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Temperature Cycling and Fatigue in Electronics 
Cheryl Tulkoff, ASQ CRE 
DfR Solutions 
Senior Member of the Technical Staff 
ctulkoff@dfrsolutions.com 
SMTAI 2014 
Rosemont, Il 
1
Abstract 
The majority of electronic failures occur due to thermally induced stresses and strains caused by excessive differences in coefficients of thermal expansion (CTE) across materials. 
CTE mismatches occur in both 1st and 2nd level interconnects in electronics assemblies. 
1st level interconnects connect the die to a substrate. 
This substrate can be underfilled so there are both global and local CTE mismatches to consider. 
2nd level interconnects connect the substrate, or package, to the printed circuit board (PCB). This would be considered a “board level” CTE mismatch. 
Several stress and strain mitigation techniques exist including the use of conformal coating. 
The purpose of this presentation is to show that accelerated testing can be successfully used to predict solder joint and plated through hole (PTH) fatigue behavior. 
2
Describes the potential for product failure when subjected to periodic changes in environmental stress or an overstress event that are thermal or mechanical in nature 
What types of thermal or mechanical stress could cause failure in today’s electronics? 
Focus in this presentation is temperature cycling 
Thermo/Mechanical Reliability 
3
Due to Solar Loading 
Temperature Cycling 
Due to Power Dissipation 
4
Failures are not always about electrical overstress (EOS)! 
Recent studies suggest that the majority of electronic failures are thermo-mechanically related* 
Why Care About Temperature Cycling? 
*Wunderle, B. and B. Michel, “Progress in Reliability Research in Micro and Nano Region”, Microelectronics and Reliability, V46, Issue 9-11, 2006. 
5
Why Care About Temperature Cycling? 
Everything is Hot 
Everything is Mobile 
Everything is Everywhere 
M2M Technology 
6
Use many different materials 
Semiconductors, Ceramics, Metals, Polymers 
Bond these different materials together 
Plating, Solder, Adhesive 
Materials expand/contract at different rates 
Why Do Electronics Fail Under Temperature Cycling? 
7
Why do Solder Joints Fail under Temperature Cycling? 
Two different expansion/contraction behaviors 
Because solder is connecting two materials that are expanding / contracting at different rates (GLOBAL) 
Because solder is expanding / contracting at a different rate than the material to which it is connected (LOCAL) 
8
Differential expansion and contraction introduces stress into the solder joint 
Stress causes the solder to deform (aka, elastic and plastic strain) 
Extent of this strain (that is, strain range or strain energy) tells us the lifetime of the solder joint 
Higher the strain, the more the solder joint is damaged, the shorter the lifetime 
Why do Solder Joints Fail under Temperature Cycling? (cont.) 
9
Knowing the critical drivers for solder joint fatigue allows development of predictive models and design rules 
Drivers for Solder Joint Thermo- Mechanical Failures 
CTE of Board 
Elastic Modulus (Compliance) of Board 
CTE of Component Elastic Modulus (Compliance) of Component Length of Component 
Volume of Solder 
Thickness of Solder 
Solder Fatigue Properties 
10
CTE Mismatch 
Effect of CTE Mismatch on Solder Joint Strain 
11
Typical Field Conditions 
Field Conditions for Various Industries 
IPC-SM-785, Guidelines for Accelerated Reliability Testing of Surface Mount Solder Attachments 
12
JESD47G Conditions Used in Accelerated Tests 
13 
Stress-Test-Driven Qualification of Integrated Circuits, Nonhermetic package temperature cycling requirements
Mfg Provided Laminate Properties 
Weave Illustration showing X and Y Fiber Orientation in FR-4 
Isola 370HR Laminate and Prepreg Datasheet, http://www.isola- group.com/wp-content/uploads/2014/04/370HR-Laminate-and-Prepreg-Data- Sheet-Isola.pdf 
14
Out-of-plane CTE (CTEz) is almost always provided on the laminate datasheet 
Sometimes in ppm/C above and below the Tg 
Sometimes in % between 50-260C 
Out-of-plane modulus (Ez) is almost never provided on the laminate datasheet 
Requires calculation based on in-plane laminate properties, glass fiber properties, glass fiber volume fraction, and Rule-of-Mixtures / Halpin-Tsai models 
Laminate Datasheets 
1/Elaminate = Vepoxy/Eepoxy + Vfiber/Efiber 
15
Impact of Glass Style on Modulus of Elasticity & CTE 
16
Solder Joint Structure 
Solder Joint Structure: BGAs, BTCs. 
