期刊文献+

冲击-气膜式蒸汽冷却叶片数值模拟研究 被引量:1

Numerical Simulation of Impingement-film Steam-cooling Turbine Blades
下载PDF
导出
摘要 在纯气膜蒸汽冷却叶片结构基础上,在其前腔设计加装了冲击冷却套筒,目的是对纯气膜冷却中叶片出现的高温区采用射流冲击冷却方式来进一步降低高温区的温度,强化了换热效果。为得到叶片内部流道的流动情况和叶片外表面压力分布、温度分布情况,借助ANSYS CFX软件对其进行流热固耦合数值模拟,并对其进行对比分析。结果表明,采用冲击-气膜组合冷却方式与传统气膜冷却方式相比,可使叶片高温区最多再降低150K,整体冷却效率可达到60%。 Based on the pure steam film cooling blades, add a cooling set in front of the blade. Use of jet impact cooling to reduce the temperature of the high-temperature region. Analysis and numerical simulation of flow field and temperature field in finite element analysis software CFX. Then get the flow field of the inner flow channel, the pressure and temperature of the outside surface of the blade. The calculated results show that the impingement-film steam-cooling is a better method than the traditional film one. The impingement-film steam-cooling method can further reduced the blade temperature up to 150K, and the overall cooling efficiency up to 60%.
出处 《汽轮机技术》 北大核心 2013年第3期185-188,共4页 Turbine Technology
关键词 蒸汽冷却 射流冲击 数值模拟 steam cooling jet impingement numerical simulation
  • 相关文献

参考文献5

  • 1韩介琴,桑地普?杜达,斯瑞纳斯?艾卡德著.程代京,谢永慧,译.燃气轮机传热和冷却技术[M].西安:西安交通大学出版社,2005.
  • 2GUO TAO. Mist/steam cooling in a heated horizontal tube [ J ].Clemson : Clemson University, 1998.
  • 3倪萌,朱惠人,裘云,许都纯,刘松龄.航空发动机涡轮叶片冷却技术综述[J].燃气轮机技术,2005,18(4):25-33. 被引量:91
  • 4Stecco S. S. ,Facchini B.,A simplified thermodynamic analysis ofblade cooling effects in combined power plants[ A]. Proceeding ofsecond ASME Cogenturbo[ C]. Montreux, Switzerland, 1988. 299-304,ASME-GT-270.
  • 5胡宗军,吴铭岚.采用蒸汽冷却的各种燃气轮机循环性能分析[J].上海交通大学学报,1999,33(3):335-338. 被引量:11

二级参考文献81

共引文献100

同被引文献20

  • 1胡捷,苏生,刘建军,安柏涛.透平导叶闭式蒸汽冷却方案研究[J].工程热物理学报,2008,29(7):1121-1124. 被引量:2
  • 2Liu J Z,Gao J M,Gao T Y,et al.Heat transfer characteristics in steam-cooled rectangular channels with two opposite rib-roughened walls[J].Applied Thermal Engineering,2013,50(1):104-111.
  • 3Shui L Q,Gao J M,Shi X J,et al.Effect of duct aspect ratio on heat transfer and friction in steam-cooled ducts with 60° angled rib turbulators[J].Experimental Thermal and Fluid Science,2013,49:123-134.
  • 4Shui L Q,Gao J M,Xu L,et al.Numerical investigation of heat transfer and flow characteristics in a steam-cooled square ribbed duct[C]//Proceedings of ASME Turbo Expo 2010:Power for Land,Sea,and Air.Glasgow,UK:ASME,2010:163-171.
  • 5Facchini B,Ferrara G,Innocenti L.Blade cooling improvement for heavy duty gas turbine:the air coolant temperature reduction and the introduction of steam and mixed steam/air cooling[J].International Journal of Thermal Sciences,2000,39(1):74-84.
  • 6Najjar Y S H,Alghamdi A S,Al-Beirutty M H.Comparative performance of combined gas turbine systems under three different blade cooling schemes [J].Applied Thermal Engineering,2004,24(13):1919-1934.
  • 7Bohn D,Wolff A,Wolff M,et al.Experimental and numerical investigation of a steam-cooled vane [C]//Proceedings of ASME Turbo Expo 2002:Power for Land,Sea,and Air.Amsterdam,The Netherlands:ASME,2002:477-484.
  • 8Bohn D,Ren J,Kusterer K.Cooling performance of the steam-cooled vane in a steam turbine cascade [C]//Proceeding of ASME Turbo Expo 2005:Power for Land,Sea,and Air.Reno Tahoe,Nevada,USA:ASME,2005:217-226.
  • 9Wang T,Gaddis J L,Li X C.Mist/steam heat transfer of multiple rows of impinging jets[J].International Journal of Heat and Mass Transfer,2005,48(25-26):5179-5191.
  • 10Guo T,Wang T,Gaddis J L.Mist/steam cooling in a heated horizontal tube,Part 1:Experimental system[J].Journal of Turbomachinery,1999,122(2):360-365.

引证文献1

二级引证文献8

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部