A model for predicting the lift-off height of premixed jets in vitiated cross flow

Michael Kolb, Denise Ahrens, Christoph Hirsch, Thomas Sattelmayer

Publikation: Beitrag in Buch/Bericht/KonferenzbandKonferenzbeitragBegutachtung

7 Zitate (Scopus)

Abstract

Lean premixed single-stage combustion is state of the art for low pollution combustion in heavy-duty gas turbines with gaseous fuels. The application of premixed jets in multi-stage combustion to lower nitric oxide emissions and enhance turndown ratio is a novel promising approach. At the Lehrstuhl für Thermodynamik, Technische Universität München, a large scale atmospheric combustion test rig has been set up for studying staged combustion. The understanding of lift-off behavior is crucial for determining the amount of mixing before ignition and for avoiding flames anchoring at the combustor walls. This experiment studies jet lift-off depending on jet equivalence ratio (0.58-0.82), jet preheat temperature (288-673 K), cross flow temperature (1634-1821 K) and jet momentum ratio (6-210). The differences to existing lift-off studies are the high cross flow temperature and applying a premixed jet. The lift-off height of the jet flame is determined by OH chemiluminescence images, and subsequently, the data is used to analyze the influence of each parameter and to develop a model that predicts the lift-off height for similar staged combustion systems. A main outcome of this work is that the lift-off height in a high temperature cross flow cannot be described by one dimensionless number like Damköhler-or Karlovitz number. Furthermore, the ignition delay time scale τign also misses part of the lift-off height mechanism. The presented model uses turbulent time scales, the ignition delay and a chemical time scale based on the laminar flame speed. An analysis of the model reveals flame stabilization mechanisms and explains the importance of different time scale.

OriginalspracheEnglisch
TitelCombustion, Fuels and Emissions
Herausgeber (Verlag)American Society of Mechanical Engineers (ASME)
ISBN (elektronisch)9780791856680, 9780791856680
DOIs
PublikationsstatusVeröffentlicht - 2015
VeranstaltungASME Turbo Expo 2015: Turbine Technical Conference and Exposition, GT 2015 - Montreal, Kanada
Dauer: 15 Juni 201519 Juni 2015

Publikationsreihe

NameProceedings of the ASME Turbo Expo
Band4A

Konferenz

KonferenzASME Turbo Expo 2015: Turbine Technical Conference and Exposition, GT 2015
Land/GebietKanada
OrtMontreal
Zeitraum15/06/1519/06/15

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