A Variable-nozzle Ejector for a 120kW PEMFC Stack: Design and Performance

被引:0
|
作者
Lu Y. [1 ]
Wang X. [1 ,2 ]
Xu S. [1 ]
机构
[1] School of Automotive Studies, Tongji University, Shanghai
[2] China Automotive Engineering Research Institute Co.,Ltd, Chongqing
来源
关键词
ejector; entrainment ratio; proton exchange membrane fuel cell; variable-nozzle;
D O I
10.11908/j.issn.0253-374x.22059
中图分类号
学科分类号
摘要
The ejector acts as a critical component in the hydrogen recirculation system for proton exchange membrane fuel cells which realizes anode exhaust recirculation via a supersonic jet. Traditional fixed-geometry ejectors are commonly designed according to the stack’s rated condition and achieve poor performance in off-design conditions. In contrast, variable-nozzle ejectors can adjust the throat’s opening dynamically and enlarge the operating range. Based on Sokolov’s theory,a one-dimensional model for the ejector was built to study its working characteristics,and a design methodology for the variable-nozzle ejector was later proposed. The results show that the ejector’s performance is mainly affected by its operating pressure, the throat diameter, and the mixing chamber’s diameter. By shrinking the throat and raising primary pressure,the working nozzle can be kept critical,which has little effect on entraining performance under high stack load. However,under low stack load,the entrainment ratio can be significantly improved,and the operating range expands toward low stack load. © 2023 Science Press. All rights reserved.
引用
收藏
页码:1625 / 1632
页数:7
相关论文
共 13 条
  • [1] XUE H,, WANG L,, ZHANG H,, Et al., Design and investigation of multi-nozzle ejector for PEMFC hydrogen recirculation [J], International Journal of Hydrogen Energy, 45, 28, (2020)
  • [2] Design and characterization of an electronically controlled variable flow rate ejector for fuel cell applications[J], International Journal of Hydrogen Energy, 37, 5, (2012)
  • [3] KREWER U., Improved PEM fuel cell system operation with cascaded stack and ejector-based recirculation[J], Applied Energy, 195, (2017)
  • [4] HOSSEINZADEH E,, ROKNI M,, JABBARI M,, Et al., Numerical analysis of transport phenomena for designing of ejector in PEM forklift system [J], International Journal of Hydrogen Energy, 39, 12, (2014)
  • [5] HUANG B. J., CHANG J. M., WANG C. P., Et al., A 1-D analysis of ejector performance[J], 22, 5, (1999)
  • [6] CHEN W, CHONG D,, Et al., A 1D model to predict ejector performance at critical and sub-critical operational regimes[J], International Journal of Refrigeration, 36, 6, (2013)
  • [7] ZHU Y, LI Y., New theoretical model for convergent nozzle ejector in the proton exchange membrane fuel cell system[J], Journal of Power Sources, 191, 2, (2009)
  • [8] SOKOLOV E., Jet apparatuses[M], (1970)
  • [9] TANG Y, LI Y,, Et al., A double-choking theory as an explanation of the evolution laws of ejector performance with various operational and geometrical parameters [J], Energy Conversion and Management, 206, (2020)
  • [10] WANG X, ZHANG B., Control method of ejector's mass flow rate for 80 kW fuel cell stack[J], Journal of Tongji University(Natural Science), 46, S1, (2018)