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Multiple Environment Over Stress Testing (MEOST) A Primer with Examples from an Automotive Component Supplier October 26, 2011 John Kreucher Delphi Powertrain Auburn Hills, Michigan 810-577-9344 [email protected]
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Multiple Environment Over Stress Testing

(MEOST)

A Primer with Examples from an Automotive

Component Supplier

October 26, 2011

John Kreucher

Delphi Powertrain

Auburn Hills, Michigan

810-577-9344

[email protected]

Multiple Environment Over Stress Testing

(MEOST)

Acknowledgements:S. Shaffer

B. Phegley

F. Couillot

A. Kleyner

AGENDA:

• Accelerated Testing Basics

• Time Compression

• Accelerated Life Testing (Constant Stress)

• MEOST

• HALT

Multiple Environment Over Stress Testing (MEOST)

A Primer with Examples from an Automotive Component Supplier

Accelerated Testing BasicsFor Field-Correlated Tests

• Analytical models must align with physics of usage/damage and environmental loading

• Failure modes under accelerated conditions must correlate to field failure modes

• No “unnatural” or foolish failure modes

• Shape parameter at each stress level (e.g. Beta for 2-P Weibull) should be the same

• Normally, to correlate an accelerated test, we “chase” a particular failure mode of

concern

• Other failure mechanisms occur at different rates and are disregarded analytically

• Reliability demonstration is possible, but assumes that part variation is representative

• Because of variability of field usage and environments, and uncertainty in material

constants, a precise acceleration model is impossible to obtain

• The best we can hope for is a useful test

1.Compress time

2.Increase the stresses that generate failures (accelerated stress testing)

� Elevated (Constant) Stress Testing

� Multiple Stress Level Testing (MEOST)

� Qualitative Methods

Problem: Available Test Time < Expected Product Lifetime

Solution::

TIME COMPRESSION

1. Remove non-damaging events

and/or

2. Accelerate the number of cycles per unit of time (apply stress

more frequently than it occurs in service)

TIME COMPRESSION

Automotive Trunk Lid Closure Test

10 cycles/hr x 100 hrs = 50 cycles/hr x 20 hrs = 1000 cycles

Five times as fast

for 1/5 of the time

Consider a test that opens and closes an automotive trunk lid 8000 times in 10 hrs…

What might you miss??

1.Compress time

2.Increase the stresses that generate failures (accelerated stress testing)

� Elevated (Constant) Stress Testing

� Multiple Stress Level Testing (MEOST)

� Qualitative Methods

Problem: Available Test Time < Expected Lifetime

Solution::

Stress – Strength Conceptual ModelR

ela

tive F

requency

Customer

Stress

Component

or Subsystem

Strength

Test Severity

(%tile User)

In testing, we usually work here

Q: Would you expect a higher field or test reliability?

A: Unless you are missing environments, or unless your parts do not

represent manufacturing variation, then:

Field Reliability > Test Reliability

Stress – Strength Conceptual ModelR

ela

tive F

requency

Customer

Stress

Component

or Subsystem

Strength

Test Severity

(%tile User)

In testing, we usually work here

• For the sake of conservatism, testing is often conducted at higher than nominal

levels, say 97.5 %-tile

• It’s OK to test at “only” 97..5 %-tile stress, because:

1. If your test has multiple environments, the likelihood of having extreme

exposures for each of the environments concurrently is extremely small, and

2. More mistakes are made by missing environments and/or misrepresentative

parts.

Accelerated Life Testing

Critical assumption: The same failure mechanisms will be

present at the higher stress levels and will act in the same

manner as at normal stress levels.

tn = time to failure under normal stress

ta = time to failure at high stress level

then tn = AF x ta where AF is an acceleration factor

Time to Failure

Str

ess

1. Life Distributions determined

experimentally at high stress levels

2. Stress model used to predict life

at normal use levels

Customer Usage

Level

“One Life”

Accelerated Life Testing

Accelerated Life Testing

Stress Models

� Inverse Power Law

� General mechanical stress model

� Thermal and mechanical fatigue (Coffin Manson)

� Arrhenius Model

� Chemical/material reactions driven by temperature

� Eyring Models

� Temperature + Other (Mechanical, Humidity, Current Density)

� Kemeny Model

� Temperature + Voltage

Case Study 2:

Accelerated Heater Cycling TestDELPHI PLANAR OXYGEN SENSOR (OSP)

• Stoichiometric Switching Sensor

• Heater Integrated within the Sensing Element

• In Production Since 2002

Sensing Element

Accelerated Life Testing

Example

• Test Plan: Test (40) pcs to failure, (10) ea. @ 21V, 22V, 23V, and 24V

• Failure Definition: Failure is resistance increase >/= 10% of original value, or open heater. Resistance checks once/day.

