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Ensuring reliability in lean new product development part2of2 24
This document discusses using Failure Mode and Effects Analysis (FMEA), Design Failure Mode and Effects Analysis (DFMEA), Design for Reliability (DFR), testing, and failure analysis in lean new product development. It covers key elements of lean NPD like defining value from the customer perspective, front-loading processes with knowledge, and eliminating waste. Methods like functional block diagrams, boundary diagrams, parameter diagrams, and process flow diagrams can help focus lean FMEAs on new design elements. Characteristics critical to customer value should be identified. Accelerated testing and failure analysis capture knowledge for continuous improvement.
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Ensuring reliability in lean new product development part2of2 24
- 1. Part 2: Part 2: Using FMEA, DFR, Test and Failure Analysis in Lean NPD John J. Paschkewitz ©2011 ASQ & Presentation John Presented live on Feb 24th, 2011 http://reliabilitycalendar.org/The_Re liability_Calendar/Short_Courses/Sh liability Calendar/Short Courses/Sh ort_Courses.html
- 2. ASQ Reliability Division ASQ Reliability Division Short Course Series Short Course Series The ASQ Reliability Division is pleased to present a regular series of short courses featuring leading international practitioners, academics, and consultants. academics and consultants The goal is to provide a forum for the basic and The goal is to provide a forum for the basic and continuing education of reliability professionals. http://reliabilitycalendar.org/The_Re liability_Calendar/Short_Courses/Sh liability Calendar/Short Courses/Sh ort_Courses.html
- 3. Part 2: Using FMEA,DFR, Test and Failure Analysis in Lean NPD
- 4. Overview • Introduction andDefinitions • Part 1: Lean Product Development – Lean vs. Traditional Product Development – Key Elements of Lean NPD • Customer Defines Value • Front Loaded and Knowledge Based • Eliminate Redesign Waste – Reliability Requirements • Part 2: Reliability Elements of Lean NPD – Lean FMEA and DRBFM – Critical Characteristics – DFR and Physics of Failure – Accelerated Testing to Failure – Failure Analysis and Knowledge Capture
- 5. Lean FMEA • Someteams attempt to lean FMEA process by creating product family FMEAs but fail to update FMEA for new applications or changes • Instead Lean FMEA Should Focus on New Design Features and Changes to Baseline Design to Assess Associated Risks
- 6. Tools to FocusLean FMEA • Diagramming Tools – Functional Block Diagram – Boundary Diagram – Parameter Diagram – Process Flow Diagram • Highlight Changes to Product or Process on the Diagrams
- 7. Functional Block Diagram AnnotateRetained and Changed Items & Functions
- 8. Boundary Diagram Construction Subsystem 1 Subsystem 3 Subsystem 2 Interface -Physical Interface -Info Transfer -Data Transfer Consider a Functional Block Diagram of the System -External Input With Modules and Interfaces FMEA Boundary
- 9. Parameter Diagram of Product, Process, System Noise • Forces Beyond Control Factors • Cause Output Variation • Environment Factors Response Signal (Output, Function) (Inputs) Product, Process, or System • Performance Mean, Std Dev • Controlled by Input Function • Static or Dynamic • Customer Requirement • May be Variable Control Factors • Functional Design Parameters • Fixed or Adjustable • Fundamental to Design of Function • Reduce Variation Elements of the P-Diagram
