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  • Laser Solutions Short Courses

    Short Course #4

    Optimizing Laser Machining Processes for Yield and Throughput

    in Manufacturing using DOE (Design of Experiments)

    Arzu Ozkan Course Instructor

    Sunday, September 26 2:00PM Room: Orange County 1

  • Optimizing Laser Machining using Design of Experiments (DOE)

    Principles

    A Case Study: Application of Shainin Techniques in Medical Device

    Manufacturing

    Arzu Ozkan, Lumyn Technologies LLC

    2220 Oakland Rd, San Jose, CA 95131650.733.6060 www.lumyntech.comICALEO 2010, Anaheim CA

    2220 Oakland Rd, San Jose, CA 95131

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    Outline

    Part I: INTRODUCTION

    1. D.O.E.: The Need and The Benefits

    2. Decision-making

    3. Summary of D.O.E Tools and Their Relative Effectiveness

    Part II: APPROACHES TO DESIGN OF EXPERIMENTS

    4. Possible Objectives of Experiments

    5. Cause and Effect Diagram

    6. Controlled Experiments

    7. Responses

    8. Example I: Material Removal Rate

    9. Example II: Feature Size

    10. Example III: Hole Diameter

    11. Example IV: Taper

    12. Example V: Surface Finish

    13. Example VI: Heat Affected Zone (HAZ)

    14. Factors

    15. Example I: Laser Wavelength

    16. Example II: Laser Power

    17. Example III: Laser Pulse Width

    18. Variables Held Constant

    19. Blocking Concept

    20. Randomization Concept

    21. Confounding Concept

    PART III: SHAININ DESIGN OF EXPERIMENTS

    22. Dorian Shainin

    23. Paretos Law

    24. The Green Y

    25. Likert Scale

    26. Seven Step Problem Solving Framework

    27. Finding the Red X

    28. Multi-Vari Analysis

    29. Separating Important Parameters: Paired Comparison

    30. Process Characterization: Variables Search

    31. Validation: B vs. C

    32. Process Optimization: Scatter Plot

    PART IV: CASE STUDY

    33. Laser Optimization--A Case Study

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    Part I: INTRODUCTION

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    1a: Design Of Experiments

    D.O.E. is a systematic approach to engineering problem-solving

    Experimental based modeling

    Proposed by Ronald A. Fisher, in his book The Design of

    Experiments in 1935.

    Some pioneers of D.O.E: R. Fisher, G. Taguchi, D. Montgomery,

    R. Myers, and D. Shainin.

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    1b: The Need for D.O.E.

    Your time is valuable.

    Are you in the market for a laser? Which laser is the best?

    Are you a researcher in academia or a member of an applications

    laboratory for a laser manufacturer? How to generate concise defendable data in a short time?

    Are you a member of senior management in a laser company? How to determine specification of a new laser product?

    Are you a laser or manufacturing engineer at a medical device

    manufacturing, electronics, semiconductor, or solar company? While best complying with FDA or other regulatory agencies, how can you differentiate your

    product from the competition and run your laser production maintenance-free?

    Are you an integrator or OEM? Which laser is the best? Second source?

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    1c: The Benefits of D.O.E

    Most knowledge gained with minimal

    expenditure of time and money

    Reduce time to market

    Identify important and unimportant

    variables and open up tolerances to

    reduce costs

    Ensures generation of valid and

    defensible engineering conclusions

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    2a: Decision-making

    Speculation

    Opinions

    Ideas

    Thoughts

    Theory

    Assumption

    Supposition

    Creativity

    Brainstorming

    Knowledge

    Facts

    Truth

    Evidence

    Confirmation

    Verification

    Proof

    Validation

    Do

    Check

    Act

    Plan

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    2b: Problem Solving Process

    In Six Sigma, the PDSA cycle is called "define, measure, analyze,

    improve, control" (DMAIC).

    Experiment

    HypothesisImplementation

    Evaluation

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    Source: http://timoelliott.com/blog/2007/06/intestine_based_decision_makin.html

  • 3: Summary of D.O.E Tools and Their Effectiveness

    Classical Taguchi Shainin

    Technique

    Effectiveness

    Cost

    Complexity

    StatisticalValidity

    Applicability

    Ease ofImplementation

    Several Approaches Fractional Factorials,EVOP..

