期刊文献+

非轴对称端壁造型技术在透平中的应用和发展 被引量:6

Application and Development of the Non-Axisymmetrical Endwall Contouring in the Turbomachinery
在线阅读 下载PDF
导出
摘要 非轴对称端壁的设计和应用可以有效地减少透平叶栅中的二次流损失,提高透平机械通流部分的气动性能。对非轴对称端壁造型技术的应用背景、端壁造型方法及其在透平机械中的研究现状进行了综述,详细介绍了非轴对称端壁对叶栅和透平级气动性能的影响,阐述了气动性能得以提高的机理,结合实验结果介绍了非轴对称端壁对叶栅和透平级变工况特性的影响。在透平叶栅非轴对称端壁成型研究进展的基础上,对非轴对称端壁造型技术在高负荷透平叶片研发和叶片三维造型中的应用前景进行了展望。 Design and application of the non-axisymmetrical endwall contouring in the turbine have been proved to decrease the secondary flow losses effectively and improve the aerodynamic performance of the gas turbine.The application background and the development of research about the non-axisymmetrical endwall contouring are summarized and the method of the endwall is generated.The effects of the non-axisymmetrical endwall contouring on the cascade and turbine stage are presented to demonstrate the reason of the performance improvement.Moreover,with the help of the experiment results,this paper also shows the influences of the non-axisymmetrical endwall contouring on the cascade and turbine stage in the off-design conditions.Finally,the applications of the non-axisymmetrical endwall contouring in the development of high loaded turbine blade profile and three-dimensional parameterized vane are presented.
出处 《热力透平》 2012年第1期18-25,共8页 Thermal Turbine
关键词 透平机械 非轴对称端壁 二次流 turbomachinery non-axisymmetrical endwall contouring secondary flow
  • 相关文献

参考文献20

  • 1Lakshminarayana B.Fluid Dynamics and Heat Transfer ofTurbomachinary[M].John Wiley&Sons.Inc,1996.
  • 2Gregory-Smith D G,Ingram G,et al.Non-Axisymmetric TurbineEnd Wall Profiling[J].IMechE,2001,215:A03501.
  • 3Morris A W H,Hoare R G.Secondary Loss Measurements in aCascade of Turbine Blades With Meridional Wall Profiling[C].ASME Paper,No.75-WA/GT-13,1975.
  • 4Atkins M J.Secondary Losses and End-Wall Profiling in aTurbine Cascade[J].I Mech.E C255/87,1987:29–42.
  • 5Rose M G.Non-axisymmetric Endwall Profiling in the HP NGVsof an Axial Flow Gas Turbine[C].ASME Paper,No.94-GT-249,1994.
  • 6Harvey N,Rose M,Seaman P,Newman D and McManus D.Nonaxisymmetric Turbine End Wall Design:PartⅠ-Three-Dimensional Linear Design System[J].ASME J.Turbom.
  • 7Hartland J C,Smith D G,Harvey N,Rose M.Non-AxisymmetricTurbine End Wall Design:Part II-Experimental Validation[J].ASME J.Turbomach,2000,122(2):286–29.
  • 8Germain T,Nagel M G,et al.Improving Efficiency of a HighWork Turbine Using Non-Axisymmetric Endwalls-PartⅠ:Endwall Design and Performance[J].ASME J.T.
  • 9Brennan G,Harvey N,Rose,M G,et al.Improving the Efficiencyof the Trent 500-HP Turbine Using Non-Axisymmetric Endwalls-Part 1:Turbine Design[J].ASME J.
  • 10PraisnerT J,Allen-Bradley E,Grover E A.Application of Non-Axisymmetric Endwall Contouring to Conventional and High-LiftTurbine Airfoils[C].ASME Paper.

二级参考文献11

  • 1马晓勇 李国君 李亮.可压缩性对两方程紊流模型的影响[A]..2004年中国工程热物理年会学术会议[C].西安,2004..
  • 2Menter F R. Two- equation eddy viscosity turbulence models for engineering application[J]. AIAA J, 1994, 32(11): 1 598-1 605.
  • 3Marc G, Nagel Ralf D B. Experimental verified numerical optimization of a 3D-parametrised turbine vane with non-axisymmetric end walls[A]. Proceedings of ASME Turbo Expo 2003, Atlanta, USA, 2003.
  • 4Rose M G. Non-axisymmetric end wall profiling in the HP NGVs of an axial flow gas turbine[A]. Proceedings of ASME Turbo Expo 1994 Power for Land, Sea & Air, New York, USA ,1994.
  • 5Harvey N W, Rose M G. Non-axisymmetric turbine end wall design: three-dimensional linear design system[A]. Proceedings of ASME Turbo Expo 1999 Power for Land, Sea & Air, New York, USA, 1999.
  • 6Hartland J C, Gregory-Smith D. Non-axisymmetric turbine end wall design: experimental validation[A]. Proceedings of ASME Turbo Expo 1999 Power for Land, Sea & Air, New York, USA, 1999.
  • 7Rose M G, Harvey N W. Improving the efficiency of the trend 500HP turbine using non-axisymmetric end walls: experimental validation[A]. Proceedings of ASME Turbo Expo 2001 Power for Land, Sea & Air, New Orleans, USA, 2001.
  • 8Harvey N W, Rose M G. Improving turbine efficiency using non-axisymmetric end walls: validation in the multi-row environment and with low aspect ratio blading[A]. Proceedings of ASME Turbo Expo 2002, Amsterdam, The Netherlands, 2002.
  • 9Ingram G, Gregory-Smith D, Rose M G. The effects of end-wall profiling on secondary flow and loss development in a turbine cascade[A]. Proceedings of ASME Turbo Expo 2002, Amsterdam, The Netherlands, 2002.
  • 10郑金,李国君,李军,张兄文.一种新非轴对称端壁成型方法的数值研究[J].航空动力学报,2007,22(9):1487-1491. 被引量:28

共引文献56

同被引文献35

引证文献6

二级引证文献9

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