Thermally induced deformation of solder joints in real packages: Measurement and analysis

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  • atiem

    n S

    n Un

    Received 27 July 2005; received in revised form 2 October 2005Available online 18 November 2005

    condition, etc. In the point of view of solid mechanics, accelerated test routines and failure statistic based dataanalysis. On the other hand, the interest in the physics-based, predictive methodologies is notably growingdriven mainly by the time and cost reduction for newpackage development, design and prototyping. The

    0026-2714/$ - see front matter 2005 Elsevier Ltd. All rights reserved.

    * Corresponding author.E-mail address: hlu@ryerson.ca (H. Lu).

    Microelectronics Reliability 46 (1. Introduction

    The global transition to lead-free solders has given anew thrust to the packaging reliability research e.g., [16]. The solder joint reliability performance as commonlyacknowledged is a complex issue due to its sensitivity tovarious factors such as the package structure and geo-metric scale, the manufacturing process and the service

    the stress and strain dictate the solder joint failure. Thedecades long studies have led to the establishment of aframework for quantitatively assessing the solder jointreliability. Based on that, some bunch mark structuresimulation and material modeling have provided neededguidance to the understanding of failure mechanismsunder dierent circumstances. Yet to date the packagethermal reliability assessment is heavily relied on theAbstract

    The paper presents a hybrid experimental and analytical approach to track the deformation of solder joints in anelectronic package subject to a thermal process. The solder joint strain is directly measured using a computer visiontechnique. The strain measurement is analyzed following an approach that is devised based on an established solderconstitutive relation. The analysis leads to the determination of the solder joint stress and in turn, to the separationof the elastic, plastic and creep strain from the measured total strain. The creep strain rate and stressstrain hysteresisloop are also obtained. Two case studies are presented to illustrate the applications and to show the viability of theapproach. Each case involves a resistor package with SAC (Sn95.5Ag3.8Cu0.7) solder joints, which is subjected to atemperature variation between ambient and 120 C. The results conrm that shear is a dominant strain componentin such solder joints. The shear strain varies nearly in phase with the temperature whereas the shear stress exhibits adierent trend of variation due to stress relaxation. The peak shear stress of around 10 MPa to 15 MPa are found,which occur at near 70 C in both cases, when the temperature ramps up at approximately 3 C/min. The creep shearstrain goes up to 0.02 and accounts for over 80% of the total shear strain. The creep strain rate is in the order of mag-nitude of 105 s1. Responding to the temperature cycling with such moderate rate, the creep strain shows modest rat-cheting while the stressstrain hysteresis stabilizes in two cycles. 2005 Elsevier Ltd. All rights reserved.Thermally induced deformpackages: Measur

    Hua Lu *, Hele

    Department of Mechanical and Industrial Engineering, Ryersodoi:10.1016/j.microrel.2005.10.002on of solder joints in realent and analysis

    hi, Ming Zhou

    iversity, 350 Victoria Street, Toronto, Canada ON M5B 2K3

    2006) 11481159

    www.elsevier.com/locate/microrel

  • other, the solder joint creep fatigue can be demonstrated

    tor is dened and related to the motion of the points in asubset of the deformed image with respect to the corre-sponding points in the un-deformed counterpart. Themotion is assumed to obey the continuum mechanicsbased deformation kinematics. An iterative algorithmis adopted to assess the factor initially calculated withgross estimates of the deformation parameters, and sub-sequently to improve the parameters. The iteration pro-

    Fig. 1. Experimental setup used for strain measurement: (a) asketch of the system layout and (b) a picture of the system.

    H. Lu et al. / Microelectronics Reliability 46 (2006) 11481159 1149by the stressstrain hysteresis, and the per-cycle damagecan be quantied by the area enclosed in a stabilized hys-teresis loop. For a practical assessment, it is desirable toconduct such an evaluation on real assembly packagessubjected to a non-accelerated, operating thermal pro-cess. In a pioneering work, Hall et al. [17] used opticaland strain gauge techniques to observe the thermal defor-mation of LCCC (leadless ceramic chip carrier) assem-blies. Pan and Pao [18] studied the solder jointdeformation using a beam specimen. In both studiesthe solder joint hysteresis loops are examined. The pres-ent study, though similarly motivated, uses the methodof digital speckle correlation (DSC) to measure a solderjoint of a package. Specically, the strain variation withthe temperature in a stress concentrated local area isobtained. The analysis uses a scheme that yields the solu-tion of solder joint stress based on the strain measure-ment. This in turn enables the separation of the elastic,plastic and creep strain components from the measuredtotal strain, and the determination of the creep rateand the strain energy density.