Filleted Solder Joint Structure 
17
Solder Fatigue Crack Formation 
Grains grow as the solder joint is stressed 
Growing grains cause micro-voids to appear at the grain boundaries 
Micro-voids connect with each other to create micro-cracks and eventually macro-cracks 
Solder joints in Electronics: Design for Reliability, Werner Engelmaier 
18
Knowing the drivers and how to predict provides powerful insight to the design process 
Identify which designs and environments are at potential risk of solder joint fatigue 
Quantitatively benchmark material changes 
Develop accurate accelerated life tests 
Thermo-Mechanical Design Rules 
19
Predictive Models – Physics of 
Failure (PoF) 
 Modified Engelmaier for Pb-free Solder (SAC305) 
 Semi-empirical analytical approach 
 Energy based fatigue 
 Determine the strain range (Dg) 
 C is a correction factor that is a function of dwell time 
and temperature, LD is diagonal distance, a is 
coefficient of thermal expansion (CTE), DT is 
temperature cycle, h is solder joint height 
T 
h 
L 
C 
s 
D Dg  DaD 
20
Predictive Models – Physics of 
Failure (PoF)(cont.) 
 Determine the shear force applied to the solder joint 
 F is shear force, L is length, E is elastic modulus, A is 
the area, h is thickness, G is shear modulus, and a is edge 
length of bond pad 
 Subscripts: 1 is component, 2 is board, s is solder joint, c 
is bond pad, and b is board 
 Takes into consideration foundation stiffness and 
both shear and axial loads 
    
 
 
  
 
 
  
 
 
  
 
 
 
 
 D        
A G G a 
h 
A G 
h 
E A 
L 
E A 
L 
T L F 
c c b 
c 
s s 
s 
9 
2 
1 1 2 2 
2 1 
 
a a 
21
Predictive Models – Physics of 
Failure (PoF)(cont.) 
 Determine the strain energy dissipated by the 
solder joint 
 Calculate cycles-to-failure (N50), using energy 
based fatigue models 
  1 0.0019  N  DW f 
s A 
F 
DW  0.5Dg  
22
Glass Style Impact on Fatigue Life for 2512 Resistors 
23
Modeling Works 
24
25 
Thermal Cycling: SnPb vs. SAC 
Where does SnPb outperform Pb-free? 
Leadless, ceramic components 
Leadless ceramic chip carriers (crystals, oscillators, resistor networks, etc.) 
SMT resistors 
Ceramic BGAs 
Severe temperature cycles 
-40 to 125ºC 
-55 to 125ºC 
Syed, Amkor 
“Overview of Reliability Models and Data Needs,” Ahmer Syed, Amkor Technology
Time to 1% Failure for 2512 Resistors Attached with SAC and SnPb Solder 
Time to 1% Failure for TSOPs attached with SAC and SnPb with Long Dwells (8 hours) 
26 
•At small changes in temperature, SnPb fails first but performs better at higher temperature changes 
•Longer dwell times allow more stress relaxation of solder and are thought to cause more damage as a result 
•Longer dwell times at higher temperatures also cause more damage than long dwell times at low temperatures
The dominant failure mode in PTH tends to be barrel fatigue 
Barrel fatigue is the circumferential cracking of the copper plating that forms the PTH wall 
Driven by differential expansion between the copper plating (~17 ppm) and the out-of-plane CTE of the printed board (~70 ppm) 
How do PTH’s Fail? 
