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双辐板涡轮盘盘腔流动换热分析 被引量:1

Flow and heat transfer for rotating cavity of twin-web rotor disk
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摘要 基于UG软件建立了双辐板涡轮盘的三维模型,基于CFX软件对双辐板涡轮盘盘腔内的流动换热现象进行了数值模拟,获得了典型工况下旋转盘腔内的流场和温度场分布,初步总结了该盘腔结构内的流动换热规律。结果表明:该盘腔结构内的流动形式为典型的源-汇流动,冷气的总压和温度沿径向均逐渐增大,总压增和温度差随转速的增加而增大、随冷气流量的增加而减小,对流换热系数在不同流场区域表现出不同的分布特征。为双辐板涡轮盘的进一步结构优化设计提供了参考。 The three dimensional model was established with UG, the flow and heat transfer were simulatedwith CFX, the flow field and temperature field in typical working status of the rotating cavity for twin-webrotor disk were calculated and the conclusions of flow and heat transfer of rotating cavity were summarized.The results show that the flow structure in the rotating cavity is source-sink flow, total pressure and temper-ature of the cooling gas gradually increase along the radial direction; their increment increase with rotatingspeed and decrease with mass flow rate and heat transfer coefficient has different distributional features indifferent flow regions, which supports the further optimized design of structure for twin-web rotor disk.
出处 《燃气涡轮试验与研究》 北大核心 2017年第3期48-52,共5页 Gas Turbine Experiment and Research
关键词 航空发动机 双辐板涡轮盘 旋转盘腔 冷却 流动 换热 数值模拟 aero-engine twin-web rotor disk rotating cavity cooling flow heat transfer numerical simulation
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  • 1金捷,钟燕.先进航空发动机设计与制造技术综述[J].航空制造技术,2012,55(5):34-37. 被引量:12
  • 2周光华.燃气轮机涡轮盘寿命分析和预测[J].燃气轮机技术,1989(2):1-8. 被引量:1
  • 3万玉慧,徐永东,潘文革,张立同,成来飞.反应熔体浸渗法制备C/SiC复合材料的结构与力学性能[J].玻璃钢/复合材料,2005(5):20-24. 被引量:11
  • 4Mattinglg J D(美) 侯志兴(译).航空发动机设计[M].科学出版社,1992..
  • 5Pilbrow R, Karabay H, Wilson M, et al. Heat transfer in a "cover-plate" pre-swirl rotating disk system[ J]. Journal of Turbomachinery, 1999,121:249 - 256
  • 6Karabay H, Chen J X, Pilbrow R, et al. Flow in a "cover- plate" preswirl rotator-stator system [ J ]. Journal of Turbomachinery, 1999,121:160 - 166
  • 7罗翔.复杂旋转盘腔内冷气的流动和换热特性研究[D].北京:北京航空航天大学能源与动力工程学院,2003
  • 8Menter F R. Two-equation eddy-viscosity turbulence models for engineering applications[J]. AIAA-Journal, 1994,32(8) :1598 - 1605
  • 9航空涡喷、涡扇发动机结构设计准则(研究报告)(第二册):轮盘[R].中国航空工业总公司发动机系统工程局,1997.
  • 10U.S. Department of Defence. Integrated high performance turbine engine technology (IHPTET) [ R]. Gas Turbine Forecast, Archived, 2006.

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