期刊文献+

采用Modelica和Dymola的燃气涡轮的变比热仿真计算模型 被引量:4

Variable Specific Heat Model for Gas Turbines Simulation Calculations Using Modelica and Dymola
下载PDF
导出
摘要 结合模块化建模的方式,引入容积效应,推导了燃气涡轮变比热计算的数学模型。此外,还采用新型面向对象的仿真语言Modelica,建立可扩展的燃气涡轮仿真库;同时在Dymola平台上,利用仿真库和其它程序库,搭建单轴燃气涡轮发动机模型,对燃气涡轮动态过程进行变比热计算。与软件Gasturb和定比热计算结果对比,证明变比热计算的合理性和有效性,验证了该仿真方法的可行性,表明该方法有推广应用的价值。图7参5。 Considering volumetric effects, combined with modular modeling, a mathematical model for calculating the varying specific heat in gas turbines has been deduced. Furthermore, an extensible simulation library for gas turbines has been elaborated by using the new object-oriented simulation language ——Modelica. Simultaneously, by using the simulation library and other program libraries, a single shaft gas turbine model is built on the platform Dymola and the dynamic behavior of the turbine calculated with specific heat considered variable. Compared with the calculation result by software Gasturb as well as that obtained by the constant specific heat method, the present method is verified to be reasonable and effective, the simulation used to be feasible and its application worthy of popularization.
出处 《动力工程》 EI CSCD 北大核心 2006年第6期799-803,共5页 Power Engineering
关键词 动力机械工程 燃气涡轮 变比热 仿真 power and mechanical engineering gas turbine variable specific heat simulation
  • 相关文献

参考文献4

  • 1廉小纯,吴虎.航空燃气轮机原理(下册)[M].北京:国防工业出版社,2000.
  • 2王乃行,徐敦镳,庄表南,廉小纯,等.航空燃气涡轮发动机原理[M],北京:国防工业出版社,1981.
  • 3Carl J D.Digital computer program for generating dynamic turbofan engine models (DIGTEM)[R].NASA TM 83446.
  • 4Jonas Eborn,Hubertus Tummescheit,Falko Wagner.ThermoFluid A themo-hydraulic library in modelica documentation[M].Department of Automatic Control Lund University,Sweden and Department of Energy Engineering Technical University of Denmark.

共引文献3

同被引文献27

  • 1聂恰耶夫.航空动力装置控制规律与特性[M].单凤桐译.北京:国防工业出版社,1999.
  • 2[俄]聂恰耶夫著,单凤桐,程振海译.航空动力装置控制规律与特性[M].北京:国防工业出版社,1999-5.
  • 3AGARD.In-flight thrust determination[R].SAE AIR-1703.
  • 4AGARD.Guide to in-flight thrust measurement of turbojets and fan engines[R].AGARD-AG-237.
  • 5Paul W C. A comprehensive approach to in-flight thrust determination[R]. NATC-TM-79-3.
  • 6Couch B D,Bishop B M.ALCM pre-flight test thrust uncertainty analysis[R].AEDC-TR-81-2.
  • 7Abernethy R B. Handbook of uncertainty in gas turbine measurements[R].AEDC-TR-73-5.
  • 8Blevins J,Wagner D. An uncertainty assessment of thrust determination in altitude ground test facilities[R].AIAA-2000- 0413.
  • 9MIDAP Study Group. Guide to In-Flight Thrust Measurement of Turbojets and Fan Engines[R]. AGARD-AG-237, 1979 : 27-62.
  • 10Abernethy R B, Roberts J, Adams G, et al. In-Flight Thrust Determination[R]. SAE AIR- 1703,1985 : 5-25.

引证文献4

二级引证文献15

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