• Requirement: Elements must survive 50,000 thermal cycles at 13.5V

Case Study 2:

Accelerated Heater Cycling Test

DELPHI PLANAR OXYGEN SENSOR (OSP)

Accelerated Life Testing

Example

Case Study 2:

Accelerated Heater Cycling Test

DELPHI PLANAR OXYGEN SENSOR (OSP)

Accelerated Life Testing

Example

1.Compress time

2.Increase the stresses that generate failures (accelerated stress testing)

� Elevated (Constant) Stress Testing

� Multiple Stress Level Testing (MEOST)

� Qualitative Methods

Problem: Available Test Time < Expected Lifetime

Solution::

• Multiple environment test to failure after achieving one life

• All parts should fail on or before the last step of overstress (at the Destruct Limit)

• Combined environments allow for interactions which are potentially more

relevant than single environment tests

MEOST

Multiple Environment Over-Stress Test

MEOST

Multiple Environment Over-Stress Test

• Primarily Qualitative, but can be made “semi-quantitative” with some rigor

• Good alternative for newer product lines or significant product changes, when

failure mode(s) and failure times are uncertain

• Can be done on small sample size, therefore a good option when parts are

expensive

• Best done w/ special equipment (fast ramp chambers and pneumatic

shock/vibe equipment), but can be very usefully administered on standard

equipment

MEOST

Test Time

Co

mb

ine

d T

es

t S

tre

ss

100%

One Life

Destruct Limit

MEOST PROCESS

1. Define Operating Rectangle for each Environment

2. Establish Destruct Limit for each Environment (measure or estimate)

3. Calculate Overstress Levels (stress and time steps)

4. Conduct Test to Failure (fix design if failure occurs within one life)

5. Plot Weibull results as % Stress-Time

1

2

3

MEOST

Operating Rectangle

1. Which environments are present? Which might interact to cause relevant failure modes? Conversely, too many environments lead to test complexity and cost.

2. Instrument your product in the field and record data for each important environment.

3. Analyze data to determine the (say) 97.5th %-tile user : The “Design Level”

4. Define the operating profile and one life on test.

Easy Level

MEOST

Potential Environments:

• Vibration (random, sine)

• High Temperature

• Low Temperature

• Temp Cycling

• Humidity

• Pressure

• Voltage

• Power Cycling

• Mechanical Actuations

• Etc.

MEOST

Conduct Test to One Life

1. Test 10 to 12 randomly selected units for one life within the operating rectangle.

• You should expect to pass!

2. Find and fix any failures, and restart the test.

• This might include design or quality improvements

3. Proceed to step stress testing with the same parts.

MEOST

Test Time

Co

mb

ine

d T

es

t S

tre

ss

100%

One Life

Destruct Limit

MEOST PROCESS

1. Define Operating Rectangle for each Environment

2. Establish Destruct Limit for each Environment (measure or estimate)

3. Calculate Overstress Levels (stress and time steps)

4. Conduct Test to Failure (fix design if failure occurs within one life)

5. Plot Weibull results as % Stress-Time

1

2

3

MEOSTDestruct Limit

• The Destruct Limit (or Foolish Failure Limit) is the stress level where a product is

expected to fail with a high degree of certainty.

• The associated failure mode can be either related or unrelated to the failure

mode expected in the field environment.

• Example 1: Plastic case melting at 180 deg C.

• Example 2: PCB cracking at 10 Grms random vibration.

• Destruct Limits are best determined by testing parts under each environment

separately. Otherwise, analysis may be used (e.g. solder melt temp).

• Sometimes it is difficult or impossible to determine the Destruct Limit for a particular

environment due to test equipment limitations

• This may or may not compromise the integrity of the test plan

MEOST

Test Time

Co

mb

ine

d T

es

t S

tre

ss

100%

One Life

Destruct Limit

MEOST PROCESS

1. Define Operating Rectangle for each Environment

2. Establish Destruct Limit for each Environment (measure or estimate)

3. Calculate Over-Stress Levels (stress and time steps)

4. Conduct Test to Failure (fix design if failure occurs within one life)

5. Plot Weibull results as % Stress-Time

1

2

3

Over-Stress StepsCommon Mistake:

0 3.2 15 23 115 150

Vibration (grms) High Temperature (C)

Design

LevelDesign

Level

Destruct

LevelDestruct

Level

Easy

Level

Easy

Level

• It is not appropriate to overstress each environment to its Destruct

Level.

