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小流量下的转静系盘腔传热特征分析 被引量:4

Heat Transfer Characteristic of Rotor-Stator System With Small Radial Outflow
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摘要 在一些情况下,燃机透平中用于供给轮缘密封的气体流量要小于自由盘的夹带流量。本文采用气热耦合数值计算的方法,并结合轮盘一维导热模型,分析了小流量下(λ_t<0.22)转静腔室传热特点及其中关键的影响因素。研究结果表明,对于小流量下的转静系盘腔系统,可以根据盘面传热系数随冷气量的变化定义一个临界流量λ_(t,c),当冷气流量大于λ_(t,c)时,盘面传热系数随冷气量增加缓慢增大,近似等于自由盘状态;当冷气量小于λ_(t,c)时,盘面传热系数随冷气量减小而迅速减小。文中给出了一种估算动盘面传热系数随冷气量变化的方法。文章同时分析了转速对于轮盘传热(λ_(t,c)<λ_t<λ_(t,fd))的影响,当转速对应的Ecb等于Ecb,c时,轮盘的体平均温度最低。 In some cases,the mass flow rate needed to prevent ingress through rim seals in turbine is smaller than that entrained by free disk.In order to obtain the heat transfer features of the rotor-stator system at such a small mass flow rate,a combined computational and theoretical study is carried out.It is found that the average Nusselt number(Nu_(av))on the rotor drops quickly down to zero with decreasing turbulent flow parameter(λ_t)whenλ_t is smaller thanλ_(t,c)(λ_(t,c)λ_(t,fd)),while Nu_(av)almost keeps constant whenλ_t is larger thanλ_(t,c).A correlation between Nu_(av)andλ_t is therefore built up.It has been identified that the average temperature of the disk(whenλ_(t,c)λ_tλ_(t,fd)) reaches a minimum at a certain rotating speed which corresponds to Ec_(b,c)under different conditions.
出处 《工程热物理学报》 EI CAS CSCD 北大核心 2012年第7期1122-1126,共5页 Journal of Engineering Thermophysics
基金 国家"973"项目(No.2007CB210100)
关键词 转静系盘腔 气热耦合 埃克特数 一维模型 rotor-stator system conjugate heat transfer Eckert number one dimensional model
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参考文献6

  • 1Daily J W, Nece R E. Chamber Dimension Effects on Induced Flow and Frictional Resistance of Enclosed Ro- tating Disks [J]. Journal of Basic Engineering, 1960, 82: 217-232.
  • 2Poncet S, Chauve M P, Legal P. Turbulent Rotating Disk Flow With Inward Throughfiow [J]. Journal of Fluid Me- chanics, 2005, 522:253 -262.
  • 3Poncet S, Chauve M P, Schiestel R. Batchelor Versus Stewartson Flow Structures in a Rotor-Stator Cavity With Throughflow [J]. Physics of Fluids, 2005, 17:075110.
  • 4Haynes C M, Owen J M. Heat Transfer From a Shrouded Disk System With a Radial Outflow of Coolant [J]. Jour- nal of Engineering for Power, 1975, 97:28 -36.
  • 5Owen J M, Rogers R H. Flow and Heat Transfer in Ro- tating Disc Systems, Vol. 1: Rotor-Stator Systems [M]. Taunton: Research Studies Press, New York: Wiley, 1989.
  • 6Chen J X, Gan X, Owen J M. Heat Transfer in an Air- Cooled Rotor-Stator System [J]. Journal of Turbomachin- ery, 1996, 118:444-451.

同被引文献43

  • 1张崇,罗翔,徐国强,陶智.中心进气复杂旋转盘压力特性的实验研究[J].北京航空航天大学学报,2005,31(4):385-388. 被引量:2
  • 2杨成凤,张靖周.高旋转雷诺数下预旋进气转-静盘腔流动换热特性[J].航空动力学报,2006,21(2):326-330. 被引量:6
  • 3徐国强,张笙,罗翔,丁水汀,陶智,雷斌.高位垂直进气径向出流旋转盘腔换热的实验研究[J].航空动力学报,2006,21(5):820-823. 被引量:5
  • 4罗翔,徐国强,蔡毅,陶智,丁水汀.中心进气转静盘腔的流量分配特性试验[J].航空动力学报,2007,22(6):873-876. 被引量:2
  • 5陶智,徐国强,丁水汀,等.航空发动机传热学[M].北京:北京航空航天大学出版社,2005.
  • 6Poncet S,Schiestel R,Chauve M. Centrifugal flow in a ro- tor-stator cavity[J]. Journal of Fluids Engineering, 2005, 127(4) : 787-794.
  • 7Owen J M. An approximate solution for the flow between a rotating and a stationary disk[J]. Journal of Turbomach- inery,1989,111(7) :323-332.
  • 8Soghe R D, Facchini B, Innocenti L. Analysis of gas turbine rotating cavities by a one-dimensional model: definition of new disk friction coefficient correlations set[J]. Journal of Turbomachinery,2011,133(4) :021020.1-021020.8.
  • 9Haaser F,Jack J, McGreehan W. Analysis and validation of turbine disc cooling[R]. ASME Paper 87-GT-164,1987.
  • 10Antonio A,Riccardo D, Bruno F. Turbine stator well CFD studies:effects of coolant supply geometry on cavity seal- ing performance[J]. Journal of Turbomachinery, 2011,133 (4) :021008.1-021008.11.

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