Package Vibration Testing - Westpak & PACKAGE VIBRATION TESTING ... (springs), A/A plots – Design...

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PRODUCT & PACKAGE TESTING VIBRATION & SHOCK Dec 2015 Herb Schueneman Chairman, WESTPAK, Inc. PRODUCT & PACKAGE VIBRATION TESTING Herb Schueneman Founder, Chairman WESTPAK, INC. March 2016

Transcript of Package Vibration Testing - Westpak & PACKAGE VIBRATION TESTING ... (springs), A/A plots – Design...

What’s This All About?

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• Why, how, and when do we mechanically test products and package systems?

• What do we learn from this?

• What do we do with the information?

Agenda

• Background, terminology, etc.

• Vibration Dynamics

– Spring/Mass Models; Forces vs. Free Response

– Types of Excitation; Sine, Random, Acoustic, Sources of input

– Resonance, Transmissibility, Damping, Fatigue

– Package Cushioning (springs), A/A plots

– Design for Vibration

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Dynamics

• The study of mass that is moving in a flexible environment

• “Flexibility” implies springs so the study of dynamics starts with a thorough understanding of “Spring/Mass Systems”

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AN INPUT APPLIED HERE RESULTS IN “FREE VIBRATION” OF THE MASS

AN INPUT APPLIED HERE RESULTS IN “FORCED VIBRATION” OF THE MASS

SDOF Spring/Mass System

MASS

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SDOF Spring/Mass System

MASS

Maximum strain energy

Maximum velocity

Natural or Resonant Frequency

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As earlier noted, excitation of the mass results in motion we call free vibration or “Natural Frequency”, fn.

Excitation of the base results in “forced vibration” of the mass. When the forcing frequency = fn, the mass response is max and is said to be in resonance.

SDOF vs. MDOF “Normal” products are pretty complex. A multiple degree of freedom (MDOF) model is more appropriate however much more complex and difficult to analyze.

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Non-Linear / Hardening Spring

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dd

k

2kd

tan (def)

2d SPRING FORCE =

Spring Types

Non-Linear / Softening Spring

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DEFLECTION

F

1

k

SPRING FORCE =kd tanh d

def

Spring Types

• SDOF models assume linear springs

• Most flexibility in systems is non-linear

• However, most systems can be analyzed in a “near linear” portion of their deflection range so that’s why we use the linear model

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Spring Types

(Printed Circuit Boards)

Coupling

M

A B

F1

F2

F 3

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Coupled vs. Uncoupled Motion

• The mass is a homogenous rigid block with center of gravity (cg) at point A.

• The response of the block to F1 is pure vertical motion.

• The response of the block to F2 is pure rotational motion.

• The response of the block to F3 is pure horizontal motion.

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Coupled vs. Uncoupled Motion

• If (cg) is at point B, F1

produces both vertical and rotational motion of the block. In this case, the motion is said to be coupled.

• With (cg) at point B, F3 produces uncoupled horizontal motion.

Coupling

M

A B

F1

F2

F 3

Resonance occurs when a component or system is forced at its fn.

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• Spring/Mass response is amplified at resonance.

• This is where damage, fatigue, etc. is most likely to happen.

Resonance

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Vibration Machine

Example

Types of Equipment • Electrodynamic shaker • Hydraulic shaker

• Single or multi-axis • Acoustic (reverberant) chamber

How the Test is Conducted

Excitation can be:

• Sinusoidal

• Random or pseudo-random

• Acoustic

• Other

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Types of Mechanical Excitation

All Spring/Mass systems respond at their natural frequencies because they can’t do anything else.

Type Positive Not-So-Positive

Sinusoidal • Easy to understand • Good visual feedback • Grandfathered tried & true

• Gives false amplification values • Over-test for fatigue potential • Doesn’t account for constructive and

destructive interferences between systems

Random • Quicker • Less fatigue potential • Realistic • Matches “real life”

• More complex • Requires a specific controller

Acoustic

• Usable for heavy systems • Good high frequency

• Very expensive • Requires large chamber & analytical

capability

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Excitation: the Good & the Bad

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Damping (Rc) is expressed as a ratio of observed damping to “Critical Damping” in a system.

Damping

“Critical Damping” is where the mass returns to its initial position in the minimum time without overshoot.

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Damping

Fatigue is the weakening of a material caused by repeatedly applied loads. It is the progressive and localized structural damage that occurs when a material is subjected to cyclic loading. Resonance is the prime contributor. Non-critical damping is a factor.

