Fluid mechanics

Premixed Gas Mixing Performance of Lobe-Forced Mixer at Different Configurations

  • WANG Yulan ,
  • MU Yong ,
  • LU Haitao ,
  • FAN Xiongjie ,
  • XU Gang
Expand
  • 1. Key Laboratory of Light-Duty Gas-Turbine, Institute of Engineering Thermophysics, Chinese Academy of Sciences, Beijing 100190, China
    2. University of Chinese Academy of Sciences, Beijing 100049, China

Online published: 2023-12-01

Supported by

The authors gratefully acknowledge the financial support received from the National Science and Technology Major Project (Project No. 2017-Ⅲ-0007 -0032). The work is also supported by National Defense Science and Technology Innovation Special Zone Project.

Copyright

Science Press, Institute of Engineering Thermophysics, CAS and Springer-Verlag GmbH Germany, part of Springer Nature 2022

Abstract

The mixing process of pre-evaporated afterburner fuel at different positions upstream of the mixers and airflow was numerically simulated in a straight channel, with semicircular mixer, rectangular mixer, triangular mixer and chevron mixer respectively. The effects of vortices generated by mixers on fuel distribution and mixing characteristics were studied. The results show that: (1) The scale, strength and breaking speed of the streamwise vortex and the development speed of normal vortex are different downstream of the four mixers, which accelerate the mixing process of fuel and airflow. (2) The fuel distribution at the outlet of mixers, downstream of straight section and downstream of the crest and trough is mainly affected by secondary flow, the streamwise vortex and the normal vortex respectively. (3) The fuel mixing uniformity downstream of the four mixers is increased by about 80% compared with no mixer. In the limited distance, the mixing performance of chevron mixer is the best, while the triangular mixer is the worst Rectangular mixer has the fastest mixing speed and superior comprehensive performance. In addition, the effect of the channel wall on the mixing process downstream of mixers cannot be ignored.

Cite this article

WANG Yulan , MU Yong , LU Haitao , FAN Xiongjie , XU Gang . Premixed Gas Mixing Performance of Lobe-Forced Mixer at Different Configurations[J]. Journal of Thermal Science, 2022 , 31(3) : 895 -906 . DOI: 10.1007/s11630-022-1507-y

