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变循环发动机地面起动建模及控制规律设计方法

  • Northwestern Polytechnical University Xian
  • Aero Engine Corporation of China

科研成果: 期刊稿件文章同行评审

9 引用 (Scopus)

摘要

To solve the problem of discontinuous isentropic efficiency of rotating components, a method of using correct torque instead of isentropic efficiency was proposed.The extrapolation method of low speed characteristics of rotating components was given, and the full speed characteristics of rotating components were obtained.A burner stability model considering ignition and burn stability was proposed.Finally, a component⁃level starting model of the variable cycle engine was established.Considering the eight variable parameters of the variable cycle engine, the differential evolution algorithm was used to optimize the starting process of the variable cycle engine in the double bypass and single bypass modes.The results showed that the starting time of the variable cycle engine in the double bypass and single bypass modes was 17.2 s and 12.8 s, respectively.In the double bypass mode, the fuel flow, nozzle throat area and outer bypass area of rear variable area bypass injector need to be adjusted.In the single bypass mode, the fuel flow, nozzle throat area and low pressure turbine inlet guide vane area need to be adjusted.When the free stream Mach number was equal to 0.04, the starting time of the variable cycle engine in the double bypass and single bypass modes was 0.2 s less than the static state.

投稿的翻译标题Ground starting modeling and control law design method of variable cycle engine
源语言繁体中文
页(从-至)152-164
页数13
期刊Hangkong Dongli Xuebao/Journal of Aerospace Power
37
1
DOI
出版状态已出版 - 1月 2022

关键词

  • Component characteristics
  • Component⁃level starting model
  • Control law design
  • Differential evolution algorithm
  • Variable cycle engine

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