    Moderate (3:1 Improvement) Retrogression Possible

    Moderate Average of 50 experiments

    Moderate Full ANOVA required

    Low Higher order & 2nd order interaction effects confounded with main effects To a lesser extent, even 2nd order interaction effects confounded

    Requires hardware Main use in production

    Moderate Engineering and statistical knowledge required

    One Approach Orthogonal Arrays

    Low to Moderate (Up to 2:1 Improvement) Retrogression Likely

    High Average of 50 to 100 experiments

    High Inner and outer array multiplication S/N,ANOVA

    Poor No randomization Even 2nd order interaction effects confounded with main effects

    Primary use as a substitute for Monte Carlo Simulation - Questionable Results

    Difficult Engineers not likely to use technique

    Characteristics

    Minimum of 8 Approaches

    Extremely powerful (100% to Up to 50:1 improvement) No Retrogression

    Low Average of 20 to experiments

    Low Experiments can be Implemented by line operator.

    High Excellent separation and quantification of main and interaction effects

    Requires hardware Can be used as early as prototype and engineering run stage

    Easy Even line workers conduct experiments

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    Part II: APPROACHES TO DESIGN OF

    EXPERIMENTS

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    4: Possible Objectives of the Experiment

    Find the variables that have a significant effect on the response

    Find where to set the significant variables so that a desired

    response is obtained

    Find where to set the significant variables so that the response

    has small variability

    Find where to set the significant variables so that the effect of

    nuisance variables on the response is small

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    5: Cause and Effect Diagram

    A brainstorming tool developed by Ishikawa to find possible

    causes for a defined effect.

    Sometimes referred to as a fishbone diagram

    Material Laser Galvo Scanner

    power

    pulse width

    wavelength

    repetition rate

    M^2flatness

    coating

    roll direction

    alloy type

    thickness

    duty cycle

    divergence

    power stabilitypulse rise time

    pulse fall time

    polarization

    beam spot size

    scanner speed

    laser on delay

    laser off delay

    jump speed

    field size

    Beam perpendicularity

    Rayleigh Range

    Working Distance

    Contr

    ast R

    atio

    Of M

    ark

    ed C

    hara

    cte

    rs

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    6: Designed (Controlled) Experiment

    Systematic controlled changes of the inputs (factors) to a

    process in order to observe corresponding changes (effects) in

    the output (response).

    Controlled experiments can be used to establish cause and

    effect relationships.

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    7: Responses

    Response is the measured variable of interest

    There may be more than one response

    Plan how you will measure the response variable(s)

    Examples: material removal rate (MRR), kerf width, hole diameter,

    taper, circularity, scribe depth, even layer by layer removal, surface

    finish (roughness, recast, flash, debris), metallurgical

    characteristics & Heat Affected Zone (HAZ)

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    11: Taper

    Courtesy of Mr. Xinbing Lui of Panasonic Boston Laboratory

    Nozzle diameter standarddeviation not to exceed 2%

    Stringent taper tolerancerequired to fabricate inkjetnozzle plates

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    12b: Surface Finish: Micro-cracking

    UV grade fused silica Infrasil Fused quartz

    266 nm DPSS

    Pulsed CO2

    Ultrafast

    Q-switched CO2

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    13: Heat Affected Zone (HAZ)

    Disk laser cutting of Nitinol

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    14a: Factors

    Factors are the controlled variables of interest in the experiment

    They are the variables that are changed during the experiment

    in a controlled manner

    Examples: Laser, beam delivery, motion system, assist gas,

    material parameters, etc.

