    T

    kr

    r

    r

    1

    p

    =

    +

    ÷

    ø

    ö

    ç

    è

    æ

    +

    ÷

    ø

    ö

    ç

    è

    æ

    r

    &

    (5)

    (1)

    where r and z refer to radial and axial directions; k, ρ, and

    p

    C

    respectively refer to thermal conductivity, density, and specific heat of material; T and t refer to temperature and time variable respectively, and

    Q

    &

    depicts internal heat generation per unit time and unit volume. The associated boundary condition can be stated as

    (

    )

    (

    )

    0

    T

    T

    T

    T

    h

    q

    n

    T

    k

    4

    0

    4

    0

    s

    =

    -

    +

    -

    +

    -

    se

    (6)

    (2)

    where k refers to thermal conductivity normal to surface; h and

    e

    depict surface heat transfer co-efficient and emissivity respectively;

    s

    is Stefan- Boltzmann constant, and T0 is the ambient temperature. A lumped heat transfer co-efficient is used combining the convective and radiative heat loss by considering h, as [2]

    61

    .

    1

    3

    T

    10

    4

    .

    2

    h

    ×

    ×

    *

    =

    -

    e

    (7)

    III. Adaptive Heat Source

    In the present work, the energy input due to the laser beam is considered as a surface heat flux with Gaussian energy distribution and subsequently, as an adaptive volumetric heat source. The surface heat flux is considered till the top surface under the laser beam has reached melting point temperature. Once a melt pool of finite dimensions is formed, an adaptively defined volumetric heat source is considered that corresponds to the size and the shape of the growing weld pool. The mathematical expression of surface heat flux distribution considering Gaussian energy distribution is given as

    ÷

    ÷

    ø

    ö

    ç

    ç

    è

    æ

    -

    =

    2

    eff

    2

    lb

    2

    eff

    lb

    gau

    s

    r

    r

    .

    d

    exp

    r

    d

    )

    (

    P

    q

    p

    h

    (8)

    Where P refers to the beam power,

    gau

    h

    the absorption coefficient of the laser beam at the work-piece surface,

    eff

    r

    the effective radius of the focussed laser beam, and

    lb

    d

    the beam distribution parameter of the laser beam profile. The mathematical expression of adaptive volumetric heat source is given as

    ï

    þ

    ï

    ý

    ü

    =

    =

    ÷

    ÷

    ø

    ö

    ç

    ç

    è

    æ

    -

    -

    =

    p

    w

    b

    2

    2

    2

    b

    2

    2

    b

    vol

    w

    p

    2

    w

    l

    where

    p

    z

    3

    l

    r

    3

    exp

    p

    l

    )

    (

    P

    3

    6

    q

    p

    p

    h

    &

    (9)

    In equation (9), wp and ww represent the instantaneous values of weld penetration (or depth) and weld width respectively that are computed from the numerical model. The parameters,

    vol

    h

    ,

    q

    &

    , lb, and p refer to absorption coefficient of laser beam within weld pool, volumetric heat input, and the extent of heat source in longitudinal and axial directions respectively. At time t = 0, the numerical calculations for heat transfer analysis considers the irradiated laser beam as a surface heat flux on the top surface. Once a weld pool of finite size is formed in a subsequent time-step, the volumetric heat source term is activated within the melt volume. The calculated values of weld width (ww) and weld penetration (wp) are assigned respectively to

    b

    l

    and p as indicated in equation (9). The values of ww and wp change as the weld pool grows in size in subsequent time-steps for the total laser on-time. Thus, equation (9) does not need a-priori knowledge of the final weld pool shape that is otherwise required in similar expressions used earlier [7-8, 18-19].

    The symmetry of a stationary laser beam, permits a symmetric boundary condition to be applied along z-axis as

    0

    r

    T

    =

    (10)

    (6)

    As, the process is transient in nature, an additional boundary condition is defined at time t = 0 as

    (

    )

    0

    T

    0

    ,

    z

    ,

    r

    T

    =

    (11)

    (7)

    The details of finite element discretization followed in this present study is as per the formulation details given by Amit et al. [21].

