285
Views
3
CrossRef citations to date
0
Altmetric
Original Articles

Phase Resolved Analysis of Flame Structure in Lean Premixed Swirl Flames of a Fuel Staged Gas Turbine Model Combustor

, , , &
Pages 421-434 | Received 15 May 2013, Accepted 19 Nov 2013, Published online: 23 Apr 2014

REFERENCES

  • Adachi, S., Iwamoto, A., Hayashi, S., Yamada, H., and Kaneko, S. 2007. Emissions in combustion of lean methane-air and biomass-air mixtures supported by primary hot burned gas in a multi-stage gas turbine combustor. Proc. Combust. Inst., 31, 3131–3138.
  • Barbosa, S., Scouflaire, P., and Ducruix, S. 2009. Time resolved flowfield, flame structure and acoustic characterisation of a staged multi-injection burner. Proc. Combust. Inst., 32, 2965–2972.
  • Boxx, I., Arndt, C., Carter, C., and Meier, W. 2012. High-speed laser diagnostics for the study of flame dynamics in a lean premixed gas turbine model combustor. Exp. Fluids, 52, 555–567.
  • Boxx, I., Stöhr, M., Carter, C., and Meier, W. 2010. Temporally resolved planar measurements of transient phenomena in a partially pre-mixed swirl flame in a gas turbine model combustor. Combust. Flame, 157, 1510–1525.
  • Chockalingam, P., Galeazzo, F.C.C., Kasabov, P., Habisreuther, P., Zarzalis, N., Beck, C., Krebs, W., and Wegner, B. 2011. Analysis of NOX formation in an axially staged combustion system at elevated pressure conditions. In Proceedings of the ASME Turbo Expo, Vancouver, British Columbia, Canada, May 8–11. ASME, New York, GT2011-45239.
  • Duan, X.R., Meier, W., Weigand, P., and Lehmann, B. 2005. Phase-resolved laser Raman scattering and laser Doppler velocimetry applied to periodic instabilities in a gas turbine model combustor. Appl. Phys. B, 80, 389–396.
  • Fritsche, D., Füri, M., and Boulouchos, K. 2007. An experimental investigation of thermoacoustic instabilities in a premixed swirl-stabilized flame. Combust. Flame, 151, 29–36.
  • Geigle, K.P., Meier, W., Aigner, M., Willert, C., Jarius, M., Schmitt, P., and Schuermans, B. 2006. Phase resolved laser diagnostic measurements of a downscaled, fuel staged gas turbine combustor at elevated pressure and comparison with LES predictions. In Proceedings of the ASME Turbo Expo, Barcelona, Spain, May 8–11. ASME, New York, GT2006-90875.
  • Giezendanner, R., Keck, O., Weigand, P., Meier, W., Meier, U., Stricker, W., and Aigner, M. 2003. Periodic combustion instabilities in a swirl burner studied by phase-locked planar laser-induced fluorescence. Combust. Sci. Technol., 175, 721–741.
  • Gounder, J.D., Boxx, I., Kutne, P., Biagioli, F., and Luebcke, H. 2013. An investigation of the effects of fuel staging on flame structure in a gas turbine model combustor. In Proceedings of the ASME Turbo Expo, San Antonio, TX, June 3–7. ASME, New York, GT2013-95520.
  • Grinstein, F.F., and Fureby, C. 2005. LES studies of the flow in a swirl gas combustor. Proc. Combust. Inst., 30, 1791–1798.
  • Haber, L.C., and Vandsburger, U. 2003. A global reaction model for OH* chemiluminescence applied to a laminar flat-flame burner. Combust. Sci. Technol., 175, 1859–1891.
  • Hardalupas, Y., and Orain, M. 2004. Local measurements of the time-dependent heat release rate and equivalence ratio using chemiluminescent emission from a flame. Combust. Flame, 139, 188–207.
  • Hayashi, S., Yamada, H., and Makida, M. 2005. Extending low-NOx operating range of a lean premixed–prevaporized gas turbine combustor by reaction of secondary mixtures injected into primary stage burned gas. Proc. Combust. Inst., 30, 2903–2911.
  • Johnson, M.R., Littlejohn, D., Nazeer, W.A., Smith, K.O., and Cheng, R.K. 2005. A comparison of the flowfields and emissions of high-swirl injectors and low-swirl injectors for lean premixed gas turbines. Proc. Combust. Inst., 30, 2867–2874.
  • Jones, W.P., Marquis, A.J., and Prasad, V.N. 2012. LES of a turbulent premixed swirl burner using the Eulerian stochastic field method. Combust. Flame, 159, 3079–3095.