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    14b: List of Possible Factors

    Laser

    Power Power Stability Wavelength Spectral Width Repetition Rate Pulse Width Duty Cycle Pulse Rise & Fall time Beam Divergence Beam M^2 Focused Spot Size Focused Spot Rayleigh Range Beam perpendicular to

    processing plane

    Process Gas and Delivery

    Assist Gas Type Assist Gas Purity Level Assist Gas Pressure Nozzle Diameter Nozzle Design Nozzle Beam Alignment Nozzle Stand-off Exhaust Rate Exhaust Location Water Assist

    Motion System

    Linear Motion Speed(Cutting Speed)

    Acceleration andDeceleration

    Motion System Tuning Corner Angle & Radius Scanner delay times Cut Program Direction

    Material

    Type (Alloy, Composite) Mechanical Properties Optical Properties Surface Condition Thickness Uniformity Tube Circularity Flatness Waviness Roll Direction

    Ambient

    Temperature Humidity

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    18: Variables Held Constant

    These are the variables controlled at fixed levels

    Their effect on the response is not of interest in the experiment

    Examples: parameters fixed due to laser, beam delivery or

    motion system architecture, assist gas type and pressure,

    nozzle diameter, focused spot size, etc

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    19: Blocking Concept

    It is possible to have small differences in: Composition of various batches of raw material

    Methods used by various operators

    Temperature, humidity, etc on various days

    Blocking is a technique to define groupings with homogeneous

    conditions of: raw material, operators, days, etc that may affect

    the experiment

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    20a: Randomization Concept

    Randomization is done to balance out the effect of noise and

    extraneous variables that may affect the response

    Randomization should include:

    The order (sequence) of conducting the experimental runs

    The selection and assignment of materials, operators, machines,

    subjects, locations, etc. to experimental conditions

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    20b: Table of Random Numbers

    80 14 67 29 70 44 69 53 51 58 40 45 4 31 85 25 6 31 74 14 55 13 34 95 3448 58 6 90 36 35 19 94 38 13 25 42 21 79 44 94 13 4 56 70 27 67 42 34 3969 63 85 3 17 82 5 22 26 54 84 78 47 0 91 29 87 90 47 74 32 27 54 83 6639 65 78 11 40 48 40 23 30 25 45 32 15 9 3 12 14 4 28 68 89 49 73 50 8761 18 41 7 27 3 83 48 10 88 22 66 22 32 45 30 6 86 5 80 33 72 10 21 7

    15 66 33 12 4 90 82 6 33 70 83 57 49 96 12 47 9 73 18 89 80 80 95 24 7379 12 39 88 47 37 8 18 99 69 31 89 46 64 6 50 48 47 81 51 66 16 10 83 5027 95 81 3 65 75 84 46 62 60 92 95 15 44 89 41 61 31 28 11 56 61 47 62 3934 62 68 17 22 27 56 90 53 45 21 84 83 43 71 57 86 34 64 31 55 72 44 19 7557 16 83 35 96 13 39 71 72 93 42 3 71 92 50 63 24 59 37 34 49 80 31 87 49

    3 74 9 96 37 29 11 25 26 30 44 85 78 39 31 50 75 7 35 22 78 66 71 82 3021 49 58 38 12 72 74 55 91 52 59 25 79 39 10 73 73 13 38 19 56 79 10 23 611 8 72 1 8 11 19 88 12 53 3 46 91 4 72 58 26 90 69 37 96 69 43 77 717 92 88 46 16 1 14 31 9 43 85 28 54 31 99 1 21 42 89 87 90 5 10 66 170 35 91 61 58 51 71 83 74 61 91 8 15 42 95 96 23 86 42 82 44 16 97 91 51

    69 65 46 7 6 41 49 47 49 35 47 5 54 15 36 8 80 8 71 18 28 87 3 32 6791 11 32 74 42 38 72 55 49 63 27 68 23 4 70 8 52 87 6 76 45 25 35 4 6690 12 32 72 44 80 14 83 88 71 74 88 72 99 80 46 29 2 19 95 90 4 84 79 9739 91 70 7 15 72 84 78 86 96 33 50 5 30 39 55 86 65 96 26 55 90 14 49 7742 16 79 69 40 1 93 70 59 12 30 30 45 26 5 67 29 77 7 2 7 14 59 57 49