• Doing so may result in failure mode(s) not representative of your

product and application.

• In this example, the product is much closer to failing for

temperature than for vibration under normal usage conditions.

l l l l l l l l l ll l l l l l l l l l

Over-Stress StepsCalculate Over-Stress Step Size for each environment:

1002

1 ∗∆

∆=% OVER-STRESS =

Destruct Limit - Design Limit

Design Limit – Easy Limit=

-

Operating

Range

∆1

∆2

Str

ess

Destruct Limit

time

Design Limit

Easy Limit

100∗

The Lowest % Over-Stress will be used to compute the step size for each stress

and to determine the time interval for each Over-Stress Step.

Over-Stress StepsExample: Electronic Component Test

Standard Validation Test:

• Temp Cycles between -40C and 115C

• Random vibration profile with energy of 3.2 grms

• One Life on this test is considered to be 400 Hrs

1. Operating Rectangle

• Stresses (Easy - Design Limit):

• High Temperature (23C - 115C)

• Vibrational Energy (0g - 3.2g)

• Low Temp: Held at -40C

• One Life = 400 Hrs

2. Destruct Limits:

• High Temp: 150C (softening temperature of plastic case)

• Vibration: 15grms (based on vibration test in worst-case orientation)

Over-Stress Steps – Electronic

Component Example

3. Over-Stress Levels:

High Temperature:

38 %

LOWEST OVERSTRESS

% OVERSTRESS =150 - 115

115 - 23

-=

Vibration:

369 %% OVERSTRESS =15 - 3.2

3.2 - 0

-=

For each environment, the step size will be 3.8% of the Operating Range (38% ÷ 10 Steps)

Over-Stress Steps – Electronic

Component Example

Over-Stress Step Size:

(Stress and Time)StepsofNumberDesired

StressOverLowestRangeOperating

% −×

• Temp: (115 – 23) x 38%10

= 3.5C

• Vibe: (3.2 – 0) x 38%10

= 0.12g

• Time: 400 Hrs x 38%10

= 15.2 Hrs

Total Test Time =400 + 152 = 552 Hrs

Operating Rectangle:

400 hrs

Temp Cycles: -40 to 115 °C

Vibe: 3.2 GRMS

STEP 1

STEP 2

STEP 3

STEP 4

STEP 5

STEP 6

STEP 7

STEP 8

STEP 9

STEP 10High Stress Limit: 150°C (Destruct Limit), 4.4gRMS

3.5°C

0.12 gRMS

15.2 hrs

MEOST Plan:

Over-Stress Steps – Electronic

Component Example

MEOST

Test Time

Co

mb

ine

d T

es

t S

tre

ss

100%

One Life

Destruct Limit

MEOST PROCESS

1. Define Operating Rectangle for each Environment

2. Establish Destruct Limit for each Environment (measure or estimate)

3. Calculate Over-Stress Levels (stress and time steps)

4. Conduct Test to Failure (fix design if failure occurs within one life)

5. Plot Weibull results as % Stress-Time

1

2

3

Multiple Environment Over Stress Test (MEOST)

Q: So how do you make a Weibull plot of the failures if each overstress step involves an

increase in stress as well as time?

A: If stress and time are normalized to “100%” of the O.R., and if overstress steps are equal

increments of %stress and %time, then failure data can be plotted on a Weibull Stress*Time

plot…

Step Stress Test

Test Time

Co

mb

ine

d T

est

Str

ess

One Life

Stress Limit

x

x

xx

x

100% time

10

0%

Str

ess

0.01

0.05

0.10

0.50

1.00

5.00

10.00

50.00

99.00

1.0

STRESS TIME PERCENT

PE

RC

EN

T F

AIL

ED

β=31.94, η=1.52, ρ=0.92

1.1 1.2 1.3 1.4 1.5 1.6 1.7 1.8 1.9 2.0

2.0

1 Life

MEOST – Example

Delphi Probe Air Meter

Standard “Hot Vibe” Test:

• 3 Grms with Underhood Chasis PSD

• -40 to 125C Thermal Cycles

• 6 hrs/axis

Problem:

• Parts rarely fail this test

• Would like to learn the failure mode(s)

on test and the margin to customer

requirement.

