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

被引:33
作者
Christodoulou, L [1 ]
Larsen, JM
机构
[1] Def Adv Res Projects Agcy, Def Sci Off, Arlington, VA 22203 USA
[2] USAF, Res Lab, Mat & Mfg Directorate, Wright Patterson AFB, OH 45433 USA
关键词
Fatigue Life; Life Prediction; Crack Size; Defense Advance Research Project Agency; Defense Advance Research Project Agency;
D O I
10.1007/s11837-004-0027-4
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Performance and life limits for structural materials in complex mechanical systems are often established based heavily on a fear of failure. Conventional approaches for avoiding structural failure often involve extensive periodic inspections, lengthy maintenance processes, and highly conservative "go, no-go" operational decisions, all of which may significantly impair system readiness. This article summarizes a typical present-day life-management process for an advanced system and then presents the key elements of an alternative life-management approach known as materials damage prognosis.
引用
收藏
页码:15 / 19
页数:5
相关论文
共 5 条
  • [1] Kitagawa H., 1976, P 2 INT C MECH BEHAV, P627
  • [2] The role of near-threshold small-crack behavior in life prediction of titanium alloys for use in advanced turbine engines
    Larsen, JM
    John, R
    Russ, SM
    Maxwell, DC
    Worth, BD
    Rosenberger, AH
    Li, K
    Porter, WJ
    [J]. SMALL FATIGUE CRACKS: MECHANICS, MECHANISMS, AND APPLICATIONS, 1999, : 131 - 142
  • [3] *NORTHR GRUMM CORP, 2003, AVIATION WEEK SPACE, V159, P13
  • [4] *US AIR FORC, 2002, 1783B US AIR FORC ST
  • [5] 2003, COMMERCE BUSINE 0106