A lean-premixed advanced vortex combustor (AVC) has been developed and tested. The natural gas fueled AVC was tested at the U.S. Department of Energy’s National Energy Technology Laboratory in Morgantown, WV. All testing was performed at elevated pressures and inlet temperatures and at lean fuel-air ratios representative of industrial gas turbines. The improved AVC design exhibited simultaneous NOxCO∕unburned hydrocarbon (UHC) emissions of 440ppmv (all emissions corrected to 15% O2 dry). The design also achieved less than 3ppmvNOx with combustion efficiencies in excess of 99.5%. The design demonstrated marked acoustic dynamic stability over a wide range of operating conditions, which potentially makes this approach significantly more attractive than other lean-premixed combustion approaches. In addition, the measured 1.75% pressure drop is significantly lower than conventional gas turbine combustors, which could translate into an overall gas turbine cycle efficiency improvement. The relatively high velocities and low pressure drop achievable with this technology make the AVC approach an attractive alternative for syngas fuel applications.

1.
Steele
,
R. C.
,
Cowell
,
L. H.
,
Cannon
,
S. M.
, and
Smith
,
C. E.
, 2000, “
Passive Control of Combustion Instability in Lean Premixed Combustors
,”
ASME J. Eng. Gas Turbines Power
0742-4795,
122
, pp.
412
419
.
2.
Richards
,
G. A.
, and
Janus
,
M. C.
, 1998, “
Characterization of Oscillations During Premix Gas Turbine Combustion
,”
ASME J. Eng. Gas Turbines Power
0742-4795,
120
, pp.
294
302
.
3.
Hsu
,
K. Y.
,
Goss
,
L. P.
, and
Roquemore
,
W. M.
, 1998, “
Characteristics of a Trapped Vortex Combustor
,”
J. Propul. Power
0748-4658,
14
(
1
), pp.
57
65
.
4.
Bucher
,
J.
,
Edmonds
,
R. G.
,
Steele
,
R. C.
,
Kendrick
,
D.
,
Chenevert
,
B.
, and
Malte
,
P.
, 2003, “
The Development of a Lean Premixed Trapped Vortex Combustor
,” ASME Paper No. GT2003-38236.
5.
Straub
,
D. L.
,
Casleton
,
K. H.
,
Lewis
,
R. E.
,
Sidwell
,
T. G.
,
Maloney
,
D. J.
, and
Richards
,
G. A.
, 2005, “
Assessment of Rich-Burn Quick-Mix, Lean-Burn Trapped Vortex Combustor for Stationary Gas Turbines
,”
ASME J. Eng. Gas Turbines Power
0742-4795,
127
, pp.
36
41
.
6.
Edmonds
,
R. G.
,
Steele
,
R. C.
, Williams, J. T..,
Straub
,
D. L.
,
Casleton
,
K. H.
, and
Bining
,
A.
, 2006, “
Ultra-Low NOx Advanced Vortex Combustor
,” ASME Paper No. GT2006-90319.
7.
Sidwell
,
T.
,
Richards
,
G.
,
Casleton
,
K.
,
Straub
,
D.
,
Maloney
,
D.
,
Strakey
,
P.
,
Ferguson
,
D.
,
Beer
,
S.
, and
Woodruff
,
S.
, 2004, “
Optically Accessible Pressurized Research Combustor for Computational Fluid Dynamics Model Validation
,”
AIAA J.
0001-1452,
44
(
3
), pp.
434
443
.
8.
SAE, 1996–2001, “
Procedure for the Calculations of Gaseous Emissions from Aircraft Turbine Engines
,” Society of Automotive Engineers, Warrendale, PA, SAE Report No. ARP 1533.
You do not currently have access to this content.