- 10. Process Flow Diagram Annotate Retained and Changed Process Steps
- 11. Selecting Process Stepsfor Analysis • On Process Flow Map: – Identify Steps Being Modified – Identify New Steps Required for New Product • Drill Down to Identify Sub-Steps Within the Target Steps Identified for Analysis • Complete Lean PFMEA on Selected Process Steps • Integrate with Previous PFMEA on Standard / Unchanged Process Steps
- 12. Key Characteristics • Include: – Product Features – Manufacturing Processes – Assembly Characteristics • That Significantly Affect: – Product Performance – Form, Fit, Function • Lean NPD Focuses on the Critical Few Characteristics the Customer Values
- 13. Key Characteristics Requirements Documents •CustomerSpecification •Regulatory •Dimensions •Appearance Requirements Document Drawings Robustness Tools Field History •Functional Block Diagram •Boundary DiagramItem / Process Step Potential Failure Potential Effect(s) of S e C l a Potential Cause(s)/ O c c Current Design Controls D e t R P Response & Recommended Target Action Results Action S O D R •P-Diagram Mechanism(s) Actions Complete E C E P Mode Failure v s u e N Taken Of Failure Date V C T N Function s r c Prevent Detect •Interface Matrix DFMEA & PFMEA Component Manufacture Mandrel to main shaft bore I.D. Re-load fixture #2 and mandrel Chain adj sub assy to housing Pre-load main shaft oil seal to PRE-LOAD DOWEL PINS TO Pre-load bearing to fixture #2 Wave washer to shifter lever Move or stage for final assy Retaining ring to top groove Retaining ring to top groove Shifter lever to shifter tube PRE-LOAD JACK SHAFT Lubricate bushing & seal HOUSING BUSHING TO Process Steps Shipping Damage Customer Vehicle Assembly Material handling Shifter tube to housing Receive Material Assemble shifter lever Que for final assy line PRE-LOAD PRIMARY Assessment Severity Primary Drive Manufacturing Process Steps Housing to fixture #2 Housing to fixture #1 Clamp to shifter tube O-ring to shifter tube SEAL TO FIXTURE Reload fixture #1 Housing to table Op 100 Step 1 Op 100 Step 2 Op 100 Step 3 Operate press Operate press Operate press Special Characteristics Potential Critical and Significant Matrix Reserved FIXTURE FIXTURE mandrel OP 340 Op 430 Op 520 Op 445 Op 500 Op 510 Op 530 Op 535 Op 120 Op 200 Op 210 Op 330 Op 110 Op 220 Op 230 Op 300 Op 310 Op 320 Op 350 Op 400 Op 410 Op 420 Op 20 Op 10 Direction of Improvement 1.090 TO 1.110 " FACE OF PRIMARY HOUSING BUSHING TO FACE OF JACK SHAFT SEAL 5 G F DOWEL PINS 0.260 TO 0.270 " TO 3 FACE JACK SHAFT SEAL AGAINST 9 H F SHOULDER H F BEARING FLUSH TO SNAP RING FACE3 G F G Technical Requirements, SEAL COMPRESSION HEIGHT 9 H G H HF HH PRIMARY GASKET SEAL SURFACE FINISH F 9 F Y HH HH H GG SERATION DAMAGE 5 F 261 81 81 72 41 27 54 54 81 27 45 Weighted Importance 0 0 0 0 9 0 3 0 3 0 0 0 9 9 0 0 0 0 0 0 0 Tools Identify Special Relative Importance Product Characteristics Characteristics Matrix
- 14. Identifying Key Characteristics 10 9 8 7 Severity 6 5 4 3 2 1 1 2 3 4 5 6 7 8 9 10 Occurrence Potential Critical Characteristic Possible Annoyance Zone Potential Key Characteristic