    2. Solder joint strain measurement

    2.1. DSC technique

    The key of the study is to obtain direct strain mea-surement in the solder joints, which relies mainly onthe application of a technique called digital speckle cor-relation (DSC). With its high and adjustable resolution,existing solder joint failure theories are diverse as over-viewed and categorized by Lee et al. [7] in 2000, whichare recently enriched by the additions devoted to lead-free solders e.g., [812]. A class of the models [1316] thathave gained wide acceptance attributes the thermal creepfatigue to the solders microstructure damage that accu-mulates as the temperature cycles. Given that the damageand the strain energy dissipation are correlated to each

    Abbreviations

    SAC Sn95.5Ag3.8Cu0.7 alloyDSC digital speckle correlationDSC enables a gross search for the sites of strain concen-tration in a package, if necessary. When such sitesbecome apparent, the system can be zoomed in to obtaindetailed measurement. In Fig. 1 a sketch and a photo aregiven to help illustrate the experimental setup used. Themethodology is based on evaluating the correlationbetween a pair of the images that are recorded at dier-ent deformation states of a surface. A de-correlation fac-LCCC leadless ceramic chip carrierPCB printed circuit boardceeds to turn the deformed image back to its originalshape, evidenced by the progressively improved imagecorrelation. A good correlation reached at the end ofthe process signies that the deformation parametersat the subset center have been converged to the respec-tive true values. The deformation of an area is deter-mined in a point-by-point manner repeating the aboveprocess. The computer vision technique is quick in

  • generating large quantities of measurements upon thetest completion. And its features of non-contact andnon-coherent make it suitable for thermal applications.Detailed descriptions of the methodology and the mea-surement procedures can be found in Refs. [1921].

    2.2. Test vehicles and sample preparation

    The test vehicles used in the study are the type ofceramic resistor packages chosen to use in a Pb-free reli-ability research by National Electronics ManufacturesInitiative (NEMI). Fig. 2 gives a three-dimensionalsketch and another of a cross-section detailing the pack-age structure. The packages feature dimensions arelisted in Table 1. The sample preparation includescross-sectioning, polishing, photographing and specklecoating, etc. Fig. 3 gives photos of a partial cross-sectionshowing the solder llet and the surrounding area beforeand after a speckle pattern is applied to. The articialspeckle pattern provides a desired random variation oflight reectivity across the surface, which is criticallyrequired by the image correlation calculation. Should anaked cross-section be measured, the grey-value varia-tion across the image would be contributed mainly bythe surface texture or by variable reectivity of individ-ual solder grains and cell boundaries in case a very large

    optical magnication is used. Yet under heat and stress,the solder grains will grow to cause the solder micro-structure coarsening, which could aect the macroscopicappearance of the surface texture. Given that the meth-odology attributes the image de-correlation only to thesurface deformation, the microstructure coarseninginduced surface texture change could confuse the corre-lation calculation and thus cause measurement error.

    2.3. Image recording and processing

    In this study, each test records a series of images ofthe area centered at the solder joint llet, as typically

    Ceramic thickness(mm)

    PCB thickness(mm)

    Data area(mm2)

    0.508 1.15 0.032 0.0440.508 1.15 0.050 0.044

    Fig. 3. Pictures showing a solder joint and its vicinity: (a) aphoto of a joint llet and surrounding area with no specklecoverage, (b) a photo of same area covered by speckles, and (c)a sketch giving geometric dimensions of the joint.

    1150 H. Lu et al. / Microelectronics Reliability 46 (2006) 11481159Fig. 2. A 3D sketch and a sketch of a XY cross-section of atest package.