    16 49 20 58 56 75 44 82 68 78 34 55 25 55 37 96 71 4 43 34 21 37 49 68 108 73 64 39 27 99 97 54 58 63 98 71 95 15 19 90 55 54 11 34 10 72 30 18 3885 2 70 67 40 94 74 38 49 33 29 82 94 51 6 8 89 74 42 81 95 25 29 27 018 45 98 50 14 3 57 15 14 90 52 60 45 92 97 33 44 90 94 76 95 81 33 17 4977 27 24 53 8 73 76 28 93 74 49 62 57 47 67 55 47 33 23 3 43 47 19 9 73

    43 40 76 93 60 45 2 82 51 24 56 89 90 75 88 1 13 31 66 69 45 60 7 7 765 67 50 60 7 69 77 74 54 37 32 28 7 96 40 37 38 57 53 63 73 0 96 7 1930 35 40 31 60 53 58 76 92 77 86 97 4 13 34 29 59 96 9 75 54 54 85 24 9138 40 85 73 33 27 79 42 41 54 39 73 48 45 4 32 62 9 1 70 37 75 20 71 3126 53 35 39 64 82 61 1 55 35 71 77 76 41 17 23 60 78 37 37 61 9 73 92 72

    56 83 50 74 40 22 50 35 34 40 35 7 41 34 35 14 66 78 87 83 43 77 88 59 5737 47 15 8 1 65 9 41 94 52 40 19 62 84 64 43 89 21 77 54 56 94 57 17 723 93 15 95 92 40 20 5 92 91 97 99 45 4 43 87 80 30 32 52 96 97 84 7 6632 66 85 76 53 14 4 51 43 11 69 70 35 32 11 39 91 95 55 55 85 36 5 79 082 82 59 19 21 24 71 64 65 81 11 45 14 31 73 97 11 66 62 5 67 87 68 89 20

    42 57 30 94 10 98 25 52 45 93 69 16 76 34 62 9 32 93 6 11 69 36 79 37 1341 56 71 3 9 35 21 28 22 8 74 78 81 76 21 83 3 93 54 37 76 35 43 53 5020 24 77 27 5 9 21 7 20 52 14 11 1 89 54 22 96 29 26 82 73 94 85 32 019 62 31 92 88 76 14 49 65 8 71 69 91 66 86 56 66 50 13 74 55 54 25 78 2348 40 52 61 27 67 1 4 20 62 52 33 44 51 79 40 45 74 83 59 83 32 80 43 12

    Source: K. Bhote, World Class Quality

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    21: Confounding Concept

    If two or more factors are confounded and show significanteffect, we will not be able to distinguish and single out thesignificant factor.

    Experiment:

    Response: Increased gas mileage

    Possible factors: expensive higher octane gas, higher quality oil

    Treatment: switch to both at the same time

    Results: Mileage improves significantly

    Results are confounded, it is not possible to tell is the improvementis due to gas or oil.

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    PART III: SHAININ DESIGN OF EXPERIMENTS

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    22a: Dorian Shainin

    A quality engineering pioneer, Dorian Shainin (19142000), isresponsible for the development of over 20 statistical engineeringtechniques.

    He worked to improve the quality and reliability of an array of products,including paper, printing, textiles, rubber, nuclear energy, airplanes,automobiles, cassette decks, space ships, light bulbs, representingover 200 different industries, ranging from the U.S. Department ofDefense, Rolls Royce Ltd. and Exxon to Polaroid, Hewlett-Packard,AT&T and Ford Motor.

    During the 1960s Shainin worked for Grumman Aerospace as areliability consultant for NASA's Apollo Lunar Module. Theeffectiveness of his approach was demonstrated by zero failures ineleven manned missions, six of which featured moon landings. Whenthe command module became uninhabitable during the failed Apollo 13mission, the Lunar Module became the lifeboat that brought the Apollo13 astronauts to lunar orbit and back to Earth.

    During the years that Shainin served as a reliability consultant for Pratt& Whitney Aircraft, he worked on the hydrogen-oxygen fuel cell thatpowered Apollo environmental life support in addition to the RL-10cryogenic liquid rocket engine. The RL-10 soon became America'smost reliable space engine, at one point logging 128 ignitions in spacewithout a single failure.

