Electrothermal Analysis OfElectric Resistance Spot Welding Processes by a 3-D Finite Element

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  • 8/17/2019 Electrothermal Analysis OfElectric Resistance Spot Welding Processes by a 3-D Finite Element

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    ELSEVIER

    Joumal

    of

    Materials Pro eSSing Te..imology 63 1997) 672-677

    JournaJof

     aterials

     rocessing

    Technology

    Electrothermal Analysis ofElectric Resistance Spot Welding Processes by a 3-D Finite Element

    Method

    H Huhand W J Kang

    Dept.

    of

    Mechanical Engineering

    Korea Advanced Institute

    of

    Science

     n

    Technology

    373 1 Kusongdong Yusonggu Taejon 305 701 Korea

      bstract

    Electric resistance spot welding which is an important process in auto-body assembly is simulated by a 3-D finite element code

    developed. The main interest in the simulation is the quality

    of

    welding and the durability of electrodes, which needs electrothermal

    analysis for temperature distribution in both electrodes and welded sheets. A finite element formulation is derived for both electric

    analysis and thermal analysis that are coupled together. The contact resistance between electrodes and sheets is especially treated with

    artificial interface elements in which the material properties for electric and thermal analysis are artificially imposed for physically

    reasonable simulation.

    1. Introduction

    Electric resistance spot welding is an important process in the

    industry.

    In

    electric resistance spot welding, the overlapping

    work is positioned between the water-cooled electrodes, then the

    heat is obtained

    by

    passing a large electrical current for a shot

    period of time. Auto-body assembly needs 7000 to 12000 spots

    of welding according

    to

    the size of a car, so the spot welding is

    an important process in auto-body assembly. Each spot welding

    is not performed on the same condition because of the alignment

    of sheets and electrodes as well as the surface condition. For that

    reason, a spot welding process needs the optimum process

    condition that can afford allowance in parametric values for good

    quality of welding. The optimum condition has to consider the

    amount and duration

    of

    electric current, the shape and material

    properties of electrode, and the surface condition and alignment

    of sheets. The main interest in spot welding process is the

    quality of welding and the durability of electrodes, which needs

    electrothermal analysis for temperature distribution in both

    electrodes and welded sheets[IJ[2J[3]. The shape

    of

    electrode is

    an important parameter determining the shape and size of the

    nugget which has large effects on the stress concentration and

    fatigue strength of welding parts. The stress distribution in the

    lap joint of spot-welded steel is calculated by finite element

    method[4]. The effect of a space angle of line contact is

    analytically calculated[5].

    In this paper, a finite element formulation is derived for both

    electric analysis and thermal analysis that are coupled together.

    Two sets of formulation are uncoupled after finite dimensional

    approximation to a time-incremental analysis. First, the electric

    0924-0136/97/ 15.00

     

    1997 Elsevier Science S All rights reserved

    PII S0924-0136 96)02705-7

    potential is obtained for the entire field and scaled according to

    the given electric current. The electric field obtained is used to

    calculate the energy dissipation due

    to

    the electric resistance of

    materials. The energy dissipation calculated from the electric

    analysis is substituted for the heat generation in the heat

    conduction equation to calculate the temperature distribution in

    the entire domain. After the calculation, all material properties

    are updated element-wise for the next step according

    to the

    calculated temperature. The finite element code developed

    simulates electric resistance spot welding processes with the

    variation of process parameters such as the electric current, the

    contact resistance, and the material properties

    of

    electrodes and

    sheets. The contact resistance between electrodes and sheets is

    especially treated with artificial interface elements in which the

    material properties for electric and thermal analysis are

      r t i f i i ~ l l y imposed for physically reasonable simulation. The

    numerical result provides the electric potential field, the electric

    current distribution, and the temperature distribution. Elliptic

    electrodes are studied with the variation

    of ellipticities on

    condition of the same tip area. The results informs that the shape

    of electrodes is important in distribution

    of

    the electric current

    and thus the heat generation. On the same welding condition

    such as the welding current, the weldtime and the pressure, the

    size of nuggets obtained

    by

    various shapes

    of

    electrodes which

    have the same contact area are different from each other.

