航空发动机性能差异问题的故障部件快速检验方法
A simple fault diagnosis method for aeroengine performance
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摘要: 提出了一种航空发动机性能差异问题的故障部件快速检验方法.该方法以部件特性曲线为基础,可以快速检测出航空发动机各部件的自身特性变化而排除由于其它部件性能变化引起的工作线变动带来的影响,从而快速判断出故障的部件.该方法特别适用于仿制发动机与原型发动机性能变化原因的查找.Abstract: A simple fault diagnosis method for aeroengine's performance was developed.Based on component characteristics,this method could detect quickly the inherent change of aeroengine's components and judge the faulty components.Meanwhile,the fault influence of other component can be removed.This method is particularly suitable for finding out aeroengine performance changes between copying engine and typical engine.
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Key words:
- aerospace propulsion system /
- component characteristics /
- fault diagnosis /
- performance
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[1] 肖洪,薛倩,廉筱纯.基于部件特性未知的航空发动机故障诊断技术[J].航空动力学报,2005,20(5):746-751.XIAO Hong,XUE Qian,LIAN Xiaochun.Fault diagnosis for aeroengine without components'performance[J].Journal of Aerospace Power,2005.20(5):746-751. [2] 廉筱纯,吴虎.航空发动机原理[M].西安:西北工业大学出版社,2005. [3] 应勇.航空发动机故障监控系统设计与方法研究[D].西安;西北工业大学.2007.YING Yong.Fault monitor design of aeroengine[D].Xian:Northwestern Polytechnical University,2007. [4] 徐一艳.航空发动机早期故障诊断方法研究[D].西安:西北工业大学.2006.XU Yiyan.Fault diagnosis design of aeroengine[D].Xi'an:Northwestern Polytechnical University.2006 [5] Urban L A.Parameter selection for multiple fault diagnostics of gas turbine engines[J].Journal of Engineering for Power,April,1975:225-230. -
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