Skip to main content
Erschienen in: Experiments in Fluids 3/2012

01.03.2012 | Research Article

Residence time measurement of an isothermal combustor flow field

verfasst von: Liangta Cheng, Adrian Spencer

Erschienen in: Experiments in Fluids | Ausgabe 3/2012

Einloggen

Aktivieren Sie unsere intelligente Suche, um passende Fachinhalte oder Patente zu finden.

search-config
loading …

Abstract

Residence times of combustors have commonly been used to help understand NOx emissions and flame blowout. Both the time mean velocity and turbulence fields are important to the residence time, but determining the residence time via analysis of a measured velocity field is difficult due to the inherent unsteadiness and the three-dimensional nature of a high-Re swirling flow. A more direct approach to measure residence time is reported here that examines the dynamic response of fuel concentration to a sudden cutoff in the fuel injection. Residence time measurement was mainly taken using a time-resolved planar laser-induced fluorescence (PLIF) technique, but a second camera for particle image velocimetry (PIV) was added to check that the step change does not alter the velocity field and the spectral content of the coherent structures. Characteristic timescales evaluated from the measurements are referred to as convection and half-life times: The former describes the time delay from a fuel injector exit reference point to a downstream point of interest, and the latter describes the rate of decay once the effect of the reduced scalar concentration at the injection source has been transported to the point of interest. Residence time is often defined as the time taken for a conserved scalar to reduce to half its initial value after injection is stopped: this equivalent to the sum of the convection time and the half-life values. The technique was applied to a high-swirl fuel injector typical of that found in combustor applications. Two test cases have been studied: with central jet (with-jet) and without central jet (no-jet). It was found that the relatively unstable central recirculation zone of the no-jet case resulted in increased transport of fuel into the central region that is dominated by a precessing vortex core, where long half-life times are also found. Based on this, it was inferred that the no-jet case may be more prone to NOx production. The technique is described here for a single-phase isothermal flow field, but with consideration, it could be extended to studying reacting flows to provide more insight into important mixing phenomena and relevant timescales.

Sie haben noch keine Lizenz? Dann Informieren Sie sich jetzt über unsere Produkte:

Springer Professional "Wirtschaft+Technik"

Online-Abonnement

Mit Springer Professional "Wirtschaft+Technik" erhalten Sie Zugriff auf:

  • über 102.000 Bücher
  • über 537 Zeitschriften

aus folgenden Fachgebieten:

  • Automobil + Motoren
  • Bauwesen + Immobilien
  • Business IT + Informatik
  • Elektrotechnik + Elektronik
  • Energie + Nachhaltigkeit
  • Finance + Banking
  • Management + Führung
  • Marketing + Vertrieb
  • Maschinenbau + Werkstoffe
  • Versicherung + Risiko

Jetzt Wissensvorsprung sichern!

Springer Professional "Technik"

Online-Abonnement

Mit Springer Professional "Technik" erhalten Sie Zugriff auf:

  • über 67.000 Bücher
  • über 390 Zeitschriften

aus folgenden Fachgebieten:

  • Automobil + Motoren
  • Bauwesen + Immobilien
  • Business IT + Informatik
  • Elektrotechnik + Elektronik
  • Energie + Nachhaltigkeit
  • Maschinenbau + Werkstoffe




 

Jetzt Wissensvorsprung sichern!