27
Historically, two material properties of concern 
Out-of-plane coefficient of thermal expansion (CTEz) 
Out-of-plane elastic modulus (‘stiffness’)(Ez) 
Key Assumption: No exposure to temperatures above the glass transition temperature (Tg) 
The two material properties (CTE and E) are driven by choices in resin, glass style, and filler 
PCB Materials and PTH Reliability 
28
Round Robin Reliability Evaluation of Small Diameter (<20 mil) Plated Through Holes in PWBs 
Activity initiated by IPC and published in 1988 
Objectives 
Confirm sufficient reliability 
Benchmark different test procedures 
Evaluate influence of PTH design and plating (develop a model) 
IPC TR-579 
29
IPC TR-579 (cont.) 
Determine stress applied (σ) 
Assumes perfectly elastic deformation when below yield strength (Sy) 
Linear stress-strain relationship above Sy 
h 
PTV Height 
d 
PTV Diameter 
t 
Plating Thickness 
E 
Elastic Modululs 
a 
Coefficient of Thermal Expansion 
T 
Temperature (oC) 
30
IPC TR-579 (cont.) 
Determine strain range (Δε) 
31
IPC-TR-579 (Calibration Constants) 
Strain distribution factor, Kd (2.5 –5.0) 
2.5 recommended 
Quality index, KQ (0 –10) 
Extraordinary (KQ = 10) 
Superior (KQ = 8.7) 
Good (KQ = 6.7) 
Marginal (KQ = 4.8) 
Poor (KQ = 3.5) 
Some companies assume KQ = 5 
32
Influence of Glass Style on Properties 
Glass Style 
Modulus of Elasticity Ez (MPa) 
CTEz (ppm) 
1027 
4380.4 
73.9 
1037 
4380.4 
73.9 
106 
4478.2 
72.3 
1067 
4478.2 
72.3 
1035 
4528.7 
71.5 
1078 
4580.3 
70.7 
1080 
4742.7 
68.4 
1086 
4799.3 
67.6 
2313 
5040.4 
64.4 
2113 
5170.2 
62.8 
2116 
5237.6 
62.0 
3313 
5237.6 
62.0 
3070 
5450.9 
59.7 
1647 
5603.1 
58.1 
1651 
5603.1 
58.1 
2165 
5603.1 
58.1 
2157 
5603.1 
58.1 
7628 
5764.0 
56.5 
33
Glass Style Influence on PTH Fatigue 
34
Majority of failures in electronics are caused by thermo-mechanical loads 
Solder fatigue is the major failure mechanism 
CTE mismatch between the board, component and attach materials creates stresses in the solder and the plating material 
Experimental data for solder fatigue predictions and basic models can be used to predict solder fatigue for surface mount components 
Conclusions 
35 
35
PCB designers can change component placement and board laminate material to alleviate fatigue since component level design changes are usually not an option 
PCB design also affects PTH reliability. 
PCB designer influences PTH reliability by modifying drill diameters, laminate material, and plating parameters. 
Solder and PTH fatigue are just two of the many effects of thermo-mechanical loads but they can be predicted and prevented 
Conclusions 
36
Presenter Biography 
Cheryl has over 20 years of experience in electronics manufacturing focusing on failure analysis and reliability. She is passionate about applying her unique background to enable her clients to maximize and accelerate product design and development while saving time, managing resources, and improving customer satisfaction. 
Throughout her career, Cheryl has had extensive training experience and is a published author and a senior member of both ASQ and IEEE. She views teaching as a two-way process that enables her to impart her knowledge on to others as well as reinforce her own understanding and ability to explain complex concepts through student interaction. A passionate advocate of continued learning, Cheryl has taught electronics workshops that introduced her to numerous fascinating companies, people, and cultures. 
Cheryl has served as chairman of the IEEE Central Texas Women in Engineering and IEEE Accelerated Stress Testing and Reliability sections and is an ASQ Certified Reliability Engineer, an SMTA Speaker of Distinction and serves on ASQ, IPC and iNEMI committees. 
Cheryl earned her Bachelor of Mechanical Engineering degree from Georgia Tech and is currently a student in the UT Austin Masters of Science in Technology Commercialization (MSTC) program. She was drawn to the MSTC program as an avenue that will allow her to acquire relevant and current business skills which, combined with her technical background, will serve as a springboard enabling her clients to succeed in introducing reliable, blockbuster products tailored to the best market segment. 
