Overcoming 25 year life reliability challenges in solar electronics

78
© 2004 - 2007 © 2004 - 2010 © 2004 2010 Overcoming 25 Year Life Reliability Challenges in Solar Electronics DfR Solutions Webinar September 27, 2012

description

Reliability issues associated with achieving a 25 year warranty

Transcript of Overcoming 25 year life reliability challenges in solar electronics

Page 1: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010 © 2004 – 2010

Overcoming 25 Year Life Reliability Challenges in Solar Electronics

DfR Solutions Webinar

September 27, 2012

Page 2: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Solar Panel “Scams” in the News… http://www.bbb.org/blog/2012/06/dont-fall-for-a-solar-paneling-scam-this-summer/

Page 3: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Leading Causes of “Hard” Photovoltaic (PV) System Failures

o Central Inverter: 37%

from 2009 Sandia

Study

o IGBT most common

component

o 3 basic fail categories

o Manufacturing Quality

o Inadequate Design

o Defective Electronic

Components

J. Granata, Sandia; 2009 PV

Reliability Conference

IGBT = insulated gate bipolar transistor

Page 4: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Leading Causes of “Hard” PV System Failures

o Central Inverter: 51%

from Sun Edison 2008-

2010 study

o Communications: 11%

o Weather Station: 7%

“Owner/Operator Perspective on Reliability Customer Needs and

Field Data”, Sandia National Laboratories, Utility-Scale Grid-Tied

PV Inverter Reliability Workshop, January 2011.

Page 5: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Leading Causes of Calls for PV Inverter Failures

o “Other” is largest

o Control software:

16%

o Printed Circuit Board:

11%

Page 6: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Leading Root Causes of “Hard” PV Inverter Failures

o Parts & Materials:

57%

o Software: 16%

Page 7: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Reliability by Inverter Type

Page 8: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

PV System Reliability & Availability

o Every alert must be

addressed

o Most software &

communication issues

can be handled quickly

o Hardware takes longer

to resolve

o Potentially easier to

improve availability

by focusing on

software &

communication!

o Tend to be hardware

biased!

Page 9: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

PV System Failures: Utility Perspective

o Leading failure causes in US:

o Poor Design

o Poor Installation

o Code Infraction

o Ambiguous Instructions

o Lack of information and documentation

o Leading failure causes in developing countries:

o Selling PV systems to users and financing them privately or by soft loans

o Encouraged purchase of cheap, poor quality components and minimal maintenance

o Led to early failures and poor long term sustainability

Evaluation of the PREP Component : PV

Systems for Rural Electrification in Kiribati &

Tuvalu (7 ACP RPR 175)

DESIGN REVIEW AND APPROVAL OF GRID-

TIED PHOTOVOLTAIC SYSTEMS

Page 10: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Inverter Overview

o Inverters perform two key functions

o Converts the direct current (DC) coming from the

panels to the alternating current (AC) used by the

electric grid

o Perform algorithms to maximize the power

produced by the system.

Page 11: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Types of PV Inverters

Graph courtesy of Doron Shmilovitz, Tel Aviv University, Israel

Page 12: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Central Inverters

o PV modules feed into a central dc-dc converter stage that

has:

o Maximum power point tracking (MPPT)

o DC-AC inverter to connect to the utility grid.

o Can’t maximize energy extraction from all modules

Page 13: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Micro-Inverters vs Central Inverters

o Better Reliability & Availability o Lack of single failure point

o Longer warranty: 15-25 years versus 5-10 years

o Lower DC Voltages, less vulnerable to arcing

o Optimized Maximum Power Point Tracking (MPPT) per module

o PV Module level real-time monitoring

Images courtesy of Paul Parker, SolarBridge

Page 14: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Micro-Inverters

o The electronic components used in a micro-inverter are commercial off-the-shelf (COTS)

o Parts designed for consumer electronics but need to survive 25 years in solar installations

o Outdoor/Partially Protected & Temp Not Controlled

Page 15: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Distributed Inverters

o Similar advantages as Micro

o Designed to work with power optimizers

o Standard 10-12 year warranty, some extended to 20-25 years

o Built-in module-level monitoring receiver with communication to internet via broadband or wireless

o Because MPPT & voltage management are handled separately for each module by the power optimizer, the inverter is only responsible for DC to AC inversion. So potentially less complicated, expensive & more reliable

Page 16: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Micro vs Distributed Inverters

o From a system reliability and maintainability perspective,

both offer advantages over Central inverters.

o All inverter types face the same environmental and

electronics failure modes.

o Both regarded as more cost effective for commercial

applications vs utilities

o Both add significant software complexity for optimizing and

monitoring functions

Page 17: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Micro vs Distributed Distinctions

o Component Selection o Life limits of Electrolytic Caps versus Ceramic Caps

o Use of ASICs to reduce discreet parts count

o Derating o Power optimizers are low voltage devices and more easily highly derated

o Efficiency & Heat Dissipation Differences

o Distributed/string benefits are true only if designed for the specific optimizer o One company doing this as a complete system

o No current standard for DC Optimizers, so other string inverter companies may be hesitant to design a product around a specific vendors’ optimizer.