    Table 1Geometric dimensions of the package cross-section

    Test Solder-joint thickness(mm)

    Copper trace thickness(mm)

    Case A 0.044 0.068Case B 0.044 0.063

  • shown by Fig. 3(b). The image processing involves a pairat a time, namely a reference image taken at the ambientand another at an elevated temperature. The processingrestricts to a portion of the image that covers a part ofthe solder joint. To exactly outline the solder joint underthe speckle coverage is assisted by feature lines andpoints that are commonly identiable in both images.Upon the determination of the rectangular area andthe measurement resolution, a processing grid is laiddown in the reference image. The area is indicated bythe solid-line box in both schematics shown inFig. 3(a) and (c), as well as by the processing left traceson the image as seen in Fig. 3(b). Each processingobtains a set of the measurements at a grid point, includ-ing two displacement components and four displace-ment partial derivatives. It is noted that the DSCtechnique yields the six parameters simultaneously andindependently. Raw measurements in the solder layerobtained at a particular temperature are typically shownin Fig. 4 in the form of area contours. The displacementcomponents u and v are the direct output. The partialderivatives ou/ox and ov/oy are also direct output andrepresent approximately the respective normal strains.And the shear strain is obtained via ou/oy + ov/ox.Within the processed area, a small portion near the sol-der joint llet is named the data area. This chosen

    directly attached to the test package. The test data andthe results from a nite-element thermal modeling both

    H. Lu et al. / Microelectronics Reliability 46 (2006) 11481159 1151sub-area, as indicated by a dash-line box in bothFig. 3(a) and (c), has linear dimensions of a few dozenmicrons. Based on the original data, the average shear

    Fig. 4. Typical contour maps of strain and displacement

    components directly obtained from image processing.conrm a fairly uniform temperature distribution acrossthe sample surface and in the body. The modelingproves that the temperature in-uniformity throughoutthe package is limited and ranges from a fraction of adegree to a couple of degree Celsius. In actual testing,additional monitoring of the sample temperature is pro-vided by thermal couples attached to the sample stand atthe samples very vicinity. The system vibration and theair circulation, enhanced by the use of large optical mag-nication, are the main sources of disturbance to aectthe image stability and thus to cause scattered measure-ments. The chamber temperature control is automatedby adjusting the air ow, which functions well in keepinga limited temperature uctuation during dwelling. Thenature of the control, however, appears to have contrib-uted to the data scatter. The troubling instable air owbecomes apparently severer in the dwell periods duringwhich the feedback controls the electric fan to be alter-nately on and o. The resulted turbulence causes theoptical refractive index of the air to vary, and in turn,the image to distort. An eort made to counter that isto manually turn the fan o for a few seconds beforeeach image recording. This however results in that thesample temperature quickly drops from the preset testprole by as much as 10 degree Celsius.

    3. Strain analysis leading to solutions of stress and

    separation of strain components

    3.1. Solder constitutive relations

    Numerous constitutive equations have been pro-posed for dierent solder alloys. This study gives theattention to those that are based on testing actual assem-blies e.g., [13,22,23]. For surface mount packages, it is awell documented e.g., [2] phenomenon that the sheardominates the thermally induced solder joint deforma-tion. This analysis focuses on the shear strain despitethe availability of normal strain measurements. Adoptedstrain in the sub-area is calculated for o-setting the ran-dom errors that exist in the single-point measurements.In the analysis to follow, this average shear strain isreferred to as the measured total shear strain.

    2.4. Temperature control

    A forced convective thermal chamber as seen inFig. 1(b) is used. The chamber temperature can be setto vary between 70 C and 250 C with chosen ratesand at the accuracy of 3.5 C. Since the sample tem-perature always lags behind the chamber reading, a sep-arate calibration test is conducted using thermal couplesas follows is a commonly accepted, additive constitutive

  • 3.2. Solder deformation basics

    Some basic aspects of the solder deformation arenoted in formulating the stress solution as presented inthe next section. First, the measured strain generallyconsists of mechanical and thermal components. Themechanical part is stress related and usually has morethan one contributor as indicated by Eq. (1); the thermalpart represents the materials thermally induced dimen-sional change while the material is under no force andconstraints. The thermal strain is usually non-stress

