期刊文献+

旋转对称支承机座的热分析与变工况计算 被引量:2

Partial Load Calculation and Thermal Analysis of Rotational Symmetric Struts Support
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摘要 考虑高温气体对燃气轮机旋转对称支承机座的作用,利用计算流体动力学软件CFX对支承板机座进行热流固耦合分析,并运用Workbench进行热固耦合计算。通过变换热气通道进口温度的计算方法,得到变工况条件下旋转对称支承板机座表面温度场分布,进而得到变工况下机座的热变形、热应力的变化关系。研究结论具有一定的理论意义和实用价值。 The role of high-temperature gas on rotational symmetric struts support was considered. Flux solid coupling analysis of the struts support was made by computational fluid dynamics software CFX. Then heat solid coupling calculation was done by Work- bench. By calculation method transforming inlet temperature of heat channel, the distribution of temperature field of rotational symmet- ric struts support under partial load was gotten. Then the relationship between thermal deformation and thermal stress of the struts sup- port under the partial load was gotten. The research results have certain theoretical si^aificance and practical value.
出处 《机床与液压》 北大核心 2013年第1期35-37,共3页 Machine Tool & Hydraulics
基金 国家重点基础研究发展计划(973计划)资助项目(2007CB707706) 国家自然科学基金面上资助项目(11072209)
关键词 支承板机座 热流固耦合 温度场 变工况 Struts support Heat flux solid coupling Temperature field Partial load
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参考文献5

  • 1黄文虎,夏松波,等著.旋转机械非线性动力学设计基础理论与方法[M].北京:科学出版社,2006:1-21.
  • 2FULLER E J, SMITH C E. Integrated CFD Modeling of Gas Turbine Combustors [ C ]// AIAA/SAE/ASME/ASEE 29th Joint Propulsion Confemece and Exhibit, 1993.
  • 3GHENI Mamtimin, LI Zhenshi, CHENG Wei, et al. Study on Numerical Simulation Method of Periodic Symmetric Struts Support Coupling with Heat Flow and Solid[ J]. Key Engineering Materials, 2011,462/463:985 - 989.
  • 4刘子亘,邹积国,于剑锋,冀洵.某型汽轮机速度级流场气动性能的数值研究[J].汽轮机技术,2010,52(4):241-243. 被引量:3
  • 5李维特,黄保海.汽轮机变工况热力计算[M].北京:中国电力出版社,2003.

二级参考文献10

  • 1冯永明,刘顺隆.舰船燃气轮机变几何动力涡轮三维粘性流场的数值分析[J].哈尔滨工程大学学报,2005,26(5):580-585. 被引量:12
  • 2刘子亘,刘建成,梅雪艳,沈卓野.船用汽轮机变工况超临界与超流问题的研究[J].汽轮机技术,2005,47(6):447-450. 被引量:6
  • 3刘顺隆,冯永明,刘敏,王林.船用燃气轮机动力涡轮可调导叶级的流场结构[J].热能动力工程,2005,20(2):120-124. 被引量:17
  • 4Ieutenart Ormond L. Curtis Turbine Design[ J]. Journal of the American Society for Naval Engineers. 2009,23 (2) : 31 -458.
  • 5Ensign Paul E. Description and Test of 27 - inch Curtis Turbine for 50 -Foot U. S. Navy Cutter[ J]. Journal of the American Society for Naval Engineers. 2009, ( 19 ) :927 - 932.
  • 6Steven W. Burd and Terrence W. Simon. Flow Measurements in a Nozzle Guide Vane Passage with a Low Aspect Ratio and Endwall Contouring [ J ]. Journal of Turbomachinery, 2000,122 ( 4 ) : 659 - 670.
  • 7Francesco Soranna,Yi - Chih Chow and Joseph Katz. The Effect of Inlet Guide Vanes Wake Impingement on the Flow Structure and Turbulence Around a Rotor Blade[J]. Journal of Turbomachinery, 2006,128 ( 1 ) :82 -96.
  • 8C. Kapteijn and J. Amecke, Aerodynamic Performance of a Transonic Turbine Guide Vane with Trailing Edge Coolant Ejection: Part I--Experimental Approach [ J]. Joumal of Turbomachinery, 1996,118(3) : 519 -529.
  • 9Chow, Y. C. , Uzol, O. , and Katz, J. On the Flow and Turbulence Within the Wake and Boundary Layer of a Rotor Blade Located Downstream of an IGV [ R ]. Proceedings of ASME Turbo Expo, 2003 - GT38599.
  • 10刘顺隆,冯永明.一个典型舰船动力涡轮三维粘性流动的数值分析[J].哈尔滨工程大学学报,2003,24(6):617-621. 被引量:5

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