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单筒形氢氧燃烧室壁面冷却结构及特性研究
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  • 英文篇名:Research on Wall Cooling Structure and Cooling Performance of a Single Cylinder H_2-O_2 Combustion Chamber
  • 作者:高佳佳 ; 路昆 ; 魏小林
  • 英文作者:GAO Jiajia;LU Kun;WEI Xiaolin;Huadian Electric Power Research Institute;Institute of Mechanics,Chinese Academy of Sciences;
  • 关键词:氢氧燃烧室 ; 壁面冷却 ; 数值模拟 ; 实验研究
  • 英文关键词:H2-O2 combustor;;wall cooling;;numerical simulation;;experimental study
  • 中文刊名:DONG
  • 英文刊名:Journal of Chinese Society of Power Engineering
  • 机构:华电电力科学研究院;中国科学院力学研究所;
  • 出版日期:2018-05-15
  • 出版单位:动力工程学报
  • 年:2018
  • 期:v.38;No.281
  • 语种:中文;
  • 页:DONG201805005
  • 页数:8
  • CN:05
  • ISSN:31-2041/TK
  • 分类号:31-38
摘要
针对新型氢氧燃机热力循环系统,提出了一种壁面水冷氢氧燃烧室,通过CFD软件优化了其壁面冷却结构,并在此基础上对其水冷壁面冷却特性进行了实验研究。结果表明:相同条件下,小深宽比的冷却结构的冷却效果优于大深宽比冷却结构的冷却效果;在设计的不同负荷下,燃烧室壁面温度最高不超过400K;在主燃区轴向距离x≈0.035m处,冷却水体积流量为0.8m~3/h时壁面局部热流密度最大值约为246.5kW/m~2,壁面局部热流密度随着冷却水体积流量的增加而增加。
        A novel single cylinder H_2-O_2 combustion chamber with wall cooling was proposed based on the new hydrogen and oxygen gas turbine thermal cycle system.The wall cooling structure was optimized by CFD,based on which,experimental studies were carried out on the water cooling characteristics.Results show that,the cooling performance of the cooling structure with small depth-to-width ratio is better than that with high depth-to-width ratio.The wall temperatures of the combustion chamber are all below 400 K at different loads.In the primary zone around x=0.035 m,the maximum local wall heat flux is about 246.5 kW/m~2 for the cooling water flow rate of 0.8 m~3/h;the local wall heat flux increases with the rise of cooling water flow rate.
引文
[1]JUSTE G L.Hydrogen injection as additional fuel in gas turbine combustor.Evaluation of effects[J].International Journal of Hydrogen Energy,2006,31(14):2112-2121.
    [2]SINGH K,VARATHARAJAN B,YILMAZ E,et al.Effect of hydrogen combustion on the combustion dynamics of a natural gas combustor[C]//ASME Turbo Expo 2008:Power for Land,Sea,and Air.Berlin,Germany:ASME,1045-1050.
    [3]居重艳,李政,麻林巍,等.燃氢燃气轮机的变工况特性[J].动力工程学报,2010,30(10):755-762.JU Chongyan,LI Zheng,MA Linwei,et al.Characteristics of hydrogen gas turbine in off-design state[J].Journal of Chinese Society of Power Engineering,2010,30(10):755-762.
    [4]WU Jianfan,BROWN P,DIAKUNCHAK I,et al.Advanced gas turbine combustion system development for high hydrogen fuels[C]//ASME Turbo Expo2007:Power for land,Sea,and Air.Montreal,Canada:Siemens Power Generation,2007.
    [5]KOBAYASHI N,MANO T,ARAI N.Fuel-rich hydrogen-air combustion for a gas-turbine system without CO2 emission[J].Energy,1997,22(2/3):189-197.
    [6]FUNATSU T,FUKUDA M,DOHZONO Y.Start up analysis of a H2-O2fired gas turbine cycle[C]//ASME 1997International Gas Turbine and Aeroengine Congress and Exhibition.Orlando,Florida,USA:ASME,1997.
    [7]SOUFI M G,FUJII T,SUGIMOTO K,et al.A new Rankine cycle for hydrogen-fired power generation plants and its exergetic efficiency[J].International Journal of Exergy,2004,1(1):29-46.
    [8]COCCHI S,PROVENZALE M,CINTI V,et al.Experimental characterization of a hydrogen fuelled combustor with reduced NOxemissions for a 10 MW class gas turbine[C]//Proceedings of ASME Turbo Expo 2008:Power for Land,Sea,and Air.Berlin,Germany:ASME,2008:991-1000.
    [9]RAZAK A M Y.Industrial gas turbines:performance and operability[M].Boca Raton,USA:CRC Press,2007.
    [10]KIZUKA N,SAGAE K,ANZAI S,et al.Conceptual design of the cooling system for 1 700℃-class,hydrogen-fueled combustion gas turbines[J].Journal of Engineering for Gas Turbines and Power,1999,121(1):108-115.
    [11]焦树建.燃气轮机燃烧室[M].北京:机械工业出版社,1981.
    [12]钟芳源.燃气轮机设计基础[M].北京:机械工业出版社,1987.
    [13]LI Juan,ZHAO Zhenwei,KAZAKOV A,et al.An updated comprehensive kinetic model of hydrogen combustion[J].International Journal of Chemical Kinetics,2004,36(10):566-575.
    [14]孙淮清,王建中.流量测量节流装置设计手册[M].2版.北京:化学工业出版社,2005.
    [15]萨顿G P,比布拉兹O.火箭发动机基础[M].7版.洪鑫,张宝炯,译.北京:科学出版社,2003.
    [16]杨世铭,陶文铨.传热学[M].4版.北京:高等教育出版社,2006.

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