期刊文献+

一级半轴流式透平的非定常流动干涉与时序效应 被引量:11

Interaction and Clocking Effect of Unsteady Flow in a One and a Half Axial-flow Turbine Stage
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摘要 对Aachen一级半轴流式透平进行了全三维粘性非定常流动数值模拟,分析了相邻叶排间主要干涉现象和时序效应.结果表明:相邻叶排的压力有势场存在势干涉,动叶与第2列静叶间的势干涉更为强烈,势干涉定量反应为静压波动,并以一定的速度向上、下游传播;被动叶截断的上游静叶尾迹在动叶通道中发生变形而周期性地出现在绝对坐标系的固定位置,为时序效应的产生创造条件,通过分析动叶出口熵值的时空分布图可确定下游静叶的最优时序位置;透平级出口非定常熵值定性决定了非定常效率,为透平的非定常优化设计提供了目标参数. The unsteady flow in a one and a half of Aachen axial-flow turbine stage was investigated by full three-dimensional viscous numerical simulation, and the main interaction phenomenon of adjacent blade rows and clocking effect were discussed. Results indicate that between adjacent blade rows the interaction of pressure potential field happens, which is more intense between the rotor and the second stator. The interaction of pressure potential field is quantified by the fluctuation of static pressure on the surface of blade and propagates upstream and downstream at certain speed respectively. Truncated by the blade, the wake caused by upstream stator, which is distorted in the rotor passage occurs at certain position in the absolute coordinate system periodically, which creates a condition for clocking effect. The best clocking position for the second stator can be determined through analyzing the space-time diagram of entropy at the exit of rotor. Qualitatively, the entropy at the exit of the turbine decides the efficiency of turbine stage, which provides a new objective parameter for unsteady optimization and design of turbines.
出处 《动力工程》 CAS CSCD 北大核心 2009年第2期111-116,共6页 Power Engineering
基金 国家973资助项目(2007CB210107)
关键词 一级半透平 非定常流动 时序效应 全三维 数值模拟 one and a half turbine unsteady flow clocking effect full three-dimensional numerical simulation
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参考文献11

  • 1陈海生,谭春青.叶轮机械内部流动研究进展[J].机械工程学报,2007,43(2):1-12. 被引量:29
  • 2DeNOS R, PANIAGUA G. Effect of vane-rotor interaction on the unsteady flowfield downstream of a transonic high pressure turbine[J]. Journal of Power and Energy, 2005, 219(6) :431-442.
  • 3GADEA J. Effect of clocking on the second stator pressure field of a one and a half stage transonic turbine[C]//ASME Turbo Expo 2004. Vienna, Austria:[s. n. ], 2004.
  • 4HUMMEL F. Wake-wake interactions and its potential for clocking in a transonic high-pressure turbine [J]. Journal of Turbomachinery, 2002,124 (1) : 69-76.
  • 5MARCONCINI M. Numecal investigation of wake-shock interactions and clocking in a transonic high pressure turbine[C]//ASME Turbo Expo 2003. Atlanta, Georgia:[s. n. ], 2003.
  • 6CLARK J P. The effect of airfoil scaling on the predicted unsteady loading on the blade of a 1 and 1/2 stage transonic turbine and a comparison with experimental results [C]//ASME Turbo Expo 2000. Munich, Germany:[s. n.], 2000.
  • 7RAI M M. Three-dimensional navier-stokes simulations of turbine rotor-stator Interaction, Part I-Methodology [J]. Journal of Propulsion and Power, 1989, 5(3) :305-311.
  • 8杨宁,戴韧,陈康民.进口湍流对透平叶栅内部流动影响的数值研究[J].动力工程,2005,25(3):325-330. 被引量:3
  • 9RYAN M. Unsteady aerodynamics and interactions between a high pressure turbine vane and rotor[C]// ASME Turbo Expo 2004, Vienna, Austria.. [s. n. ], 2004.
  • 10ARNONE A. Numecal investigation of three-dimensional clocking effects in a low pressure turbine[C]// ASME Turbo Expo 2003. Atlanta, Georgia: [s. n. ], 2003.

二级参考文献21

  • 1刘艳明,钟兢军,李海滨,王松涛.不同长度端壁翼刀对压气机叶栅二次流影响的数值研究[J].航空动力学报,2004,19(5):666-670. 被引量:18
  • 2刘景梅,周盛.叶轮机械新流型探索雏议[J].航空动力学报,1995,10(3):205-209. 被引量:6
  • 3姚征,Hirsch,C.多级叶轮机三维流动计算的级间混合方法分析[J].工程热物理学报,1996,17(4):417-422. 被引量:16
  • 4Sieverding C H, Van Hove W, Boletis E. Experimental study of the three-dimensional flow field in an annular turbine nozzle guidevane [J]. Journal of engineering for gas turbine and power, 1984(106) :437~444.
  • 5Wang H P, Olson S J, Goldstein R J, Eckert E R G. Flow visualization in a linear turbine cascade of high performance turbine blades [J]. Journal of turbomachinery, 1997(119):1~8.
  • 6Numeca User Mannual: Fine/Tuobo 6.10, 2003. [M].
  • 7Baldwin B S, Lomax H. Thin layer approximation and algebraic model for separated turbulence flows [D] . AIAA,1978:78~257.
  • 8Spalart P R,Allmaras S R. A one-equation turbulence model for aerodynamics flows [D]. AIAA paper, 92~0439.
  • 9Yang Z, Shih T H. A k-ε model for turbulence and transitional boundary layer Near-wall turbulent flows, R. M.C. So. , C. G. Speziale and B. E. Launder [M] . ElsevierScience Publishers B.V., pp. 165 ~ 175.
  • 10Langston L S, Nice M L, Hooper R M. Three-dimensional flow within a turbine cascade passage [J]. ASME Journal of engineering for power, 1977, 99(1) :21~28.

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