Colorless distributed combustion (CDC) has shown to provide ultra-low emissions of NO, CO, unburned hydrocarbons, and soot, with stable combustion without using any flame stabilizer. The benefits of CDC also include uniform thermal field in the entire combustion space and low combustion noise. One of the critical aspects in distributed combustion is fuel mixture preparation prior to mixture ignition. In an effort to improve fuel mixing and distribution, several schemes have been explored that includes premixed, nonpremixed, and partially premixed. In this paper, the effect of dual-location fuel injection is examined as opposed to single fuel injection into the combustor. Fuel distribution between different injection points was varied with the focus on reaction distribution and pollutants emission. The investigations were performed at different equivalence ratios (0.6–0.8), and the fuel distribution in each case was varied while maintaining constant overall thermal load. The results obtained with multi-injection of fuel using a model combustor showed lower emissions as compared to single injection of fuel using methane as the fuel under favorable fuel distribution condition. The NO emission from double injection as compared to single injection showed a reduction of 28%, 24%, and 13% at equivalence ratio of 0.6, 0.7, and 0.8, respectively. This is attributed to enhanced mixture preparation prior to the mixture ignition. OH* chemiluminescence intensity distribution within the combustor showed that under favorable fuel injection condition, the reaction zone shifted downstream, allowing for longer fuel mixing time prior to ignition. This longer mixing time resulted in better mixture preparation and lower emissions. The OH* chemiluminescence signals also revealed enhanced OH* distribution with fuel introduced through two injectors.

References

1.
Arghode
,
V. K.
, and
Gupta
,
A. K.
,
2010
, “
Effect of Flowfield for Colorless Distributed Combustion (CDC) for Gas Turbine Combustion
,”
Appl. Energy
,
87
(5), pp.
1631
1640
.
2.
Arghode
,
V. K.
, and
Gupta
,
A. K.
,
2013
, “
Role of Thermal Intensity on Operational Characteristics of Ultra-Low Emission Colorless Distributed Combustion
,”
Appl. Energy
,
111
, pp.
930
956
.
3.
Khalil
,
A. E. E.
, and
Gupta
,
A. K.
,
2011
, “
Swirling Distributed Combustion For Clean Energy Conversion in Gas Turbine Applications
,”
Appl. Energy
,
88
(
11
), pp.
3685
3693
.
4.
Khalil
,
A. E. E.
, and
Gupta
,
A. K.
,
2011
, “
Distributed Swirl Combustion for Gas Turbine Application
,”
Appl. Energy
,
88
(
12
), pp.
4898
4907
.
5.
Tsuji
,
H.
,
Gupta
,
A. K.
,
Hasegawa
,
T.
,
Katsuki
,
M.
,
Kishimoto
,
K.
, and
Morita
,
M.
,
2003
,
High Temperature Air Combustion: From Energy Conservation to Pollution Reduction
,
CRC Press
,
Boca Raton, FL
.
6.
Gupta
,
A. K.
,
Lilley
,
D. G.
, and
Syred
,
N.
,
1984
,
Swirl Flows
,
Abacus Press
,
Tunbridge Wells, UK
.
7.
Huang
,
Y.
,
2008
, “
Combustion Dynamics of Swirl-Stabilized Lean Premixed Flames in an Acoustically Driven Environment
,”
Ph.D. thesis
, University of Iowa, Iowa, IA.
8.
Roux
,
S.
,
Lartigue
,
G.
,
Poinsot
,
T.
,
Meier
,
U.
, and
Berat
,
C.
,
2005
, “
Studies of Mean and Unsteady Flow in a Swirled Combustor Using Experiments, Acoustic Analysis, and Large Eddy Simulations
,”
Combust. Flame
,
141
(1–2), pp.
40
54
.
9.
Lefebvre
,
A. H.
,
1998
,
Gas Turbine Combustion
, 2nd ed.,
Taylor and Francis
, Boca Raton, FL.
10.
Khalil
,
A. E. E.
, and
Gupta
,
A. K.
,
2012
, “
Mixture Preparation Effects on Distributed Combustion for Gas Turbine Applications
,”
ASME J. Energy Resour. Technol.
,
134
(
3
), p.
032201
.
11.
Arghode
,
V. K.
,
Khalil
,
A. E. E.
, and
Gupta
,
A. K.
,
2012
, “
Fuel Dilution and Liquid Fuel Operational Effects on Ultra-High Thermal Intensity Distributed Combustor
,”
Appl. Energy
,
95
, pp.
132
138
.
12.
Khalil
,
A. E. E.
, and
Gupta
,
A. K.
,
2015
, “
Towards Ultra-Low Emission Distributed Combustion With Fuel Air Dilution
,”
Appl. Energy
,
148
, pp.
187
195
.
13.
Khalil
,
A. E. E.
, and
Gupta
,
A. K.
,
2013
, “
Dual Injection Distributed Combustion for Gas Turbine Application
,”
ASME J. Energy Resour. Technol.
,
136
(
1
), p.
011601
.
14.
Leong
,
M. Y.
,
Samuelsen
,
G. S.
, and
Holdeman
,
J. D.
,
1997
, “
Mixing of Pure Air Jets With a Reacting Fuel-Rich Crossflow
,” NASA Lewis Research Center, Cleveland, OH, Report No.
NASA
-TM-107430.
15.
Turns
,
S. R.
,
2000
,
An Introduction to Combustion: Concepts and Applications
, 2nd ed.,
McGraw-Hill
, New York.
16.
Stone
,
R.
,
Clarke
,
A.
, and
Beckwith
,
P.
,
1998
, “
Correlations for the Laminar-Burning Velocity of Methane/Diluent/Air Mixtures Obtained in Free-Fall Experiments
,”
Combust. Flame
,
114
(3–4), pp.
546
555
.
You do not currently have access to this content.