发明名称 USAGE MONITOR RELIABILITY FACTOR USING AN ADVANCED FATIGUE RELIABILITY ASSESSMENT MODEL
摘要 According to one non-limiting embodiment, a method includes accessing flight regime rates of occurrence distributions associated with one or more flight regimes for a fleet of aircraft. Using the accessed flight regime distributions, a factor for at least one of the flight regimes is determined that provides a predetermined amount of reliability for a component on each aircraft on the fleet of aircraft known to be affected through at least fatigue damage by the at least one flight regime.
申请公布号 US2010235108(A1) 申请公布日期 2010.09.16
申请号 US20090566743 申请日期 2009.09.25
申请人 ADAMS DAVID O;ZHAO JACK Z 发明人 ADAMS DAVID O.;ZHAO JACK Z.
分类号 G06F19/00;G06F17/18 主分类号 G06F19/00
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