Using materials prognosis to maximize the utilization potential of complex mechanical systems

JOM

Volumn 56, Issue 3, 2004, Pages 15-19

  Christodoulou, Leo ^a   Larsen, James M ^b  

^a DEFENSE ADVANCED RESEARCH PROJECTS AGENCY   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

FAILURE (MECHANICAL); FEATURE EXTRACTION; INSPECTION; LIFE CYCLE; MAINTENANCE; PERFORMANCE; PRODUCT DESIGN; SENSORS; SIGNAL PROCESSING; TURBINES;

COMPLEX MECHANICAL SYSTEMS; LIFE LIMITS; LIFE MANAGEMENT PROCESS; MATERIALS DAMAGE PROGNOSIS; STRUCTURAL FAILURE;

AIRCRAFT PARTS AND EQUIPMENT;

EID: 1942486385     PISSN: 10474838     EISSN: None     Source Type: Journal    
DOI: 10.1007/s11837-004-0027-4     Document Type: Article

References (6)

1. Defense Advanced Research Projects Agency (DARPA), FedBizOpps, Commerce Business Daily (6 January 2003).
2. Northrop Grumman Corporation, Aviation Week & Space Technology, 159 (19) (November 2003), p. 13.
3. Graham Warwick, Flight International (16-22 December 2003).
4. U.S. Air Force, Engine Structural Integrity Program, Military Standard 1783B (Wright-Patterson Air Force Base, OH: Aeronautical Systems Center, 31 May 2002), .
5. H. Kitagawa and S. Takahashi, Proceedings of the Second International Conference on Mechanical Behavior of Materials (Metals Park, OH: ASM, 1976), pp. 627-631.
6. J. Larsen et al., "The Role of Near-Threshold Small-Crack Behavior in Life Prediction of Titanium Alloys for Use in Advanced Turbine Engines," Small Fatigue Cracks: Mechanics, Mechanisms, and Applications, ed. K.S. Ravichandran, R.O. Ritchie, and Y. Murakami, (Oxford, UK: Elsevier Science Ltd., 1999) pp. 131-142.