Skip to main content
Log in

Visualization of flashback in a premixed burner with swirling flow

  • Published:
Science in China Series E: Technological Sciences Aims and scope Submit manuscript

Abstract

In this study, the measurement object is a flame propagating in a premixed burner with swirling flow in order to investigate unsteady flame behavior in a gas turbine premixer. During flashback, the flame propagating upstream was visualized with a high-speed camera. Moreover, we established the technique to measure the instantaneous flow fields of unburned fuel-air mixture in a swirling premixed burner using particle image velocimetry (PIV). As a result, the characteristics of flame behavior propagating upstream were examined. And it was found that a low velocity region existed in the vicinity of the flame tip. The relationship between low velocity region and flame behavior was discussed in detail.

This is a preview of subscription content, log in via an institution to check access.

Access this article

Price excludes VAT (USA)
Tax calculation will be finalised during checkout.

Instant access to the full article PDF.

Similar content being viewed by others

Abbreviations

D :

inner diameter of cylindrical glass (mm)

L :

length of cylindrical glass (mm)

Q air :

air flow rate (NL/min)

Q fuel :

fuel flow rate (NL/min)

S :

swirl number

S u :

burning velocity (m/s)

V f :

flame speed (m/s)

V y :

axial velocity component (m/s)

V ϑmax :

maximum tangential velocity component (m/s)

x :

radial direction in a burner

y :

axial direction in a burner

α :

exit angle of the swirler (degree)

λ :

air ratio

ρ b :

burned gas density

ρ u :

unburned gas density

References

  1. Fritz J, Korner M, Sattelmayer T. Flashback in a swirl burner with cylindrical premixed zone. In: Proceedings of ASME Turbo Expo 2001, June 4–7, 2001, New Orleans, Louisiana. GT-2001-0054

  2. Kroner M, Fritz J, Sattelmayer T. Flashback limits for combustion induced vortex breakdown in a swirl burner. In: Proceedings of ASME Trubo Expo 2002, June 3–6, 2002, Amsterdam, The Netherlands. GT-2002-30075

  3. Owaki T, Umemura A. Premixed swirl combustion modes emerging for a burner tube with converging entrance. Proc Combust Inst, 2007, 31: 1067–1074

    Article  Google Scholar 

  4. Shtork S I, Cala C E, Fernandes E C. Experimental characterization of rotating flow field in a model vortex burner. Exp Therm Fluid Sci, 2007, 31: 779–788

    Article  Google Scholar 

  5. Turrell M D, Stopford P J, Syed K J, et al. CFD simulation of the flow within and downstream of a high-swirl lean premixed gas turbine combustor. In: Proceedings of ASME Turbo Expo 2004, June 14–17, 2004, Vienna, Austria. GT-2004-53112

  6. Jochmann P, Sinigersky A, Hehle M, et al. Numerical simulation of a processing vortex breakdown. Int J Heat Fluid Flow, 2006, 27: 192–203

    Article  Google Scholar 

  7. Konle M, Kiesewetter F, Sattelmayer T. Simultaneous high repetition rate PIV-LIF-measurements of CIVB driven flashback. Exp Fluids, 2008, 44: 529–538

    Article  Google Scholar 

  8. Ishizuka S, Murakami T, Hamasaki T, et al. Flame speeds in combustible vortex rings. Combust Flame, 1998, 113: 542–553

    Article  Google Scholar 

  9. Ishizuka S. Flame propagation along a vortex axis. Prog Energ Combust, 2002, 28: 477–542

    Article  Google Scholar 

  10. Ishizuka S, Motodamari T, Shimokuri D. Rapidly mixed combustion in a tubular burner. Proc Combust Inst, 2007, 31: 1085–1092

    Article  Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to Masaharu Komiyama.

Rights and permissions

Reprints and permissions

About this article

Cite this article

Tanimura, S., Komiyama, M., Takeishi, K. et al. Visualization of flashback in a premixed burner with swirling flow. Sci. China Ser. E-Technol. Sci. 53, 40–45 (2010). https://doi.org/10.1007/s11431-010-0019-2

Download citation

  • Received:

  • Accepted:

  • Published:

  • Issue Date:

  • DOI: https://doi.org/10.1007/s11431-010-0019-2

Keywords

Navigation