期刊文献+

蒸汽/空气两种介质在涡轮叶片中冷却性能对比的试验研究 被引量:8

Comparative Experiment of Cooling Performance in a Turbine Blade Cooled by Steam and Air Flow
下载PDF
导出
摘要 搭建了高温风洞环形叶栅试验台,分别对冷却叶片通蒸汽和空气进行冷却,利用红外热像仪测量叶片吸力面在这2种冷却介质冷却下的温度分布,并对这2种冷却介质冷却下的叶片的冷却性能进行了对比,研究表明:蒸汽冷却相对于空气冷却并不能明显改变叶片表面冷却效率分布特征,但是蒸汽冷却下叶片表面的冷却效率得到提高,相对温度明显降低,在流量比ω=0.026的设计工况下,叶片吸力面前部区域的平均冷却效率在蒸汽冷却下比空气冷却时提高了15.5%,相对温度降低0.011,叶片吸力面后部区域蒸汽冷却平均冷却效率比空气冷却提高了13.4%,相对温度降低0.017。相对于传统的空气冷却技术,蒸汽冷却的优势十分明显。 An annular cascade test was conducted in a high temperature tunnel. One blade in the annular cascade was respectively cooled by super-heated steam and air. The temperature distributions on the suction surface of the blade cooled by the two coolants were both measured by an infrared camera, and the cooling performance of the two coolants was compared with each other. Results show that: the steam cooling does not significantly change cooling efficiency distribution on blade surface, but the cooling performance for steam flow is obvious better than that for air flow. For example, in the design working condition of flow ratio ω =0.026, the area-averaged cooling efficiencies of the front part and rear part of the suction surface are respectively increased by 15.5% and 13.4% in steam cooling than that in air cooling. At the same time, the relative temperatures of the two parts are reduced by 0.011 and 0.017, respectively. Comparing with traditional air cooling in blade, the advantages of steam cooling are very obvious.
出处 《中国电机工程学报》 EI CSCD 北大核心 2016年第6期1650-1657,共8页 Proceedings of the CSEE
基金 国家自然科学基金项目(51206109)~~
关键词 燃气轮机 高温风洞 蒸汽冷却 空气冷却 冷却效率 gas turbine high-temperature tunnel steam cooling air cooling cooling efficiency
  • 相关文献

参考文献21

  • 1Liu 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.
  • 2Shui 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.
  • 3Shui 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.
  • 4WANG Wei,GAO Jianmin,XU Liang,SHI Xiaojun.Flow and Heat Transfer Characteristics in Rotating Two-pass Channels Cooled by Superheated Steam[J].Chinese Journal of Aeronautics,2012,25(4):524-532. 被引量:7
  • 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.

二级参考文献103

  • 1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
  • 2董威,黄维娜.某型发动机涡轮冷却叶片的流动换热耦合计算研究[J].燃气涡轮试验与研究,2006,19(2):14-17. 被引量:3
  • 3杨凡,郑洪涛,李智明.前缘气膜孔对涡轮静叶冷却效果影响的数值模拟[J].热能动力工程,2006,21(4):345-349. 被引量:1
  • 4杨凡,曹辉,郑洪涛,李智明.涡轮静叶前缘气膜冷却数值模拟[J].汽轮机技术,2006,48(4):269-271. 被引量:2
  • 5[3]Matta R K,Mercer G D,Tuthill R S.Power Systems for the 21st Century-‘H'Gas Turbine Combined-Cycles.GE Power Systems,GER-3935B,1995
  • 6[4]Nomoto H,Konga A,Ito S,et al.The Advanced Cooling Technology for the 1500℃ Class Gas 2-hrbine:Steam-Cooled Vanes and Air-Cooled Blades.Journal of Engineering for Gas Turbine and Power,1997,119:624-632
  • 7[5]Corman J C,Paul T C.Power Systems for the 21st Century-‘H'Gas Turbine Combined-Cycles.GE Power Systems,GER-3935B,1995
  • 8[6]Dieter Bohn,Eckhard Martens.Analysis of the Influence of Cooling Steam Conditions on the Cooling Efficiency of Steam-Cooled Vane Using the Conjugate Calculation Technique.ASME Paper GT-2001-0166,2001
  • 9[7]Dieter Bohn,Andreas Wolff,Michael Wolff,et al.Experimental and Numerical Investigation of a Steam-Cooled Vane.ASME GT-2002-30210,2002
  • 10[8]Dieter Bohn,Jing Ren,Karsten Knsterer.Cooling Performance of the Steam-Cooled Vane in a Steam Tubine Cascade.ASME GT-2005-68148,2005

共引文献161

同被引文献106

引证文献8

二级引证文献37

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