- 15. Potential Critical andSignificant SEAL FACE SHOULDER SERATION DAMAGE Matrix JACK SHAFT SEAL AGAINST SEAL COMPRESSION HEIGHT DOWEL PINS 0.260 TO 0.270 " TO Relative Importance Weighted Importance BUSHING TO FACE OF JACK SHAFT BEARING FLUSH TO SNAP RING FACE Special Characteristics Direction of Improvement PRIMARY GASKET SEAL SURFACE FINISH 1.090 TO 1.110 " FACE OF PRIMARY HOUSING 5 9 9 3 9 3 5 Severity 0 Receive Material 81 Material handling H 81 Shipping Damage H 72 Component Manufacture M M 0 Vehicle Assembly Op 100 Step 1 9 PRE-LOAD DOWEL PINS TO M FIXTURE Op 100 Step 2 41 PRE-LOAD JACK SHAFT L L M SEAL TO FIXTURE Op 100 Step 3 PRE-LOAD PRIMARY 0 HOUSING BUSHING TO FIXTURE Op 110 0 Pre-load bearing to fixture #2 Op 120 27 Pre-load main shaft oil seal to M mandrel Op 200 54 M M Housing to fixture #1 Op 210 261 H H H H M Operate press Op 220 3 L Retaining ring to top groove Op 230 0 Reload fixture #1 Op 300 54 M M Housing to fixture #2 Op 310 81 H M M Operate press Process Steps Op 320 3 H Retaining ring to top groove Characteristics from Requirements and DFMEA Op 330 0 Mandrel to main shaft bore I.D. OP 340 0 Operate press Op 350 0 Re-load fixture #2 and mandrel Op 400 27 M Housing to table Op 410 Primary Drive Manufacturing Process Steps 0 Reserved Op 420 45 H Chain adj sub assy to housing Op 430 9 L Lubricate bushing & seal Op 445 9 L Move or stage for final assy Op 10 0 O-ring to shifter tube Op 500 0 Shifter tube to housing Op 510 0 Clamp to shifter tube Op 20 0 Assemble shifter lever Op 520 0 Wave washer to shifter lever Op 530 0 Shifter lever to shifter tube Op 535 0 Que for final assy line Characteristics Process Steps from Flow Chart Effect of Step on Special Characteristics Matrix Customer Assessment
- 16. Developing the ControlPlan • Prioritize Process Risks Identified in the PFMEA and the Special Characteristics Matrix • Process Flow Diagram • Lessons Learned from Similar Processes • Process Control Data from Related Processes • Measurements Required for Process Control • SPC Control Limits • Complete the Items in Control Plan Template
- 17. Control Plan Items Machine,Device, Jig, For each operation that is described, identify the processing equipment machine, device, Tools for Mfg. jig, or other tools for manufacturing, as appropriate. No. Enter a cross reference number from all applicable documents such as, but not limited to, process flow diagram, numbered blue print, FMEAs, and sketches. Product Features or properties of a part, component or assembly that are described on drawings or other primary engineering info. Compilation of important product characteristics. Process Process variables that have a cause and effect relationship with the identified product characteristic. Identify those process characteristics for which variation must be controlled to minimize product variation. There may be more than one process characteristic for each product characteristic. Product/Process Specifications/tolerance may be obtained from various engineering documents, such as, but Specifications/ not limited to, drawings, design reviews, material standard, computer aided design data, Tolerance manufacturing, and/or assembly requirements. Evaluation/ Identify the measurement system being used, including, gages, fixtures, tools, and/or test Measurement/ equipment required to measure the part/process/manufacturing equipment. Technique Sample When sampling is required list the corresponding size and frequency. Control Method Brief description of how the operation will be controlled, including procedure numbers where applicable. Operations may be controlled by SPC, inspection, attribute data, mistake proofing, sampling plans, and other. If elaborate control procedures are used, reference document by ID name/number. Reaction Plan Specify the corrective actions necessary to avoid producing nonconforming products or operating out of control. May also refer to a specific reaction plan number and identify the person responsible for the action.
