期刊文献+

叶栅通道内热斑迁移受动静干涉和叶顶间隙高度影响的研究 被引量:1

Effect of Rotor/Stator Interaction and Tip Clearance Height on Hot Streak Migration in Turbine Passage
原文传递
导出
摘要 本文考虑在透平进口存在热斑时,对受动静干涉和叶顶间隙影响的热斑非定常迁移特性以及近壁面区域的热负荷变化规律进行研究。结果表明:热斑在动叶通道中的形态发生较大变化,并存在冷热流体分离现象;在通道涡、泄漏流以及密度梯度产生的次流涡等涡系的联合作用下,压力面侧的热斑流体逐渐向上下端壁延伸,而吸力面侧逐渐向中叶展聚集;随着顶部间隙高度的增大,泄漏涡与通道涡的干涉作用增强,流道中心流体受泄漏涡的挤压而向压力面侧偏移,引起压力面附近温度梯度的增大,同时由于泄漏量的增加,使叶顶附近壁面两侧的传热环境均趋于恶化。 This paper focuses on the unsteady migration of hot streak and the heat load variation near rotor blade surface in a gas turbine with inlet hot streak,which are under the influence of rotor/stator interaction and tip clearance.The results indicate that in rotor passage the shape of hot streak varies greatly,and hot and cold fluid will separate from each other.Under the combined influence of passage vortex,leakage flow and the secondary flow induced by density gradient,the hot streak fluid near pressure side will extend to both endwalls,while near suction side the hot fluid will gather together to mid span.With the increase of tip clearance height,the interactions between leakage flow and passage vortex rise,so the fluid in rotor passage will be squeezed by leakage flow and migrates towards pressure side,subsequently,the temperature gradient could be raised up near pressure side.Meanwhile,due to the increase of leakage flow,the heat transfer environment along both sides near tip region is further aggravated.
出处 《工程热物理学报》 EI CAS CSCD 北大核心 2015年第11期2344-2347,共4页 Journal of Engineering Thermophysics
基金 国家自然科学基金重点项目(No.51336007)
关键词 热斑 非定常流动 热负荷 动静干涉 叶顶间隙高度 hot streak unsteady flow heat load rotor/stator interaction tip clearance height
  • 相关文献

参考文献13

  • 1Barringer M D, Thole K A, Polanka M D, et al. Migra- tion of Combustor Exit Profiles Through High Pressure Turbine Vanes JR]. ASME Paper, GT2007-27157, 2007.
  • 2Povey T, Chana K S., .Jones T V, et al. Tile Effect of Hot- Streaks on HP Vane Surface and Endwall Heat Transfer: An Experimental and Numerical Study [J]. ASME Journal of Turbomachinery, 2007, 129(1): 32 43.
  • 3Mathison R M, Haldeman C W, Dunn M G. Aerodynam- ics and Heat Transfer for a Cooled One and One-Half Stage High-Pressure Turbine-Part I Vane Inlet Tempera- ture Profile Generation and Migration [J]. ASME Journal of Turbomachinery, 2012, 134(1): 011006.
  • 4Jenny P, Lenherr C, Kalfas A I, et al. Effect of Hot Streak Migration on Unsteady Blade Row Interaction in an Axial Turbine [R]. ASME Paper, GT2010-23034, 2010.
  • 5Ong J, Miller H J. Hot Streak and Vane Coolant Migration in a Downstream Rotor JR]. ASME Paper, GT2008-50971, 2008.
  • 6Smith C I, Chang D, Tavoularis S. Effect of Inlet Tem- perature Non-uniformity on High-Pressure Ihlrbine Per- formance [R]. ASME Paper, GT2010- 22845, 2010.
  • 7Simone S, Montomoli F, Martelli F, et al. Analysis on the Effect of a Nonuniform Inlet ProfiIe oll Heat Transfer and Fluid Flow in Turbine Stages [J]. ASME Journal of 151rbomachinery, 2012, 134:011012.
  • 8Liu Z F, Liu Z, Feng Z P. Unsteady Analysis on th Ef- fects of Tip Clearance Height on Hot Streak Migration Across Rotor Blade Tip Clearance [J]. ASME Journal of Engineering for Gas Turbines and Power, 2014. 136(8): 082605.
  • 9Timko L P. Energy Efficient Engine High Pressure Turbine Component Test Performance Report [R]. NASA/CR- 1984-168289. 1984.
  • 10祁明旭,丰镇平,KANGShun,HIRSCHCharles.动静干涉效应对轴流透平级气动性能的影响[J].工程热物理学报,2003,24(1):39-42. 被引量:10

二级参考文献12

  • 1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
  • 2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:30
  • 3DeNOS 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.
  • 4GADEA 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.
  • 5HUMMEL F. Wake-wake interactions and its potential for clocking in a transonic high-pressure turbine [J]. Journal of Turbomachinery, 2002,124 (1) : 69-76.
  • 6MARCONCINI 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.
  • 7CLARK 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.
  • 8RAI 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.
  • 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.

共引文献19

同被引文献22

引证文献1

二级引证文献11

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