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Topic
  • History and evolution of civil and military fatigue requirements
  • Introduction to fatigue mechanism
  • Design considerations
  • Fatigue properties
  • Fatigue strength
  • Stress intensity factors
  • Fracture mechanics
  • Fatigue loads and spectra
  • Fatigue damage accumulation
  • Introduction to non-destructive inspection
  • Fatigue and failure of joints and structure
  • Damage tolerance of repairs and alteration
  • Widespread Fatigue Damage and Limit of Validity
  • Featuring case studies and examination of lessons learned from accidents.
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About the Instructor

Dr. Patrick Safarian, P.E.
Fatigue and Damage Tolerance Senior Technical Specialist, Finite Element Methods and Composite Material Professor

Since 1997, Dr. Safarian has been involved in ensuring safety of the existing fleet and certification of new airplane models, such as 747-8, 787 and 777-9, 737MAX and A350 at Federal Aviation Administration (FAA). His involvement includes new rulemaking activities, including Parts 25 and 26, plus preparation of the advisory circulars and training material for metallic and composite material structures. Prior to FAA Patrick was employed at the Boeing Company for eleven years as a stress analyst. During that time, he contributed to development of methods and allowables for fatigue and damage tolerance standards for stress engineers. He also performed analytical and computational stress analyses of highly complex structures, including failure analysis in support of airplane design, in-service problems and accident investigations.

Patrick received his BSME from Northrop University in 1983, MSME from California State University, Fullerton, in 1985, and completed his PhD work in Mechanical Engineering at University of California, Davis, in 1987. In June 2004 he completed his Doctorate in Theological studies at Bakke Graduate School. Patrick has taught damage tolerance and advance engineering mathematics courses while at Boeing for over ten years. He has been teaching post-graduate engineering courses in the fields of fatigue, fracture mechanics, finite element analysis and composite material at University of Washington and Central Washington University since 1998. He has been teaching two courses in fatigue and damage tolerance to the industry since 2008. He has also offered the industry courses in finite element methods and applications since 2017. Patrick is married to Annette and they have two children, Natasha and Christopher.

Dr. Safarian interacts constantly with the industry experts in developing and application of the latest simulations tools and provides key guidance to aviation industry in analyzing metallic and composite material structures.

 

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Learn:
  • Concepts of fatigue, fracture mechanics and damage tolerance in aerospace structure.
  • Analytical and numerical methods of fatigue and damage tolerance analysis.
  • Tools to apply and solve fatigue and damage tolerance problems.
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Who Should Attend
  • Aircraft Certification engineers
  • Design Approval Representatives
  • Airline Engineers
  • DAH Engineers, TC and STC holders
  • Anyone who performs damage tolerance analysis
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Contact Us

For more information about the event, please contact +65 8363 3065 or email marketing@k2binternational.com

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What past delegates said about our past training courses?

The trainer is very knowledgeable and the materials was very well organized and delivered. We have gained a comprehensive understanding in radar system for radar application. Thanks a lot!.”

Senior Member of Technical Staff, DSO National Laboratories

Radar Systems Design and Engineering, July 2012

 

K2B International has a good selection of trainer. The trainer is knowledgeable and his presentation was clear.”

Research Engineer, Electronic Systems Division, DSO National Laboratories

Radar Systems Design and Engineering, July 2012

 

The course was well presented and the trainer showed good knowledge of topics.”

Senior Software Engineer, ST Aerospace

Radar Signal Processing 2010

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