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Aeroengine Safety

Institute of Thermal Turbomachinery and Machine Dynamics
Graz University of Technology

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You are here: Aeroengine Safety » 12. Material Behavior » 12.6 Dynamic Fatigue » 12.6.3 High-Cycle Fatigue (HCF)

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  • 1. Introduction
  • 2. Trends and Statistical Observations
  • 3. Superordinate Issues
  • 4. Aircraft Accident Investigation
  • 5. External Factors
  • 6. Fretting
  • 7. Rubbing and Maintaining Clearances
  • 8. Housing Stress due to Rotor Fragments
  • 9. Fires and Explosions
  • 10. Engine Mounts
  • 11. Operating Behavior
  • 12. Material Behavior
    • 12.1 Demands on Material Technology
    • 12.2 Crack Growth
    • 12.3 Overload Fractures
    • 12.4 Damaging Temperatures and Environmental Effects
    • 12.5 Creep
    • 12.6 Dynamic Fatigue
      • 12.6.1 Low-Cycle Fatigue (LCF)
      • 12.6.2 Thermal Fatigue
      • 12.6.3 High-Cycle Fatigue (HCF)
        • 12.6.3.1 Vibration Excitement and Vibration Stress in the HCF Range
        • 12.6.3.2 Fundamentals of HCF Behavior of Materials
        • 12.6.3.3 Damage due to HCF
        • 12.6.3.4 Remedies for HCF Damage
  • 13. Damage-Minimizing Construction
  • 14. Technological Development
  • 15. Material Flaws
  • 16. Finishing
  • 17. Quality Assurance
  • 18. Handling, Packaging, Transport, Storage
  • 19. The Maintenance
  • 20. Assembly and Disassembly
  • 21. Overhaul and repair of used parts.
  • 22. Systems and consumables.
  • 23. Selected machine elements of the aeroengine technology
  • 24. Problems in connection with test rigs
  • 25. Aeroengine monitoring
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  • 12.6.3 High-Cycle Fatigue (HCF)
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12/126/1263/1263.txt · Last modified: 2020/08/18 20:34 by 127.0.0.1

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