    Table 2Solder constitutive parameters [13]

    G0 (GPa/Mpsi) 19.3/2.8

    G1 (MPa/K/Kpsi/K) 69/10C6 2.04 1011

    m 4.39C (K/s/Pa/K/s/psi) 0.454 106/3.13 103

    a 1500n 5.5Q (eV) 0.5

    Fig. 5. Test temperature vs. time curve: (a) for test package A

    1152 H. Lu et al. / Microelectronics Reliability 46 (2006) 11481159relation that regards the shear strain as a linear superpo-sition of separate components, each representing contri-bution of a dierent deformation mechanism. The totalshear strain ctl is expressed as

    cel cpl ccr ctl 1where cel, cpl and ccr are, respectively, the elastic, plasticand creep strain components. The specic model andparameters adopted are proposed by Darveaux et al.[13]. Darveauxs model extends to several solder alloys(60Sn40Pb, 96.5Sn3.5Ag, 97.5Pb2.5Sn and 100In, etc.),covers a wide strain range and incorporates temperatureeects in all the three components.

    For the elastic portion, the model applies Hookeslaw as follows:

    cel sG

    2

    In the equation s is the shear stress, G is the temperaturedependent shear modulus expressed as G = G0 G1(T 273) where T is the temperature in Kelvin, G0is the shear modulus at 0 C and G1 is a constant.

    The RambergOsgood type relation is used for thetime independent plastic deformation:

    cpl C6sG

    m3

    cpl C6sG

    m3a

    Eqs. (3) and (3a) are used when s is positive and nega-tive, respectively. C6 and m are material constants, thevalues for Sn3.8Ag0.7Cu are unavailable and are substi-tuted by those for Sn3.5Ag for the strain analysis. Con-sidering the similarities between their composition andmicrostructure as well as the minor plastic content inthe total strain, the substitution should contribute lim-ited error in the outcomes of this analysis.

    Assuming the primary creep is negligible, the domi-nant steady state creep strain is expressed in a hyperbolicsine rate equation as follows:

    dcsdt

    C GT

    sin h a0

    sG

    h inexp

    QkT

    4

    dcsdt

    C GT

    sin h a0

    sG

    h inexp

    QkT

    4a

    Similar as Eqs. (4) and (4a) are used alternately for po-sitive and negative shear stress. In both equations, C is aconstant characteristic of the underlying micro-mecha-nism, G denotes the temperature dependent shear mod-ulus, a0 prescribes the stress level at which the power lawdependence breaks down, n is the stress exponent, Q isthe activation energy for the deformation process, k isthe Boltzmanns constant and T is the temperature inabsolute scale [13]. The values of the constitutive param-

    eters used in the analysis are listed in Table 2. and (b) for test package B.

  • related. Macroscopically, the solder materials may beconsidered as thermally isotropic. For such isotropicmaterials, temperature change induces no shear termof thermal strain. Second, the elastic strain componentis instant and recovers upon stress relaxation; the instantplastic strain and the time-lagged creep strain are bothpermanent and therefore stress-history dependent.

    3.3. Step-wise stress formulation

    For a test that obtains a set of n images, n 1 imagepairs and n 1 sets of solder joint deformation data canbe obtained upon processing. Let ti be the time instantthat the image i is recorded in a sequence ofi = 0, . . . , n 1, and Dti = ti+1 ti be the ith time inter-val where i = 1, . . . , n. The formulation aims to solvethe shear stress si in the interval Dti assuming that si isconstant. si is related to the elastic and plastic straincel and cpl at ti by Eqs. (2) and (3), respectively. si andthe creep increment Dccri in Dti are related to each otherby integrating Eq. (4) over Dti as follows:

    Dccri ZDti

    _csidt

    ZDti

    CGT i

    sin h a0

    siG

    h inexp

    QkT i

    dt if si > 0

    5

    or

    Dccri ZDti

    C GT i

    sin h a0

    siG

    h in

    exp QkT i

    dt if si < 0 5a

    At the instant ti, the accumulated creep strain ccri is thealgebraic sum of all previous increments, namely

    ccri Xij1

    Dccrj 6

    Combining the Eqs. (2, 3 and 6), si and the measuredtotal shear strain ctli are put in one equation as follows:

    H. Lu et al. / Microelectronics Reliability 46 (2006) 11481159 1153Fig. 6. Measured shear strain vs. time and tting curve: (a) for test package A and (b) for test package B.

