期刊文献+

基于Matlab的燃气轮机热参数故障诊断的标准数学模型建立 被引量:1

Establishment of Standard Mathematical Model of Gas Turbine Fault Diagnosis about Heat Parameter Based on Matlab
下载PDF
导出
摘要 针对燃气轮机标准数学模型建立过程中难以得到解析关系式的问题,提出了Matlab回归函数法的新型建模思路;并以某型三轴燃气轮机压气机部分为例,对此方法进行了验证与说明。此外,推导出的数学模型可用于燃气轮机的无故障状态参数的计算。 A new method of establishing math model based on MATLAB regression function is presented. In order to get the analytic relationship during the course of establishing the gas turbine standards math model. Taking a certain type of gas turbine compressor parts for example, the method is verified and illuminated. In addition, the mathematical model is derived which can be used to calculate the no fault of the state gas turbine's parameters.
作者 蒋磊 杨朔
出处 《科学技术与工程》 2009年第5期1254-1257,共4页 Science Technology and Engineering
关键词 标准数学模型 回归函数法 燃气轮机 standard mathematical model regression function method gas turbine
  • 相关文献

参考文献3

二级参考文献9

  • 1[1]Diakunchak IS. Performance deteriorations in industrial gas-turbine [J].ASME Joumal of Engineering for Gas-turbines and Power, 1992, 114:161-8.
  • 2[2]S. 0. T. 0gaji, S. Sampath, R. Singh, S. D. Probert. Parameter selection for diagnosing a gas-turbine's performance-deterioration[J]. Applied Energy,2002, (73) :25 - 46.
  • 3[3]Urban L. A. Gas Path Analysis Applied To Turbine Engine Condition Monitoring[J].AIAA 1972,72- 1082.
  • 4[4]Zaita AV, Bulet G, Karlsons G. Performance deterioration modeling in aircraft gas-turbine engines [J]. ASME Journal of Engineering for Gastubines and Power, 1998,120:344 - 9.
  • 5[5]Tabakoff, Lakshminarasimba, Pasin. Simulation of Compressor Performance Deterioration Due to Erosion[J] .Journal of Turbomachinery, 1990,112.
  • 6Zhu P,J Engineering for Gas Turbines and Power,1992年,114期,180页
  • 7Wang Yonghong,J Engineering for Gas Turbines and Power,1991年,113期,106页
  • 8翁史烈,燃气轮机性能分析,1987年
  • 9谢志武,王永泓,洪波,陈德来.逆算法对涡轮特性柯特略尔估算的改进[J].热能动力工程,1998,13(3):185-188. 被引量:3

共引文献11

同被引文献8

引证文献1

二级引证文献1

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