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基 于 自 激 扫 掠 喷 嘴 的 加 力 燃 烧 效 率 试 验

  • Shiqi Wang*
  • , Quan Wen
  • , Zhigang Jia
  • , Yixin Cheng
  • , Lin Li
  • , Chi Zhang
  • , Weiye Huo
  • , Liang Ma
  • *此作品的通讯作者
  • Aero Engine Corporation of China
  • Beihang University
  • North China Institute of Aerospace Engineering
  • Civil Aviation University of China

科研成果: 期刊稿件文章同行评审

摘要

To prove the feasibility of applying the self-excited sweeping nozzle in the afterburner,and the effectiveness of high frequency dynamic sweeping fuel injection methods for improving the efficiency of afterburner combustion,this study designed a fuel spray bar integrated with the self-excited sweeping nozzles,tested its basic working characteristics,such as flow rate,frequency and sweeping angle,and further compared these characteristics with the plain-orifice spray bar. Then,based on the rectangular afterburner test rig,under the same test conditions and the fuel-to-air ratio range,the overall combustion efficiencies are tested and the dynamic wall pressure pulsation information is monitored,employing the plain-orifice spray bar and self-excited sweeping spray bar respectively. The results show that multiple self-sweeping nozzles can be integrated into the spray bar with the diameter limitation of 10mm. the flow capability of the self- excited sweeping spray bar is increased by 23%,compared to the plain-orifice spray bar with the equivalent geometric flow area. For the nozzles in the same spray bar,their operating frequency and sweeping angle responses to the pressure drop are basically the same and have good consistency. The afterburner combustion efficiency is improved by 3. 7%,by employing the self-excited sweeping spray bar,and no dynamic pressure pulsation frequency is detected which is the same or close to the operating frequency of self-excited sweeping nozzle,indicating that high frequency dynamic sweeping fuel injection has no direct impact on the flame thermoacoustic oscillation mode and large scale shedding vortex structure downstream the flameholder.

投稿的翻译标题Experiment on afterburner combustion efficiency based on self-excited sweeping nozzle
源语言繁体中文
期刊论文编号130621
期刊Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
46
2
DOI
出版状态已出版 - 25 1月 2025

关键词

  • afterburner
  • dynamic pressure pulsation
  • fluidic oscillator
  • high frequency dynamic sweeping fuel injection
  • oscillation frequency
  • self-excited sweeping nozzle

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