期刊文献+

基于CBM策略的航空发动机在翼寿命预测研究 被引量:4

Life on Wing Prediction of Aeroengine Based on CBM Strategy
下载PDF
导出
摘要 为了给航空公司制定航空发动机拆换计划提供科学合理的依据,基于视情维修方式,对航空发动机的在翼寿命进行了研究。首先,根据发动机历史拆换记录,基于比例危险-比例优势模型建立了发动机维修决策控制限的数学模型。然后,利用基于最小二乘支持向量机的时间序列预测方法对发动机状态参数进行了趋势预测,进而结合维修决策控制限模型便可得到发动机在翼寿命的预测结果。最后通过实例验证了该方法的有效性和实用价值。 Based on CBM strategy,the life on wing prediction of aeroengine was made herein,aiming at providing airlines with a scientific and reasonable basis for the engine's plans of removal.Firstly,according to the aeroengine's historical data of removal,a mathematical model of the maintenance decision-making control limit was established.And the establishment of this model was based on the proportional hazards-proportional odds model.Then using time series prediction method based on least squares support vector machine,and combined with the condition trend prediction of engine,life on wing of engine was predicted.Finally,in the case study of a concrete instance,the method was proved to be effective and to have a high practical value.
出处 《中国机械工程》 EI CAS CSCD 北大核心 2015年第13期1725-1730,共6页 China Mechanical Engineering
基金 中央高校基本科研业务费专项资金资助项目(ZXH2012P007)
关键词 航空发动机 视情维修 性能衰退 维修决策控制限 比例危险-比例优势模型 在翼寿命 aeroengine condition based maintenance(CBM) performance degradation maintenance decision-making control limit proportional hazards-proportional odds model life on wing
  • 相关文献

参考文献12

  • 1Moubray J. Reliability Centred Maintenance[M]. London: Butterworth-Heinemann Ltd. , 1999.
  • 2劳立斯 J F.寿命数据中的统计模型和方法[M].刘忠,茆诗松译.北京:中国统计出版社,1998.
  • 3Samrout M,Chtelet E,Kouta R,et al. Optimization of Maintenance Policy Using the Proportional Haz- ard Model[J]. Reliability Engineering & System Safety, 2009,94 ( 1 ) : 44-52.
  • 4Elsayed E A,Zhang H. Design of Optimum Multi pie-stress Accelerated Life Testing Plans Based on Proportional Odds Model[J]. International Journal of Product Development,2009,7(3/4) 186-198.
  • 5Huang T,Elsayed E A,Jiang T. An ALT Propor- tional Hazard-proportional Odds Model[C]//Proc. of the 14th ISSAT International Conference on Reli- ability and Quality in Design. Orlando, Florida, USA, 2008 : 39-43.
  • 6袁风,左洪福.航空发动机性能衰退率计算方法研究[J].航空维修与工程,2009(2):46-48. 被引量:3
  • 7Zbigniew Michalewicz. Genetic Algorithms+ Data Structures = Evolution Programs . Berlin: Springer Verlag, 1996.
  • 8段玉倩,贺家李.遗传算法及其改进[J].电力系统及其自动化学报,1998,10(1):39-52. 被引量:175
  • 9左洪福,张海军,戎翔.基于比例风险模型的航空发动机视情维修决策[J].航空动力学报,2006,21(4):716-721. 被引量:50
  • 10王革丽,杨培才,毛宇清.基于支持向量机方法对非平稳时间序列的预测[J].物理学报,2008,57(2):714-719. 被引量:38

二级参考文献42

共引文献281

同被引文献40

引证文献4

二级引证文献13

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部