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Experimental Investigation on Flame Formation and Propagation Characteristics in an Ethylene Fuelled Wave Rotor Combustor

机译:乙烯燃料波转子燃烧器火焰形成和传播特性的实验研究

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摘要

To find the flame formation and propagation characteristics in an ethylene fuelled wave rotor combustor (WRC), a simplified WRC test system was established. It is a single-channel multiple-cycle WRC with a rotating inlet/outlet port. Through varying the parameters such as the filling speed of the air-fuel mixture, rotating speed of the inlet/outlet port, and equivalence ratio of the combustive air-fuel mixture, the flame formation and propagation characteristics in an ethylene fuelled WRC are presented and discussed. While the rotating speed of the inlet/outlet port increases, the propagation speed of the flame also gradually increases. When the rotating speed of the inlet/outlet port is 1500 rpm, the propagation speed of the flame reaches 45 m/s. A higher rotating speed of the inlet/outlet port leads to a faster expansion of the reaction zone. Furthermore, the inclination angle and corrugation of the flame front in the channel of the WRC with a different rotating speed and different equivalence ratio are presented and discussed.
机译:为了找到乙烯燃料波转子燃烧器(WRC)中的火焰形成和传播特性,建立了简化的WRC测试系统。它是具有旋转入口/出口端口的单通道多周期WRC。通过改变诸如空气燃料混合物的填充速度,入口/出口的旋转速度以及可燃空气燃料混合物的当量比之类的参数,呈现了乙烯燃料WRC中的火焰形成和传播特性,并且讨论过。当入口/出口的旋转速度增加时,火焰的传播速度也逐渐增加。当入口/出口的旋转速度为1500rpm时,火焰的传播速度达到45m / s。入口/出口的较高旋转速度导致反应区更快的膨胀。此外,提出并讨论了不同旋转速度和不同当量比的WRC通道中火焰前缘的倾斜角和波纹。

著录项

  • 来源
    《Energy & fuels》 |2018年第2期|2366-2375|共10页
  • 作者单位

    Nanjing Univ Aeronaut & Astronaut, Key Lab Aeroengine Thermal Environm & Struct, Minist Ind & Informat Technol, 29 Yudao St, Nanjing 210016, Jiangsu, Peoples R China;

    Aero Engine Acad China, Simulat Technol Res Ctr, Beijing 101300, Peoples R China;

    Army Engn Univ PLA, Sch Natl Def Engn, 88 Biaoying Rd, Nanjing 210007, Jiangsu, Peoples R China;

    Nanjing Univ Aeronaut & Astronaut, Key Lab Aeroengine Thermal Environm & Struct, Minist Ind & Informat Technol, 29 Yudao St, Nanjing 210016, Jiangsu, Peoples R China;

    Nanjing Univ Aeronaut & Astronaut, Key Lab Aeroengine Thermal Environm & Struct, Minist Ind & Informat Technol, 29 Yudao St, Nanjing 210016, Jiangsu, Peoples R China;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);美国《生物学医学文摘》(MEDLINE);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

  • 入库时间 2022-08-18 00:39:05

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