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.
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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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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