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Measurements of Thermo- Mechanical Characteristics of PEMs for Failure Analysis and Reliability Evaluation Measurements of Thermo- Mechanical Characteristics of PEMs for Failure Analysis and Reliability Evaluation Alexander Teverovsky QSS Group, Inc.\Goddard Operations [email protected] Ashok Sharma NASA/GSFC [email protected]

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Measurements of Thermo-Mechanical Characteristics of PEMs for Failure Analysis and Reliability

Evaluation

Measurements of Thermo-Mechanical Characteristics of PEMs for Failure Analysis and Reliability

EvaluationAlexander Teverovsky

QSS Group, Inc.\Goddard [email protected]

Ashok SharmaNASA/GSFC

[email protected]

iMAPS’04 2

PurposePurpose

Review the effect of TM characteristics of MC in PEMs, in particular Tg, on environmental reliability stress testing (HAST and HTSL).Demonstrate the value of TMA for reliability evaluation and failure analysis of plastic encapsulated devices.

Review the effect of TM characteristics of MC in PEMs, in particular Tg, on environmental reliability stress testing (HAST and HTSL).Demonstrate the value of TMA for reliability evaluation and failure analysis of plastic encapsulated devices.

iMAPS’04 3

OutlineOutline

What is Tg and how it can be measured?Typical Tg values and temperatures for reliability testing of PEMs.How Tg might affect reliability stress testing:• HAST• HTSL

Application of TMA for evaluation and FA:• Pop-corning effect in Ta capacitors;• Delaminations after HAST;• Wire bond failures in parts with silicone die

coating.

What is Tg and how it can be measured?Typical Tg values and temperatures for reliability testing of PEMs.How Tg might affect reliability stress testing:• HAST• HTSL

Application of TMA for evaluation and FA:• Pop-corning effect in Ta capacitors;• Delaminations after HAST;• Wire bond failures in parts with silicone die

coating.

iMAPS’04 4

Measurements of the Glass Transition Temperature

Measurements of the Glass Transition Temperature

Tg can be measured using anyProperty = f(T) technique.The value of Tg depends on the used method.Most popular techniques used for Tg measurements: DSC, TMA, DTMA.

Tg can be measured using anyProperty = f(T) technique.The value of Tg depends on the used method.Most popular techniques used for Tg measurements: DSC, TMA, DTMA.

Thermo-mechanical analysis (TMA) is most suitable technique for PEMs. It allows obtaining coefficients of thermal expansion, CTE, and/or analyzing anomalies in package deformations.

Thermo-mechanical analysis (TMA) is most suitable technique for PEMs. It allows obtaining coefficients of thermal expansion, CTE, and/or analyzing anomalies in package deformations.

iMAPS’04 5

TMA MeasurementsTMA Measurements

TMA2940PEM

Quartz probe

Thermocouple

iMAPS’04 6

Typical Screening and Qualification Tests for High-Reliability ApplicationsTypical Screening and Qualification

Tests for High-Reliability ApplicationsTEST BI HTOL TC HAST HTSL

STDMIL-STD-883, TM

1015

MIL-STD-883, TM

1005

MIL-STD-883, TM

1010

JESD22 -A110/118

JESD22-A103B

Typical condition

125 °C 160 hrs

125 °C 1000 hrs

-65 °C to +150 °C

130 °C, 85% RH, 96 hrs

150 °C 1000 hrs

Typical values of Tg for MCs:Multifunctional and orthocresol novolac: Tg ~ 150 to 190 °C.Low mechanical stress biphenyl epoxy: Tg ~ 120 °C. Green molding compounds: Tg ~140 oC

• Some parts are tested at temperatures up to 175 oC.• It is possible that some tests are performed at T>Tg.• Are these tests valid?

• Some parts are tested at temperatures up to 175 oC.• It is possible that some tests are performed at T>Tg.• Are these tests valid?

iMAPS’04 7

Does Thermal Stability of MC Depend on Tg?

Does Thermal Stability of MC Depend on Tg?

TGA for MC with different TgTGA for MC with different Tg TGA measurements of MCs with different Tgshowed that materials with Tg ~135 oC had higher stability compared to MC with Tg ~ 175 oC.The most thermally stable polymers, silicone rubbers and Teflon, have extremely low Tg of-20 to -120 oC for the rubbers and -90 oC for Teflon.

TGA measurements of MCs with different Tgshowed that materials with Tg ~135 oC had higher stability compared to MC with Tg ~ 175 oC.The most thermally stable polymers, silicone rubbers and Teflon, have extremely low Tg of-20 to -120 oC for the rubbers and -90 oC for Teflon.