Page 18: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Micro vs Distributed Distinctions

o Ceramic versus electrolytic capacitors

o DC/DC converters rely on ceramic capacitors which have a low, fixed rate of aging. o Possible due to the relatively high

switching frequency used in converters.

o Micro inverters require large input capacitance due to the grid low frequency. o In some cases, this is implemented

with electrolytic capacitors which have a significantly shorter lifetime.

Graphic courtesy of SolarEdge

Page 19: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Component Failures

Image Courtesy of SolarBridge

Page 20: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Micro vs Distributed Distinctions

o ASICs allow embedding many electronics into the chip,

thereby

o Reduces number of discreet components and potential points

of failure.

o Reduced component count on the circuit board also allows

manufacturers of power optimizers to decrease the overall

size of the product and raise MTBF

Page 21: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Micro vs Distributed Distinctions

o Derating

o Power optimizers are low voltage devices and more easily

highly derated

o A lower derating factor may shorten the lifetime of the

product due to increased stress under operating

conditions.

Page 22: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Micro vs Distributed Distinctions

o Efficiency & Heat Dissipation Differences

o Micro-inverters have lower efficiencies than power

optimizers. The highest known efficiency of micro-

inverter brands is 96%, meaning 4% heat

dissipation to the module.

Page 23: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Micro vs Distributed Distinctions

o Distributed/string benefits are true only if

designed for the specific optimizer

o One company doing this as a complete system

o No current standard for DC Optimizers, so other string

inverter companies may be hesitant to design a product

around a specific vendors’ optimizer.

Page 24: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Inverter Field Failure Mechanisms

o Solder joint fatigue failure

o Plated through hole fatigue failure

o Conductive anodic filament formation (CAF)

o Shock or Vibration (shipping and in use)

o Component wear out

o Potting Induced Failure

Page 25: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

o Solder joints “wear out” or fatigue and fail under

the long term influence of temperature cycling

and mechanical stresses.

Solder Fatigue

Page 26: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Plated Through Hole Fatigue o When a printed circuit board experiences temperature

cycling, expansion/contraction in the z-direction is much

higher than that in the x-y plane

o High stress can build up in the copper via barrels resulting

in cracking near the center of the barrel as shown in the

cross section photos below.

Page 27: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Conductive Anodic Filament Formation

(CAF) o CAF formation is a risk when Plated Through Hole (PTH) vias

are so close together that damage from drilling can open up a

pathway between vias.

o Copper from the via can migrate along the pathway and

eventually cause shorting.

Page 28: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010 28

Failure after Exposure to Vibration

o Mechanical shock and vibration also leads to solder joint

failures

o Can occur during transportation, installation or use

Page 29: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Potting Electronic Assemblies

o Potting is the process of filling an

electronic assembly with a resin

compound

o Provides resistance to shock and

vibration, and excludes moisture

and corrosives.

Page 30: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Printed Circuit Board Warpage due to

Potting Shrinkage

Page 31: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

o The use of underfills, potting compounds and thick

conformal coatings greatly influences the failure behavior

under temperature cycling

o Any time a material goes through its glass transition (Tg)

temperature problems tend to occur

o Underfills designed for enhancing shock robustness do not enhance

thermal cycling robustness

o Potting materials can cause PCB warpage and tensile stresses on

electronic packages that greatly reduce time to failure

Potting Rules of Thumb

Page 32: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Some Questions You Should Ask Your Inverter Supplier

o How have you evaluated reliability?

o Not MTBF, certifications or specifications but evaluation under

stress conditions to failure

o What is your field failure history & repair rate?

o What fails & why?

o How long and how many units in the field?

o Who installs them?

o What software monitoring options are available?

Page 33: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010 © 2004 – 2010

An Effective Means to Model the

Life of Inverter Electronics

Page 34: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Micro-Inverter Requirements

o The electronic components used in a micro-inverter

are off-the-shelf which means they were designed

for consumer electronics.

o How will such electronic assemblies survive the

demands of the solar industry?

Consumer Electronics Micro-Inverter Electronics

Expected Life 5-7 years 20-25 years

User Environment Indoor/Protected Outdoor/Partially Protected

Temp Controlled Temp Not Controlled

Page 35: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

What can be done?

o How can a micro-inverter supplier design the product to meet

the requirements AND convince the customer of this?

o This talk will discuss a novel new method to model the

reliability of an electronic assembly in a variety of conditions

based on the design (before building anything).

o Design for Reliability (DfR) concepts and Physics of Failure

(PoF) are used. .

o A comprehensive software package was developed to

simplify this modeling, thus making it available to design

engineers.