  • siG C6 siG

    mXij1

    Dccrj ctli 7

    Knowing all the relevant constitutive constants and test-ing parameters, shear stress si can be solved from Eq. (7).Noting that the inelastic content of the strain is cumula-tive, the stress solution is pursued step-by-step beginningwith the interval Dt1. Eq. (7) is a general form and theimplementation of it needs to consider specic stress con-dition at a respective time instant. This is in particularregarding the sign and the trend of variation of the stress.For instance, given that the plastic strain is instant andcumulative, Eq. (3) applies only up to an instant tk whena positive and increasing stress reaches the peak value.With a declining stress following tk, the plastic strain isheld at cplmax C6 skG

    muntil the stress falls further into

    the negative territory. The change of stress direction sig-nals the sign reversal for both elastic strain and newinelastic strain. When that happens, the new plastic andcreep strain increments must be handled by Eqs. (3a)

    and (5a), respectively. Finally, the total inelastic (plasticplus creep) strain at any current time instant ti is the alge-braic sum of the portions that are reached in the previousperiods and possibly in dierent signs. The stress solutionfrom Eq. (7) is obtained numerically using a computerprogram. Diculties may arise at certain points due tothe discrete and scattering input. To tackle that, ctli inEq. (7) is replaced by the value of a regression functionthat appropriately ts the raw data. Upon solving thestress si the elastic, plastic, and creep strains at ti are sep-arated via Eqs. (2, 3) and (6), respectively, and the creepstrain rate is calculated with Eq. (4).

    4. Case studies

    4.1. Case study A

    Case A is designed to study the solder joint stressrelaxation and the creep behavior. The test prole in

    0

    5

    10

    15

    .)

    Shea

    r stre

    ss (M

    Pa)

    0t (m

    1154 H. Lu et al. / Microelectronics Reliability 46 (2006) 114811590 10 20 30t (min(a)

    0 20 40 60 8-15

    -10

    -5

    0

    5

    10

    15

    Shea

    r stre

    ss (M

    Pa)

    (b)

    Fig. 7. Shear stress solution vs. time curve: (a) fo100 120 140 160 180in.)40 50 60r test package A and (b) for test package B.

  • Fig. 5(a) shows a temperature ramp-up period followedby a dwell period, during which the package tempera-ture increases from the ambient at a rate of 3 C/minfor 30 min, followed by 30 min dwelling at 120 C. Atotal of 31 images are recorded in every 2 min, fromwhich 30 sets of data are obtained. The average strainis calculated based on 3 14 data points in an area of32 lm 44 lm. The strain data of the ramp periodand dwell period are t with a cubic polynomial regres-sion function and a linear function, respectively.

    4.2. Case study B

    Case B aims to study solder joint behavior inresponding to thermal cycling. The test subjects thepackage to two full temperature cycles as shown byFig. 5(b) to simulate a service condition. The tempera-

    ture ramps 3 C/min and dwells at 120 C and 27 C.Each ramp and holding period has 30 and 20 min dura-tion, respectively. A total of 91 images are recorded toyield 90 datasets. The average shear strain at 4 16 datapoints within a 50 lm 44 lm area is calculated for eachtemperature. The stress, the strain rate, and the elastic,plastic and creep strain components in the solder jointllet area are solved. The stressstrain curve is plottedto show the hysteresis loops.

    5. Result presentation and discussion

    5.1. Total shear strain measurement

    A comparison of the strain contours obtained as typ-ically shown in Fig. 5 conrms the shear dominance in

    0 10 20 30 40 50 600

    0.005

    0.01

    0.015

    0.02

    t (min.)