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Mechanical Fatigue

Sources of Vibration Input

Sources of input include:

• Operation

– Rotating equipment (cooling fans, motors, etc.)

– Nearby influences

– Strong air currents

– Earthquakes

• Non-Operating

– Transportation, shipping (the biggest), logistics

– Normal movement within intended environment

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Typical Test Procedures

• Sine search & dwell is still used (problems..)

• Random dwell is more common

• Margin test (to failure) has gained wide acceptance (HALT)

• Imposed by third party

• Attempt to duplicate the in-use environment (military vehicles & weapons)

• Lots of creativity in test procedures…. (be VERY careful here….)

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Common Test Specs

• ASTM D3580 (doesn’t say much)

• IEC 60068-2-6, -47 (similar)

• Federal Std 101-C (very dated)

• ISO – various standards

• JIS - Japanese Industrial Standards

• MIL STD 167, 810

• Telcordia GR-63 CORE (Bell System origin; POTS – Plain Old

Telephone System)

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Establishing the Test Plan

• Design of Experiment (DoE)

• Characterize environments EUT will see

• Define test inputs to cover all environments

• Consider Combined Environments

• Remember shipping / distribution (severe!)

• Determine acceptance criteria / inspections

• Quantitative when possible

• Cosmetic, functional, safety

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Establishing the Test Plan

• Start Small

• First: Test temperature and basic mechanical vibration

• Second: Comprehensive testing (single environment)

• Third: Combined Environment testing (as applicable)

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Combined Environment Test Inputs

• Every product will see different environments

• Sample EUT: Ruggedized Laptop Computer

• Test inputs discussed

• Temperature + Vibration

• Impact Testing + Temperature Extremes

• Freefall Drop Testing + Temperature Extremes

• Mechanical Cycling + Temperature Extremes

• Temperature + Pressure

• Fluid Submersion + Temperature + Pressure

• Thermal Shock

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Temperature + Vibration • Background of “AGREE” Testing • Typical Test

• Cyclic functional operation • Temperature by application • X, Y, Z axis in single direction • Random frequency domain by application

• Transport (1Hz – 300Hz) • Bare Product (5Hz – 2,000Hz)

• Test Standards • MIL-STD-883, MIL-HDBK-781

• Variations of Testing • Common Issues / Results

• Unsupported / surface mount component failure • Permanent failure to operate correctly

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End Result

• Ruggedized product

• Free of latent mechanical defects

• Good to great reliability out of the box

• A prioritized list of improvements to be made

• Verification for meeting a spec requirement

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How About the Package Cushion?

• One of the functions of a cushion system is to dampen vibration input at those frequencies where the product is sensitive.

• In essence, we need to know the dynamic spring rate of the cushion.

• Now we know the PRODUCT vibration sensitivity.

• Now we need to determine the CUSHION vibration characteristics so that an optimum package system can be designed.

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Vibration Cushion Dynamics

• “Vibration Cushion Curves” (called “Amplification/Attenuation Plots”) are developed by loading a cushion, shaking it, and measuring the response.

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Guided Test Block

Method

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Alternate Method

Vibration Cushion Dynamics

CUSHION

CUSHION

CUSHION

RESPONSE ACCELEROMETER

INPUT ACCELEROMETER

VIBRATION TABLE VIBRATION TABLE

CUSHION

CUSHION

MASS ADHERED TO FOAM

SO THAT THE “SPRING”

(CUSHION) WORKS IN BOTH

TENSION AND COMPRESSION

MASS ISOLATED BETWEEN

TWO “SPRINGS”

(CUSHIONS) THAT WORK

IN COMPRESSION ONLY

MASS

MASS

T-C MODEL C-C MODEL

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Vibration Cushion Dynamics

CUSHION TEST SAMPLE

CUSHION TEST SAMPLE

ELECTRODYNAMIC SHAKER

For either method, the S/M system is excited (random or sine vibration) and the response/input ratio is plotted as a function of frequency.

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Vibration Cushion Dynamics

The important points on this plot are identified here:

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A

C B

Vibration Cushion Dynamics

The mass on the cushion is changed and the process (transmissibility plot) is repeated.

After 5 (min) plots, the data might look like this:

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Vibration Cushion Dynamics

The data is then transferred to the Amplification/Attenuation plot

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Vibration Cushion Dynamics