| Literature DB >> 33266588 |
Xuelian Zhou1, Yongchuan Tang1,2.
Abstract
As a typical tool of risk analysis in practical engineering, failure mode and effects analysis (FMEA) theory is a well known method for risk prediction and prevention. However, how to quantify the uncertainty of the subjective assessments from FMEA experts and aggregate the corresponding uncertainty to the classical FMEA approach still needs further study. In this paper, we argue that the subjective assessments of FMEA experts can be adopted to model the weight of each FMEA expert, which can be regarded as a data-driven method for ambiguity information modeling in FMEA method. Based on this new perspective, a modified FMEA approach is proposed, where the subjective uncertainty of FMEA experts is handled in the framework of Dempster-Shafer evidence theory (DST). In the improved FMEA approach, the ambiguity measure (AM) which is an entropy-like uncertainty measure in DST framework is applied to quantify the uncertainty degree of each FMEA expert. Then, the classical risk priority number (RPN) model is improved by aggregating an AM-based weight factor into the RPN function. A case study based on the new RPN model in aircraft turbine rotor blades verifies the applicable and useful of the proposed FMEA approach.Entities:
Keywords: ambiguity measure (AM); dempster–shafer evidence theory (DST); failure mode and effects analysis (FMEA); risk management; risk priority number (RPN); uncertainty measure
Year: 2018 PMID: 33266588 PMCID: PMC7512425 DOI: 10.3390/e20110864
Source DB: PubMed Journal: Entropy (Basel) ISSN: 1099-4300 Impact factor: 2.524
Figure 1The framework of the new RPN based on the AM.
Figure 2The framework of the new FMEA approach where the ambiguity measure in DST is adopted to measure and aggregate the uncertainty consisted in the assessments of FMEA experts.
BPAs of experts’ assessment information for (adopted from [52]).
| Risk Factor | Expert 1 | Expert 2 | Expert 3 |
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AM and aggregated rating values of each expert for .
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| 2.8148 | 2.3129 | 2.2946 |
A comparison of RPN values.
| FMEA Item | The New Method | MVRPN [ | Improved MVRPN [ | GERPN [ |
|---|---|---|---|---|
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| 46.4875 | 42.56 | 42.56 | 3.4910 |
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| 64.7921 | 64.00 | 64.05 | 3.9994 |
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| 30.0000 | 30.00 | 30.00 | 3.1069 |
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| 17.5822 | 18.00 | 17.97 | 2.6205 |
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| 3.6671 | 4.17 | 3.14 | 1.6095 |
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| 60.0000 | 60.00 | 60.00 | 3.9143 |
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| 21.0000 | 21.00 | 21.00 | 2.7586 |
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| 16.2000 | 15.00 | 15.00 | 2.4660 |
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| 70.5947 | 78.92 | 79.57 | 4.2881 |
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| 60.0000 | 60.00 | 60.00 | 3.9143 |
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| 50.0000 | 50.00 | 50.00 | 3.6836 |
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| 53.8039 | 50.00 | 50.00 | 3.6836 |
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| 49.3333 | 50.00 | 50.00 | 3.6836 |
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| 60.6337 | 60.00 | 60.04 | 3.9143 |
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| 41.9161 | 42.00 | 42.09 | 3.4756 |
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| 21.2967 | 23.88 | 23.86 | 2.8794 |
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| 31.2810 | 30.05 | 30.05 | 3.1089 |
Figure 3FMEA ranking of the compressor rotor blade (FMEA Items 1–8) and the turbo rotor blade (FMEA Items 9–17) based on the proposed method, as well as the methods in [51] (MVRPN), [52] (the improved MVRPN) and [53] (GERPN).