In her free time, Cheryl loves to run! She’s had the good fortune to run everything from 5k’s to 100 milers including the Boston Marathon, the Tahoe Triple (three marathons in 3 days) and the nonstop Rocky Raccoon 100 miler. She also enjoys travel and has visited 46 US states and over 20 countries around the world. Cheryl combines these two passions in what she calls “running tourism” which lets her quickly get her bearings and see the sights in new places. 
37

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Temperature Cycling and Fatigue in Electronics

  • 1. Temperature Cycling and Fatigue in Electronics Cheryl Tulkoff, ASQ CRE DfR Solutions Senior Member of the Technical Staff ctulkoff@dfrsolutions.com SMTAI 2014 Rosemont, Il 1
  • 2. Abstract The majority of electronic failures occur due to thermally induced stresses and strains caused by excessive differences in coefficients of thermal expansion (CTE) across materials. CTE mismatches occur in both 1st and 2nd level interconnects in electronics assemblies. 1st level interconnects connect the die to a substrate. This substrate can be underfilled so there are both global and local CTE mismatches to consider. 2nd level interconnects connect the substrate, or package, to the printed circuit board (PCB). This would be considered a “board level” CTE mismatch. Several stress and strain mitigation techniques exist including the use of conformal coating. The purpose of this presentation is to show that accelerated testing can be successfully used to predict solder joint and plated through hole (PTH) fatigue behavior. 2
  • 3. Describes the potential for product failure when subjected to periodic changes in environmental stress or an overstress event that are thermal or mechanical in nature What types of thermal or mechanical stress could cause failure in today’s electronics? Focus in this presentation is temperature cycling Thermo/Mechanical Reliability 3
  • 4. Due to Solar Loading Temperature Cycling Due to Power Dissipation 4
  • 5. Failures are not always about electrical overstress (EOS)! Recent studies suggest that the majority of electronic failures are thermo-mechanically related* Why Care About Temperature Cycling? *Wunderle, B. and B. Michel, “Progress in Reliability Research in Micro and Nano Region”, Microelectronics and Reliability, V46, Issue 9-11, 2006. 5
  • 6. Why Care About Temperature Cycling? Everything is Hot Everything is Mobile Everything is Everywhere M2M Technology 6
  • 7. Use many different materials Semiconductors, Ceramics, Metals, Polymers Bond these different materials together Plating, Solder, Adhesive Materials expand/contract at different rates Why Do Electronics Fail Under Temperature Cycling? 7
  • 8. Why do Solder Joints Fail under Temperature Cycling? Two different expansion/contraction behaviors Because solder is connecting two materials that are expanding / contracting at different rates (GLOBAL) Because solder is expanding / contracting at a different rate than the material to which it is connected (LOCAL) 8
  • 9. Differential expansion and contraction introduces stress into the solder joint Stress causes the solder to deform (aka, elastic and plastic strain) Extent of this strain (that is, strain range or strain energy) tells us the lifetime of the solder joint Higher the strain, the more the solder joint is damaged, the shorter the lifetime Why do Solder Joints Fail under Temperature Cycling? (cont.) 9
  • 10. Knowing the critical drivers for solder joint fatigue allows development of predictive models and design rules Drivers for Solder Joint Thermo- Mechanical Failures CTE of Board Elastic Modulus (Compliance) of Board CTE of Component Elastic Modulus (Compliance) of Component Length of Component Volume of Solder Thickness of Solder Solder Fatigue Properties 10
  • 11. CTE Mismatch Effect of CTE Mismatch on Solder Joint Strain 11
  • 12. Typical Field Conditions Field Conditions for Various Industries IPC-SM-785, Guidelines for Accelerated Reliability Testing of Surface Mount Solder Attachments 12
  • 13. JESD47G Conditions Used in Accelerated Tests 13 Stress-Test-Driven Qualification of Integrated Circuits, Nonhermetic package temperature cycling requirements