Anhänge
Nur mit Berechtigung zugänglich
Literatur
Zurück zum Zitat Adrian RJ (1991) Particle-imaging techniques for experimental fluid mechanics. Ann Rev Fluid Mech 23:261–304CrossRef Adrian RJ (1991) Particle-imaging techniques for experimental fluid mechanics. Ann Rev Fluid Mech 23:261–304CrossRef
Zurück zum Zitat Arai M, Nomura T, Hiroyasu H (1998) Residence time measurement in a swirl type combustor with helium tracer. Jap Soc Mech Eng 86(1302A):2619–2625 Arai M, Nomura T, Hiroyasu H (1998) Residence time measurement in a swirl type combustor with helium tracer. Jap Soc Mech Eng 86(1302A):2619–2625
Zurück zum Zitat Cheng L, Dianat M, Spencer A, McGuirk JJ (2010) SPIV/PLIF validation of LES predictions of scalar mixing in high-swirl fuel injector flows. In: ETMM8: 8th Int. ERCOFTAC Symp. Marseille, France. (Invited to Jnl Flow Turb. And Comb.) Cheng L, Dianat M, Spencer A, McGuirk JJ (2010) SPIV/PLIF validation of LES predictions of scalar mixing in high-swirl fuel injector flows. In: ETMM8: 8th Int. ERCOFTAC Symp. Marseille, France. (Invited to Jnl Flow Turb. And Comb.)
Zurück zum Zitat Chigier NA, Beer JM (1972) Combustion aerodynamics. Applied Science, England Chigier NA, Beer JM (1972) Combustion aerodynamics. Applied Science, England
Zurück zum Zitat Di Nardo A, Calchetti G, Mongiello C, Giammartini S, Rufoloni M (2009) CFD Modelling of an experimental scaled model of a trapped vortex combustor. In: Proceedings of the European combustion meeting Di Nardo A, Calchetti G, Mongiello C, Giammartini S, Rufoloni M (2009) CFD Modelling of an experimental scaled model of a trapped vortex combustor. In: Proceedings of the European combustion meeting
Zurück zum Zitat Driscoll J, Chen RH, Yoon Y (1992) Nitric oxide levels of turbulent jet diffusion flames: effects of residence time and Damkohler number. Comb Flame 88:37–49CrossRef Driscoll J, Chen RH, Yoon Y (1992) Nitric oxide levels of turbulent jet diffusion flames: effects of residence time and Damkohler number. Comb Flame 88:37–49CrossRef
Zurück zum Zitat Dunham D, Spencer A, McGuirk JJ, Dianat M (2009) Comparison of unsteady reynolds averaged navier–stokes and large eddy simulation computational fluid dynamics methodologies for air swirl fuel injectors. J Eng Gas Turbines Power 131:011502. doi:10.1115/1.2969096 Dunham D, Spencer A, McGuirk JJ, Dianat M (2009) Comparison of unsteady reynolds averaged navier–stokes and large eddy simulation computational fluid dynamics methodologies for air swirl fuel injectors. J Eng Gas Turbines Power 131:011502. doi:10.​1115/​1.​2969096
Zurück zum Zitat Giordano D, Giammartini S, Manfredi F, Guj G (2001) Non dimensional numbers dependency on a Dry Low NOx Annular Burner Analysed with PIV technique. In: 9th National Conference AIVELA, Ancona, 2001 Giordano D, Giammartini S, Manfredi F, Guj G (2001) Non dimensional numbers dependency on a Dry Low NOx Annular Burner Analysed with PIV technique. In: 9th National Conference AIVELA, Ancona, 2001
Zurück zum Zitat Heywood JB, Fay JA, Lindern LH (1970) Jet aircraft air pollutant production and dispersion. AIAA 70-115 Heywood JB, Fay JA, Lindern LH (1970) Jet aircraft air pollutant production and dispersion. AIAA 70-115
Zurück zum Zitat Huang Y, Yang V (2005) Effect of swirl on combustion dynamics in a lean-premixed swirl-stabilized combustor. Proc Comb Inst 30:1775–1782 Huang Y, Yang V (2005) Effect of swirl on combustion dynamics in a lean-premixed swirl-stabilized combustor. Proc Comb Inst 30:1775–1782
Zurück zum Zitat Janus B, Dreizler A, Janicka J (2007) Experiments on swirl stabilized non-premixed natural gas flames in a model gasturbine combustor. Proc Comb Inst 31:3091–3098CrossRef Janus B, Dreizler A, Janicka J (2007) Experiments on swirl stabilized non-premixed natural gas flames in a model gasturbine combustor. Proc Comb Inst 31:3091–3098CrossRef
Zurück zum Zitat Lieuwen T (2006) The gas turbine handbook. Department of Energy, USA Lieuwen T (2006) The gas turbine handbook. Department of Energy, USA
Zurück zum Zitat Meier W, Weigand P, Duan XR, Giezendanner-Thoben R (2007) Detailed characterization of the dynamics of thermoacoustic pulsations in a lean premixed swirl flame. Comb Flame 150 Meier W, Weigand P, Duan XR, Giezendanner-Thoben R (2007) Detailed characterization of the dynamics of thermoacoustic pulsations in a lean premixed swirl flame. Comb Flame 150