Solution:

• Conduct MEOST

MEOST – Example

Air MeterStresses:

� High Temperature: The 97.5%-tile field temperature at the hybrid

circuit board was measured to be 65ºC. Destruct limit = 183ºC for

eutectic Sn/Pb solder.

� Vibration: The “Underhood Chassis” vibration spectrum is appropriate

for this Air Meter. One life is represented by 6 hrs/axis with this profile at

3 Grms. Destruct limit was determined to be more than 38 grms on test.

Equipment limitation prohibited exact determination.

� Note 1: Low temperature has not been observed to cause field concerns, as seen on

warranty and other customer returns. It will be fixed at -40ºC.

� Note 2: Humidity will not be comprehended in this test because humidity related failure

modes have not been observed in field returns.

MEOST – Example

Air Meter

Over-Stress Levels:

%274 %1002265

65183 %100 =

−=

−xx

EasiestDesign

DesignDestructHigh Temperature (ºC):

%1671 %100 03

338 %100 =

−=

−xx

EasiestDesign

DesignDestructVibration Level (grms):

Lowest Stress Increase

Step Size:

MEOST – Example

Air Meter

Test Plan:

1. Test 9 parts total.

2. Run operating rectangle. Rotate parts every 6 hrs: 6 hrs/axis = 18 hrs total.

3. Increase part stresses simultaneously according to step size determined above. Run each step for 1.6 hrs/axis.

4. Continue to increase part stresses, until failure or until all units reach destruct limit (10 steps).

Test Time

Co

mb

ined

Str

ess

1

25

No. of Failures

100%

18 Hrs

Destruct/Test Limit

(183C; 11.2 g's)

MEOST – Example

Air Meter

Step Stress TimeStress Time

Percent

First Anomaly

S/N

O.R. 1.000 100.0

1 1.274 127.4

2 1.548 154.8

3 1.822 182.2

4 2.096 209.6

5 2.370 237.0

6 2.644 264.4

7 2.918 291.8

8 3.192 319.2 901

9 3.466 346.6 898, 914, 480, 476, 926

10 3.740 374.0 906, 478

100.00 1000.00

1.00

5.00

10.00

50.00

99.00

µ

σ

σ

Stress*Time

Un

relia

bili

ty,

F(t

)

One Life

Fo

oli

sh

Fail

ure

Lim

it

MEOST – Example

Air Meter

Lognormal Distribution of

Stress*Time Intervals

(Soft Failures)

MEOST – Example

Delphi Multec Fuel InjectorF. Couillot

Standard Pressure Cycling Test:

• Fluid Pressure Cycling 3 to 250 bar

• Pressure Wave Frequency - fixed

• Temperature: Ambient

• Test Fluid: Oil

• Target Life: 10M Cycles

Problem:

• Prior design did not meet customer requirements

• Lengthy Test and Fix loops

• No efficient method to evaluate design improvements and

determine margin to requirements

Solution:

• Use MEOST strategies to evaluate design improvements

MEOST – Example

Delphi Multec Fuel Injector

Stresses:

� High Pressure: The design limit for purposes of this test was selected

to be the customer requirement: 250 bar. The destruct limit is 600 bar

(based on material properties).

Test Plan:

1. Test 6 pcs each of two design alternatives (“Proto A” and “Proto B”)

2. Run operating rectangle. 10M Cycles between 3 and 250 bar.

3. Increase high pressure in (7) Over-Stress steps of 20% (50 bar and 2M

cycles)

4. Continue to increase part stresses until failure or until all units reach

destruct limit (7 steps).

MEOST – Example

Delphi Multec Fuel Injector

MEOST – Example

Delphi Multec Fuel Injector

“Proto A”

“Proto B”

1.Compress time

2.Increase the stresses that generate failures (accelerated stress testing)

� Elevated (Constant) Stress Testing

� Multiple Stress Level Testing (MEOST)

� Qualitative Methods

Problem: Available Test Time < Expected Lifetime

Solution::

HALT - Highly Accelerated Life Test

• Combined Temperature Cycling, Vibration, and Power Cycling (most

common)

• HALT is performed in specially designed chambers.

• 6 DOF “Repetitive shock” type of vibration

• The HALT test can be carried out in one or two days

• Most often employed with electronic assemblies

The principal idea in HALT is to find the weak links as quickly as possible and then fix

them. After improving one weak link, the next weak link then is found and improved

and so on until there are no weak links left that would cause field failures

HALT is not intended for a quantitative reliability demonstration

Thank you!

John Kreucher

Staff Validation & Reliability Engineer

Delphi Powertrain Systems Division

[email protected]

810-577-9344


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