    My particular technique is to say to people, Lets stop guessing.Instead, lets find cluessources of knowledge that you just would nothave otherwise.Dorian Shainin --Wikipedia

    Talk to the parts.--Dorian Shainin

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    22b: Weakness of Classical/Taguchi D.O.E.

    Interaction are effects confused with main effects

    Engineering guesses instead of talking to the parts or process

    One or two approaches vs. several different approaches

    Higher cost

    Difficult for engineers to understand and implement

    Longer time

    Poorer results - no breakthrough

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    23: Paretos Law and The Green Y, Red X

    Effect/Output

    Response/Green Y

    50%

    0%

    1 2 3 4 5 6 7 20...

    The Vital Few The Trivial Many

    Red X

    Pink X

    Pale Pink X

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    24: Defining the Problem: The Green Y

    Before the start of D.O.E., it is important to describe, define and

    quantify the problem, the Green Y.

    1. State problem in one sentence or one paragraph as a maximum.

    2. Quantify the Green Y in terms of i.e. defect levels (# of laser

    drilled holes with flash etc)?

    3. Can the Green Y be transformed into an variable on a scale, say,

    of 1 to 10 - with 1 being the worst and 10 being the best. This is

    known as a Likert scale.

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    0 1 2

    3 4 5

    25: Likert Scale

    best

    worst

    Source: K. Bhote, World Class Quality

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    Define the problem to be solved - The GreenY

    Time-to-Time(Temporal)

    Unit-to-Unit(Cyclical)

    Within Unit(Positional)

    Week-to-Week Day-to-Day Shift-to-Shift Hour-to-Hour

    Variation bw/consecutive unitsVariation amonggroup of unitsLot-to-Lot

    PositionComponentMachine-to-MachineTester-to-Tester

    6:1Ratio

    Determine Measurement Accuracy

    Do Multi-Variance Analysis

    26: Finding the Red X

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    1. Define the Problem (The Green Y)

    2. Quantify and measure the Green Y

    3. Review problem history

    4. Generate clues Multi-Variance analysis Components Search Paired Comparisons Product/Process Search

    5. Design of Experiments Variables Search Full Factorials B vs C

    6. Turn the problem on and off - B vs C

    7. Establish realistic specifications andtolerances

    27a: Seven Step Problem Solving Framework

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    27b: Clue Generating Tools

    Multi-Variance Chart

    Component Search

    Paired Comparison

    Product & Process Search

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    28: Finding the Red X: Multi-Variance Analysis

    Objective: Reduces a large number of unrelated, unmanageable

    potential causes to a family of fewer and related ones, such as

    time-to-time, part-to-part within part, machine-to-machine, test

    position-to-test position. Detects non-random trends.

    Where: Determines how a product/process is running; a quick snapshot

    without massive historical data that is of very limited usefulness.

    Replaces process capability studies in some white collar

    applications.

    When: At engineering pilot run, production pilot run or in production.

    Study Size: Min. 9-15 or until 80% of historic variation is captured.

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    29a: Paired Comparison

    Objective: Provides clues to the Red X by determining a repetitive

    difference between pairs of differently performing products.

    Separating important parameters that distinguishes bad from good.

    Where: There are matched sets of differently performing products

    (labeled good and bad) with that cannot be disassembled.

    When: At engineering pilot run, production pilot run or in production.

    Study Size: 6 to 8 pairs.

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    29b: Paired Comparison

    Procedure:

    1. Select one best unit and one worst unit from a number of good

    and bad units. Call this pair one. Observe and note differences

    between these two units. Differences can be visual,

    dimensional, electrical, mechanical, chemical including x-ray,

    electron scanning microscopes or any other method.

    2. Select a second pair of the 2nd best and 2nd worst unit.

    Observe and note differences, as in step one.

    3. Repeat the search process with a third, forth and fifth pair, etc.

    4. Usually by the fifth or sixth pair of observations, the difference

    will be repeated three or four times, providing a strong clue for

    the major cause of variation.