90

92

94

96

98

100

300 400 500 600temperature, oC

wei

ght,

%

170 C138 C173 C174 C133 CTg~173 oC

Tg~135 oC

Tg is not an indicator of thermal stability of MC

Tg is not an indicator of thermal stability of MC

iMAPS’04 8

HAST: Mechanisms of Tg EffectHAST: Mechanisms of Tg Effect

Compression caused by the shrinkage of encapsulantprevents water needed for corrosion from accumulating at the bond pad surface. At T>Tg, the probability of delaminations increases.Mechanical stresses in the presence of moisture:

Compression caused by the shrinkage of encapsulantprevents water needed for corrosion from accumulating at the bond pad surface. At T>Tg, the probability of delaminations increases.Mechanical stresses in the presence of moisture:

[ ]δαασ ×−−×−×∝ CMETTgE SiMC )()(

Moisture swelling might have an effect equivalent to temperature increase on 50 to 70 oC.

Moisture swelling might have an effect equivalent to temperature increase on 50 to 70 oC.

iMAPS’04 9

HAST: Test ResultsHAST: Test Results24 part types encapsulated in different plastic packages (mostly linear devices) were tested in a HAST chamber.Test conditions:130 oC, 85% RH, 250 hrs under bias.Sample size: 30 pcs.

24 part types encapsulated in different plastic packages (mostly linear devices) were tested in a HAST chamber.Test conditions:130 oC, 85% RH, 250 hrs under bias.Sample size: 30 pcs.

HAST failures for differentPEMs vs. Tg of MCs

HAST failures for differentPEMs vs. Tg of MCs

020406080

100

120 130 140 150 160 170 180

Tg, oC

HA

ST fa

ilure

s, %

• No correlation between Tg and HAST failures.• Tg is not the major factor; however, it might affect test

results.

• No correlation between Tg and HAST failures.• Tg is not the major factor; however, it might affect test

results.

iMAPS’04 10

HAST: FA ResultsHAST: FA Results

SOIC16 SSOP28 TO220

•Excessive delaminations after HAST is a common effect in PEMs.

•The probability of delaminations might depend on Tg.•Delaminations might introduce new failure mechanisms.

•Excessive delaminations after HAST is a common effect in PEMs.

•The probability of delaminations might depend on Tg.•Delaminations might introduce new failure mechanisms.

Acoustic microscopy of parts before (left) and after (right) HAST at 130 oC/85% RH/96 hrs.

iMAPS’04 11

HTSL: WB Degradation, Mechanism IHTSL: WB Degradation, Mechanism I

Au/Al WB degradation limits reliability of PEMs at high temperatures.Degradation mechanism involves:• release of chemically active molecules from

MC; • diffusion of the molecules to bonds;• chemical reaction with the Al/Au intermetallic

(dry corrosion).If diffusion limits the process, then exceedingTg might accelerate transport of the corrosive molecules.

Au/Al WB degradation limits reliability of PEMs at high temperatures.Degradation mechanism involves:• release of chemically active molecules from

MC; • diffusion of the molecules to bonds;• chemical reaction with the Al/Au intermetallic

(dry corrosion).If diffusion limits the process, then exceedingTg might accelerate transport of the corrosive molecules.

intermetallic

voids

• There is no evidence that diffusion of corrosive molecules is the limiting factor of the process.

• D(T) characteristics are not known.

• There is no evidence that diffusion of corrosive molecules is the limiting factor of the process.

• D(T) characteristics are not known.

iMAPS’04 12

HTSL: WB Degradation, Experimental Data

HTSL: WB Degradation, Experimental Data

Arrhenius plots for mean life of parametric and WB failures,

175 <T< 225 oC

Arrhenius plots for mean life of parametric and WB failures,

175 <T< 225 oC

At T < 190 oC:Ea ~1.3 to 1.8 eV.

At 190 < T < 225 oCEa ~0.55 to 0.68 eV.

Different activation energies below and above Tc ~190 oCindicate changes in degradation mechanism.

At T < 190 oC:Ea ~1.3 to 1.8 eV.

At 190 < T < 225 oCEa ~0.55 to 0.68 eV.

Different activation energies below and above Tc ~190 oCindicate changes in degradation mechanism.

