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Solder Fatigue Analysis
For Intermediate Users Dr. Natalie Hernandez
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Agenda Introduction Fundamental theories Examples
What’s the problem we’re all trying to solve? What’s the cause? Fundamental theories Engelmaer the Blattau model Examples Modeling leaded components Surface mounts BGA (simple array and non-traditional array) Through-hole Radial Modeling leadless components QFN
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WHAT’S THE PROBLEM
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UNEXPECTED SOLDER FAILURES
Increasing number of companies reporting early life failures during the manufacturing process or during testing or in the field UNEXPECTED SOLDER FAILURES Classic solder fatigue approaches do not seem to be capturing these risks
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WHAT’S THE CAUSE?
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With the advance of technology…
Electronics are shrinking and becoming denser and more complex iPhone 8 Space Controller
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Fundamental Theories
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STRAIN RANGE + CLOSED FORM EQUATIONS
𝑁 𝑓 = ∆𝛾 2𝜀 𝑓 𝑐 ∆𝛾=𝐶 𝐿 𝐷 ℎ 𝑠 ∆𝛼∆𝑇 𝜀 𝑓 =0.325 Distance to neutral? Brilliant Deriving key constants based on flawed test conditions (Wild)? Problem Isothermal mechanical (not actual behavior) Between 25C and 100C (overestimates creep) 4 to 300 cycles per hour (underestimates creep) 𝑐= −0.442 − 6𝑥 10 −4 𝑇 𝑠 +(1.74𝑥 10 −4 )[ ln 1+𝑓 ] Engelmaier, W.; , "Fatigue Life of Leadless Chip Carrier Solder Joints During Power Cycling," Components, Hybrids, and Manufacturing Technology, IEEE Transactions on , vol.6, no.3, pp , Sep 1983
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STRAIN ENERGY + FINITE ELEMENT ANALYSIS (FEA)
Strain energy (work) used to predict crack initiation and crack propagation 𝑁 0 =𝐾1 ∆𝑊 𝑎𝑣𝑔 𝐾2 𝑑𝑎 𝑑𝑁 =𝐾3 ∆𝑊 𝑎𝑣𝑔 𝐾4 𝑁 𝑓 = 𝑁 0 + 𝐷 𝑑𝑎 𝑑𝑁 Darveaux, R., “Solder Joint Fatigue Life Model,” Proceedings of TMS Annual Meeting, Orlando FL, February 1997, pp
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STRAIN ENERGY + CLOSED FORM EQUATIONS
Closed Form, PCB Stiffness, Strain Energy, E (T), Tg, Die Shadow N. Blattau and C. Hillman, “An Engelmaier Model for Leadless Ceramic Chip Devices with Pb-Free Solder,” Journal of the Reliability Information Analysis Center, First Quarter 2007, 6-11
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Solder Fatigue Tool
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Defining your environments
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Life Cycles User guide Webinar Edit Properties: Defining Phases
Edit Properties: Define reliability metric Defining Phases Environment: MIL-217 or TR-332 Duration of Phase must cover all events Temperature cycle must begin and end at same temperature
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Closer Look at Thermal Cycles
Example of a generic temp cycle (-10 to 100°C) The whole board is changing temperature But the Min and Max temps of the board can be different than (-10°C) od 100°C Let’s look at a demo!
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Thermal Maps Sources: Apply thermal maps
IR camera Board side Thermal analysis MIN and MAX Direct measurement You can have 4 maps for 1 temp cycle Any Picture Align the board and legend Legend orientation Let’s look at a demo!
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Defining your materials
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Laminate Manager
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Material Manager
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Package Manager
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Defining your leads
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Lead Modeling C-Lead, J-Lead, Gullwing, Stub, leadless QFP FETS
BGA Balls More details provided in user guide
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BGA Ball Modeling “Ball” tab in the part editor
Ball Modeling: Enabled One or two elements Patterns Full Perimeter Channel Island Corner depopulate balls Using the ball count Only works for regular patterns Use mount point method for specialized patterns Use with “Potting” Underfill Corner staking Edge bonding
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Examples
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LIFE CYCLE Test condition
-40°C to +125°C, dwell 20 minutes hot and cold, 15°C/min ramp rate Field conditions Standard day: 15°C to 50°C, 90-min hot dwell, 360-min cold dwell, 2300 cycles Tropical day: 32°C to 70°C, 90-min hot dwell, 360-min cold dwell, 800 cycles
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MPC5554 – PACKAGE DIMENSIONS
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MPC5554 – BALL DIMENSIONS Provided by cross-section results
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MPC5554 – 3D MODEL CONFIRMATION
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MPC5554 – DIE DIMENSIONS Die Size Die Thickness
35% of exterior dimensions: 0.35 x 27 = 9.45mm Die Thickness Overmold thickness – 0.2 (for wire bond) – 0.1 (for die attach) = 0.3mm
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RESULTS – MPC5554 Cycles to failure (TEST): 4263
Board CTE: ppm/C Damage: 19.9 Cycles to failure (FIELD): 117,299 Damage: 0.02
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TPS54622 – PACKAGE DIMENSIONS
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Tg Correction of effective CTE & E
Elastic Modulus
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TPS54622 – PAD DIMENSIONS
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TPS54622 – FLAG DIMENSIONS
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TPS54622 – DIE DIMENSIONS Die Size Die Thickness
Equivalent to the thermal pad 2.05 x 2.05 Die Thickness 0.9 – 0.2 (leadframe) – 0.2 (for wire bond) – 0.1 (for die attach) = 0.4mm
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RESULTS – QFN Cycles to failure (TEST): 10682
Board CTE: ppm/C Damage: 7.94 Cycles to failure (FIELD): Damage: 0.014
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Dr. Natalie Hernandez, Product Manager
Questions? Dr. Natalie Hernandez, Product Manager
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