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    29c: Rank Analysis (Tukey Test)

    Procedure:

    1. Rank all readings of each quality characteristic from lowest to

    highest or vice-versa.

    2. Determine if each reading is good or bad.

    3. Draw a line near the top of the readings where the all bad

    change good or visa-versa. This is the top end count.

    4. Draw a line near the bottom of the readings where the all good

    changes to bad or visa versa. This is the bottom end count.

    5. Add the top and bottom end counts.

    6. A minimum of six total end counts is needed for a 90%

    confidence that there is a significant difference between the

    good and bad for that particular quality characteristic.

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    30: Variables Search

    STAGE OBJECTIVE

    1Ball Park

    2Elimination

    3Capping Run

    4Factorial Analysis

    To determine Red X. Pink X areamong the causes being considered.Assures repeatability of the disassembly and re-assembly process.

    To eliminate all unimportant causes and their associated interaction effects.

    To verify that the important causes aretruly important and that the unimportantcauses are truly unimportant.

    To quantify the magnitudes of the important main causes and their interaction effect.

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    31a: Validation: Better B vs. Current C

    4 Distributions of B vs. C Processes

    Worse Better

    1 C B Null Hypothesis(No Difference)

    C = Current Process B = Better (?) Process

    RESULTS

    2

    C BPink X

    3C B

    Red X

    4

    CB

    Super Red X

    Source: K. Bhote, World Class Quality

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    K = Difference between means of C and B,expressed in number of standard deviations

    Minimum Spacing: XB - XC K C

    Where:XB is the average of the B product/process.Xc is the average of the C product/process.

    B & C is the standard deviations of the B & C product/process respectively.K is 2.9 for a 90% confidence if B = C.K is 3.7 for a 90% confidence if B C.

    Meanof C

    Meanof B

    C B

    K

    31b: Permanency of Improvement

    Source: K. Bhote, World Class Quality

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    When You Expect:

    An improvement

    Design Change Process Improvement Yield Improvement Mfg. Method Change Improved Reliability, Life Use of New Equipment

    An Economy Gain

    Cost Improvement Cycle Time Improvement Safety Improvement Less Variation Open a Tolerance Ease of Manufacturing Space Reduction Eliminate an Operation/Test Faster Set-up Time Less Expensive Tooling Machine Efficiency Environmental Improvement Reduced Equipment Maintenance Increased Up-Time Use of an Alternate Vendor Use of an Alternate Component

    31c: Applications of B vs. C Trials

    Source: K. Bhote, World Class Quality

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    32a: Process Optimization: Scatter Plots

    Y

    XPositive Correlation

    (A) (B)

    Y

    XUnclear Positive Correlation

    Y

    XNegative Correlation

    (C)

    Y

    XNo Correlation

    (D)

    Source: K. Bhote, World Class Quality

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    Y

    XNon-Linear Correlation

    Y

    XInsufficient Data Range

    (E) (F)

    Y

    XCorrelation Through Stratification

    (G)

    32b: Process Optimization: Scatter Plots

    Source: K. Bhote, World Class Quality

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    Y

    XiRealistic

    Manufacturing Tolerance

    Regression Lineor Curve

    30 Random Examplesof Units Made to theCurrent Tolerance95% of Total Effect

    of Mfg Factors OtherThan X

    Cu

    sto

    me

    r R

    eq

    uir

    em

    en

    ts

    Hi

    Lo

    33c: Realistic Tolerances

    Source: K. Bhote, World Class Quality

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    PART IV: CASE STUDY

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    33a: Definition of The Case Study Scenario

    A medical device company manufactures a polymer mesh used

    to wrap broken bones after they are set

    This polymer mesh is cut and marked with laser

    Polymer meshes have been observed to crack in testing

    It is very important that time and cost efficient Shainin

    techniques are used to identify & quickly solve the problem

    because the time to create a single usable mesh is several days

    Milestone deadline is approaching

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    33b: Bone Mesh Manufacturing Process

    1. Custom expansion of polymer using a balloon

    2. Laser cutting of mesh and marking with a serial code

    3. Coating with a substance that makes the mesh neutral to the

    immune system

    4. Slicing the ends

    5. Sterilization

    6. Packaging

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    Process # of

    Parameters

    Balloon Expansion 11

    Laser Cutting 9

    Drying 5

    Anti-immune

    Coating

    12

    Slicing the Ends 8

    Sterilization 9

    Packaging 7

    Total Parameters 61

    33c: Application

    Goal: To find the Red X or keyparameter that affects polymer meshcracking and propose process tominimize cracks.