Zurück zum Zitat Midgley KK (2005) An isothermal experimental study of the unsteady fluid mechanics of gas turbine fuel injector flowfields. Ph.D. thesis, Loughborough University, UK Midgley KK (2005) An isothermal experimental study of the unsteady fluid mechanics of gas turbine fuel injector flowfields. Ph.D. thesis, Loughborough University, UK
Zurück zum Zitat Midgley K, Spencer A (2005) Unsteady flow structures in radial swirler fed fuel injectors. ASME J Eng Gas Turbine Power 127:755–764CrossRef Midgley K, Spencer A (2005) Unsteady flow structures in radial swirler fed fuel injectors. ASME J Eng Gas Turbine Power 127:755–764CrossRef
Zurück zum Zitat Noble D, Zhang Q, Shareef A, Tootle J, Meyers A, Lieuwen T (2006) Syngas mixture composition effects upon flashback and blowout. ASME 2006-90470 Noble D, Zhang Q, Shareef A, Tootle J, Meyers A, Lieuwen T (2006) Syngas mixture composition effects upon flashback and blowout. ASME 2006-90470
Zurück zum Zitat Ozdemir IB, Peters N (2001) Characteristics of the reaction zone in a combustor operating at mild combustion. Exp Fluids 30:683–695CrossRef Ozdemir IB, Peters N (2001) Characteristics of the reaction zone in a combustor operating at mild combustion. Exp Fluids 30:683–695CrossRef
Zurück zum Zitat Pantano C, Sarkar S, Williams FA (2003) Mixing of a conserved scalar in a turbulent reacting shear layer. J Fluid Mech 481:291–328MATHCrossRef Pantano C, Sarkar S, Williams FA (2003) Mixing of a conserved scalar in a turbulent reacting shear layer. J Fluid Mech 481:291–328MATHCrossRef
Zurück zum Zitat Read R, Hochgreb S (2010) Isothermal flow measurements in a gas turbine combustor using a fast flame ionization detector. Meas Sci Technol 21:1–10CrossRef Read R, Hochgreb S (2010) Isothermal flow measurements in a gas turbine combustor using a fast flame ionization detector. Meas Sci Technol 21:1–10CrossRef
Zurück zum Zitat Roffe GK, Venkataramani KS (1978) Emissions measurements for lean premixed propane/air systems at pressures up to 30 atmospheres. NASA CR-159421 Roffe GK, Venkataramani KS (1978) Emissions measurements for lean premixed propane/air systems at pressures up to 30 atmospheres. NASA CR-159421
Zurück zum Zitat Spencer A (1998) Gas turbine combustor port flows. Ph.D. thesis, Loughborough University, UK Spencer A (1998) Gas turbine combustor port flows. Ph.D. thesis, Loughborough University, UK
Zurück zum Zitat Spencer A, Cheng L (2010) Combustor residence time measurement using planar laser induced fluorescence. In: Proc ASME Turbo Expo GT2010-22573 Spencer A, Cheng L (2010) Combustor residence time measurement using planar laser induced fluorescence. In: Proc ASME Turbo Expo GT2010-22573
Zurück zum Zitat Spencer A, McGuirk J, Midgley K (2008) Vortex breakdown in swirling fuel injector flows. ASME J Eng Gas Turbines Power 130:021503.1–021503.8CrossRef Spencer A, McGuirk J, Midgley K (2008) Vortex breakdown in swirling fuel injector flows. ASME J Eng Gas Turbines Power 130:021503.1–021503.8CrossRef
Zurück zum Zitat van der Lans RP, Glarborg P, Dam-Johansen K, Larsen PS (1997) Residence time distributions in a cold, confined swirl flow: implications for chemical engineering combustion modeling. Chem Eng Sci 52:2743–2756CrossRef van der Lans RP, Glarborg P, Dam-Johansen K, Larsen PS (1997) Residence time distributions in a cold, confined swirl flow: implications for chemical engineering combustion modeling. Chem Eng Sci 52:2743–2756CrossRef
Zurück zum Zitat Winterfield G (1965) On processes of turbulent exchange behind flame holders, The Combustion Institute, pp 1265–1275 Winterfield G (1965) On processes of turbulent exchange behind flame holders, The Combustion Institute, pp 1265–1275
Metadaten
Titel
Residence time measurement of an isothermal combustor flow field
verfasst von
Liangta Cheng
Adrian Spencer
Publikationsdatum
01.03.2012
Verlag
Springer-Verlag
Erschienen in
Experiments in Fluids / Ausgabe 3/2012
Print ISSN: 0723-4864
Elektronische ISSN: 1432-1114
DOI
https://doi.org/10.1007/s00348-011-1085-3

Weitere Artikel der Ausgabe 3/2012

Experiments in Fluids 3/2012 Zur Ausgabe

    Marktübersichten

    Die im Laufe eines Jahres in der „adhäsion“ veröffentlichten Marktübersichten helfen Anwendern verschiedenster Branchen, sich einen gezielten Überblick über Lieferantenangebote zu verschaffen.