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基于特征值和特征向量的测量参数选择 被引量:5

Selection of measurement parameters based on eigenvalues and eigenvectors
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摘要 研究了航空发动机气路故障诊断中测量参数如何选择的问题。利用发动机故障诊断矩阵,提出了基于特征值和特征向量比较不同测量参数选择系统之间优劣的简易快速算法,该算法可以从几何角度直观地展现整体解空间和解矢量的方向等变化情况。通过一个单轴涡喷发动机测量系统对比案例有效地表明:地面测试系统的最大与最小特征值比为33,机载系统的最大与最小特征值比为1008,在该单轴涡喷发动机气路故障诊断方面,地面测试系统比机载系统明显更有利于气路故障诊断。该算法可用于优化机载发动机测量传感器布局、台架测量系统中测量传感器布局,指导工程中测量参数的选择等。 The problem of how to choose the parameters in the aero engine gas path fault diagnosis was studied.Using engine fault diagnosis matrix,a simple and fast algorithm based on eigenvalues and eigenvectors to compare the advantages and disadvantages between different measurement systems was proposed.The algorithm can directly show the change of the global solution space and the direction of vectors from a geometric perspective.A comparison case study of a single-axis turbojet engine test system showed that the maximumminimum eigenvalue ratio of the ground test system was 33,and the maximum-minimum eigenvalue ratio of the airborne system was 1 008.The ground test system is more advantageous to the fault diagnosis of the single-axis turbojet engine than the airborne system.The algorithm can be used to optimize the layout of sensors in airborne engines,measure sensor layout in bench measurement system,and guide the selection of measurement parameters in engineering.
作者 白磊 杨磊 胡骏 黄顺洲 周人治 BAI Lei;YANG Lei;HU Jun;HUANG Shunzhou;ZHOU Renzhi(College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016 ,China;Sichuan Gas Turbine Establishment,Aero Engine Corporation of China,Chengdu 610500,China)
出处 《航空动力学报》 EI CAS CSCD 北大核心 2019年第1期195-200,共6页 Journal of Aerospace Power
关键词 故障诊断 测量参数选择 特征值 特征向量 奇异值分解 fault diagnostics selection of measurement parameter eigenvalue eigenvector singular value decomposition
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  • 1范作民,孙春林,林兆福.发动机故障诊断的主因子模型[J].航空学报,1993,14(12). 被引量:14
  • 2Torella G, Torella R. Probabilistic expert system for the diagnostics and trouble-shooting of gas turbine apparatuses [R]. AIAA 99-2842.
  • 3Urban L A. Gas path analysis applied to turbine engine condition monitoring[R]. AIAA 72-1082.
  • 4Urban L A. Parameter selection for multiple fault diagnostics of gas turbine engines[R]. ASME 74-GT-82.
  • 5Kos J M. Multiple fault gas path analysis applied to a twin spoolmixed flow[R]. ADA 019183,1975.
  • 6Stamatis A, Mathioudakis K, Papiliou K, et al. Jet engine fault detection with differential gas path analyses at discrete operating points[R]. ISABE 89-7133,1989.
  • 7Rama K, Shankar Y P, Siddiqi M. Modeling, diagnostics and prognostics of a two spool turbofan engine[R]. AIAA 2005-4344.
  • 8Li Y G. Performance analysis based gas turbine diagnostics:a review[J]. Journal Power and Energy, 2002, 216 (5):363-377.
  • 9陈大光,航空动力学报,1994年,9卷,4期
  • 10范作民,航空学报,1993年,14卷,12期

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