- 18. Using the ControlPlan • For Critical Characteristics, Use Control Plan to Identify: – Measurements: How, When, How Often – Controls to Keep Characteristic in Tolerance – Actions if Characteristic Out of Tolerance • Containment • Corrective Actions • Robust Design + Controlled Processes = Reliable Products
- 19. DRBFM and DRBTR DesignReview Based on Failure Modes & Test Results Key Elements of Mizenboushi (Reliability Problem Prevention) GD3 (Good Design, Good Discussion, Good Dissection) Toyota’s “Creative FMEA” Method
- 20. Problem Prevention –GD3 • Good Design = Robust Design – Design for Reliability (DFR) – Design for Six Sigma (DFSS) • Good Discussion = Eliminate Risk – Apply Design Review Based on Failure Modes (DRBFM) to identify problems and develop countermeasures or corrections • Good Dissection = Effective Validation – Apply Design Review Based on Test Results (DRBTR) to Evaluate Effectiveness. Test to Failure & Analysis of Test Failures is Critical
- 21. GD3 Problem Resolution Total Problems to be Solved Good Design OBJECTIVE: (Robust Design Discover To Prevent & Resolve Problems) Unknown All Problems Problems Before Launch Discovered Good Discussion Problems Good Dissection Development Pre-Production (Discover Unknown Problems) Validation
- 22. DRBFM Approach • Elementsfrom FMEA, FTA, and Design Review – These tools previously used for management and control of projects – Toyota developed “creative FMEA” approach – Shift focus to improve perceptiveness and problem solving • Focus is on finding and preventing problems – not completing forms and checklists (which de-motivate participants)
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- 24. DRBFM is aForum for Thinking Teamwork and Participation What has changed? * What did you change? Why? * What surrounding conditions have changed outside your control? Concerns about the changes? *Your Concerns? What other concerns? * Draw on expertise and knowledge of past problems When will concerns appear? *Could concerns become causes of failures or incidents? Visualize concerns & causes What effects will there be? *How will causes effect the customer? * Consider effects on the OEM and end user What preventive measures *What has been done to assure concerns will have been & should be taken? not actually appear? *Consider other measures that can be implemented Source: Bill Haughey, DRBFM, Applied Reliability Symposium, June 2007, March 2008
- 25. How is DRBFMDone? • Preparation for the Design Review • Conducting the DRBFM • Capturing the Inputs • Assigning and Tracking Actions to Completion
- 26. Pre-Work for theDRBFM • Design Engineer or Core Team: – Functional Diagram, Operating Environment – Changes from Previous Baseline Design – Drawings and Analysis – Failed and Sectioned Parts – Draft DRBFM with Components / Changes, Concerns with Causes and Factors, Effect on Customer, Design to Eliminate Concerns • Participants (Functional Experts): – Perceptive mindset, interest in improving product – Past experience and knowledge on similar items
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- 28. Typical DRBFM Session Source:A Guide to GD3 Activities and DRBFM Technique to Prevent Trouble, Kano & Shimizu, Toyota 2001
- 29. Changes and ResultsDocumented Source: Carl Hanser Verlag, QZ, Munich, 4-2005
- 30. Linking DRBFM withFMEA • DRBFM captures the information needed for FMEA except scoring • Scoring columns can be added to fill need for FMEA if required by customer or standards
- 31. DRBFM to FMEA(1) DRBFM Form: C Potential O D R Item Item Potential Potential S l Cause(s) / c Current e . P Function Failure Effect(s) of e a Mechanism(s) c Design t . N Mode Failure v s of Failure u Controls e . s r c FMEA Form Add Scores
- 32. DRBFM to FMEA(2) DRBFM Form: D Current e R. Recommended Responsibility Action Results Design t P. Actions & Target Actions S O D R. Controls e N. Date Taken e c e P. c v c t N. FMEA Form: Add Scores Add Scores
- 33. DRBFM System Integration Source:SAE Paper 2003-01-2877, Shimizu, Imagawa, Noguchi, Reliability Problem Prevention for Automotive Components
