A counter-flow annular heat recirculating burner was designed for lean prevaporized, premixed combustion. Prior to entering the combustor, the reactants are passed through a porous media-filled preheating annulus surrounding the combustor. Kerosene is dripped by gravity onto the porous media and vaporized by the heat conducted through the combustor wall. Experiments were conducted to evaluate heat transfer and combustion performance at various equivalence ratios, heat release rates, and inlet air temperatures. Results show low CO emissions over a range of equivalence ratios. NOx emissions were high at high heat release rates, indicating inadequate prevaporization and premixing of fuel with air. Heat recirculation and heat loss characteristics are presented at various operating conditions.

1.
Razdan
,
M. K.
, 1999, “
Fuel/Air Preparation in the Design of Low Emissions Gas Turbine Combustion Systems
,”
NATO RTO Meeting Proceedings 14 on Gas Turbine Combustion Emissions and Alternative Fuels
, Lisbon, Portugal, October 12–16, 1998, Paper No. 34.
2.
Ripplinger
,
Th.
,
Zarzalis
,
N.
,
Meikis
,
G.
,
Hassa
,
C.
, and
Brandt
,
M.
, 1999, “
NOx Reduction by Lean Premixed Prevaporized Combustion
,”
NATO RTO Meeting Proceedings 14 on Gas Turbine Combustion Emissions and Alternative Fuels
, Lisbon, Portugal, October 12–16, 1998, Paper No. 7.
3.
Wedlock
,
M. I.
,
Tilston
,
J. R.
, and
Seoud
,
R. E.
, 1999, “
The Design and Evaluation of a Piloted Lean Burn, Premixed, Prevaporized Combustor
,”
NATO RTO Meeting Proceedings 14 on Gas Turbine Combustion Emissions and Alternative Fuels
, Lisbon, Portugal, October 12–16, 1998, Paper No. 23.
4.
Samuelsen
,
S.
, and
McDonell
,
V.
, 1999, “
Advanced Fuel Injection Strategies for High Performance gas Turbine Engines
,”
NATO RTO Meeting Proceedings 14 on Gas Turbine Combustion Emissions and Alternative Fuels
, Lisbon, Portugal, October 12–16, 1998, Paper No. 24.
5.
Tacina
,
R. R.
,
Wey
,
C.
,
Laing
,
P.
, and
Mansour
,
A.
, 2001, “
A Low NOx Lean-Direct Injection, Multipoint Integrated Module Combustor Concept for Advanced Aircraft Gas Turbines
,” Clean Air Conference, Portugal.
6.
Lefebvre
,
A. H.
, 1995, “
The Role of Fuel Preparation in Low-Emission Combustion
,”
ASME J. Eng. Gas Turbines Power
0742-4795,
117
, pp.
617
654
.
7.
Weinberg
,
F. J.
, 1971, “
Combustion Temperatures: The Future?
Nature (London)
0028-0836,
223
, p.
239
241
.
8.
Hardesty
,
D. R.
, and
Wienberg
,
F. J.
, 1974, “
Burners Producing Large Excess Enthalpies
Combust. Sci. Technol.
0010-2202,
8
, pp.
201
214
.
9.
Lloyd
,
S. A.
, and
Wienberg
,
F. J.
, 1974, “
A Burner for Mixtures of Very Low Heat Content
,”
Nature (London)
0028-0836,
251
, pp.
47
49
.
10.
Kotani
,
Y.
, and
Takeno
,
T.
, 1982, “
An Experimental Study on Stability and Combustion Characteristics of an Excess Enthalpy Flame
,”
Proc. Combust. Inst.
1540-7489,
19
, pp.
1503
1509
.
11.
Sathe
,
S. B.
,
Kulkarni
,
M. R.
,
Peck
,
R. E.
, and
Tong
,
T. W.
, 1990, “
An Experimental and Theoretical Study of Porous Radiant Burner Performance
,”
Proc. Combust. Inst.
1540-7489,
23
, pp.
1011
1018
.
12.
Howell
,
J. R.
,
Hall
,
M. J.
, and
Ellzey
,
J. L.
, 1996, “
Combustion of Hydrocarbon Fuels Within Porous Inert Media
,”
Prog. Energy Combust. Sci.
0360-1285
22
, pp.
121
145
.
13.
Mital
,
R.
,
Gore
,
J. P.
, and
Viskanta
,
R.
, 1997, “
A Study of the Structure of Submerged Reaction Zone in Porous Ceramic Radiant Burners
,”
Combust. Flame
0010-2180,
111
, pp.
175
184
.
14.
Trimis
,
D.
,
Durst
,
F.
,
Pickenäcker
,
Ó.
, and
Pickenäcker
,
K.
, 1997, “
Porous Medium Combustor Versus Combustion Systems With Free Flames
,”
Proceedings From the 2nd Intl. Symposium on Heat Transfer Enhancement and Energy Conservation
, ISHTEEC, Guangzhou, China, June 16–19, pp.
339
345
.
15.
Marbach
,
T. L.
, and
Agrawal
,
A. K.
, 2003, “
Experimental Study of Surface and Interior Combustion Using Composite Porous Media
,” ASME Paper No. GT2003-38713.
16.
Heatly
,
R. J.
, and
Agrawal
,
A. K.
, 2003, “
Combustion of Pre-Vaporized, Pre-Mixed Fuel Using Porous Inert Media
,”
AIAA/ASME/SAE/ASEE Joint Propulsion Conference
, Vol.
39
, AIAA Paper No. AIAA-2003-5089.
17.
Kaplan
,
M.
, and
Hall
,
M.
, 1995, “
The Combustion of Liquid Fuels Within a Porous Media Radiant Burner
,”
Exp. Therm. Fluid Sci.
0894-1777,
11
, pp.
13
20
.
18.
Tseng
,
C.
, and
Howell
,
J.
, 1996, “
Combustion of Liquid Fuels in a Porous Radiant Burner
,”
Combust. Sci. Technol.
0010-2202,
112
, pp.
141
161
.
19.
Jugjai
,
S.
, and
Narongsak
,
W.
, 2002, “
The Combustion of Liquid Fuels Using a Porous Medium
,”
Exp. Therm. Fluid Sci.
0894-1777,
26
, pp.
15
23
.
20.
Marbach
,
T.
, and
Agrawal
,
A.
, 2003, “
Fuel Vaporization and Combustion With the Use of Porous Inert Media
,”
AIAA/ASME/SAE/ASEE Joint Propulsion Conference
, Vol.
39
, AIAA Paper No. AIAA-2003-5090.
21.
Liedtke
,
O.
,
Schulz
,
A.
, and
Wittig
,
S.
, 2003, “
Emission Performance of a Micro Gas Turbine LPP-Combustor With Fuel Film Evaporation
,” ASME Paper No. GT2003-38697.
22.
Newburn
,
E. R.
, and
Agrawal
,
A.
, 2005, “
Lean Premixed Combustion Using Heat Recirculation Through Annular Porous Media
,”
43rd AIAA Aerospace Sciences Meeting and Exhibit
, AIAA Paper No. 2005-0934.
You do not currently have access to this content.