期刊文献+

高负荷风扇级环境下叶片反问题设计 被引量:4

Design of High Loading Fan Blade Using Inverse Method in Stage Environment
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摘要 在对国内外各类叶片三维反问题深入分析的基础上,针对高效、高负荷风扇的设计需求,提出了级环境下风扇叶片三维反问题设计的技术思路。以高压比单级风扇为例,利用数值模拟、流动分析等技术手段,采用从基元截面、单排到单级环境逐步深入的方式,对级环境下三维反问题设计方法的可行性进行了验证,初步探索了级环境下叶片载荷分布规律,进一步发展并完善了高效、高负荷风扇叶片的三维反问题设计技术。 The detailed analysis on all kinds of national and international technical data of three-dimensional inverse method was carried out. According to the design requirements of high efficiency and high loading fan, the idea of fan airfoil design in stage environments by using three-dimensional inverse method was proposed. Numerical simulation and flow field analysis were performed in high pressure ratio single-stage fan. The feasibility of the inverse method in stage environments was validated from basic elements, single row to single stage. The blade loading distribution law was preliminarily studied. The airfoil in- verse design technique of high efficiency and high loading fan was improved and developed further through above methods.
出处 《燃气涡轮试验与研究》 北大核心 2012年第3期1-6,共6页 Gas Turbine Experiment and Research
基金 基于全三维反问题的高效高负荷风扇叶片设计技术研究(2009ZB24003) 高通流 跨音双排串列斜流转子单级风扇设计技术初探(2011ZB24002)
关键词 三维反问题 高负荷 风扇 数值模拟 叶片载荷分布规律 three-dimensional inverse method high loading fan numerical simulation blade loading distribution law
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参考文献13

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二级参考文献15

  • 1杜磊,宁方飞.基于控制理论的压气机叶型数值优化方法[J].航空动力学报,2009,24(3):615-625. 被引量:4
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  • 5Medd A J, Dang T Q, Larosiliere L M. 3D Inverse Design Loading Strategy for Transonic Axial Compressor Blading [R]. ASME GT2003-38501,2003.
  • 6Watanabe H, Zangeneh M. Design of the Blade Geometry of Swept Transonic Fans by 3D Inverse Design[R]. ASME GT2003-38770,2003.
  • 7Peixin H, Zangeneh M. On Design of Transonic Fan Ro- tors by 3D Inverse Design Method[R]. ASME GT2006-91173,2006.
  • 8Bonaiuti D, Pitigala A, Zangeneh M, et al. Redesign of a Transonic Compressor Rotor by Means of a Three-Dimen- sional Inverse Design Method: A Parametric Study[R]. ASME GT2007-27486,2007.
  • 9Mileshin V I, Orekhov I K, Fateyev V A, et al. Effect of Tip Clearance on Flow Structure and Integral Performanc- es of Six-Stage HPC[R]. ISABE 2007-1179,2007.
  • 10Mileshin V I, Orekhov I K, Shchipin S K, et al. 3D Inverse Design of Transonic Fan Rotors Efficient for a Wide Range of RPM[R]. ASME GT2007-27817,2007.

共引文献8

同被引文献32

  • 1冯秀莲,金东海,桂幸民.叶片弯掠对压气机静子叶片气动性能影响的三维数值模拟[J].航空动力学报,2009,24(10):2338-2343. 被引量:5
  • 2綦蕾,刘火星,陈浮,候安平.低速压气机不同静叶弯角对流动特性影响的数值模拟[J].燃气涡轮试验与研究,2006,19(3):11-18. 被引量:1
  • 3Jonathan M, Steven R W, Severin K. 3D Numerical Investi- gation of Tandem Airfoils of a Core Compressor Rotor[R]. ASME GT2008-50427,2008.
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  • 7Roidl B, Ghaly W. Redesign of a Low Speed Turbine Stage Using a New Viscous Inverse Design Method [J]. Journal of Turbomachinery , 2010, 133:011009.
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二级引证文献3

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