- 34. Applying DRBFM inLean NPD • Use “Missing Knowledge” Decision Flow from Lean QFD as starting point • These unknowns and known changes from current technology or design are the greatest risks • Focus DRBFM on these unknown and changed areas during concept and prototype team reviews & Integration Points
- 35. Integrating Product &Process Design • DFMA – Design for Manufacturing and Assembly • Integrated Product and Process FMEA / DRBFM • Concurrent Engineering Team • Visual Management – Decision Flow and Value Stream Map to Manage Tasks
- 36. Impact of LeanFocused FMEA • Allocation of Resources Targeted to Reduce Highest Risks and Unknowns • Impact Product and Process Design • Drive Test Planning and Analysis to Resolve Issues and Understand Unknowns • Verify Corrective Action Effectiveness • Critical Characteristics and Process Measurement / Control
- 37. Lean FMEA Summary •Focus FMEA on Changes in Design or Process • Use Supporting Tools to Narrow Focus: – Parameter & Boundary Diagrams – Process Flow Charts – DRBFM Techniques – Characteristics Matrix • Use Lean NPD Tools to Identify Unknowns, Apply Resources, Assign Tasks
- 38. Design for Reliabilityand Robustness
- 39. How do weDesign-in Reliability? • Stress Analysis and Test – Find Product Limits & Understand User Needs – Products fail due to variation or in limit environments where stress exceeds strength – Stress and strength distributions:
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- 42. Reducing Stress /Strength Interference • Increase strength of the part – Understand operating environment stresses – Select more robust parts or materials – Increase design margin – Supplement deterministic design with probabilistic tools • Reduce part strength variability – Understand sources of part variation and deterioration – Controlled production process (SPC) – Protect vulnerable components • ROBUST DESIGN + CONTROLLED PROCESSES = RELIABLE PRODUCT
- 43. Robust Design Tools DFSSand DFR Tools: Differences and Commonality
- 44. Probabilistic Design Applied ReliabilityEngineering, Rousch and Webb, Center for Reliability Engineering, University of Maryland, College Park, MD. Jan 2006
- 45. Reliability Based Design Optimization
- 46. Elements of ProbabilisticDesign • Understand physics of failure and stresses that precipitate failure • Use predictive modeling and accelerated test to failure to estimate probability of failure • Consider variability of applied stresses and variability of product strength • Eliminate stress-strength interference
- 47. Physics of FailureApproach • Robust Design Considerations • FMEA or DRBFM Methods – Design Review Based on Failure Modes Integrates FMEA and Design Review • Test to Failure and Understand Cause Mechanisms • Failure Analysis Methods
- 48. Understand Physics ofFailure • What physical phenomenon in the part is caused by the stresses applied? • If we understand the root cause, we can improve strength or reduce variability to prevent or mitigate the failure. • Most hardware failures can be traced to four physical categories / mechanisms: – Wear – Corrosion / Contamination – Mechanical Failure (fatigue, vibration resonance, etc.) – Overstress (electrical or mechanical, transients)
- 49. Physics of FailureTools • Tools Used in Physics of Failure Analysis – Principal Physics Model – CAD Drawings / Solid Modeling – Finite Element Analysis • Dynamic Simulation (Transients) • Fatigue Analysis (Cumulative Damage) • Thermal Analysis • Accelerated Testing • Simulation
- 50. Design of Experiments(DOE) • Tool to Evaluate Design Alternatives • Determine Factors and Response • May need Two Phased DOE Approach – Fractional Design to Find Main Factors – Full Factorial Design to Evaluate Effects and Interactions on Reduced Set of Factors – Consider Time and Cost • Analysis of Results and Optimization of Solution
- 51. Iterative DOE Process LarryGonzales, Raytheon, Experiment Design for Engineers & Scientists, Applied Reliability Symposium, 2009.
