刘洪健,姚军,李佩昌.基于最弱t-模的飞机起落架模糊故障树分析[J].装备环境工程,2017,14(7):103-108. LIU Hong-jian,YAO Jun,LI Pei-chang.Fuzzy Fault Tree Analysis of Aircraft Landing Gear Based on Weakest T-norm[J].Equipment Environmental Engineering,2017,14(7):103-108.
基于最弱t-模的飞机起落架模糊故障树分析
Fuzzy Fault Tree Analysis of Aircraft Landing Gear Based on Weakest T-norm
投稿时间:2017-03-18  修订日期:2017-07-15
DOI:10.7643/ issn.1672-9242.2017.07.021
中文关键词:  模糊故障树分析  最弱t-模  飞机起落架  模糊数  可靠性评估
英文关键词:fuzzy fault tree analysis  weakest t-norm  aircraft landing gear  fuzzy number  reliability assessment
基金项目:
作者单位
刘洪健 北京航空航天大学 可靠性与系统工程学院,北京 100191 
姚军 北京航空航天大学 可靠性与系统工程学院,北京 100191 
李佩昌 北京航空航天大学 可靠性与系统工程学院,北京 100191 
AuthorInstitution
LIU Hong-jian School of Reliability and System Engineering, Beihang University, Beijing 100191, China 
YAO Jun School of Reliability and System Engineering, Beihang University, Beijing 100191, China 
LI Pei-chang School of Reliability and System Engineering, Beihang University, Beijing 100191, China 
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中文摘要:
      目的 针对飞机起落架部件失效的模糊性以及传统模糊故障树分析中采用扩展原理或区间运算而导致模糊积累的缺点,提出了一种基于最弱t-模的飞机起落架模糊故障树分析新方法。方法 采用梯形模糊数表示飞机起落架部件模糊失效概率,给出最弱t-模的模糊运算法则,并利用最弱t-模法则进行模糊故障树分析。结果 得到了飞机起落架系统的模糊失效概率以及部件的重要度。结论 与传统模糊故障树分析方法比较,该方法具有更加灵活适用的优点,为飞机起落架可靠性评估奠定了基础。
英文摘要:
      Objective According to disadvantages of fuzziness on failure of landing gear components and application of extension principle and interval arithmetic in traditional fuzzy fault tree analysis leading to accumulation of fuzziness, this paper aims to propose a new analysis method for fuzzy fault of aircraft landing gear based on the weakest t-norm. Methods The fuzzy failure probability of aircraft landing gear components was represented by trapezoidal fuzzy number, and the fuzzy operation rules of the weakest t- mode were given, and the fuzzy fault tree analysis was carried out with the weakest T- norm rule. Results The fuzzy failure probability of aircraft landing gear system and the importance of components were obtained. Conclusion Compared with the traditional fuzzy fault tree analysis method, the proposed method is more flexible and applicable, which lays a foundation for the reliability assessment of aircraft landing gear.
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