    Problem: There are 55 parameters inthe whole process chain. No time toproduce enough meshes for testingand evaluating each processcondition.

    Solution: Use Shainin Techniques toreduce sample quantity and still getabove 99% confidence in processchanges.

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    Best Marginal

    End Slicing Temp. ( C) 30 50

    Anti-Immune Coating Thickness

    (um)

    15 25

    Coating Drying Temp. Low High

    Sterilization Temp. ( C) 45 50

    Laser Power (W) 3.0 3.5

    Polymer Purity > 90% < 80%

    Wall Thickness (mm) 1 1.4

    Sample Units 3 3

    33d: Step 1-- Confirmation of Key Parameters

    Assume:

    Wall thickness is the Red X for radial strength.

    Sterilization is another important factor affecting cracking.

    Packaging conditions will affect cracking.

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    Sample After Testing I After Testing II

    Visual (# cracks ) Visual (# cracks)

    1T 34 49

    2T 28 55

    4T 37 54

    3C No cracks No cracks

    5C No cracks No cracks

    6C No cracks No cracks

    D/d =54:3=18 > 1.25, No overlap between the groups. This

    suggests that the Red X is in the selected process parameters.

    33e: Total # of cracks at one day after packaging

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    Sample After Testing I After Testing II

    Visual (# cracks) Visual (# cracks)

    1Ta 46 78

    2Ta 27 43

    4Ta 34 50

    3Ca 2 3

    5Ca 2 2

    6Ca 1 4

    D/d =49:18.5= 2.65 > 1.25, No overlap between the groups. This

    suggests again that the Red X is in the selected process parameters.

    33f: Number of cracks 14 days after packaging

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    Run 1 Run 2 Run 3 Run 4 Run 5 Run 6 Run 7 Run 8 Run 9Run

    10

    Run

    11

    Run

    12

    End Slicing

    Temp 50 C 30 C 50 C 30 C 50 C 30 C 50 C 30 C 50 C 30 C 50 C 30 C

    Anti-Immune

    Coating

    Thickness

    15 25 15 25 25 15 25 15 25 15 25 15

    Coating

    Drying TempLow High High Low Low High High Low High Low High Low

    Sterilization

    Temperature45 50 C 50 C 45 50 C 45 45 45 50 C 45 50 C 45

    Cutting

    Power3 W 3.5 W 3.5 W 3 W 3.5 W 3 W 3.5 W 3 W 3 W 3.5 W 3.5 W 3 W

    Wall

    thickness1 mm 1 mm 1 mm 1 mm 1 mm 1 mm 1 mm 1 mm 1 mm 1 mm 1 mm 1 mm

    Polymer

    Purity> 90% < 80% < 80% > 90% < 80% > 90% < 80% > 90% < 80% > 90% > 90% < 80%

    Sample Units 4 4 4 4 4 4 4 4 4 4 4 4

    33g: Step 2--Variables Search for Finding the Red X

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    Run 1 Run 2

    End Slicing Temperature ( C) 30 50

    Anti-Immune Coating Thickness

    (um)

    17 20

    Coating Drying Temp. Low High

    Sterilization Temp. ( C) 45 50

    Cutting Power (W) 3.5 3

    Polymer Purity < 80% > 90%

    Wall Thickness (mm) 1 1

    Sample Units 4 4

    33h: Step 3--Capping Run or Confirming the Effects

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    Stent Crack Variable Search

    -10

    0

    10

    20

    30

    40

    50

    60

    70

    80

    0 2 4 6 8 10 12

    Parameters

    Nu

    mb

    er

    of

    Cra

    cks

    Center Line

    Decision

    Limits

    Marginal

    Decision

    Limits Best

    Crack Variable Search

    Parameters

    Decision

    Limits

    Marginal

    Decision

    Limits

    Best

    33j: Chart for Step 1, 2 and Capping Run

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    33k: Conclusions from Step 1, 2 and Capping Run

    Key Parameters affecting mesh cracking:

    Red X End Slicing Temperature

    Pink X Coating Drying Temperature

    Laser cutting power, anti-immunity coating thickness and

    polymer purity at t=3 days have no effect on the number of

    mesh cracks tested.

