考虑二层因素影响的综合因子可靠性分配法

中国机械工程

考虑二层因素影响的综合因子可靠性分配法

张强;李坚;谢里阳;何雪浤

东北大学航空动力装备振动及控制教育部重点实验室，沈阳，110819

出版日期:2019-10-10 发布日期:2019-10-10
基金资助:
国家自然科学基金辽宁联合基金资助项目（U1708255）

Integrated Factor Reliability Allocation Method Considering Influences of Two-layer Factors

ZHANG Qiang;LI Jian;XIE Liyang;HE Xuehong

Key Laboratory of Vibration and Control of Aero-propulsion System of Ministry of Education,Northeastern University,Shenyang,110819

Online:2019-10-10 Published:2019-10-10

摘要/Abstract

摘要： 为了处理考虑多层影响因素下的复杂机械系统可靠性分配问题，分析了传统的综合因子可靠性分配方法，提出了一种考虑二层因素影响的综合因子可靠性分配法，即对传统的可靠性影响因素进行层次划分，建立考虑二层因素影响的全局指标数学模型，进而确定各子系统的全局指标权重，分配得到各子系统的可靠度。通过一个工程案例说明了该方法的具体应用并证明了其简单有效性。

关键词: 多层次, 综合因子分配法, 可靠性分配, 航空发动机

Abstract: In order to deal with the reliability allocation problem considering multi-layer factors of complex mechanical systems, the traditional integrated factor reliability allocation method was analyzed, an integrated factor reliability allocation method was proposed considering the influences of two-layer factors. In this method, the levels of traditional reliability influencing factors were divided, a global index mathematical model was established considering the influences of two-layer factors, and then the global index weights of each subsystem were determined, the reliability of each subsystem was allocated. Finally, an engineering case was given to illustrate specific applications of the method and the simplicity and effectiveness.

Key words: multilevel, integrated factor allocation method, reliability allocation, aeroengine

中图分类号:

TB114.3

张强;李坚;谢里阳;何雪浤. 考虑二层因素影响的综合因子可靠性分配法[J]. 中国机械工程.

ZHANG Qiang;LI Jian;XIE Liyang;HE Xuehong. Integrated Factor Reliability Allocation Method Considering Influences of Two-layer Factors[J]. China Mechanical Engineering.

参考文献

[1]梅启智,廖炯生,孙惠中.系统可靠性工程基础[M].北京:科学出版社,1992:446-460.
MEI Qizhi, LIAO Jiongsheng, SUN Huizhong. System Reliability Engineering Fundamentals [M]. Beijing: Science Press, 1992:446-460.
[2]BONA G D, FORCINA A. Analytic Critical Flow Method (ACFM): a Reliability Allocation Method Based on Analytic Hierarchy Process [J]. Journal of Failure Analysis & Prevention, 2017,17(6):1149-1163.
[3]FELICE F D, BONA G D, FALCONE D, et al. New Reliability Allocation Methodology: the Integrated Factors Method [J]. International Journal of Operations & Quantitative Management, 2010, 16(1):67-85.
[4]杜丽, 黄洪钟, 宋巍. 采用多级模糊评价的柴油机可靠性分配[J]. 机械设计与研究,2009,25(1):107-110.
DU Li, HUANG Hongzhong, SONG Wei. Reliability Allocation Based on Multi-stage Fuzzy Evaluation Method[J]. Mechanical Design and Research. 2009,25(1):107-110.
[5]周新建,李志强. 基于故障维修数据的兆瓦级永磁直驱风力发电机可靠性分配[J]. 煤矿机械,2016, 37(9):84-87.
ZHOU Xinjian, LI Zhiqiang. Reliability Allocation of MW Scale Permanent Magnet Direct-drive Wind Power Generator Based on Failure Maintenance Date[J]. Coal Mining Machinery, 2016,37(9):84-87.
[6]谢静，范文正，谢镇波. 某型军用发动机使用可靠性评估[J]. 航空发动机，2012，38(6)：43-47.
XIE Jing, FAN Wenzheng, XIE Zhenbo.Evaluation of the Service Ability of a Military Engine[J]. Aeroengine, 2012,38(6):43-47.
[7]SAATY T L. How to Make a Decision: the Analytic Hierarchy Process[J]. European Journal of Operational Research, 1994, 48(1):9-26.
[8]邓雪, 李家铭, 曾浩健,等. 层次分析法权重计算方法分析及其应用研究[J]. 数学的实践与认识,2012, 42(7):93-100.
DENG Xue, LI Jiaming, ZENG Haojian，et al. Analytic Hierarchy Process Weight Calculation Method Analysis and Application Research [J]. Mathematics Practice and Understanding, 2012,42(7): 93-100.

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