  • 14. Mfg Provided Laminate Properties Weave Illustration showing X and Y Fiber Orientation in FR-4 Isola 370HR Laminate and Prepreg Datasheet, http://www.isola- group.com/wp-content/uploads/2014/04/370HR-Laminate-and-Prepreg-Data- Sheet-Isola.pdf 14
  • 15. Out-of-plane CTE (CTEz) is almost always provided on the laminate datasheet Sometimes in ppm/C above and below the Tg Sometimes in % between 50-260C Out-of-plane modulus (Ez) is almost never provided on the laminate datasheet Requires calculation based on in-plane laminate properties, glass fiber properties, glass fiber volume fraction, and Rule-of-Mixtures / Halpin-Tsai models Laminate Datasheets 1/Elaminate = Vepoxy/Eepoxy + Vfiber/Efiber 15
  • 16. Impact of Glass Style on Modulus of Elasticity & CTE 16
  • 17. Solder Joint Structure Solder Joint Structure: BGAs, BTCs. Filleted Solder Joint Structure 17
  • 18. Solder Fatigue Crack Formation Grains grow as the solder joint is stressed Growing grains cause micro-voids to appear at the grain boundaries Micro-voids connect with each other to create micro-cracks and eventually macro-cracks Solder joints in Electronics: Design for Reliability, Werner Engelmaier 18
  • 19. Knowing the drivers and how to predict provides powerful insight to the design process Identify which designs and environments are at potential risk of solder joint fatigue Quantitatively benchmark material changes Develop accurate accelerated life tests Thermo-Mechanical Design Rules 19
  • 20. Predictive Models – Physics of Failure (PoF)  Modified Engelmaier for Pb-free Solder (SAC305)  Semi-empirical analytical approach  Energy based fatigue  Determine the strain range (Dg)  C is a correction factor that is a function of dwell time and temperature, LD is diagonal distance, a is coefficient of thermal expansion (CTE), DT is temperature cycle, h is solder joint height T h L C s D Dg  DaD 20
  • 21. Predictive Models – Physics of Failure (PoF)(cont.)  Determine the shear force applied to the solder joint  F is shear force, L is length, E is elastic modulus, A is the area, h is thickness, G is shear modulus, and a is edge length of bond pad  Subscripts: 1 is component, 2 is board, s is solder joint, c is bond pad, and b is board  Takes into consideration foundation stiffness and both shear and axial loads                      D        A G G a h A G h E A L E A L T L F c c b c s s s 9 2 1 1 2 2 2 1  a a 21
  • 22. Predictive Models – Physics of Failure (PoF)(cont.)  Determine the strain energy dissipated by the solder joint  Calculate cycles-to-failure (N50), using energy based fatigue models   1 0.0019  N  DW f s A F DW  0.5Dg  22
  • 23. Glass Style Impact on Fatigue Life for 2512 Resistors 23
  • 25. 25 Thermal Cycling: SnPb vs. SAC Where does SnPb outperform Pb-free? Leadless, ceramic components Leadless ceramic chip carriers (crystals, oscillators, resistor networks, etc.) SMT resistors Ceramic BGAs Severe temperature cycles -40 to 125ºC -55 to 125ºC Syed, Amkor “Overview of Reliability Models and Data Needs,” Ahmer Syed, Amkor Technology
  • 26. Time to 1% Failure for 2512 Resistors Attached with SAC and SnPb Solder Time to 1% Failure for TSOPs attached with SAC and SnPb with Long Dwells (8 hours) 26 •At small changes in temperature, SnPb fails first but performs better at higher temperature changes •Longer dwell times allow more stress relaxation of solder and are thought to cause more damage as a result •Longer dwell times at higher temperatures also cause more damage than long dwell times at low temperatures
  • 27. The dominant failure mode in PTH tends to be barrel fatigue Barrel fatigue is the circumferential cracking of the copper plating that forms the PTH wall Driven by differential expansion between the copper plating (~17 ppm) and the out-of-plane CTE of the printed board (~70 ppm) How do PTH’s Fail? 27
  • 28. Historically, two material properties of concern Out-of-plane coefficient of thermal expansion (CTEz) Out-of-plane elastic modulus (‘stiffness’)(Ez) Key Assumption: No exposure to temperatures above the glass transition temperature (Tg) The two material properties (CTE and E) are driven by choices in resin, glass style, and filler PCB Materials and PTH Reliability 28