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    33l: Coating Drying Temperature Study

    -2

    8

    18

    28

    38

    48

    58

    68

    Nu

    mb

    er

    of

    Cra

    cks

    Day 1

    Day 7

    Day 26

    Effect of Coating Drying Temperature on Product Life

    Low temp High temp

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    Process Coating Drying

    Temp

    Process Time

    Best Conditions Low 30 min

    Current Conditions High 60 min

    33m: Step 4--Confirming the New Process is Better

    Number of cracks at testing counted at day 1 and day 14 after

    sterilization.

    Radial strength tested at day 1 and day 14 after sterilization

    Implant performance is tested

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    33n: B vs C Study-- Summary of Results

    Mesh inspections and crack counts confirmed that the B

    process is better

    Implant evaluation for B process is equivalent to C process

    Proposed implementation of B process

    Low Temp Coating Drying Temperature

    Reduce drying process time

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    Number Process Total Cracks

    1 B 1

    2 B 3

    3 B 4

    4 B 5

    5 B 5

    6 B 5

    7 B 5

    8 B 6

    9 B 7

    10 C 7

    11 C 8

    12 B 10

    13 C 12

    14 C 13

    15 C 14

    16 C 14

    17 C 17

    18 C 17

    19 C 23

    20 C 30

    1. All samples were testedrandomly.

    2. Total end count = 16.5Confidence level > 99%

    (more than 10 end counts)

    3. Beta Risk

    Xb - Xc = 15.5 -5.1 = 10.4

    K = 1.03

    K x number of C samples= 10.3 < 10.4

    Beta Risk of 5% or Confidence level >

    95%

    4. Conclusion: B process is betterthan C process.

    33o: B vs. C Study--Cracks at Day 1: Tukey Test

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    33p: B vs. C-- Implant Testing

    Drug Released Rate

    0%

    10%

    20%

    30%

    40%

    50%

    60%

    70%

    80%

    90%

    100%

    1 hr 2 hrs 4 hrs 24 hrs

    Pe

    rfo

    rma

    nce

    Current

    Best

    Time (hour)

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    33q: Reported Testing Conclusions

    With limited time and sample size, it was found that end slicing and

    coating drying temperatures are important factors that affect mesh

    cracking.

    By adding a coating drying study, coating drying temperature was

    identified to have more effects on mesh cracking than process time.

    The proposed coating drying process from this study will benefit all

    polymer products since it significantly minimizes mesh cracks and

    extents life time of implant.

    IP rights have been created for new process tested by Shainin

    technique.

    Shainin D.O.E. techniques save resources and time for process

    optimization and is recommended for future process development.

  • ICALEO 2010 Laser Solutions Short Course Evaluation

    Course #4: Optimizing Laser Machining Processes for Yield and Throughput in Manufacturing using DOE (Design of Experiments) Course Instructor: Arzu Ozkan Please rate the following: (circle) Very Course Excellent Good Good Fair Poor Overall Course 5 4 3 2 1 Course Instructor 5 4 3 2 1 Presentation of material 5 4 3 2 1 Organization of material 5 4 3 2 1 Course well paced 5 4 3 2 1 Would you recommend this course to others in your profession? yes no

    What was the strongest feature of the course? What was not covered that you felt should have been covered (if anything)? What would you like to hear more about next time? What was covered that left an impression/impact on you? Suggestions & Comments (for this course or courses you would like in the future): Name: (optional)

    Please Use Reverse Side for Additional Comments.

    Please return evaluation form to the Registration Desk by Thursday afternoon

    or fax 407.380.5588 to LIA upon your return home.