- 52. Use Trade-Off Curvesto Capture Knowledge • Point Data from Analysis and Experiments • Relationship Between Key Parameters • Apply to Support Design Decisions
- 53. Trade-Off Curves Capture Knowledge from Point Solutions
- 54. Trade Off CurveExample
- 55. Key is Understanding • Methods Build Knowledge of Alternatives – Physics of Failure – Design of Experiments – Design for Robustness and Reliability • Enable Better Design Decisions • Eliminate or Reduce Redesign Waste
- 56. Reliability Testing andData Analysis
- 57. Phased Robustness Testing •Prototype Phase – Accelerated Test to Failure (Well beyond Spec – HALT, Step Stress, Specific Stresses and Failure Modes) • Design Verification Phase – Quantitative Accelerated Life Test – Selected Qualification Tests • Production Validation – Demonstrate Corrective Action is Effective – Validate Final Product Made on Production Tools
- 58. Robustness Indicator Figure Requirement or Margin or Specification Robustness of Design Factor If Requirement Exceeds Test Result or has Small Margin, Design is Not Robust Factors (Temperature, Vibration, Humidity etc) Analysis & Test Results for Each Factor on current or (Can be Created in Excel using Radar Chart) new product
- 59. General Approach toAccelerated Life Test (ALT) • Understand Failure mechanisms • Understand Operating and Design Limits • Clarify Use Level Stress Application • Conduct Qualitative tests like HALT or step- stress tests to define product limits and failure modes • Conduct Quantitative ALT to extrapolate life at use level conditions – Times to Failure at Accelerated Stress Levels – Use life-stress relationships and distributions
- 60. ALT Plan • Stresses to be Considered • Life-Stress Relationship for Each Stress • Application Use Level for Each Stress • Use Level Failure Criteria / Threshold • Test Duration and Resources Available • Consider Use of DOE to help estimate: – Stress Factors with Most Effect – Probability of Failure at Specified Use Level – Probability of Failure at Maximum Stress – Interactions to Help Define Life-Stress Relationship
- 61. Highly Accelerated LifeTest (HALT) – Qualitative ALT 1. Improve Reliability by Finding Weaknesses and Correcting Them Early. 2. Establish Upper and Lower Operating and Destruct Limits of Environmental Stressors 3. Typically done in Temperature & Vibration Chamber for Electronics & Electromechanical Products 4. Concept can be Applied to Other Stressors (Voltage, Current, Mechanical Loads, etc.)
- 62. Quantitative ALT • Testto Failure at Multiple Accelerated Stress Levels • Use Analysis to Extrapolate Reliability or Life at Application Use Level Stress • Can be Used to Demonstrate Ability to Meet Reliability Requirements
- 63. Cautions on Acceleration •Understanding product limits helps prevent accelerating to unrepresentative stresses and failure modes • Time – Consider Heat Buildup – Effects of Cycling • Temperature – Material Phase transitions – Non-linear response – High temperature or thermal cycling? • Power – Protective and limit devices – Transients • Vibration – Mechanical limits or resonances • What failure mechanism are we accelerating?
- 64. Data Collected • TestParameters Measured – Temperature, Power Density, Cycle Rate, Vibration, Humidity, Voltage, etc. applied – Product Response or Function (monitor during test) • Time to Failure or Run Time (Suspended) – At least 3 Different Stress Levels – Fit Data Points to Appropriate Distribution • Product Limits from Step Stress Test • Failure Mode Observations
