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高温升蒸发型燃烧室的设计

Design of a High-temperature-rise Evaporation Type Combustor

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【作者】 黎明吴二平唐明

【Author】 LI Ming,WU Er-ping,TANG Ming(College of Power and Energy Source,Northwest Polytechnic University,Xi’an,China,Post Code:710072)

【机构】 西北工业大学动力与能源学院

【摘要】 为了满足某地面实验设备对燃烧室高温升的要求,设计了温升为1350K的蒸发型燃烧室。根据燃烧室总体结构,设计了燃烧室的主要部件。通过对燃烧室的气动热力计算,确定出了燃烧室总体和火焰筒开孔的尺寸,并对燃烧室进行了一定的性能实验。实验及应用结果表明,所设计的燃烧室具有工作安全可靠、结构简单、空间利用率高、升温速度快及排气清洁的特点。在整个工作范围内,燃烧效率达到0.95~0.97,出口温度场不均匀度低于0.09,符合设计要求。

【Abstract】 To meet the requirement of a combustor in a ground surface test facility for a high temperature rise,designed was an evaporation type combustor with a temperature rise of 1 350 K.According to the overall structure of the combustor,its main components were designed.Through the aerodynamic and thermodynamic calculation of the combustor,the overall dimensions of the combustor and the opening hole dimensions of the flame tube were determined.On this basis,a performance test of the combustor was conducted to a certain extent.The test and application results show that the combustor thus designed features a safe and reliable operation,a simple structure,as well as a high space utilization rate,a quick temperature rise speed and a clean exhaust gas.In the whole operation range,the combustion efficiency can reach 0.95~0.97 and the non-uniformity of the temperature field at the outlet is lower than 0.09,thus meeting the design requirements.

【关键词】 燃气轮机高温升蒸发型燃烧室
【Key words】 gas turbinehigh temperature riseevaporation typecombustor
  • 【文献出处】 热能动力工程 ,Journal of Engineering for Thermal Energy and Power , 编辑部邮箱 ,2010年04期
  • 【分类号】V231.2
  • 【被引频次】5
  • 【下载频次】171
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