    Relation between the shape

    of

    nugget and the shape of electrode

    is important for the purpose of obtaining necessary nuggets

    which appropriate to the various stress condition and the number

    of

    spots can be reduced

    by

    selecting an adequate elliptic

    electrode.

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    H Huh W J Kang / Journal   Materials Processing Technology 63 (1997) 672-677 673

    where P is the density, cp is the specific heat per unit volume,

    kij is

    the heat conductivity, and f id heat generation calculated

    form Eqn (6).

    2.  ormul tion for electrotherm l analysis

    The heat lOr electric resistance spot welding is obtained

    by

    passing a large electric current through workpieces which have

    electric resistance in the domain and contact surfaces. The

    amount of heat generation per unit volume can be calculated by

    the electric potential in the domain and then it can be applied

    to

    the heat transfer equation

    to

    calculate the temperature

    distribution in the electrode and workpieces. The maximum

    temperature in electrodes and workpieces approaches the phase

    change temperature and the effect of latent heat is considered by

    increasing a specific heat in the temperature range

    of

    phase

    change as Eqn

     1 .

    T=T

    o

    at

    t=O

     

    D

    on aD

     7

    (8)

     9

    (1)

    where H

    L

    is a latent heat, T

    L

    is a melting temperature, and Ts is

    solidifying temperature.

    3.  inite element formul tion

    When the principle of

    the first variation is applied

    to

    Eqn

    (2)

    and Eqn (7), respectively, weakforms can be obtained

    as

    Eqn

     10 and Eqn  11 .

    2 Formulation   relectric analysis

    The electric potentia] can be expressed by Quasi-Laplace

    equation. The governing equation and its boundary condition are

    as

    follows.

      C lV - -

      Clx; Oij Clxj Vdn =0,  

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    674

      Huh W J Kang / Journal   Materials Processing Technology 63 1997) 672-677

    of

    matrix equations are obtained for electrothermal analysis

    For finite e lement simulation Eqn 16) is first solved

    to

    calculate heat generation from the electric potential. The heat

    generation calculated is substituted in Eqn 18), which is solved

    for temperature distribution at the specific time. According to the

    temperature distribution obtained, all electrothermal properties

    are updated element-wise for the next time increment step. This

    procedure continues until a desired temperature distribution is

    obtained.

    Fig. 2 through Fig. 5 show the electric and thermal properties

    for the present analysis with the variation of the temperature.

    As

    shown in Fig. 2, the electric resistance in contact interface

    between workpieces is larger than that between

    an

    electrode and

    a workpiece. Both values are decreased

    as

    the temperature

    increases[7]. The electric resistivity and Heat conductivity

    of

    a

    steel workpiece is much larger than those

    of

    a copper electrode

    as

    shown in Fig. 3 and 4.

    As

    the t emperature goes up, a steel

    workpiece experiences phase changes absorbing the heat

    energy[9]. In order to describe the phenomenon, the specific heat

    per unit volume is modified

    by

    the enthalpy method thus the

    heat capacitance is represented as shown in Fig.

    5

    Fig. 6- a) through Fig. 8- b) explains temperature

    distributions in

    an

    electrode and a workpiece with respect to

    each ellipticity. The shape

    of

    nuggets in the faying surface is

    nearly the same

    as

    the shape

    of an

    electrode tip. However, the

    amount

    of

    temperature rise and the nugget growth closely

    depends on the ellipticity. The comparison has made for various

    ellipticity in Fig. 9 to Fig. II

    Fig. 9 represents relation between the electrode ellipticity and

    the nugget ellipticity. In this curve the nugget ellipticity nearly

    follows that

    of an

    electrode except when the ellipticity is 0.25.

    Fig. 10 and Fig.

     

    represents relation between the electrode

    ellipticity and the nugget area and thickness obtained

    respectively. In contrast to the nugget ellipticity, the nugget area

    and thickness shows asymptotic behavior demonstrating the poor

    nugget growth when the ellipticity is smaller than a certain value.

