Calculation method to separation efficiency of impeller type ventilation

被引:0
|
作者
Zhang X. [1 ]
Zhu W. [1 ]
Zhang C. [1 ]
Hu L. [1 ]
机构
[1] College of Aerospace and Civil Engineering, Harbin Engineering University, Harbin
来源
关键词
Equation of motion; Impeller type ventilator; Minimum separation diameter; Separation efficiency; Separation performance;
D O I
10.13224/j.cnki.jasp.2018.04.016
中图分类号
学科分类号
摘要
In order to investigate its separation performance and establish the method for calculating the separation efficiency compliant with the requirements of engineering design, stress analysis of oil droplet was conducted, the trajectory model of oil droplet was established, and the minimum oil drop diameter under different conditions was calculated combining with the oil droplet capture condition, finally realizing the theoretical calculation of impeller ventilator separation efficiency. Research showed that in different speeds, mass flow rates, and inlet temperatures, the separation efficiency and the minimum separation diameter were in agreement with the experimental values; the maximum errors of separation efficiency were 0.95%, 1.01% and 1.01%, respectively; the maximum errors of the minimum separation diameter were 1.33%, 2.29% and 6.20%, respectively. The calculation results were in good agreement with the experimental results. This method can provide a reference for designing the impeller type ventilator and optimizing its separation performance. © 2018, Editorial Department of Journal of Aerospace Power. All right reserved.
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页码:903 / 910
页数:7
相关论文
共 16 条
  • [1] Farrall M., Hibberd S., Simmons K., Modeling oil droplet/film interaction in an aero-engine bearing chamber, Sorrento, Italy: the 9th International Conference on Liquid Atomization and Spray Systems, (2003)
  • [2] Bai C., Gosman A.D., Development of methodology for spray impingement simulation, (1995)
  • [3] Willenborg K., Klingsporn M., Tebby S., Et al., Experimental analysis of air-oil separator performance, Journal of Engineering for Gas Turbines and Power, 130, 6, pp. 1495-1505, (2008)
  • [4] Lu H., Method for separation ability price of aero motor centrifugal ventilator and rotor optimal design, Machinery Design and Manufacture, 10, pp. 44-46, (2008)
  • [5] Elsayed K., Lacor C., Optimization of the cyclone separator geometry for minimum pressure drop using mathematical models and CFD simulations, Chemical Engineering Science, 65, 22, pp. 6048-6058, (2010)
  • [6] Gruselle F., Steimes J., Hendrick P., Study of a two-phase flow pump and separator system, Journal of Engineering for Gas Turbines and Power, 132, 6, pp. 657-666, (2010)
  • [7] Shi S., Liu Z., Hu J., Calculation on aero engine oil-air separator, Aeronautical Computer Technique, 24, 1, pp. 68-71, (2012)
  • [8] Han J., Chen C., Xu R., Simulation analysis on performance of a high speed centrifugal oil-air separator, Journal of Aerospace Power, 31, 3, pp. 685-691, (2016)
  • [9] Zhao J., Liu Z., Lu Y., Computation oil/gas separation performance of axial breather with honeycomb structure, Journal of Aerospace Power, 31, 7, pp. 1583-1590, (2016)
  • [10] Yu Y., Design and numerical simulation of dynamic pressure oil-gas separator and centrifugal ventilator, (2010)