Page 36: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Design for Reliability (DfR)

o DfR: A process for ensuring the reliability of a

product or system during the design stage before

physical prototype

o Reliability: The measure of a product’s ability to

o …perform the specified function

o …at the customer (with their use environment)

o …over the desired lifetime

Page 37: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

DfR & Physics of Failure (PoF)

o Due to some of the limitations of classic DfR, there has been an increasing interest in PoF (aka, Reliability Physics) – to improve on DfR techniques.

o PoF Definition: The use of science (physics, chemistry, etc.) to capture an understanding of failure mechanisms and evaluate useful life under actual operating conditions

Page 38: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Micro-Inverter Environment

o Extreme hot and cold locations (AZ to AK)

o Possible exposure to moisture/humidity

o Large diurnal thermal cycle events (daily)

o Largest temp swings occur in desert locations where it

can reach 64C in the direct sun down to 23C at night

(Δ41C)

Page 39: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

NREL – Solar Panel Data

o Diurnal Cycles for Each Month

Page 40: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Possible Inverter Failure Mechanisms

o Solder joint fatigue failure

o Plated through hole fatigue failure

o Conductive anodic filament formation (CAF)

o Shock or Vibration (during shipping)

o Component wear out.

Page 41: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Is There a Method to Model these Failure

Mechanisms?

o Yes

o Algorithms exist to estimate the failure rate from

solder joint fatigue for different types of components.

o IPC TR-579 models PTH reliability

o Risk for CAF can be determined

o Finite Element Analysis can be used for Shock &

Vibration risk.

o MTBF calculations can be performed to estimate

component failure rates.

Page 42: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Leverage in Product Design

70% of a Product’s Total Cost is Committed by Design

http://www.ami.ac.uk/courses/topics/0248_dfx/index.html

Page 43: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Why is modeling reliability early

important?

Architectural Design for Reliability, R. Cranwell and R. Hunter, Sandia Labs, 1997

Page 44: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Earlier is Cheaper

Reduce Costs by Improving

Reliability Upfront

Page 45: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

What is the cost impact of poor reliability?

Aberdeen Group, Printed Circuit Board Design Integrity: The Key to Successful PCB Development, 2007

http://new.marketwire.com/2.0/rel.jsp?id=730231

Page 46: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Solder Joint (SJ) Wearout

o Elimination of leaded devices

o Provides lower RC and higher package densities

o Reduces compliance

Cycles to failure

-40 to 125C QFP: >10,000 BGA: 3,000 to 8,000

QFN: 1,000 to 3,000 CSP / Flip Chip: <1,000

Page 47: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

The Newest DfR Tool - Sherlock

o Sherlock – a new tool that models all the circuit card

assemblies and provides predicted life curves from

many common failure mechanisms.

o It is a Semi-Automated CAE knowledge based

program

o The Semi-Automated Features simplify model creation

and analysis

o Eliminates the long, complicated, model creation process and

the need for a PhD level expert in PoF, FEA and CFD

numerical modeling.

Page 48: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Software Coverage

o This software modeling tool predicts failures from

o Solder joint wear-out from thermal cycling (SAC305 or

eutectic SnPb)

o Plated through hole fatigue

o Conductive anodic filament formation

o 217 MTBF calculations are also generated

o In addition the software uses FEA to determine

o Board deflection and SJ failure from mechanical vibration

o The natural frequencies for the board based on the mount

points.

o Board deflection due to shock events

Page 49: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

o ODB files are preferred since they contain all the data

necessary for modeling

o Component details and placement

o PCB outline & stack-up

o Drill hole file with mount points

o Metal layers, silkscreen, solder mask layers

Data Import

Gerber Data can

also be imported

Page 50: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

PCB Details Required for Modeling

Page 51: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Establish Part Parameters

o Components identified along with packaging properties.

o Minimizes data entry through intelligent parsing and embedded package and material databases

Page 52: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Defining The Durability & Reliability Objectives

o Define the Expected Service Life

o Sets The Analysis Range And The Scale For Reliability Over Time Plots

o Life Cycle Phases

o Shows relative time spent at each phase

Page 53: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Identify Field Environment o Approach 1: Use of industry/military specifications

o MIL-STD-810,

o MIL-HDBK-310,

o SAE J1211,

o IPC-SM-785,

o Telcordia GR3108,

o IEC 60721-3, etc. o Advantages

o Sometimes very comprehensive

o Agreement throughout the industry o Disadvantages

o Most more than 20 years old

o Always less or greater than actual (by how much, unknown)

Page 54: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Field Environment (cont.)

o Approach 2: Based on actual measurements of similar products in similar environments

o Determine average and realistic worst-case

o Identify all failure-inducing loads

o Include all environments

o Manufacturing

o Transportation

o Storage

o Field

Container and Ambient Temperature

15.0

25.0

35.0

45.0

55.0

65.0

75.0

0 50 100 150 200 250 300 350 400 450

Hours

Te

mp

era

ture

(°C

)

Container Temp (°C)

Outdoor Temp (°C)

Page 55: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Input Field (or Test) Environment

Thermal Cycle

Profile

Vibration Profile

Shock Profile.

