Dry low emission (DLE) systems employing lean, premixed combustion have been successfully used with natural gas in combustion turbines to meet stringent emission standards. However, the burning of liquid fuels in DLE systems is still a challenging task due to the complexities of fuel vaporization and air premixing. Lean, premixed, and prevaporized (LPP) combustion has always provided the promise of obtaining low pollutant emissions while burning liquid fuels, such as kerosene and fuel oil. Because of the short ignition delay times of these fuels at elevated temperatures, the autoignition of vaporized higher hydrocarbons typical of most practical liquid fuels has been proven difficult to overcome when burning in a lean, premixed mode. To avoid this autoignition problem, developers of LPP combustion systems have focused mainly on designing premixers and combustors that permit rapid mixing and combustion of fuels before spontaneous ignition of the fuel can occur. However, none of the reported works in the literature has looked at altering fuel combustion characteristics in order to delay the onset of ignition in lean, premixed combustion systems. The work presented in this paper describes the development of a patented low NOx LPP system for combustion of liquid fuels, which modifies the fuel rather than the combustion hardware in order to achieve LPP combustion. In the initial phase of the development, laboratory-scale experiments were performed to study the combustion characteristics, such as ignition delay time and NOx formation, of the liquid fuels that were vaporized into gaseous form in the presence of nitrogen diluent. In the second phase, a LPP combustion system was commissioned to perform pilot-scale tests on commercial turbine combustor hardware. These pilot-scale tests were conducted at typical compressor discharge temperatures and at both atmospheric and high pressures. In this study, vaporization of the liquid fuel in an inert environment has been shown to be a viable method for delaying autoignition and for generating a gaseous fuel stream with characteristics similar to natural gas. Tests conducted in both atmospheric and high pressure combustor rigs utilizing swirl-stabilized burners designed for natural gas demonstrated an operation similar to that obtained when burning natural gas. Emission levels were similar for both the LPP fuels (fuel oils 1 and 2) and natural gas, with any differences ascribed to the fuel-bound nitrogen present in the liquid fuels. An extended lean operation was observed for the liquid fuels as a result of the wider lean flammability range for these fuels compared to natural gas.

1.
Davis
,
L. B.
, and
Black
,
S. H.
, 2000, “
Dry Low NOx Combustion Systems for GE Heavy-Duty Gas Turbines
,” General Electric Power Systems, Report No. GER 3568G.
2.
Plee
,
S. L.
, and
Mellor
,
A. M.
, 1978, “
Review of Flashback Term Reported in Prevaporizing∕Premixing Combustors
,”
Combust. Flame
0010-2180,
32
, pp.
193
203
.
3.
Oumejjoud
,
K.
,
Stuttaford
,
P.
,
Jennings
,
S.
,
Rizkalla
,
H.
,
Henriquez
,
J.
, and
Chen
,
Y.
, 2005, “
Emission, LBO and Combustion Characterization for Several Alternative Fuels
,” ASME Paper No. GT2005-68561.
4.
Maier
,
G.
, and
Wiitig
,
S.
, 1999, “
Fuel Preparation and Emission Characteristics of a Pressure Loaded LPP Combustor
,” Paper No. AIAA-99-3774.
5.
Imamura
,
A.
,
Yoshida
,
M.
,
Kawano
,
M.
,
Aruga
,
N.
,
Nagata
,
Y.
, and
Kawagishi
,
M.
, 2001, “
Research and Development of a LPP Combustor With Swirling Flow for Low NOx
,” Paper No. AIAA-2001-3311.
6.
Ikezaki
,
T.
,
Hosoi
,
J.
, and
Hidemi
,
T.
, 2001, “
The Performance of the Low NOx Aero Gas Turbine Combustor Under High Pressure
,” ASME Paper No. 2001-GT-0084.
7.
Lin
,
Y.
,
Peng
,
Y.
, and
Liu
,
G.
, 2004, “
Investigation on NOx of a Low Emission Combustor Design With Multihole Premixer-Prevaporizer
,” ASME Paper No. GT2004-53203.
8.
Lee
,
C.
,
Chun
,
K. S.
, and
Locke
,
R. J.
, 1995, “
Fuel-Air Mixing Effect on NOx Emissions for a Lean Premixed-Prevaporized Combustion System
,” Paper No. AIAA-95-0729.
9.
Michou
,
Y.
,
Chauveau
,
C.
,
Gijkalp
,
I.
, and
Carvalho
,
I. S.
, 1999, “
Experimental Study of Lean Premixed and Prevaporized Turbulent Spray Combustion
,” Paper No. AIAA 99-0332.
10.
Hoffmann
,
S.
,
Judith
,
H.
, and
Holm
,
C.
, 1998, “
Further Development of the Siemens LPP Hybrid Burner
,” ASME Paper No. 98-GT-552.
11.
Mansour
,
A.