- 65. Data Analysis • AnalyzeData and Extrapolate Life at Use Level Stress • Life-Stress Relationships (predictive models) – Arrhenius – Temperature – Eyring – Temperature or humidity – Inverse Power Law – Voltage, Power, Mechanical – Multiple Life-Stress Models • Temperature / Humidity • Temperature / Non-Thermal: Temp / Voltage or Power • General Log Linear: multiple accelerating stresses • Proportional Hazards: multiple covariates • Cumulative Damage – Time varying stress profiles
- 66. Data Analysis –Use Level ReliaSoft ALTA 7 - www.ReliaSoft.com Use Level Probability Weibull 99.000 Use Level CB@90% 1-Sided TB 90.000 Data 1 General Log-Linear Weibull 328|10|1 F=35 | S=51 Data Points Use Level Line 50.000 Top CB-I Bottom CB-I 10.000 Unreliability 5.000 1.000 0.500 John Paschkewitz Watlow Electric Mfg Co 2/4/2008 0.100 3:39:07 PM 1000.000 10000.000 100000.000 Time Beta=3.7483; Alpha(0)=-6.0220; Alpha(1)=5776.9341; Alpha(2)=-1.4340; Alpha(3)=0.6242
- 67. Data Analysis -Distribution ReliaSoft ALTA 7 - www.ReliaSoft.com Probability Density Function 3.000E-4 Pdf Data 1 General Log-Linear Weibull 328|10|1 F=35 | S=51 Pdf Line 2.400E-4 1.800E-4 f(t) 1.200E-4 6.000E-5 John Paschkewitz Watlow Electric Mfg Co 2/4/2008 0.000 3:41:01 PM 0.000 4000.000 8000.000 12000.000 16000.000 20000.000 Time Beta=3.7483; Alpha(0)=-6.0220; Alpha(1)=5776.9341; Alpha(2)=-1.4340; Alpha(3)=0.6242
- 68. Life vs. Stressas Trade-Off Re l i a S o ft AL T A 7 - w w w .Re l i a S o ft.c o m L if e v s S t r e s s 1 0 0 0 0 .0 0 0 L i fe CB@ 9 0 % 1 -S i d e d T B A L T C y c le s f r o m 2 5 0 t o 4 0 0 C Ax c e l i s AL T N i Cr W W D L -S I n v e rs e P o w e r L a w L o g n o rm a l 1 3 2 .4 F = 5 | S= 1 A L T C y c le s f r o m 2 5 0 t o 4 3 0 C M e a n L i fe L i n e T o p CB M e a n Bo tto m CB M e a n 1 5 7 .8 S tre s s L e v e l P o i n ts R eg ion of A L T C y c le s f r o m 2 5 0 t o 5 0 0 C M edia n Point I m pos ed Pdf 1 0 0 0 .0 0 0 1 8 6 .7 A c c e p ta b l e S tre s s L e v e l P o i n ts C y c le s M edia n Point W a tt D e n s i ty 2 8 1 .6 I m pos ed Pdf S tre s s L e v e l P o i n ts M edia n Point R eg ion of I m pos ed Pdf L if e , U n a c c e p ta b l e 0 . 1 6 8 " d ia s h e a t h W a tt D e n s i ty . 0 2 1 " d ia P C N iC r w ir e c y c le d u s in g 1 0 0 .0 0 0 c o n t r o lle d d u t y c y c le ram p ov er 78 m in u t e c y c le J o h n P a s c h k e w i tz W a tl o w E l e c tri c M fg Co 10/ 8/ 2009 1 0 .0 0 0 3 :0 6 :0 5 P M 5 0 .0 0 0 1 0 0 .0 0 0 132 187 282 500 700 1 0 0 0 .0 0 0 W ir e W a t t D e n s,it y s i w S td = 0 .7 9 3 7 ; K= 7 .1 3 5 0 E -1 2 ; n = 3 .6 5 5 6
- 69. Production Validation Test •Repeat selected Qualification Tests on any Changes in Product or Process • Test Samples made on Production Processes • On-Going Reliability Test (ORT) – HASS – Highly Accelerated Stress Screening – HASA – Highly Accelerated Stress Audit – Periodic HALT Re-Test on Production Units
- 70. Failure Analysis /FRACAS
- 71. Failure Analysis Tools •Basic – Recovery of Failed Samples – Electrical Test, Microscopy, Digital Photography • Non-Destructive Methods – X-Ray (Real Time Digital is Particularly Helpful) • Disassembly / De-capsulation – Tools or Chemicals to remove layers • Scanning Electron Microscopy & EDS – Defects, Corrosion, Material Failure • Acoustic Microscopy / Imaging (Voids / Defects) • Some Internal, Others at Outside Labs
- 72. NDT – ElectricalCharacteristics Curve Tracer – Showing Good and Failed Part Response
- 73. Real Time DigitalX-Ray
- 74. Real Time X-RayExample
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- 77. Example of SEM/ EDS Analysis Pt: Rh: Al 87:10 : 3 Pt : Rh : Si 82.7:10.3:6.7
- 78. PCB Failure AnalysisMethods Thomas Paquette, Insight Analytical Labs, Test & Measurement World, August 2006.