    Fig.   2 represents dynamic resistance curves vs. time with

    the variation

    of

    the ellipticity. The figure shows the global

    electric resistance decreases with the decrease of the ellipticity,

    which indicates the amount

    of

    the heat energy generated. The

    efficiency

    of

    welding decreases

    as

    the ellipticity decreases.

    When an elliptic nugget is needed for a strength purpose,

    an

    elliptic electrode

    of

    the ellipticity more than 0.4 can be selected

    to

    maintain the welding efficiency and nugget size.

      18)

      17)

      16)

    the Crank-

    with the first and initial boundary conditions.

    Eqn 17) can be integrated in time

    by

    applying

    Nicholson s

    e-

    Method

    as

    shown in Eqn 18).

      Results and discussion

    The shape and size

    of

    nuggets are calculated with a 3-D

    electrothermal finite element code developed. In the computation,

    the electric current

    of

    12000 amperes passes through the

    electrodes and workpieces during the time

    of

    l2cycles

      0.2second). The material

    of

    sheets is steel and the size is

    assumed 30mm x 30mm x 1.6mm which is sufficient for good

    simulation

    of

    a real process. The ell ipti ci ties

    of

    the elliptic

    electrodes are

    1 0 0 75 0 5

    0.4, and 0.25 with its tip area being

    constant

    as

    38.44mm

     

    so that the electric contact resistance

    in

    each case assumed the same.

    Fig. 1 represents typical finite element meshes used in this

    analysis. Because the welding system is symmetric, one eighth of

    the system can be modeled in the analysis. To consider the

    electric contact resistance, one-layered artificial interface

    elements is used on each contact surfaces. The electrothermal

    properties

    of

    artificial interface elements are carefully chosen to

    have reasonable physical meaning considering complicated

    contact phenomena[6-9]. Fig. 1 Finite element mesh

    of an

    elliptic electrode and a sheet.

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    H

    Huh

    W

    J Kang / Journal   Materials Processing Technology 63 1997 672-677

    675

    2000

    1 e l e c t o d ~

    ,- -

    - workpIece

    1\

     

    o

    500

    1000

    1500

    Tempera ture  DC

    Fig. 5 Heat capacitance in an electrode and a workpiece with

    respect to the temperature.

    1.5

    30

    0

     

    u

     x

    electrode

     

    ;>--

    1.2

    Mel

    .....

    - workpiece

    u

    :>

     

    .....

    8 20 0

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    676

      Huh J Kang / Journal   Materials Processing Technology 63 1997 672-677

    A

    . 170E 04

    0

     150E 04

    0

     160E 04

    9

    . 140E+04

    9 . 150E 04 8

    .

    130E 04

    8

    . 140E 04

    7

     120E 04

    7

    .

    130E 04

    6

    . 110E+04

    6

    . 120E 04

    5

     100E 04

    5

    . 110E 04

    4

     900E 03

    4

     100E 04

    3

     800E 03

     

    3

     900E 03

    2

     700E 03

    2

     800E 03

    1

     600E 03

    1  700E 03

    Min=25°c

    Max= I733°C

    Fig. 7- a Temperature distribution in the xy plane when the

    ellipticity is

    0.5.

    Fig. 8- b Temperature distribution in the yz plane when the

    ellipticity is

    0.25.

    Electrode ellipticity

     

    . 170E 04

    0

     160E 04

    9

    . 150E 04

    8

    .

    140E 04

    7

     130E 04

    6

     120E 04

    5

    . 110E 04

    4

     100E 04

    3

     900E 03

    2

     800E 03

    1

     700E 03

    [

     

    2

    ;>-,

    1.0

     

    u

     

    O 8

     

    -

    0.6

    Q

    0.4

      £l

      l

     

    O 2

    0.0

    O

    0

    O

    2

    O

    4 0.6

    O

    8

    1.0

     

    2

    Fig. 7- b Temperature distribution in the yz plane when the

    ellipticity is

    0.5.