100

1000

10000

100000

0.0019 0.002 0.0021 0.0022 0.00231/T, 1/K

mea

n lif

e, h

r

OP WBAD WBAD paramOP param

iMAPS’04 13

WB degradation: Mechanism II.WB degradation: Mechanism II.Discoloration of MC after HTSL

voids insideWB and alongthe periphery

T < Tc

T > Tc

air path

Discoloration of MC after HTSL

voids insideWB and alongthe periphery

T < Tc

T > Tc

air path

MC tinted not only along the surface of the package, but also along the lead frame, die, and wire bonds.

At HT there is a free pass allowing air to reach internal areas of the package.

A gap is forming at a critical temperature Tc > Tg to allow thermo-oxidative degradation of MC in vicinity of WB.

MC tinted not only along the surface of the package, but also along the lead frame, die, and wire bonds.

At HT there is a free pass allowing air to reach internal areas of the package.

A gap is forming at a critical temperature Tc > Tg to allow thermo-oxidative degradation of MC in vicinity of WB.

iMAPS’04 14

Anomalies during TMA Measurements

Anomalies during TMA Measurements

Factors affecting Tg and CTE measurements on PEMs:Warpage;Stress relief;Moisture;Lead frame;Temperature rate;Cooling vs. heating

Factors affecting Tg and CTE measurements on PEMs:Warpage;Stress relief;Moisture;Lead frame;Temperature rate;Cooling vs. heating

TMA curves measured directly on PEMs

TMA curves measured directly on PEMs

Can anomalies in TMA be used to evaluate possible reliability problems?

Can anomalies in TMA be used to evaluate possible reliability problems?

iMAPS’04 15

TMA application: Pop-corning in chip Ta capacitors?

TMA application: Pop-corning in chip Ta capacitors?

4.7 uF RT storageCycling to 200, 220, 230, and 240 oC

15 min bake at each extreme T

-505

101520253035

0 50 100 150 200 250Temperature, oC

Defo

rmat

ion,

µm 4.7 uF RT storage

Cycling to 200, 220, 230, and 240 oC15 min bake at each extreme T

-505

101520253035

0 50 100 150 200 250Temperature, oC

Defo

rmat

ion,

µm

22 uF Cycling to 220 oC

15 min bake at extreme T

-5

15

35

55

75

95

115

0 50 100 150 200 250

Temperature, oC

Def

orm

atio

n, µ

m

RT storagePCT 121 oC/100% RH

22 uF Cycling to 220 oC

15 min bake at extreme T

-5

15

35

55

75

95

115

0 50 100 150 200 250

Temperature, oC

Def

orm

atio

n, µ

m

RT storagePCT 121 oC/100% RH

condition N Average Std. Dev.long RT 5 17.61 3.72

vacuum storage 3 3.85 5.38121oC/100% RH 4 17.53 8.65

Amplitude of spikes, µm

Deformation spikes were observed during first heating up cycles (20 0C/min).There is a trend of increasing amplitude of spikes after moisture sorption.

Deformation spikes were observed during first heating up cycles (20 0C/min).There is a trend of increasing amplitude of spikes after moisture sorption.

Deformationspikes

iMAPS’04 16

TMA application: HAST-induced delaminations

TMA application: HAST-induced delaminations

Background: Multiple CSAM failures of PEMs in SOT-23-5 packages were observed after HAST.

FA purpose: Why, and is there a reliability concern?

Background: Multiple CSAM failures of PEMs in SOT-23-5 packages were observed after HAST.

FA purpose: Why, and is there a reliability concern?

Acoustic images after HASTTop side view Bottom side view

Acoustic images after HASTTop side view Bottom side view

iMAPS’04 17

HAST-induced delaminations. Cont’d.HAST-induced delaminations. Cont’d.

TMA ~1000 hrs after HAST. The time for moisture diffusion:τ = L2/4D = 520 hrs => Excessive moisture should have been released. => HAST caused irreversible swelling.

TMA ~1000 hrs after HAST. The time for moisture diffusion:τ = L2/4D = 520 hrs => Excessive moisture should have been released. => HAST caused irreversible swelling.

TMA of 3 sampleBefore HAST After HAST

TMA of 3 sampleBefore HAST After HAST

Hysteresiscondition

avr. std.dev.before HAST 0.21 0.048after HAST 0.12 0.05

dL/L, %• Swelling of MC was the reason

for excessive delaminations after HAST.

• The swelling caused creep of MC, which resulted in delaminationseven after moisture release.

• Swelling of MC was the reason for excessive delaminations after HAST.

• The swelling caused creep of MC, which resulted in delaminationseven after moisture release.

iMAPS’04 18

How critical delaminations are?How critical delaminations are?

To evaluate the risk related to delaminations, three groups of parts were subjected to preconditioning according to JEDEC JESD22-A113 (three runs through the solder reflow chamber) and 1000 temperature cycles from-55 oC to 125 oC.