- 79. Failure Analysis Summary •Progressive Use of Tools from NDT to Dissection and Cross-Section Exam • Objective is to Find Physical Evidence of Failure Mechanism • Document with Photos and Analysis to Capture Knowledge Gained • Update FMEA or DRBFM with FA Findings
- 80. FRACAS Failure Reporting, Analysis & Corrective Action System • Build Knowledge Base • Process and Tool – Reliability & Quality of Product, Service, Process or Software is Tracked, Measured, and Improved – Applies to Entire Product Life Cycle – Consistently Ranked Among the Most Important Reliability Tasks – Closed Loop: Ability to Feed Root Cause & Corrective Action Information Back Into Design Process for Further Improvement
- 81. Hierarchy of FailureCauses Customer Induced Repair Induced Manufacturing & Quality Related Failures Design Related Failures Capture Failures from Verification Test to Field Operation
- 82. Capturing FA Knowledge •Capture Failure Analysis Results in Searchable Tool – Commercial Data Base Tool – A3 Format Documents with Keywords – SharePoint (Microsoft) • Key is Ability to Retrieve Knowledge with Minimal Search Effort • Lean NPD is Knowledge Based – Key is Continually Adding to Accessible Knowledge
- 83. Summary • Features ofLean NPD for Reliability – Front End Focus to Gain Knowledge • Basis for Better Design Decisions – Design for Robustness, Reliability – Understand Physics of Failure • Testing to Learn and Verify – Test to Failure and Understand Causes • Knowledge Capture for Future Re-use • Develop & Control Critical Characteristics
- 84. References • King, JohnP. and Jewett, William S.; Robustness Development and Reliability Growth; Prentice-Hall, Boston, 2010. • SAE International, J1211, April 2009, Handbook for Robustness Validation of Automotive Electrical / Electronic Modules. • Robustness Validation Manual, ZVEI, January 2010; www.zvei.org/RobustnessValidation • Jusko, Jill; New Models for Product Development, Industry Week, April 21, 2010. • Morgan, James and Liker, Jeffrey; The Toyota Product Development System, Productivity Press, New York, 2006.
- 85. References • Sarakakis, Georgios;Fundamentals of Life Data Analysis: Concepts and Applications, Tutorial, 2010 Applied Reliability Symposium Proceedings, June 17, 2010. • Wiggins, Brian, “A Simpler Look at Product Development”, Product Design & Development, October 8, 2010. • Mascatelli, R., The Lean Product Development Guidebook, 2007. • Soderborg, Dr. Nathan, Lean Product Development, WCBF DFSS Conference, Feb. 2008 • Using DOE Results in Design of ALT, Reliability Edge, Vol 10, Issue 2, pp. 1-7.
- 86. References • SAE 2003-01-2877,Reliability Problem Prevention Method for Automotive Components, H. Shimizu, T. Imagawa, H. Noguchi. • A Guide to GD3 Activities and DRBFM Technique to Prevent Trouble, S. Kano, H. Shimizu, Toyota, 2001. • Lean Product Development, Eric Rebentisch, Oct 5, 2005, MIT Open Courseware, http://ocw.mit.edu/courses/aeronautics-and-astronautics/16-852j- integrating-the-lean-enterprise-fall-2005/lecture-notes/8_rebentisc_leng.pdf • Bill Haughey, DRBFM, Applied Reliability Symposium, June 2007, March 2008 • Lean FMEA Training, Quality Associates International, at www.quality-one.com • AIAG, FMEA, 4th Edition, June 2008, pp.135-138.
- 87. Feedback / Follow-up •Please provide your feedback on this web based short course: e-mail to jjpengr@gmail.com or to ASQ RD • One day seminar on this topic available through: http://www.hobbsengr.com/Accelerated_R eliability_Seminar_Schedule.htm – Apr 13, 2011 in Chicago, IL – May 2, 2011 in Minneapolis, MN