Flashback (FB) and self-ignition in the premixing zone of typical gas turbine swirl combustors in lean premixed operation are immanent risks and can lead to damage and failure of components. Thus, steady combustion in the premixing zone must be avoided under all circumstances. This study experimentally investigates the flame holding propensity of fuel injectors in the swirler of a gas turbine model combustor with premixing of H2–natural gas (NG)–air mixtures under atmospheric pressure and proposes a model to predict the limit for safe operation. The A2EV swirler concept exhibits a hollow, thick walled conical structure with four tangential slots. Four fuel injector geometries were tested. One of them injects the fuel orthogonal to the air flow in the slots (jet-in-crossflow injector, JICI). Three injector types introduce the fuel almost isokinetic to the air flow at the trailing edge of the swirler slots (trailing edge injector, TEI). A cylindrical duct and a window in the swirler made of quartz glass allow the application of optical diagnostics (OH* chemiluminescence and planar laser induced fluorescence of the OH radical (OH-PLIF)) inside the swirler. The fuel–air mixture was ignited with a focused single laser pulse during steady operation. The position of ignition was located inside the swirler in proximity to a fuel injection hole. If the flame was washed out of the premixing zone not later than 4 s after the ignition, the operation point was defined as safe. Operation points were investigated at three air mass flows, three air ratios, two air preheat temperatures (573 K and 673 K), and 40 to 100 percent per volume hydrogen in the fuel composed of hydrogen and natural gas. The determined safety limit for atmospheric pressure yields a similarity rule based on a critical Damköhler number. Application of the proposed rule at conditions typical for gas turbines leads to these safety limits for the A2EV burner: With the TEIs, the swirler can safely operate with up to 80 percent per volume hydrogen content in the fuel at an air ratio of two. With the JIC injector, safe operation at stoichiometric conditions and 95 percent per volume hydrogen is possible.

References

1.
EERE Information Center
,
2010
, “
Fuel Cell Technologies Program
,” U.S. Department of Energy, Technical Report No. 1-877-337-3463.
2.
Smith
,
S. H.
, and
Mungal
,
M. G.
,
1998
, “
Mixing, Structure and Scaling of the Jet in Crossflow
,”
J. Fluid Mech.
,
357
, pp.
83
122
.
3.
Han
,
D.
, and
Mungal
,
M.
,
2003
, “
Simultaneous Measurements of Velocity and CH Distribution. Part I: Jet Flames in Co-Flow
,”
Combust. Flame
,
132
(
3
), pp.
565
590
.
4.
Han
,
D.
, and
Mungal
,
M.
,
2003
, “
Simultaneous Measurements of Velocity and CH Distribution. Part II: Deflected Jet Flames
,”
Combust. Flame
,
133
, pp.
1
17
.
5.
Tieszen
,
S. R.
,
Stamps
,
D. W.
, and
O'Hern
,
T. J.
,
1996
, “
A Heuristic Model of Turbulent Mixing Applied to Blowout of Turbulent Jet Diffusion Flames
,”
Combust. Flame
,
106
(
4
), pp.
442
466
.
6.
Kalghatgi
,
G. T.
,
1984
, “
Lift-Off Heights and Visible Lengths of Vertical Turbulent Jet Diffusion Flames in Still Air
,”
Combust. Sci. Technol.
,
41
(
1–2
), pp.
17
29
.
7.
Dahm
,
W. J. A.
, and
Mayman
,
A. G.
,
1990
, “
Blowout Limits of Turbulent Jet Diffusion Flames for Arbitrary Source Conditions
,”
AIAA J.
,
28
(
7
), pp.
1157
1162
.
8.
Bradley
,
D.
,
Casal
,
J.
,
Gaskell
,
P. H.
, and
Palacios
,
A.
,
2013
, “
Jet Flames, Flares and Pool Fires: Predictions of Flame Lift-Off, Plume and Flame Height Under Choked and Unchoked Conditions
,”
Seventh International Seminar on Fire and Explosion Hazards
, pp.
200
209
.
9.
Sangl
,
J.
,
2011
, “
Erhöhung der Brennstoffflexibilität von Vormischbrennern durch Beeinflussung der Wirbeldynamik
,” Ph.D. thesis, Technische Universität München, Garching, Germany.
10.
Mayer
,
C.
,
2012
, “
Konzept zur vorgemischten Verbrennung wasserstoffhaltiger Brennstoffe in Gasturbinen
,” Ph.D. thesis, Technische Universität München, Garching, Germany.
11.
Fritz
,
Y.
,
Kröner
,
M.
, and
Sattelmayer
,
T.
,
2004
, “
Flashback in a Swirl Burner With Cylindrical Premixing Zone
,”
ASME J. Eng. Gas Turbines Power
,
126
(
2
), pp.
276
283
.
12.
Kröner
,
M.
,
Fritz
,
Y.
, and
Sattelmayer
,
T.
,
2003
, “
Flashback Limits for Combustion Induced Vortex Breakdown in a Swirl Burner
,”
ASME J. Eng. Gas Turbines Power
,
125
(
3
), pp.
693
700
.
13.
Goodwin
,
D. G.
,
Moffat
,
H. K.
, and
R. L.
Speth
,
2014
, “
Cantera: An Object-Oriented Software Toolkit for Chemical Kinetics, Thermodynamics, and Transport Processes
,” Version 2.2.1, accessed Mar. 17, 2014, https://sourceforge.net/projects/cantera/files/cantera/
14.
Otsu
,
N.
,
1979
, “
A Threshold Selection Method From Gray-Level Histograms
,”
IEEE Trans. Syst., Man, Cybern.
,
9
(
1
), pp.
62
66
.
15.
Reichel
,
T. G.
,
Göckeler
,
K.
, and
Paschereit
,
C. O.
,
2015
, “
Investigation of Lean Premixed Swirl-Stabilized Hydrogen Burner With Axial Air Injection Using OH-PLIF Imaging
,”
ASME
Paper No. GT2015-42491.
16.
Peters
,
N.
,
2006
,
Turbulent Combustion
,
Cambridge University Press
,
Cambridge, UK
.
17.
Peters
,
N.
,
1994
, “
Turbulente Brenngeschwindigkeit
,” RWTH Aachen, Technical Report No. Pe 241/9-2.
18.
Kröner
,
M.
,
2003
, “
Einfluss lokaler Löschvorgänge auf den Flammenrückschlag durch verbrennungsinduziertes Wirbelaufplatzen
,” Ph.D. thesis, Technische Universität München, Garching, Germany.
19.
Lawn
,
C.
,
2009
, “
Lifted Flames on Fuel Jets in Co-Flowing Air
,”
Prog. Energy Combust. Sci.
,
35
(
1
), pp.
1
30
.
20.
Gomes
,
J. N.
,
Kribs
,
J. D.
, and
Lyons
,
K. M.
,
2012
, “
Stability and Blowout Behavior of Jet Flames in Oblique Air Flows
,”
J. Combust.
,
2012
, p.
218916
.
21.
Hasselbrink
,
E. F.
, and
Mungal
,
M. G.
,
2001
, “
Transverse Jets and Jet Flames. Part 2. Velocity and OH Field Imaging
,”
J. Fluid Mech.
,
443
, pp.
27
68
.
22.
Kalghatgi
,
G. T.
,
1981
, “
Blow-Out Stability of Gaseous Jet Diffusion Flames Part II: Effect of Cross Wind
,”
Combust. Sci. Technol.
,
26
(
5–6
), pp.
241
244
.
You do not currently have access to this content.