    Cree

    p st

    rain

    Test A, SnAgCu

    (a)

    80

    0.014

    t (m

    H. Lu et al. / Microelectronics Reliability 46 (2006) 11481159 11550 20 40 600

    0.002

    0.004

    0.006

    0.008

    0.01

    0.012

    Cree

    p st

    rain

    (b)

    Fig. 8. Creep shear strain vs. time curve: (a) for100 120 140 160 180

    in.)

    test package A and (b) for test package B.

  • solder joint strain as commonly understood. It is notedthat the CTE mismatch and the temperature variationsubject the solder joint to a displacement/strain con-trolled boundary condition. The solder joint is sand-wiched in between the PCB (printed circuit board) andthe component substrate. Furthermore, the solder layeris two orders of magnitude thinner and much more com-pliant compared with the PCB and the substrate, thedevelopment of the solder joint deformation cannotbut closely follow the boundary displacement that isdominantly determined by the temperature variation.The above rationale appears help explain the trend ofvariation of the measured total strain as given inFig. 6. In case A, the total strain shows no substantialevolution during a 30-min dwell at 120 C. In case B,the strain varies nearly in-phase with the temperatureand the comparison between the strain magnitudes inthe two cycles nds no signicant dierence.

    5.2. Shear stress

    Fig. 7(a) shows for case A that the highest shearstress is about 15 MPa that reaches at 71 C or 16 minentering the ramp-up. The stress relaxes from that pointthrough to the end of the test. For case B, Fig. 7(b) givesthe maximum of 10 MPa that occurs at 72 C or 15 minentering the ramp-up. It is notable that the stress varia-tion in the rst half-cycle in case B resembles the trend incase A. The stress relaxation continues throughout thehigh temperature dwell and it diminishes at a pointshortly after entering the ramp-down period, andchanges the sign. The maximum negative stress isaround 13 MPa that reaches near the end of that per-iod. The variation of the stress is out of phase with thetemperature, and the two stress cycles appear similar.In general, the stress will relax whenever the temperaturedrops or holds. Notably in this study, the relaxation

    0 10 20 30 40 50 600

    0.5

    1

    1.5

    2x 10-5

    t (min.)

    Cree

    p st

    rain

    rate

    (1/s)

    (a)

    80t (m

    1156 H. Lu et al. / Microelectronics Reliability 46 (2006) 114811590 20 40 60-0.5

    0

    0.5

    1

    1.5

    2

    2.5x 10-5

    Cree

    p st

    rain

    rate

    (1/s)

    (b)

    Fig. 9. Creep shear strain rate vs. time curve: (a) fo100 120 140 160 180in.)r test package A and (b) for test package B.

  • happens during temperature ramp-up. This occursbecause that the rate (3 C/min) is insucient to exerton the solder layer a displacement boundary that isneeded to sustain a continued creep under the reachedlevel of stress.

    5.3. Creep strain and creep strain rate

    In both tests, the package temperature stays abovethe initial ambient temperature while varying. The creepstrain accumulates higher unless the stress changes sign.As seen from Fig. 8, the highest creep strain reaches0.017 in case A, and 0.011 in the rst cycle and 0.013in the second cycle in case B. Although the total shearstrain remains more or less similar comparing the twocycles, the creep strain exhibits a modest but apparenttrend of ratcheting. The highest creep strain rate goesup to 0.17 105 s1 in case A and 0.20 105 s1 incase B as seen in Fig. 9. In both cases the sharp fall of

    the creep strain rate starts during the temperature ramp-ing up, and the lowest rate occur during dwelling. Incase B the rate comes negative during the low extremedwell periods.

    5.4. Stressstrain curve, hysteresis loops

    Fig. 10 shows the shear stress vs. total shear straincurves for both cases. The stressstrain hysteresis forcase B is plotted in Fig. 10(b). The second loop notablyoverlaps the rst one, which suggests a quick stabiliza-tion of the hysteresis.

    5.5. Strain energy density

    The strain energy density of 0.146 MJ/m3 is obtainedby numerically calculating the area included in the sec-ond loop in case B.

    H. Lu et al. / Microelectronics Reliability 46 (2006) 11481159 1157Fig. 10. Creep shear stress vs. creep shear strain curves: (a) for test package A and (b) for test package B (hysteresis loops).