Handles very complex environments

Page 56: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Thermal Cycle Modeling

o The thermal cycle conditions the product will experience can be

modeled (Minor’s rule applied for multiple temperatures).

o Powered components can be assigned an added value above

ambient temperature.

Example of Diurnal TC Conditions in a hot climate

Page 57: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

TC Fatigue Analysis – Example Plot

Page 58: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Highest Risk Components

o Large Resistors provide the weakest solder joints in this example.

Page 59: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Plated Through-Hole Reliability Modeling

When a PCB experiences thermal cycling,

the expansion/ contraction in the z-

direction is much higher than that in the x-y

plane.

The glass fibers constrain the board in the

x-y plane but not through the thickness.

As a result, a great deal of stress can be

built up in the copper via barrels resulting

in eventual cracking near the center of the

barrel as shown in the cross section photos.

Page 60: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

PTH Fatigue Results - Example

Page 61: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Combined (SJ & PTH) Lifetime Prediction

o Combines analysis results into overall failure prediction curve

PTH

Solder Joint

Combined

Page 62: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Risk for Conductive Anodic Filament Formation

(CAF)

o CAF formation becomes a risk when plated through hole vias

are so close together that damage from drilling can open up a

pathway between vias.

o Copper from the via can migrate along the pathway and

eventually cause shorting.

Page 63: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

CAF Analysis

o The primary variables that effect the probability of

CAF formation are:

o Distance between vias

o Damage during drilling process

o Temperature and humidity conditions

o Voltage differential between vias

o The analysis takes into account the first two variables

only (measures distance between all PTH pairs).

o Vias identified as being too close are flagged.

Page 64: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

CAF Analysis

o Software will flag vias at high risk for CAF formation

Page 65: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Finite Element Analysis

o PCBA Example with Mesh Outlined

Page 66: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Natural Frequencies are Calculated

Select the number of

natural frequencies to

look for within the

desired frequency

range.

Components in high

strain regions are at

risk.

• Move the

components

• Move/add

mounting points.

MPs

Page 67: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Vibration Environment

Complex vibration profiles can be

modeled.

• Qualification test parameters

• Shipping/Transportation

• Field conditions

Page 68: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Random Vibration Strain

Board strain from

random vibration is

shown (calculated

for x, y, and z

directions)

Vibration set to simulate shipping

Page 69: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Vibration Results – Component Breakdown

Components most at risk for vibration fatigue damage are listed first.

Page 70: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Software Shock

o Implements Shock based upon a critical board

level strain

o Will not predict how many drops to failure

o Either the design is robust with regards to the

expected shock environment or it is not

o Additional work being initiated to investigate

corner staking patterns and material influences

Page 71: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Shock Results - Example

Page 72: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Shock Results – Component Breakdown

Components listed in order of maximum strain

experienced.

Page 73: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Constant Failure Rate Module – Components (Mil-

HNBK-217F)

This takes into account the failure rate of the

components themselves.

Page 74: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Combined Failure Rate is Provided

Page 75: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Additional Uses for Modeling

o Use Sherlock to determine thermal cycle test

requirements.

o Use to modify mount point locations

o Use to determine ESS conditions

o Component Replacement

o Determine impact of changing to Pb-free solder

o Determine expected warranty costs

Page 76: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Warranty Cost Estimate: Example

•Solder joint fatigue was the dominant

wearout mechanism, where the failure

rate is predicted ~2% after 20 yrs.

•Warranty from SJ failure = failure rate *

motherboard replacement cost * units

sold.

Page 77: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Summary

o It is important to eliminate design flaws early in development.

o Micro-Inverters must survive a challenging environment for long periods of time.

o A software tool is now available to model the primary failure mechanisms so that inverter electronics can be made more reliable.

o Sherlock modeling will enable a number of “what if” scenarios. o Changing package types

o Changing location of components

o Changing the mount point locations

o Changing laminate type, etc.

o The software can also be used to determine the TC test conditions that best simulate the field use conditions.

o Micro-Inverter designs can be built with more confidence that they will survive the challenging environments where they are placed.

Page 78: Overcoming 25 year life reliability challenges in solar electronics

© 2004 - 2007 © 2004 - 2010

Questions

Thank you for your attention.

Any questions?

[email protected]

[email protected]