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Volume 29 Issue 8
Aug.  2003
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Journal of Beijing University of Aeronautics and Astronautics  > 2003  >  29(8): 704-707.
Yao Hongwei, Wang Jun. Model of temperature-controlled air supply duct of a kind of fighter ECS based on MATLAB[J]. Journal of Beijing University of Aeronautics and Astronautics, 2003, 29(8): 704-707. (in Chinese)
Citation: Yao Hongwei, Wang Jun. Model of temperature-controlled air supply duct of a kind of fighter ECS based on MATLAB[J]. Journal of Beijing University of Aeronautics and Astronautics, 2003, 29(8): 704-707. (in Chinese)
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Model of temperature-controlled air supply duct of a kind of fighter ECS based on MATLAB

  • Dept. of Flight Vehicle Design and Applied Mechanics, Beijing University of Aeronautics and Astronautics, Beijing 100083, China

  • Received Date: 07 Jun 2002
  • Publish Date: 31 Aug 2003
    Abstract
  • The configuration and working principle of temperature-controlled air supply duct of a kind of fighter ECS (environmental control system) are detailedly introduced. Based on the mathematical model of components, the dynamic simulating model of entire ECS is established by using simulink, one of toolboxes of MATLAB. With the use of the model, the effect of every parameter of the air supply duct, such as the backing pressure of turbine, regulating range of the pulse width modulator as well as the parameters of electric motor, on the dynamic performance of the ECS is analyzed. Regulation of these parameters can improve the dynamic response performance of the system. The conclusion is helpful to design and optimization of the temperature-controlled air supply duct.

     

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  • [1] 王 浚,徐扬禾. 飞机座舱空气参数控制[M] 北京:国防工业出版社,1980 Wang J, Xu Y H. Air parameter control in the aircraft cabin[M] Beijing:National Defence industry Press,1980(in Chinese) [2] Brognaux L.翅片管热交换单相研究方法[J] 热质交换国际期刊,1997,40(18):4345~4357 Brognaux L. Single-phase heat transfer in micro-fin tubes[J] International J of Heat&Mass Transfer, 1997,40(18):4345~4357(in Chinese) [3] Mcnamara E. 未来对海军飞机环境控制系统的要求 . ASME,79-ENAs-9 Mcnamara E. Future requirements for environmental control system in naval aircraft . ASME,79-ENAs-9,1979(in Chinese)
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