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Reduce the risk of cracking by a
factor of 10 A Better by Analysis™ approach
Leon Daly
Analysis & Operations Manager
Motovated Design & Analysis Ltd
Copyright 2018
Minimum Viable Simulation (MVS)™
• Minimize batch size
• Timebox work
• Prioritize validated learning
• Use Moore’s law
• Train designers in analytical methods
• Systematise psychological safety
Email Leon@motovated.co.nz for slides
Fatigue
Material fatigue is a phenomenon where structures fail when
subjected to a cyclic load. This type of structural damage
occurs even when the experienced stress range is far below
the static material strength. Fatigue is the most common
source behind failures of mechanical structures.
https://www.comsol.com/multiphysics/material-fatigue
Email Leon@motovated.co.nz for slides
Fatigue
• Why fatigue matters
• Fatigue evaluation methods
• Fatigue concepts – stress life
• What’s really important (design killers)
• Increasing part life by a factor of ~14000; an example
Email Leon@motovated.co.nz for slides
Why fatigue matters
Email Leon@motovated.co.nz for slides
Fatigue evaluation strategies
• Good design
• Static allowable stress (rules of thumb)
• Infinite life approach (i.e. endurance limit)
• Safe life
• Fracture mechanics
Email Leon@motovated.co.nz for slides
Fatigue concepts – stress life
Email Leon@motovated.co.nz for slides
What's really important
1. Surface finish
2. Surface treatment
Email Leon@motovated.co.nz for slides
Effect of surface treatments
1. Shot peening (Steel and Aluminium) +50%
2. Nitriding (Steel): +50%
3. Weld toe grinding (Steel): +30%
4. Induction/flame hardening (Steel): +30%
Note: 50% increase in fatigue strength:
≈ 3.5 fold increase in part life (if welded)
≈ 15 fold increase in part life (typical machined part)
Email Leon@motovated.co.nz for slides
Effect of surface treatments - continued
1. Zinc plating (Steel): No change
2. Hot dip galvanising (Steel): -40%
3. Chrome, Nickel, and Cadmium plating (Steel): -50%
4. Corrosion (Steel): -50%
5. Anodising (Al alloys): -62%
Note: 50% increase in fatigue strength:
≈ 3.5 fold increase in part life (if welded)
≈ 15 fold increase in part life (typical machined part)
What's really important
1. Surface finish
2. Surface treatment
3. Preload (bolts)
Email Leon@motovated.co.nz for slides
What's really important
1. Surface finish
2. Surface treatment
3. Preload (bolts)
4. Maximising the difference between component stress and
material strength.
Email Leon@motovated.co.nz for slides
Reducing component stress
Stress reduces from top left to
bottom right of diagrams:
Email Leon@motovated.co.nz for slides
A worked example
Email Leon@motovated.co.nz for slides
A worked example
Email Leon@motovated.co.nz for slides
A worked example
Original stress = 71.8 MPa
Optimised stress = 42.9 MPa
Reduction factor = 0.6
Email Leon@motovated.co.nz for slides
A worked example
Original stress = 71.8 MPa
1. Initial life: 56 hours (50% nominal probability of failure)
2. Increase reliability to ~99%: 5 times life decrease = 11 hours
3. Reduce stress as per example above: 58 times life increase
4. Change material from medium tensile AISI 1040 to PH 17-4
stainless steel: a further 247 times life increase
5. Final life estimate: 158000 hours/6470 days
Email Leon@motovated.co.nz for slides
• 38 bogies built
• Several have hit the
1.1 million km mark!
Case study – KiwiRail passenger bogies
Email Leon@motovated.co.nz for slides
Summary
1. Lean/Agile methods can make a big difference in Simulation
2. Be aware of good fatigue design practice
3. Be careful with component surface treatments
4. Bolt preload is your friend
5. Use good materials and minimise stress
Email Leon@motovated.co.nz for slides
Thank You!
Leon Daly
Leon@motovated.co.nz
General Manager
Motovated Design & Analysis Ltd
www.motovated.co.nz
+64 3 382 5282
Email Leon@motovated.co.nz for slides
Fatigue concepts – stress life
Email Leon@motovated.co.nz for slides

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Reduce the risk of your part cracking by a factor of 10 with sensible analysis