    IV. results & discussion

    Figures 2(a) – (d) show the comparison of computed and the corresponding measured weld dimensions for 1.0 mm low carbon steel at a laser power of 1.0 kW and at on times 6, 10, 14, and 20 ms. The isotherms are zoomed in a domain of 1.0 mm x 1.0 mm near the laser beam axis, being an area of interest as regards to prediction of fusion and heat affected zone. Figures 2(a) – (d) depict that the computed dimensions of weld depth and width and they agree well with the corresponding measured results at all the four on-times.

    The legends of the temperature isotherms plotted are given in Figures 2(a)-(d) and hence, the intercepts of the 1773 K isotherm (referred to A) in the radial and in the axial directions confirm to half of the weld width and weld depth respectively. The fair agreement between the calculated and the corresponding measured shapes and sizes of the weld pool for all the on-times also indicate the robustness of the model that has considered adaptive heat source. However, such a procedure can be considered to be more effective and practical when uncertain parameters like absorption coefficient for the given laser power and laser on-time is predicted. For example, Pantsar et al. [22] has showed that at a constant value of power density, increase in laser on-time, causes increase in absorption coefficient in laser welding process. Although an increase in the value of the absorption coefficient is a reality at higher laser on-time, the present model has considered a time-averaged value of absorption coefficient and thermal conductivity. The zone encompassed between the temperature isotherms 1773 K (referred to A) and 993 K (referred to D) is presumed extent of heat affected zone. The slight discrepancies between the calculated and measured extent of heat affected zone dimensions possibly indicate a greater value of lower critical temperature than 993 K that is considered here. A greater value of lower critical temperature indicates the need of superheating for transformation from α-ferrite to γ-austenite. The non-equilibrium cooling conditions prevailing due to rapid rate of heating and cooling during laser spot welding process might have led to higher value of lower critical temperature.

    V. conclusion

    The present study has attempted to bring out the prediction of weld dimension by the numerical heat transfer model that has considered adaptive heat source. The computed values of the weld dimensions from the two-dimensional axisymmetric heat transfer analysis are validated with the corresponding measured results from experimental studies. It is also shown that the geometric dimensions of the adaptive volumetric heat source, as adapted in this work, closely follow the shape and size of the instantaneous weld pool. It is thus conceived that the approach, presented in this work, will alleviate the restricted use of volumetric heat source in the context of modeling of laser welding, in particular, and fusion welding, in general.

    Figure -2 Comparison between calculated weld dimensions and the corresponding experimentally obtained weld macrographs.

    Laser power: 1.0 kW; Sheet thickness: 1.0 mm;

    On–times (a) 6 ms (b) 10 ms (c) 14 ms (d) 20 ms

    [Isotherm legends: A – 1773 K, B – 1473 K, C – 1203 K, D – 993 K, E – 623 K]

    VI. references

    [1]D. Rosenthal: Mathematical theory of heat distribution during welding and cutting, Welding Journal, 20(5), 1941, 220s-234s.

    [2] Rykalin R R , Energy Source for Welding, Welding in the World, Vol 12, No. 9/10, p 227-248, 1974.

    [3] A. Paul and T. Debroy: Free surface flow and heat transfer in conduction mode laser welding, Metallurgical Transactions B, 19, 1998, 851-857.

    [4] S. Basu and T. Debroy: Liquid metal expulsion during laser irradiation, Journal of Applied Physics, 72(8), 2003, 3317-3322.

    [5] T. Zacharia, S. A. David, J. M. Vitek and T. Debroy: Heat transfer during Nd: YAG pulsed laser welding and its effect on solidification structure of austenitic stainless steels, Metallurgical Transactions A, 20, 1989, 957-967.

