F级燃气轮机环形燃烧室设计方法的研究

朱杰文; 刘江; 翁培奋; 高欢欢

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DOI:10.3969/j.issn.2096-8299.2020.02.012

上海电力大学学报:2020,36(2):168-172,178

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F级燃气轮机环形燃烧室设计方法的研究

朱杰文¹, 刘江^1,2, 翁培奋^1,2, 高欢欢¹

(1.上海电力大学能源与机械工程学院;2.上海电力大学上海热交换系统节能工程技术研究中心)

Design Method of Annular Combustor for F-class Heavy Duty Gas Turbine

ZHU Jiewen¹, LIU Jiang^1,2, WENG Peifen^1,2, GAO Huanhuan¹

(1.School of Energy and Mechanical Engineering, Shanghai University of Electric Power, Shanghai 200090, China;2.Shanghai Engineering Research Center of Energy-Saving in Heat Exchange Systems, Shanghai University of Electric Power, Shanghai 200090, China)

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投稿时间：2019-01-08

中文摘要: 采用总压恢复系数方法并结合数值模拟验证,进行了F级重型燃气轮机环形燃烧室的设计计算。根据燃烧室设计参数完成了环形燃烧室的总体设计方案,以及旋流器和火焰筒等部件的设计方案。采用数值模拟对设计完成的燃烧室进行性能分析,得出最优的值班燃料入口和预混燃料入口的旋流速度设定。在最优的入口旋流设定下,环形燃烧室内部流场能够形成两个旋转方向相反的回流区,保证了燃烧的稳定。此时燃烧室内的温度场、速度场和气体组成分布均能满足燃烧室的设计要求。

中文关键词: 燃气轮机环形燃烧室数值分析

Abstract:The total pressure recovery coefficient method combined with numerical simulation verification has been used for the design and calculation of annular combustion chamber of F-class heavy gas turbine.Firstly,the overall design of the annular combustor,the swirler and the flame cylinder are completed according to the design parameters of the combustor.The performance of the designed combustor is analyzed by numerical simulation and the optimal scheme of the swirl velocity setting of the duty fuel inlet and the premixed fuel inlet is obtained.Under the optimal inlet swirl setting,the internal flow field of the annular combustion chamber can form two circumfluence areas with opposite rotation directions to each other,thus ensuring the combustion stability.Meanwhile,the temperature field,the velocity field and the gas component distribution in the combustion chamber can meet the design requirements of the combustion chamber.

keywords: gas turbine annular combustion chamber numerical simulation

文章编号：20202012 中图分类号：TK474+.9 文献标志码：

基金项目:上海市科学技术委员会资助项目（16020500700）。

作者	单位	E-mail
朱杰文	上海电力大学能源与机械工程学院
刘江	上海电力大学能源与机械工程学院上海电力大学上海热交换系统节能工程技术研究中心	jiangliuxjtu@163.com
翁培奋	上海电力大学能源与机械工程学院上海电力大学上海热交换系统节能工程技术研究中心
高欢欢	上海电力大学能源与机械工程学院

Author Name	Affiliation	E-mail
ZHU Jiewen	School of Energy and Mechanical Engineering, Shanghai University of Electric Power, Shanghai 200090, China
LIU Jiang	School of Energy and Mechanical Engineering, Shanghai University of Electric Power, Shanghai 200090, China Shanghai Engineering Research Center of Energy-Saving in Heat Exchange Systems, Shanghai University of Electric Power, Shanghai 200090, China	jiangliuxjtu@163.com
WENG Peifen	School of Energy and Mechanical Engineering, Shanghai University of Electric Power, Shanghai 200090, China Shanghai Engineering Research Center of Energy-Saving in Heat Exchange Systems, Shanghai University of Electric Power, Shanghai 200090, China
GAO Huanhuan	School of Energy and Mechanical Engineering, Shanghai University of Electric Power, Shanghai 200090, China

引用文本：
朱杰文,刘江,翁培奋,等.F级燃气轮机环形燃烧室设计方法的研究[J].上海电力大学学报,2020,36(2):168-172,178.
ZHU Jiewen,LIU Jiang,WENG Peifen,et al.Design Method of Annular Combustor for F-class Heavy Duty Gas Turbine[J].Journal of Shanghai University of Electric Power,2020,36(2):168-172,178.