期刊文献+

低温透平膨胀机内平衡凝结两相流动的数值模拟 被引量:5

Numerical Simulation of Equilibrium Condensation Two-Phase Flow in Cryogenic Turboexpander
下载PDF
导出
摘要 采用Peng-Robinson方程及零压多项式拟合了低温空气二元混合物的物性,利用商业软件ANSYS CFX对设计工况下的单相流动及进口升压降温后平衡凝结两相流动进行了数值模拟,得到了全低压空气分离流程中的低温两相透平膨胀机喷嘴和工作轮的温度场、压力场、流线及带液量云图,同时推导了该工况下膨胀机的等熵效率。结果表明,工作轮流道内吸力面壁面处的涡流会延迟凝结相变发生,叶片后缘处的尾迹使得吸力面壁面处的带液量有所减小。最后,通过实验验证了模拟结果,表明利用平衡凝结相变模型能够模拟小带液量透平膨胀机流道内的两相流动。该结果可为低温两相膨胀机研究提供参考。 The binary mixture properties of cryogenic air were fitted by the PR equations and the zero pressure polynomial.The single-phase flow under the design conditions and the equilibrium condensation of two-phase flow at higher pressure and lower temperature were numerically simulated by ANSYS CFX.For a cryogenic turboexpander in air separation process,the temperature field,pressure field,streamlines and liquid mass fraction in the nozzle and impeller were obtained.The isentropic efficiency of the turboexpander was calculated.The results show that the eddy occurring on the suction side of the impeller would delay the phase-change condensation,and the wake at the trailing edge of the blade would lead to the decrease in the local liquid mass fraction.The simulation results agree well with the experimental data,confirming that the model of the equilibrium condensation can be applied to the simulation of the two-phase flow turboexpander having a small liquid mass fraction.
出处 《西安交通大学学报》 EI CAS CSCD 北大核心 2013年第7期36-39,共4页 Journal of Xi'an Jiaotong University
基金 国家自然科学基金资助项目(50976082) 高等学校博士学科点专项科研基金资助项目(20090201110006) 中央高校基本科研业务费专项资金资助项目
关键词 透平膨胀机 平衡凝结 两相流动 等熵效率 带液量 turboexpander equilibrium condensation two-phase flow isentropic efficiency liquid mass fraction
  • 相关文献

参考文献8

  • 1江楚标.透平膨胀机及发展动态[J].深冷技术,2001(5):1-9. 被引量:26
  • 2Kevin A.Kaupert.两相流空气分离透平膨胀机的设计[J].深冷技术,2010(1):47-51. 被引量:3
  • 3李瑜,李亮,钟刚云,等.低压汽轮机中平衡与非平衡凝结流动的对比研究[C]//中国工程热物理学会热机气动热力学2009年学术会议论文集.北京:中国工程热物理学会,2009:1-6.
  • 4PENG Dingyu, ROBINSON D B. A new two-constant equation of state [J]. Industrial and Engineering Chemistry, Fundamentals, 1976, 15(1): 59-64.
  • 5ANSYS Inc.. ANSYS CFX: solver theory guide [M]. New York, USA: ANSYS Inc. , 2010:145-167.
  • 6DENTON J D, DAWES W N. Computational fluid dy- namics for turbomachinery design[J]. Journal of Me- chanical Engineering Science, 1998, 213: 107-123.
  • 7GHOSH S Kr. A numerical model for the design of a mixed flow cryogenic turbine[J]. International Jour nal of Engineering, Science and Technology, 2010, 2 (1): 175-191.
  • 8WHITFIELD A, BAINES N C. Design of radial tur- bomaehines [M]. New York, USA: Longman Scien- tific & Technical, 1990: 68-82.

二级参考文献8

  • 1ARDASHEV V, PLACHENDOVSKI D. Examination of Two-Phase Regimes of Cryogenic Expansion Turbine Engines[J]. Khimicheskoe i Neftyanoe Mashinostoenie (in Russian), 1984, 4: 21-24.
  • 2DAVYDOV A, NAGAITSEVA E. Operation of a Centripetal Turboexpander in the Wet Vapor Region [ J ]. Khimicheskoe i Neftyanoe Mashinostoenie (in Russian),1975, 1: 5-9.
  • 3SWEARINGEN J.Turboexpanders and Processes that use Them [J ]. Chemical Engineering Progress, 1972, 68 (7):95-102.
  • 4LEMMON E W, JACOBSEN R T, PENONCELLO S G , et al. Thermodynamic Properties of Air and Mixtures of Nitrogen, Argon, and Oxygen from 60 to 2000K at pressures to 2000MPa[J]. Journal of Physical and Chemistry Reference Data 29, 2000 (May): 331-385.
  • 5KUNZ O, KLIMECK R, WAGNER W, et al. The GERG-2004 Wide-Range Reference Equation of State for Natural Gases and Other Mixtures [J]. GERG Technical Monograph, 2004. Fortschritt-Berichte VDI Reihe 6Nr.557 Dusseldorf, 2007.
  • 6ASHRAE. ASHRAE Handbook [ M ]. Published by American Society of Heating, Refrigerating, and Air- Conditioning Engineers, 1989.
  • 7KERRY F. Industrial Gas Handbook [M]. CRC Press, 2006.
  • 8江楚标,陈明敏.内压缩流程与外压缩流程空分装置能耗的比较[J].深冷技术,2000(3):1-4. 被引量:9

共引文献27

同被引文献52

引证文献5

二级引证文献17

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