期刊文献+

基于反方法的高负荷涡轮动叶激波控制 被引量:1

Shock Wave Control in Highly-Loaded Turbine Rotor Blade Using an Inverse Method
下载PDF
导出
摘要 为控制高负荷涡轮叶栅中的激波、改善涡轮叶栅流动状况,针对E3涡轮第二级动叶中间叶高叶型,通过修改叶型吸力面压力分布进行了弱化激波S1流面反方法研究,并基于反设计叶型,对涡轮整级性能进行了三维数值计算分析。S1流面求解器选取MISES程序,应用Mixed模式反方法对叶型表面压力分布进行修改,并在反设计过程中临时"冻结"边界层来提高计算鲁棒性,加速收敛。结果表明,S1流面反设计叶型变薄,喉道位置前移,叶栅通道内激波强度明显削弱,叶型尾迹损失明显降低;涡轮整级环境下,反设计叶型使低背压工况下的等熵效率提高了约0.55%,涡轮出口激波强度显著降低,高效运行区拓宽,变工况性能较原始涡轮得到优化,验证了本文反方法的可行性。 In order to control the shock wave and improve the flow conditions of highly-loaded turbine cascades,an inverse method study on S1 stream surface was conducted to weaken the shock wave strength using the blade profile at the mid-span of the second stage rotor blade of E3 turbine. This was realized by adjusting the pressure distribution on the blade suction side. Meanwhile,three dimensional numerical simulation was carried out to analyze the performance of the turbine stage with the inverse-designed blade. The MISES code was chosen to solve the flow field on S1 stream surface,and the pressure distribution was modified through‘mixed-inverse'mode. A temporarily‘frozen'boundary layer scheme was employed to enhance the robustness and accelerate the convergence of the inverse design process. Results indicated that the blade thickness got thinner and the throat position moved forward compared to the original geometry. The shock wave strength was reduced significantly,as well as the wake loss. In addition,under the stage environment,compared to the original turbine,the isentropic efficiency at low back pressure condition increased approximately by 0.55%,and the shock wave intensity at the turbine exit was reduced greatly. The back pressure interval with high efficiency was extended and the off-design performance was improved. These results verified the feasibility of the developed inverse method.
作者 杨金广 徐乐 刘艳 张敏 YANG Jin-guang;XU Le;LIU Yan;ZHANG Min(School of Energy and Power Engineering, Dalian University of Technology, Dalian 116024, China)
出处 《推进技术》 EI CAS CSCD 北大核心 2018年第6期1240-1249,共10页 Journal of Propulsion Technology
基金 国家自然科学基金青年项目(51606026) 辽宁省科学技术计划重大项目(2015106016) 协同创新中心基金项目
关键词 S1流面 反方法 激波控制 高负荷涡轮 S1 stream surface Inverse method Shock wave control Highly-loaded turbine
  • 相关文献

参考文献4

二级参考文献37

  • 1陈池,刘高联.基于变域变分有限元的翼型反设计[J].空气动力学学报,2004,22(4):443-446. 被引量:4
  • 2南向谊,刘波,王掩刚.考虑攻角、落后角的反方法叶型设计优化技术[J].机械设计与制造,2005(10):27-29. 被引量:1
  • 3LIGHTHILL M.A new method of two dimensional aer-odynamic designs[].Aeronautical Research Council′sReports and Memoranda.1945 被引量:1
  • 4J.M.Sanz.Automated design of controlled-diffusion blades[].Journal of TurbomachineryTransof the ASME.1988 被引量:1
  • 5Borges J E.A three-dimensional inverse method for turbo-machinery:PartⅠtheory[].ASME Journal of Turboma-chinery.1990 被引量:1
  • 6Van Rooij M P C,Dang T Q,Larosiliere L M.Improving aerodynamic matching of axial compressor blading using a three-dimensional multistage inverse design method[].Journal of Turbomachinery.2007 被引量:1
  • 7Van Rooij M P C,Dang T Q,Larosiliere L M.EnhancedBlade Row Matching Capabilities via 3D Multistage In verse Design and Pressure Loading Manager. ASMEGT2008-50539 . 2008 被引量:1
  • 8Ji M,Dang T,Cave M J.Fully three-dimensional viscous semi-inverse method for subsonic mixed-flow and radial impeller design. ASME Paper GT-2009 -59679 . 2009 被引量:1
  • 9Victor I Mileshin,Michael A. Nyukhtikov,Igor K. Orekhov.Open Counter-Rotation Fan Blades Optimization Based On 3D Inverse Problem Navier-Stokes Solution Method with the Aim of Tonal Noise Reduction. ASME, GT 2008 -51173 . 2008 被引量:1
  • 10Wang D X,Li Y S.3D direct and inverse design using NSequations and the adjoint method for turbine blades. ASME 2010-GT-22049 . 被引量:1

共引文献14

同被引文献47

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