基于贝叶斯模型平均的航空发动机可靠性分析  

Reliability analysis on aero-engine using Bayesian model averaging

作　　者：王华伟[1] 高军[2] 吴海桥[1] 

机构地区：[1]南京航空航天大学民航学院,南京210016 [2]中国人民解放军军械工程学院装备指挥与管理系,石家庄050005

出　　处：《航空动力学报》2014年第2期305-313,共9页Journal of Aerospace Power

基　　金：国家自然科学基金与中国民航局联合资助项目(U1233115;60879001);江苏省青蓝工程优秀青年骨干教师资助项目

摘　　要：针对不同失效模式的特点,利用航空发动机状态监测信息,分别采用Gamma过程、Wiener过程和Weibull分布建立可靠性分析模型.采用贝叶斯模型平均(BMA)方法,分析不同失效模式对可靠性影响,对航空发动机可靠性进行集成分析.通过算例跟踪某在翼航空发动机可靠性水平,基于贝叶斯模型平均的航空发动机可靠性模型的计算误差率低于单一可靠性分析模型,计算结果误差率低于1%.说明多模型集成可靠性技术在复杂系统运行可靠性分析中的有效性和准确性.Considering the characteristics of different failure modes with use of monito- ring information, Gamma process, Wiener process and Weibull distribution were selected to build the reliability analysis models on aero-engine. Bayesian model averaging （BMA） was used to integrate different models into one framework for reliability analysis on aero-engines, given its function for dynamically evaluating different failure mode effects. The reliability of some onwing aero-engine was analyzed by numerical example, showing that the reliability a- nalysis model using BMA had less error than single reliability analysis model, and computa- tion error rate of BMA was less than 1 %. The results demonstrate the effectiveness of the reliability analysis of multi-model integration.

关 键 词：可靠性分析 航空发动机 贝叶斯模型平均(BMA) 多失效模式 模型集成 

分 类 号：V231[航空宇航科学与技术—航空宇航推进理论与工程] TB301[一般工业技术—材料科学与工程]