期刊文献+

电厂燃气轮机气路分析的新型数学模型 被引量:2

A New Algorithm Method of Gas Turbine Gas Path Diagnosis
下载PDF
导出
摘要 为了提高传统小偏差方程组的诊断精度,提出了一套新的小偏差数学模型.在原有方法的部件特性变化量中引入修正因子,消除了匹配过程对计算结果的影响,使得新方法的计算结果更接近于真实部件变化量.将该模型应用于PG9171E型燃气轮机(燃机)的仿真结果表明:新数学模型能够更精确地反映测量参数和部件性能之间的关系;由该模型推导出的故障诊断矩阵可以提高测量参数预估与机组性能评定的精度. To increase the accuracy of linear gas path analysis (GPA) method, a new method to evaluate the partial differential equations was presented. With recent research, parameter deviations caused by re- matching procedure is the main reason in the inaccuracy of simultaneous differential equations. Therefore, matching coefficients are introduced to isolate and eliminate these matching deviations with delta pressure ratios. The ICM yielded by the new method can both increase the accuracy of measurements prediction and parameter deviations estimation. By utilizing the computer model of the PG9171E engine, the new method is demonstrated.
出处 《上海交通大学学报》 EI CAS CSCD 北大核心 2008年第3期385-388,共4页 Journal of Shanghai Jiaotong University
关键词 燃气轮机 影响系数矩阵 小偏差方程 gas turbine influence coefficient matrices equations of small changes
  • 相关文献

参考文献9

  • 1Urban L A.Parameter selection for multiple-fault diagnostics of gas-turbine engines[J].Journal of Engineering for Power,1975,110 (2):225-230.
  • 2Urban L A.Gas path analysis of commercial aircraft engines[C]//Fulton R E.Proceedings of the llth Symposium on Aircraft Integrated Data Systems.Koln:DFVLR,1982:323-357
  • 3Doel D L.TEMPER-A gas-path analysis tool for commercial jet engines[J].Journal of Engineering for Gas Turbines and Power,1994,116 (1):82-89.
  • 4Stamatis A,Mathioudakis K,Smith M,et al.Gas turbine component fault identification by means of adaptive performance modeling[C]// Dilip R.International Gas Turbine and Aeroengine Congress and Exposition.New York:ASME,1990:376-384.
  • 5Zedda M,Singh R.Gas turbine engine and sensor diagnostics[J].Journal of Propulsion and Power,2002,18(5):1019-1025.
  • 6Fuster P,Ligeza A,Aguilar M J.Diagnostic knowledge representation and reasoning with use of and/or/not causal graphs[C]// Proceedings of the 1995 12th International Conference on Systems Science.Part3.Wroclaw:Elsevier,1995:223-230.
  • 7Li Y G.Performance-analysis-based gas turbine diagnostics:A review[J].Proceedings of the Institution of Mechanical Engineers,Part A:Journal of Power and Energy,2002,216 (5):363-377.
  • 8Kamboukos P,Mathioudakis K.Comparison of linear and nonlinear gas turbine performance diagnostics[J].Journal of Engineering for Gas Turbines and Power,2005,127 (1):49-56.
  • 9夏迪,王永泓.基于热参数的单轴燃气轮机非线性故障诊断方法[J].上海交通大学学报,2008,42(3):381-384. 被引量:5

二级参考文献8

  • 1Urban L A.Parameter selection for multiple-fault diagnostics of gas-turbine engines[J].Journal of Engineering for Power,1975,110(2):225-230.
  • 2Urban L A.Gas path analysis of commercial aircraft engines[C]//Pulton R E.Proceedings of the llth Symposium on Aircraft Integrated Data Systems.Koln:DFVLR,1982:323-357.
  • 3Doel D L.TEMPER-A gas-path analysis tool for commercial jet engines[J].Journal of Engineering for Gas Turbines and Power,1994,116 (1):82-89.
  • 4Zedda M,Singh R.Gas turbine engine and sensor diagnostics[J].Journal of Propulsion and Power,2002,18(5):1019-1025.
  • 5Li Y G.Performance-analysis-based gas turbine diagnostics:A review[J].Proceedings of the Institution of Mechanical Engineers,Part A:Journal of Power and Energy,2002,216 (5):363-377.
  • 6Kamboukos P,Mathioudakis K.Comparison of linear and nonlinear gas turbine performance diagnostics[J].Journal of Engineering for Gas Turbines and Power,2005,127 (1):49-56.
  • 7Wang Y H.A new method of predicting the performance of gas turbine engines[J].Journal of Engineering for Gas Turbines and Power,1991,113 (3):106-111.
  • 8Kurz R,Brun K.Degradation in gas turbine systems[J].Journal of Engineering for Gas Turbines andPower,2001,123(2):70-77.

共引文献4

同被引文献19

引证文献2

二级引证文献16

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