  • 1. Reduce the risk of cracking by a factor of 10 A Better by Analysis™ approach Leon Daly Analysis & Operations Manager Motovated Design & Analysis Ltd Copyright 2018
  • 2.
  • 3. Minimum Viable Simulation (MVS)™ • Minimize batch size • Timebox work • Prioritize validated learning • Use Moore’s law • Train designers in analytical methods • Systematise psychological safety Email Leon@motovated.co.nz for slides
  • 4. Fatigue Material fatigue is a phenomenon where structures fail when subjected to a cyclic load. This type of structural damage occurs even when the experienced stress range is far below the static material strength. Fatigue is the most common source behind failures of mechanical structures. https://www.comsol.com/multiphysics/material-fatigue Email Leon@motovated.co.nz for slides
  • 5. Fatigue • Why fatigue matters • Fatigue evaluation methods • Fatigue concepts – stress life • What’s really important (design killers) • Increasing part life by a factor of ~14000; an example Email Leon@motovated.co.nz for slides
  • 6. Why fatigue matters Email Leon@motovated.co.nz for slides
  • 7. Fatigue evaluation strategies • Good design • Static allowable stress (rules of thumb) • Infinite life approach (i.e. endurance limit) • Safe life • Fracture mechanics Email Leon@motovated.co.nz for slides
  • 8. Fatigue concepts – stress life Email Leon@motovated.co.nz for slides
  • 9. What's really important 1. Surface finish 2. Surface treatment Email Leon@motovated.co.nz for slides
  • 10. Effect of surface treatments 1. Shot peening (Steel and Aluminium) +50% 2. Nitriding (Steel): +50% 3. Weld toe grinding (Steel): +30% 4. Induction/flame hardening (Steel): +30% Note: 50% increase in fatigue strength: ≈ 3.5 fold increase in part life (if welded) ≈ 15 fold increase in part life (typical machined part) Email Leon@motovated.co.nz for slides
  • 11. Effect of surface treatments - continued 1. Zinc plating (Steel): No change 2. Hot dip galvanising (Steel): -40% 3. Chrome, Nickel, and Cadmium plating (Steel): -50% 4. Corrosion (Steel): -50% 5. Anodising (Al alloys): -62% Note: 50% increase in fatigue strength: ≈ 3.5 fold increase in part life (if welded) ≈ 15 fold increase in part life (typical machined part)
  • 12. What's really important 1. Surface finish 2. Surface treatment 3. Preload (bolts) Email Leon@motovated.co.nz for slides
  • 13. What's really important 1. Surface finish 2. Surface treatment 3. Preload (bolts) 4. Maximising the difference between component stress and material strength. Email Leon@motovated.co.nz for slides
  • 14. Reducing component stress Stress reduces from top left to bottom right of diagrams: Email Leon@motovated.co.nz for slides
  • 15. A worked example Email Leon@motovated.co.nz for slides
  • 16. A worked example Email Leon@motovated.co.nz for slides
  • 17. A worked example Original stress = 71.8 MPa Optimised stress = 42.9 MPa Reduction factor = 0.6 Email Leon@motovated.co.nz for slides
  • 18. A worked example Original stress = 71.8 MPa 1. Initial life: 56 hours (50% nominal probability of failure) 2. Increase reliability to ~99%: 5 times life decrease = 11 hours 3. Reduce stress as per example above: 58 times life increase 4. Change material from medium tensile AISI 1040 to PH 17-4 stainless steel: a further 247 times life increase 5. Final life estimate: 158000 hours/6470 days Email Leon@motovated.co.nz for slides
  • 19. • 38 bogies built • Several have hit the 1.1 million km mark! Case study – KiwiRail passenger bogies Email Leon@motovated.co.nz for slides
  • 20. Summary 1. Lean/Agile methods can make a big difference in Simulation 2. Be aware of good fatigue design practice 3. Be careful with component surface treatments 4. Bolt preload is your friend 5. Use good materials and minimise stress Email Leon@motovated.co.nz for slides
  • 21. Thank You! Leon Daly Leon@motovated.co.nz General Manager Motovated Design & Analysis Ltd www.motovated.co.nz +64 3 382 5282 Email Leon@motovated.co.nz for slides
  • 22. Fatigue concepts – stress life Email Leon@motovated.co.nz for slides

Notes de l'éditeur

  1. Mihi Simulation Management Fatigue KR Bogie Sim mgmt. Finite, CFD - 10X Fatigue 90% Awareness Conferences Value is obvious When, how much, what to focus on?
  2. Engineers Lost in the weeds Want to be sure – more they look Rigid definition of quality – believe there is only one appropriate scope Communication burden between designers and analysts Overconservative – don’t like to be wrong
  3. 80:20 Batch - increasing in scope progressively. Get a feel for risk around what's not analysed. Timebox – separate analysis timebox from documentation timebox Learning – Tradeoffs, A3’s, system behaviour, design hardpoint identification Moores – Computer pwr doubling. Too much simplification for the time taken. Train – Wasted movement. Absolute results difficult; optimisation and comparative analysis easy to teach Psychological safety – the secret sauce. Build in. e.g. fatigue
  4. Disclaimer When a bolt fails – often fatigue Cam belt brakes Cracked heels Mountain bike weld cracks Cell phone charger port electronics The living hinge on a plastic lunch box dies - fatigue
  5. Fatigue is responsible for 90% of mechanical failures - important! key insights into fatigue that I hope will allow you to make better decisions and better designs. Fatigue is complex. The numbers I give in this presentation are real and well researched. However, nothing is black and white and there are caveats – cases where what I am saying is more or less of a factor. I’m not going to spend my 30 mins getting into the fine detail as I fear the basic points will be lost. So please don’t take these numbers directly and apply them to your circumstance without some research.
  6. Kieland Norweigian 123 Killed The little things I’m in a privileged position to learn from the success and failures of the best companies in NZ. The reason I’m doing this presentation is that I see on a monthly basis how important good fatigue design is. The difference between a robust design and a constant warranty headache are often small, seemingly insignificant design choices. I believe that a little rigour in our engineering makes the difference between that bad side of No 8 wire and the good, innovative aspect. So I’d like to kick things off by introducing a few clients https://en.wikipedia.org/wiki/Alexander_L._Kielland_(platform)
  7. Whiteboard Sample Normal distribution Endurance limit Modifiers Non linear
  8. Whiteboard Sample Normal distribution Endurance limit Modifiers Non linear
  9. Whiteboard Sample Normal distribution Endurance limit Modifiers Non linear
  10. (6470, 24hr days at 1% nominal probability of failure)
  11. The designers were the analysts Rapid evaluation and multiple analysis rounds with ever increasing level of detail were undertaken. These methods have proven incredibly powerful; even in the highly regulated aerospace and rail industries. PRV valve 27 times around the earth
  12. Whiteboard Sample Normal distribution Endurance limit Modifiers Non linear