Research on selection of statistical plans for laboratory reliability verification test

Wang, Xin; Ren, Zhanyong; Wang, Qihua; Sun, Ruifeng; Hou, Chenguang

doi:10.1109/icrms.2009.5270174

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2012

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“…Therefore, it is essential to research on the failures of flaps and slats, in order to make clear the failure position, mode, causes and failure probability of the corresponding event. So FTA (fault tree analysis) and FMEA (failure mode and effects analysis) are adapted to find out the design weakness of the flaps and slats, and to provide the basis for final troubleshooting during operation [2][3][4][5][6].…”

Section: Introductionmentioning

confidence: 99%

Research on Fault Diagnosis Method of the Aircraft Flap System Based on Weighted Fuzzy Petri Net

Cai

2012

AMM

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Accordingly to the problem that during the fault diagnosis of the flap system, the existing experience and knowledge are always uncertainty, inconsistency, incompleteness, what’s more, the different fault cause has different effect on the fault. So the Weighted Fuzzy Petri Net is adopted, and fuzzy Petri net and matrix operations are combined, then the formal process of fuzzy inference reasoning algorithm is researched in order to obtain the fault probability of each event in the fault tree of flap system. The presented method effectively makes up the deficiency of the traditional FTA and FMEA, and provides a new fault diagnosis method for complex systems, so the fault diagnosis method based on Weighted Fuzzy Petri Net has a great practical value.

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Section: Introductionmentioning

confidence: 99%

Research on Fault Diagnosis Method of the Aircraft Flap System Based on Weighted Fuzzy Petri Net

Cai

2012

AMM

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Research on selection of statistical plans for laboratory reliability verification test

Cited by 1 publication

References 1 publication

Research on Fault Diagnosis Method of the Aircraft Flap System Based on Weighted Fuzzy Petri Net

Research on Fault Diagnosis Method of the Aircraft Flap System Based on Weighted Fuzzy Petri Net

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