    Fig. 9 Relation between nugget ellipticity and electrode

    ellipticity.

    20

    Electrode area =38 44mm

    2

     

    2  2 O 4

    O

    6

    O

    8

     

    0

    Electrode

    ellipticity

    15

    < J

      l l

    10

    o

    O 0

    o  150E 04

    9 .

    140E 04

    8  130E 04

    7  120E 04

    6 . 110E 04

    5  100E 04

    4

     900E 03

    3  800E 03

    2   7 0 0 E 0 ~

    1

     600E 03

    Min=25°c

    Fig. 8- a Temperature distribution in

    xy

    plane when the

    ellipticity is

    0.25.

    Fig. 10 Relation between nugget area and electrode ellipticity.

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      uh W   Kang / Journal   Materials Processing Technology 63 (1997) 672-677

    677

    Fig. 11 Relation between nugget thickness and electrode

    ellipticity.

    1.0

     

    O

    8

    ..

     

    j)

     

    s

    j ) . - 4

    s u

    .- 4  

    O

    6

      c:

     

    .c:

     

    j)

    u

    0.4

     

    j)

      j .-

    00 p .

    00 .- 4

    ::>

    H

    z

    0

    O 2

    o

    0

    0.0

    O 2 O 4 O 6 O 8

    I

    0

    Electrode ellipticity

    I

    2

    5. Conclusion

    Electric resistance spot welding is simulated

    by

    a 3-D

    electrothermal finite element code developed considering the

    temperature dependent electrical and thermal properties.

    In

    this

    simulation elliptic electrodes are adopted and the effects of the

    variation

    of

    their ellipticities on the acquired nuggets are

    calculated. Among simulated electrodes,

    an

    circular-shaped

    electrode can produce the largest nugget under the same welding

    condition. The welding efficiency shows asymptotic relation

    to

    the ellipticity

    of an

    electrode. When

    an

    elliptic nugget is needed

    for a strength purpose, an elliptic electrode

    of

    the ellipticity

    larger than 0.4 can be selected

    to

    maintain the welding efficiency

    and nugget size. An elliptic electrode is used in this range then

    the obtained nugget have smaller stress concentration than that

    of

    circular nugget at the short edge

    of

    nugget.

    References

    150

    140

      j)

    u

    l:1

    oj

    130

     

    j)

    120

     

    u

    -x-e=1.0

    110

     Q e=O.75

    s

    e=O. 5

     .

    C l

      e=O. 4

    00

     

    e=O. 25

    90

    O 00

    O

    05

    O

    10

    O

    15

    O

    20

    O

    25

    Time (sec.)

    Fig. 12 Variation

    of

    the dynamic resistance with respect

    to

    time

    for various ellipticity.

    [1]  

    F. Houchens,

    R. E.

    Page and

    W. H.

    Yang,

    In

    Numerical

    modeling

    of

    manufacturing processes (ed.

    by R.

    F. Jones, H.

    Armen and J. T. Fong), (1977)117.

    [2] H .  

    Nied, Welding Research Supplement, (1984)123.

    [3]

    W. Rice and E.

    J.

    Funk, Welding Research Supplement, Apr.

    (1967)175.

    [4]

    D.

    H.

    Bae, J. Niisawa and

    A.

    Koiso, KSME, spring

    conference, (1987)7.

    [5] Y .

    Sano, IEEE Trans., vol. CHMT-8, (1985)228.

    [6] S. R. Robertson, IEEE Trans., VoI.CHMT-5, No.1, (1982)3.

    [7] W . L

    Roberts, The Welding Journal, Nov. (1951)1004.

    [8] J.   Greenwood, Brit. J. Appl. phys., Vol.17 (1966)1621

    [9]

    C.

    Bonacina, G. Comini,

    A.

    Fasano and

    M.

    Primicerio, Int.

    J.

    HeatMass Transfer, vol.16, (1973)1852.

    [10]

    K

    C. Wu, Welding Research Supplement, Oct,(1968) 472.

    [11] N.

     

    Freytag, Welding Research Supplement, Apr. (1965)

    145.