  • 6. Summary

    The convective heating used in this experiment isproved a main source to cause disturbance to the sampleimage recording, especially during the temperature dwellwhen non-steady air ow dominates. The imagedistortion thus incurred is the main source responsiblefor the scatter of the measurement. While furtherimprovement is desired and can be realized, the presentstudy nevertheless demonstrates a feasible experimentalapproach that uses a high resolution vision techniqueto track the solder joint deformation in real packagessubject to a thermal process. With suitable material con-stitutive equations, the strain measurement can be ana-lyzed to yield the numerical solution of the stress.With the stress, the creep strain and creep strain rate

    as well as the elastic and plastic strains are also deter-mined. The study also points out a potential applicationof this approach to estimating the thermal creep fatiguelife for solder joints based on the evaluation of the dissi-pated strain energy density.

    The case studies subject the lead-free resistor pack-ages to temperature extremes of 20 and 120 C, dwelllength of 20 or 30 min and ramp rate of 3 C/min. Undersuch circumstances, the results show that the variationof the total shear strain is synchronized with the temper-ature, whereas the shear stress is out of phase due to thestress relaxation. The peak shear stress of the magnitudeof about 1015 MPa occurs at around 70 C in bothcases. The creep strain, up to 0.02 in case A and 0.017in case B, accounts for over 80% of the total strain inboth cases (Fig. 11). Meanwhile the creep strain rate

    astic a

    1158 H. Lu et al. / Microelectronics Reliability 46 (2006) 11481159Fig. 11. Variations of measured shear strain, separated elastic, pl

    (b) for test package B.nd creep component and shear stress: (a) for test package A and

  • reaches the order of magnitude of 105 s1. Respondingto the temperature cycling, the creep strain appears rat-cheting modestly while the stressstrain hysteresisbecomes stabilized quickly. In case B, the per cycle dis-sipated strain energy density of about 0.15 MJ/m3 isobtained upon calculating the area of the second hyster-esis loop.

    and joints. In: Proceedings of 2003 electronic components

    8394.

    [9] Schubert A, Dudek R, Auerswald E, Gollhardt A, ReichlH. Fatigue life models for SnAgCu and SnPb solder jointsevaluated by experiments and simulation. In: Proceedingsof 2003 electronic components and technology conference,2003, p. 60310.

    [10] Yeo A, Lee C, Pang JHL. Flip chip solder joint fatigue lifemodel investigation. In: Proceedings of 2003 electronic

    H. Lu et al. / Microelectronics Reliability 46 (2006) 11481159 1159and technology conference, 2003, p. 22936.[6] Lau J. Dauksher W, Smetana J, Horsley R, Shanguan D,

    Castello T, Menis I, Love D, Sulllivan B. HDPUGs designfor lead-free solder joint reliability of high-density pack-ages. IPC SMEMA Council APEX, 2003.

    [7] Lee WW, Nguyen LT, Selvaduray GS. Solder joint fatiguemodels: review and applicability to chip scale packages.Microelectron Reliab 2000;40:23144.

    [8] Zahn B. Solder joint life model methodology for 63Sn37Pband 95.5Sn4Ag0.5Cu materials. In: Proceedings of 2003electronic components and technology conference, 2003, p.Acknowledgements

    The nancial support from NSERC (Natural Scienceand Engineering Research Council of Canada) andCMAP (Center for Microelectronics Assembly andPackaging of Ontario) is acknowledged. Professor J.Spelt of University of Toronto provided the test vehiclesand the material compositions and properties. Valuablediscussions with him and his students are appreciated.

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    Thermally induced deformation of solder joints in real packages: Measurement and analysisIntroductionSolder joint strain measurementDSC techniqueTest vehicles and sample preparationImage recording and processingTemperature control

    Strain analysis leading to solutions of stress and separation of strain componentsSolder constitutive relationsSolder deformation basicsStep-wise stress formulation

    Case studiesCase study ACase study B

    Result presentation and discussionTotal shear strain measurementShear stressCreep strain and creep strain rateStress ndash strain curve, hysteresis loopsStrain energy density

    SummaryAcknowledgementsReferences

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