To evaluate the risk related to delaminations, three groups of parts were subjected to preconditioning according to JEDEC JESD22-A113 (three runs through the solder reflow chamber) and 1000 temperature cycles from-55 oC to 125 oC.

Effect of TC on electrical characteristics

Effect of TC on electrical characteristics

0

0.5

1

1.5

2

2.5

init SMT220

100 TC 300 TC 1000TC

VOS,

mV

HAST SCAM failures DC0018screening CSAM failures DC 0018Uscreened DC00 20

• No failures during TC.• The parts manifested only minor changes in electrical

characteristics.

• No failures during TC.• The parts manifested only minor changes in electrical

characteristics.

iMAPS’04 19

Delaminations at Secondary BondsDelaminations at Secondary Bonds

• Delamination at gold-to-silver wire bonding at finger tips of leads is a common defect in PEMs.

• Secondary bonds are strong enough to provide reliable connection even in the presence of delaminations.

• Delamination at gold-to-silver wire bonding at finger tips of leads is a common defect in PEMs.

• Secondary bonds are strong enough to provide reliable connection even in the presence of delaminations.

Cross-section of a typical secondary bond delaminationindicates a gap above the bond area

Silver plating

iMAPS’04 20

TMA application: wire bond failures during TC

TMA application: wire bond failures during TC

PEM failures at two TC conditions

PEM failures at two TC conditions

TC conditions (25 samples in each group):• Low T range: -40 to

+105 °C• High T range: -65 to

+155 °C . Electrical tests: after 30, 100, 300, and 1000 cycles.Parts: PEMs in DIP16 packages.Catastrophic failures in both TC conditions.

TC conditions (25 samples in each group):• Low T range: -40 to

+105 °C• High T range: -65 to

+155 °C . Electrical tests: after 30, 100, 300, and 1000 cycles.Parts: PEMs in DIP16 packages.Catastrophic failures in both TC conditions.

0

20

40

60

80

100

1 10 100 1000

Number of cycles

Failu

res,

%

0

2

4

6

8

10

Failu

res,

%

-65 +155-40 +105

iMAPS’04 21

X-ray and cross-sectioning confirmed wire bond fracturesX-ray and cross-sectioning confirmed wire bond fractures

Wire bond failures during TC. Cont’d.Wire bond failures during TC. Cont’d.

Silicone die coating

Pictures courtesy of F.Felt

NormalpartNormalpart

FailedpartFailedpart

fractures

iMAPS’04 22

Wire bond failures during TC. Cont’d.Wire bond failures during TC. Cont’d.

TMA showed that package deformation above silicone is

much larger

TMA showed that package deformation above silicone is

much larger

Silicone MC

Deformation of the silicone coating caused significant strains in bonding wires, which might result in fractures.

Silicone MC

Deformation of the silicone coating caused significant strains in bonding wires, which might result in fractures.

iMAPS’04 23

Mechanism of WB Failures During TC.Mechanism of WB Failures During TC.•LT: silicone shrinks, clamps

the wire and pools it from MC.•HT: the clamp is released and

silicone slides along the wire.•Repeat cycling eventually

causes fracture.

•LT: silicone shrinks, clamps the wire and pools it from MC.

•HT: the clamp is released and silicone slides along the wire.

•Repeat cycling eventually causes fracture.

Low T

High T Low T

RT

fracture

MC

silicone

Elongation of Au wires ~ 3 to 6 %. =>This type of failures is more likely to happen with thick enough layers of die coating.Elongation of Au wires ~ 3 to 6 %. =>This type of failures is

more likely to happen with thick enough layers of die coating.

iMAPS’04 24

ConclusionsConclusions

Accelerated stress testing at T > Tg might introduce new failure mechanisms and should be considered for analysis of long-term reliability of PEMs based on high-temperature testing.TMA is a useful tool for reliability evaluation and failure analysis of plastic encapsulated devices.Swelling of MC increases the probability of delaminations during testing at T ~ Tg and might affect results of HAST.The thickness of silicone die coatings affects deformation of PEMs and the probability of wire bonds failures.

Accelerated stress testing at T > Tg might introduce new failure mechanisms and should be considered for analysis of long-term reliability of PEMs based on high-temperature testing.TMA is a useful tool for reliability evaluation and failure analysis of plastic encapsulated devices.Swelling of MC increases the probability of delaminations during testing at T ~ Tg and might affect results of HAST.The thickness of silicone die coatings affects deformation of PEMs and the probability of wire bonds failures.