  • Kolb, T., Jansohn, P., and Leuckel, W. 1988. Reduction of NO, emission in turbulent combustion by fuel-staging/effects of mixing and stoichiometry in the reduction zone. Proc. Combust. Inst., 22, 1193–1203.
  • Lefebvre, A.H., and Ballal, D.R. 2010. Gas Turbine Combustion: Alternative Fuels and Emissions, 3rd ed., CRC Press, Boca Raton, FL.
  • Littlejohn, D., and Cheng, R.K. 2007. Fuel effects on a low-swirl injector for lean premixed gas turbines. Proc. Combust. Inst., 31, 3155–3162.
  • Martin, C.E., Benoit, L., Sommerer, T., Nicoud, F., and Poinsot, T. 2006. Large-eddy simulation and acoustic analysis of a swirled staged turbulent combustor. AIAA J., 44, 741–749.
  • Meier, W., Boxx, I., Stöhr, M., and Carter, C. D. 2010. Laser-based investigations in gas turbine model combustors. Exp. Fluids, 49, 865–882.
  • Meier, W., Weigand, P., Duan, X.R., and Giezendanner-Thoben, R. 2007. Detailed characterization of the dynamics of thermoacoustic pulsations in a lean premixed swirl flame. Combust. Flame, 150, 2–26.
  • Moeck, J.P., Bourgouin, J.-F., Durox, D., Schuller, T., and Candel, S. 2012. Nonlinear interaction between a precessing vortex core and acoustic oscillations in a turbulent swirling flame. Combust. Flame, 159, 2650–2668.
  • Nogenmyr, K.J., Fureby, C., Bai, X.S., Petersson, P., Collin, R., and Linne, M. 2009. Large eddy simulation and laser diagnostic studies on a low swirl stratified premixed flame. Combust. Flame, 156, 25–36.
  • Sadanandan, R., Stöhr, M., and Meier, W. 2008. Simultaneous OH-PLIF and PIV measurements in a gas turbine model combustor. Appl. Phys. B, 90, 609–618.
  • Sadanandan, R., Stöhr, M., and Meier, W. 2009. Flowfield-flame structure interactions in an oscillating swirl flame. Combust. Explos. Shock Waves, 45, 518–529.
  • Stöhr, M., Boxx, I., Carter, C., and Meier, W. 2011a. Dynamics of lean blowout of a swirl-stabilized flame in a gas turbine model combustor. Proc. Combust. Inst., 33, 2953–2960.
  • Stöhr, M., Boxx, I., Carter, C.D., and Meier, W. 2012. Experimental study of vortex–flame interaction in a gas turbine model combustor. Combust. Flame, 159, 2636–2649.
  • Stöhr, M., Sadanandan, R., and Meier, W. 2009. Experimental study of unsteady flame structures of an oscillating swirl flame in a gas turbine model combustor. Proc. Combust. Inst., 32, 2925–2932.
  • Stöhr, M., Sadanandan, R., and Meier, W. 2011b. Phase-resolved characterization of vortex–flame interaction in a turbulent swirl flame. Exp. Fluids, 51, 1153–1167.
  • Steinberg, A.M., Boxx, I., Stöhr, M., Carter, C.D., and Meier, W. 2010. Flow–flame interactions causing acoustically coupled heat release fluctuations in a thermo-acoustically unstable gas turbine model combustor. Combust. Flame, 157, 2250–2266.
  • Therkelsen, P.L., Portillo, J.E., Littlejohn, D., Martin, S.M., and Cheng, R.K. 2013. Self-induced unstable behaviors of CH4 and H2/CH4 flames in a model combustor with a low-swirl injector. Combust. Flame, 160, 307–321.
  • Zajadatz, M., Lachner, R., Bernero, S., Motz, C., and Flohr, P. 2007. Development and design of ALSTOM′s staged fuel gas injection EV burner for NOx reduction. In Proceedings of the ASME Turbo Expo, Montreal, Canada, May 14–17. ASME, New York, GT2007-27730.

Reprints and Corporate Permissions

Please note: Selecting permissions does not provide access to the full text of the article, please see our help page How do I view content?

To request a reprint or corporate permissions for this article, please click on the relevant link below:

Academic Permissions

Please note: Selecting permissions does not provide access to the full text of the article, please see our help page How do I view content?

Obtain permissions instantly via Rightslink by clicking on the button below:

If you are unable to obtain permissions via Rightslink, please complete and submit this Permissions form. For more information, please visit our Permissions help page.