    [6] V. Pavelic, R. Tanabakuchi, O. Uyehara and P. Myers: Experimental and computed temperature histories in gas tungsten arc welding of thin plates, Welding Journal, 48(7), 1969, 295s-305s.

    [7] J. A. Goldak, B. Chakravarti and M. J. Bibby: A new finite element model for welding heat sources, Metallurgical Transactions B, 15, 1984, 229-305.

    [8] V. Kamla and J. A Goldak: Error due to two dimensional approximations in heat transfer analysis of welds, Welding Journal, 72(9), 1993, 440s-446s.

    [9] D. Grey, H. Long and P. Maropoulos: Effects of welding speed, energy input and heat source distribution on temperature variations in butt welding, Journal of Materials Processing Technology, 167, 2005, 393-401.

    [10] R. Akhter, M. Davis, J. Dowden, P. Kapadia, M. Ley and W. M. Steen: A method for calculating the fused zone profile of laser keyhole welds, Journal of Physics D: Applied Physics, 21, 1989, 23-28.

    [11] N. Sonti and M. F. Amateau: Finite element modeling of heat flow in deep penetration laser welds in aluminum alloys, Journal of Numerical Heat Transfer A, 16, 1989, 351-370.

    [12] R. Mueller: A study on heat source equations for prediction of weld shape, Proc. ICALEO’94, Orlando, USA, October 1994, 509-518

    .

    [13] J. Song, J. Y. Shanghvi and P. Michaleris: Sensitivity analysis and optimization of thermo-elasto-plastic processes with application to welding side heater design, Computer methods in applied mechanics and engineering, 193, 2004, 4541-4566.

    [14] R. G. Theissen, I. M. Richardson and J. Sietsma: Physically based modeling of phase transformations during welding of low carbon steel, Materials Science and Engineering A, 427, 2006, 223-231.

    [15] D. Deng and H. Murakawa: Numerical simulation of temperature field and residual stress in multi-pass weld in stainless steel pipe and comparison with experimental measurements, Computational Materials Science, 37, 2006, 269-277.

    [16] M. A. Wahab and M. J. Painter: Numerical models of gas metal arc welds using experimentally determined weld pool shapes as the representation of the welding heat source, International Journal of Pressure Vessels and Piping, 73, 1997, 153-159.

    [17] W. S. Chang and S. J. Na: A study on the prediction of the laser weld shape with varying heat source equations and thermal distortion of a small structure in micro-joining, Journal of Materials Processing Technology, 120, 2002, 208-214.

    [18] E. Ranatowski and A. Pocwiardowski: An analytic-numerical evaluation of the thermal cycle in the HAZ during welding, Proc. of Fourth International Seminar on Numerical Analysis of Weldability at Graz- Seggau, Austria- 4-5 September, 1997, 379-395.

    [19] W. Sudnik, D. Radaj and E. Erofeew: Computerized simulation of laser beam weld formation comprising joint gaps, Journal of Physics D: Applied Physics, 31, 1998, 3475-3480.

    [20] M. R. Frewin and D. A. Scott: Finite element model of pulsed laser welding, Welding Research Supplement, 78(1), 1999, 15s-22s.

    [21] Integrating Finite Element based Heat Transfer Analysis with Multivariate Optimization for Efficient Weld Pool Modeling By Amit Trivedi, Anand Suman, and Amitava De, ISIJ International, Vol. 46 (2006), No. 2, 267-275.

    [22] H. Pantsar and V. Kujanappa: Diode laser beam absorption in laser transformation hardening of low alloy steel, Journal of Laser Applications, 16(3), 2004, 147-153.

    [23] S. Katayama, S. Kohsaka, M. Mizutani, K. Nishizawa and A. Matsunawa: Pulse shape optimization for defect prevention in pulsed laser welding of stainless steels, ICALEO, Orlando, USA, 24-28 October 1993, 487-497.

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