References

[1] Lovett J.A., Brogan T., Philippona D.S., Development needs for advanced afterburner designs. 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 2004. DOI: 10.2514/6.2004-4192.
[2] Sekar B., Thornburg H.J., Briones A.M., Zelina J., Effect of trapped vortex combustion with radial vane cavity arrangements on predicted inter-turbine burner performance. International Energy Conversion Engineering Conference, 2013. DOI: 10.2514/6.2009-4603.
[3] Wadia A.R., James F.D., F110-GE-132: Enhanced power through low-risk derivative technology. Journal of Turbomachinery, 2001, 123(3): 544–551.
[4] Eriksson L.E., Andersson N., Development of a cooled radial flameholder for the F404/RM12 afterburner: Part III afterburner rumble prediction and suppression. ISABE, 2003.
[5] Ji H., Fan W., Yang M., Feasibility analysis of a new inner dumped afterburner concept. Aeroengines, 2006, 32(1): 35–37.
[6] Birmaher S., Zeller P.W., Wirfalt P., Neumeier Y., Zinn B.T., Fuel injection scheme for a compact afterburner without flameholders. Journal of Engineering for Gas Turbines and Power, 2008, 130(3): 27–38.
[7] Güthe F., Hellat J., Flohr P., The reheat concept: The proven pathway to ultra-low emissions and high efficiency and flexibility. Journal of Engineering for Gas Turbines and Power, 2009, 131(2): 25–31.
[8] Düsing K.M., Ciani A., Eroglu A., Effect of mixing quality on NOx emissions in reheat combustion of GT24 and GT26 engines. Proceeding of ASME Turbo Expo, Vancouver, 2011.
[9] Lu H., Liu F., Wang Y., et al., The effect of different reaction mechanisms on combustion simulation of a reverse-flow combustor. Journal of Thermal Science, 2020, 29(03): 283–302.
[10] Gutmark E.J., Schadow K.C., Yu K.H., Mixing enhancement in supersonic free shear flows. Annu Fluid Mech, 1995, 27(1): 375–417.
[11] Yang Y., Noiray N., Düsing K.M., Fuel injection device for a gas turbine. United States patent US 2016/0230668 A1. 2016, Aug 11.
[12] Yang Y., Düsing M., Lobe lance for a gas turbine combustor. United States patent US 2016/0146466 A1. 2016, May 26.
[13] Pennell D.A., Bothien M.R., Ciani A., An introduction to the Ansaldo GT36 constant pressure sequential combustor. ASME Turbo Expo: Turbomachinery Technical Conference and Exposition, 2017. DOI: 10.1115/GT2017-64790.
[14] Eckerle W.A., Sheibani H., Awad J., Experimental measurement of the vortex development downstream of a lobed forced mixer. Journal of Engineering for Gas Turbines and Power, 1992, 114(1): 63–71.
[15] Mao R., Yu S.C.M., Chua L.P., Kelvin - Helmholtz and streamwise vortices in the near wake of a single-lobe forced mixer. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2006, 220(4): 279–298.
[16] Mccormick D.C., Bennett J.C.J., Vortical and turbulent structure of a lobed mixer free shear layer. AIAA Journal, 1994, 32(9): 1852–1859.
[17] Manning T.A., Experimental studies of mixing flows with streamwise vorticity. Massachusetts Institute of Technology, Cambridge, United States, 1991.
[18] Mao R., Yu S.C.M., Zhou T., On the vorticity characteristics of lobe-forced mixer at different configurations. Experiments in Fluids, 2009, 46(6): 1049–1066.
[19] Shumpert P.K., An experimental model investigation of turbofan engine internal exhaust gas mixer configurations. AIAA 18th Aerospace Sciences Meeting, 1980. DOI: 10.2514/6.1980-228.
[20] Abolfadl M.A., Metwally M.A., EI-Messiry A.M., Ali M.A., Experimental investigation of lobed mixer performance. Journal of Propulsion and Power, 2001, 17(5): 1109–1116.
[21] Sheng Z., Wu Z., Ji J., Huang P., Chevron spoiler to improve the performance of lobed ejector/mixer. International Communications in Heat and Mass Transfer, 2016, 77: 174–182.
[22] Sheng Z., Jet mixing of lobed nozzles with spoilers located at lobe peaks. Applied Thermal Engineering, 2017, 119: 165–175.
[23] Sheng Z., Yao Y., Xu Y., Suggestions on investigations of lobed jet mixing. Aerospace Science and Technology, 2019, 86: 415–429.
[24] Koch L.D., Bridges J., Khavaran A., Mean flow and noise prediction for a separate flow jet with chevron mixers. AIAA Aerospace Sciences Meeting and Exhibit, 2004. DOI: 10.2514/6.2004-189.
[25] Zaman K., Streamwise vorticity generation and mixing enhancement in free jets by ‘delta-tabs’. AIAA Shear Flow Conference, 1993. DOI: 10.2514/6.1993-3253.
[26] Wang Y., Investigation on the mixing and combustion performances of chevron mixer for the afterburner. Nanjing University of Aeronautics and Astronautics, Nanjing, China, 2011.
[27] Di H., Investigation on the Structure and Performances of Chevron Mixer for the Afterburner. Nanjing University of Aeronautics and Astronautics, Nanjing, China, 2012.
[28] Lu B., Investigation on mixing and combustion performances of lobe forced mixer for the afterburner. Nanjing University of Aeronautics and Astronautics, Nanjing, China, 2017.
[29] Wang Y., Mu Y., LU H., Yang J., Xu G., Numerical study on fuel atomization characteristics in turbine stages. Journal of Propulsion Technology, 2019, 40(4): 825–834.
[30] Chai M., Investigation on the design and flow mechanisms of the de-swirling lobed mixer. University of Chinese Academy of Sciences, Beijing, China, 2018.
Outlines

/