中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
Thermal performance of a micro-combustor for micro-gas turbine system

文献类型:期刊论文

作者Cao, H. L.; Xu, J. L.
刊名energy conversion and management
出版日期2007-05-01
卷号48期号:5页码:1569-1578
关键词micro-combustion micro-combustor thermal performance operating range heat loss
ISSN号0196-8904
通讯作者xujl@ms.giec.ac.cn
中文摘要premixed combustion of hydrogen gas and air was performed in a stainless steel based micro-annular combustor for a micro-gas turbine system. micro-scale combustion has proved to be stable in the micro-combustor with a gap of 2 mm. the operating range of the micro-combustor was measured, and the maximum excess air ratio is up to 4.5. the distribution of the outer wall temperature and the temperature of exhaust gas of the micro-conbustor with excess air ratio were obtained, and the wall temperature of the micro-combustor reaches its maximum value at the excess air ratio of 0.9 instead of 1 (stoichiometric ratio). the heat loss of the micro-combustor to the environment was calculated and even exceeds 70% of the total thermal power computed from the consumed hydrogen mass flow rate. moreover, radiant hunt transfer covers a large fraction of the total heat loss. measures used to reduce the heat loss were proposed to improve the thermal performance of the micro-combustor. the optimal operating status of the micro-combustor and micro-gas turbine is analyzed and proposed by analyzing the relationship of the temperature of the exhaust gas of the micro-combustor with thermal power and excess air ratio. the investigation of the thermal performance of the micro-combustor is helpful to design an improved microcombustor.
英文摘要premixed combustion of hydrogen gas and air was performed in a stainless steel based micro-annular combustor for a micro-gas turbine system. micro-scale combustion has proved to be stable in the micro-combustor with a gap of 2 mm. the operating range of the micro-combustor was measured, and the maximum excess air ratio is up to 4.5. the distribution of the outer wall temperature and the temperature of exhaust gas of the micro-conbustor with excess air ratio were obtained, and the wall temperature of the micro-combustor reaches its maximum value at the excess air ratio of 0.9 instead of 1 (stoichiometric ratio). the heat loss of the micro-combustor to the environment was calculated and even exceeds 70% of the total thermal power computed from the consumed hydrogen mass flow rate. moreover, radiant hunt transfer covers a large fraction of the total heat loss. measures used to reduce the heat loss were proposed to improve the thermal performance of the micro-combustor. the optimal operating status of the micro-combustor and micro-gas turbine is analyzed and proposed by analyzing the relationship of the temperature of the exhaust gas of the micro-combustor with thermal power and excess air ratio. the investigation of the thermal performance of the micro-combustor is helpful to design an improved microcombustor. (c) 2006 elsevier ltd. all rights reserved.
WOS标题词science & technology ; physical sciences ; technology
类目[WOS]thermodynamics ; energy & fuels ; mechanics ; physics, nuclear
研究领域[WOS]thermodynamics ; energy & fuels ; mechanics ; physics
关键词[WOS]engine
收录类别SCI
原文出处http://www.sciencedirect.com/science/journal/01968904
语种英语
WOS记录号WOS:000245957800018
公开日期2010-09-27
源URL[http://ir.giec.ac.cn/handle/344007/3472]  
专题中国科学院广州能源研究所
作者单位1.Chinese Acad Sci, Guangzhou Inst Energy Convers, Wushan 510640, Peoples R China
2.Univ Sci & Technol China, Dept Thermal Sci & Energy Engn, Hefei 230026, Peoples R China
推荐引用方式
GB/T 7714
Cao, H. L.,Xu, J. L.. Thermal performance of a micro-combustor for micro-gas turbine system[J]. energy conversion and management,2007,48(5):1569-1578.
APA Cao, H. L.,&Xu, J. L..(2007).Thermal performance of a micro-combustor for micro-gas turbine system.energy conversion and management,48(5),1569-1578.
MLA Cao, H. L.,et al."Thermal performance of a micro-combustor for micro-gas turbine system".energy conversion and management 48.5(2007):1569-1578.

入库方式: OAI收割

来源:广州能源研究所

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