  • 29. Round Robin Reliability Evaluation of Small Diameter (<20 mil) Plated Through Holes in PWBs Activity initiated by IPC and published in 1988 Objectives Confirm sufficient reliability Benchmark different test procedures Evaluate influence of PTH design and plating (develop a model) IPC TR-579 29
  • 30. IPC TR-579 (cont.) Determine stress applied (σ) Assumes perfectly elastic deformation when below yield strength (Sy) Linear stress-strain relationship above Sy h PTV Height d PTV Diameter t Plating Thickness E Elastic Modululs a Coefficient of Thermal Expansion T Temperature (oC) 30
  • 31. IPC TR-579 (cont.) Determine strain range (Δε) 31
  • 32. IPC-TR-579 (Calibration Constants) Strain distribution factor, Kd (2.5 –5.0) 2.5 recommended Quality index, KQ (0 –10) Extraordinary (KQ = 10) Superior (KQ = 8.7) Good (KQ = 6.7) Marginal (KQ = 4.8) Poor (KQ = 3.5) Some companies assume KQ = 5 32
  • 33. Influence of Glass Style on Properties Glass Style Modulus of Elasticity Ez (MPa) CTEz (ppm) 1027 4380.4 73.9 1037 4380.4 73.9 106 4478.2 72.3 1067 4478.2 72.3 1035 4528.7 71.5 1078 4580.3 70.7 1080 4742.7 68.4 1086 4799.3 67.6 2313 5040.4 64.4 2113 5170.2 62.8 2116 5237.6 62.0 3313 5237.6 62.0 3070 5450.9 59.7 1647 5603.1 58.1 1651 5603.1 58.1 2165 5603.1 58.1 2157 5603.1 58.1 7628 5764.0 56.5 33
  • 34. Glass Style Influence on PTH Fatigue 34
  • 35. Majority of failures in electronics are caused by thermo-mechanical loads Solder fatigue is the major failure mechanism CTE mismatch between the board, component and attach materials creates stresses in the solder and the plating material Experimental data for solder fatigue predictions and basic models can be used to predict solder fatigue for surface mount components Conclusions 35 35
  • 36. PCB designers can change component placement and board laminate material to alleviate fatigue since component level design changes are usually not an option PCB design also affects PTH reliability. PCB designer influences PTH reliability by modifying drill diameters, laminate material, and plating parameters. Solder and PTH fatigue are just two of the many effects of thermo-mechanical loads but they can be predicted and prevented Conclusions 36
  • 37. Presenter Biography Cheryl has over 20 years of experience in electronics manufacturing focusing on failure analysis and reliability. She is passionate about applying her unique background to enable her clients to maximize and accelerate product design and development while saving time, managing resources, and improving customer satisfaction. Throughout her career, Cheryl has had extensive training experience and is a published author and a senior member of both ASQ and IEEE. She views teaching as a two-way process that enables her to impart her knowledge on to others as well as reinforce her own understanding and ability to explain complex concepts through student interaction. A passionate advocate of continued learning, Cheryl has taught electronics workshops that introduced her to numerous fascinating companies, people, and cultures. Cheryl has served as chairman of the IEEE Central Texas Women in Engineering and IEEE Accelerated Stress Testing and Reliability sections and is an ASQ Certified Reliability Engineer, an SMTA Speaker of Distinction and serves on ASQ, IPC and iNEMI committees. Cheryl earned her Bachelor of Mechanical Engineering degree from Georgia Tech and is currently a student in the UT Austin Masters of Science in Technology Commercialization (MSTC) program. She was drawn to the MSTC program as an avenue that will allow her to acquire relevant and current business skills which, combined with her technical background, will serve as a springboard enabling her clients to succeed in introducing reliable, blockbuster products tailored to the best market segment. In her free time, Cheryl loves to run! She’s had the good fortune to run everything from 5k’s to 100 milers including the Boston Marathon, the Tahoe Triple (three marathons in 3 days) and the nonstop Rocky Raccoon 100 miler. She also enjoys travel and has visited 46 US states and over 20 countries around the world. Cheryl combines these two passions in what she calls “running tourism” which lets her quickly get her bearings and see the sights in new places. 37