,
Benjamin
,
M.
,
Straub
,
D. L.
, and
Richards
,
G. A.
, 2001, “
Application of Macrolamination Technology to Lean, Premixed Combustion
,”
ASME J. Eng. Gas Turbines Power
0742-4795,
123
, pp.
796
802
.
12.
Røkke
,
N. A.
, and
Wilson
,
A. J. W.
, 2001, “
Experimental and Theoretical Studies of a Novel Venturi Lean Premixed Prevaporized (LPP) Combustor
,”
ASME J. Eng. Gas Turbines Power
0742-4795,
123
, pp.
567
573
.
13.
Roby
,
R. J.
,
Klassen
,
M. S.
, and
Schemel
,
C. F.
, 2006, “
System for Vaporization of Liquid Fuels for Combustion and Method of Use
,” U.S. Patent No. 7,089,745.
14.
Lifshitz
,
A.
, 2001, “
Chemical and Combustion Kinetics
,”
Handbook of Shock Waves
, Vol.
3
,
Academic
,
New York
.
15.
Yetter
,
R. A.
,
Dryer
,
F. L.
, and
Rabitz
,
H.
, 1991, “
A Comprehensive Reaction Mechanism for Carbon Monoxide/Hydrogen/Oxygen Kinetics
,”
Combust. Sci. Technol.
0010-2202,
79
, pp.
129
140
.
16.
Gokulakrishnan
,
P.
,
Kazakov
,
A.
, and
Dryer
,
F. L.
, 2003, “
Comparison of Numerical and Experimental Kinetic Data for Flow Reactor Systems: Mixing Effects
,”
Proceedings of the Third Joint Meeting
, The Combustion Institute.
17.
Gokulakrishnan
,
P.
,
Gaines
,
G.
,
Currano
,
J.
,
Klassen
,
M. S.
, and
Roby
,
R. J.
, 2007, “
Experimental and Kinetic Modeling of Kerosene-Type Fuels at Gas Turbine Operating Conditions
,”
ASME J. Eng. Gas Turbines Power
0742-4795,
129
, pp.
655
663
.
18.
Curran
,
H. J.
,
Gaffuri
,
P.
,
Pitz
,
W. J.
, and
Westbrook
,
C. K.
, 1998, “
A Comprehensive Modeling Study of n-Heptane Oxidation
,”
Combust. Flame
0010-2180,
114
, pp.
149
177
.
19.
Leonard
,
G.
, and
Stegmaier
,
J.
, 1994, “
Development of an Aeroderivative Gas Turbine Dry Low Emissions Combustion System
,”
ASME J. Eng. Gas Turbines Power
0742-4795,
116
, pp.
542
546
.
20.
Steele
,
R. C.
,
Tonnouchi
,
J. H.
,
Nicol
,
D. G.
,
Horning
,
D. C.
,
Malte
,
P. C.
, and
Pratt
,
D. G.
, 1996, “
Characterization of NOx, N2O and CO for Lean Premixed Combustion in High Pressure Jet-Sirred Reactor
,” ASME Paper No. 96-GT-128.
21.
Bhargava
,
A.
,
Kendrick
,
D. W.
,
Colket
,
M. B.
,
Sowa
,
W. A.
,
Casleton
,
K. H.
, and
Maloney
,
D. J.
, 2000, “
Pressure Effect on NOx and CO Emissions in Industrial Gas Turbines
,” ASME Paper No. 2000-GT-97.
22.
Correa
,
S. M.
, 1992, “
A Review of NOx Formation Under Gas-Turbine Combustion Conditions
,”
Combust. Sci. Technol.
0010-2202,
87
, pp.
329
362
.
23.
Mongia
,
R. K.
,
Tomita
,
E.
,
Hsu
,
F. K.
,
Talbot
,
L.
, and
Dibble
,
R. W.
, 1996,
Sym. (Int.) Combust., [Proc.]
0082-0784,
26
, pp.
2749
2755
.
24.
Schorr
,
M. M.
, and
Chalfin
,
J.
, 1999, “
Gas Turbine NOx Emissions Approaching Zero—Is It Worth the Price?
,” General Electric Power Generation, Report No. GER 4172.
25.
Pavri
,
R.
, and
Moore
,
G. D.
, 2001, “
Gas Turbine Emissions and Control
,” General Electric Power Systems, Report No. GER 4211.
26.
Eimers
,
R. A.
,
Smith
,
K. O.
, and
Cowell
,
L.
, 2001, “
Developments in Low Emissions Combustion Systems for Industrial Gas Turbines
,” Solar Turbines, Report No. TPSOLONOX∕901.
27.
Knodle
,
M. S.
, 1998, “
Centaur, 40, Centaur 50 and Taurus 60 Gas Turbine Product Technology Update
,” Solar Turbines Turbomachinery Technology Seminar, Paper No. TTS123∕398∕M.
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