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Experimental investigation on thermal and combustion performance of a combustor with microchannel cooling

机译:具有微通道冷却的燃烧室热和燃烧性能的实验研究

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摘要

Microchannel cooling provides an efficient thermal management method for regenerative cooling systems of advanced areo engines. In this study, a prototype combustor with microchannel cooling passages in the walls is experimentally developed. Combustion tests are systematically conducted in a range of air inlet temperature (30-70 degrees C), equivalence ratios (0.8-1.2) and flow rates of coolant (100-300 kg/m(2)s) using liquid fuel of ethanol and air mixture. Comparative studies against a combustor without micro channel cooling are also conducted to assess the feasibility of performance enhancement. The introduction of microchannel cooling was found to induce an 80% reduction of the maximum wall temperatures, and a larger than 90% reduction of the streamline wall temperature gradient. The combustor with microchannel cooling also induced a 1%-3.2% increase of the combustion efficiency and a 0.3%-1.7% reduction of the CO emissions in general compared to that without microchannel cooling. The wall temperatures and combustion efficiency of the combustor with microchannel cooling were found to increase with the increase in air inlet temperatures from 30 to 70 degrees C, whereas they tended to decrease when the equivalence ratio increased from 0.8 to 1.2. Nevertheless, the flow rate of coolant played a negligible role on the combustion performance of the combustor with microchannel cooling. (C) 2019 Elsevier Ltd. All rights reserved.
机译:微通道冷却为先进的面罩发动机的再生冷却系统提供了一种有效的热管理方法。在这项研究中,实验开发了一种在壁上具有微通道冷却通道的燃烧室原型。使用乙醇和乙醇作为液体燃料,在进气温度(30-70摄氏度),当量比(0.8-1.2)和冷却剂流速(100-300 kg / m(2)s)的范围内系统地进行燃烧测试。空气混合物。还针对没有微通道冷却的燃烧室进行了比较研究,以评估性能增强的可行性。发现引入微通道冷却引起最大壁温降低80%,并且流线壁温度梯度降低大于90%。与没有微通道冷却的燃烧器相比,具有微通道冷却的燃烧器通常还使燃烧效率提高了1%-3.2%,CO排放降低了0.3%-1.7%。发现随着进气温度从30摄氏度增加到70摄氏度,燃烧室的壁温和燃烧效率随着微通道冷却而增加,而当量比从0.8升高到1.2时,壁温和燃烧效率趋于降低。然而,在微通道冷却的情况下,冷却剂的流量对燃烧室的燃烧性能的影响可忽略不计。 (C)2019 Elsevier Ltd.保留所有权利。

著录项

  • 来源
    《Energy》 |2019年第15期|954-963|共10页
  • 作者单位

    Harbin Inst Technol, Sch Mech Engn & Automat, Shenzhen 518055, Peoples R China|Xiamen Univ, Dept Mech & Elect Engn, Xiamen 361005, Peoples R China;

    Xiamen Univ, Dept Mech & Elect Engn, Xiamen 361005, Peoples R China;

    Xiamen Univ, Dept Mech & Elect Engn, Xiamen 361005, Peoples R China;

    Xiamen Univ, Dept Mech & Elect Engn, Xiamen 361005, Peoples R China;

    Xiamen Univ, Dept Aeronaut, Xiamen 361005, Peoples R China;

  • 收录信息
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Combustion; Microchannel cooling; Regenerative cooling; Wall temperature;

    机译:燃烧;微通道冷却;蓄冷;壁温;

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