Experimental Study of Flameless Combustion in Gas Turbine Combustors
(2006) 44th AIAA Aerospace Sciences Meeting and Exhibit, 2006- Abstract
- This paper presents experimental data on investigation of novel flameless combustors in
application of gas turbine engines at atmospheric conditions. Flameless combustion is
characterized by distributed flame and even temperature distribution under the conditions
of high preheat air temperature and sufficient large amount of recirculating low oxygen
concentration exhaust gas. Extremely low emissions of NOx, CO, and UHC are reported in
this paper for flameless combustion in a multiple jets premixed gas turbine combustor and a
swirling jet combustor. Measurements on the flame chemiluminescence, CO and NOx
emissions, acoustic pressure, temperature field, and velocity field reveal... (More) - This paper presents experimental data on investigation of novel flameless combustors in
application of gas turbine engines at atmospheric conditions. Flameless combustion is
characterized by distributed flame and even temperature distribution under the conditions
of high preheat air temperature and sufficient large amount of recirculating low oxygen
concentration exhaust gas. Extremely low emissions of NOx, CO, and UHC are reported in
this paper for flameless combustion in a multiple jets premixed gas turbine combustor and a
swirling jet combustor. Measurements on the flame chemiluminescence, CO and NOx
emissions, acoustic pressure, temperature field, and velocity field reveal the influence of
preheat temperature, inlet air mass flow rate, combustor exhaust nozzle contraction ratio,
and combustor chamber diameter on emissions and combustion dynamics. The data indicate
that greater air mass flow rate, thus larger pressure drop, promotes the formation of
flameless combustion and lower NOx emissions for the same flame temperature. This
flameless combustor is in nature a premixed combustion which NOx emission is an
exponential function of the flame temperature regardless of different preheated
temperature. High preheated temperature and flow rate also helps in forming stable
combustion therefore are favorable for flameless combustion. The effects on emissions and
combustion dynamics from the combustor exhaust contraction and the combustion chamber diameter are also discussed. (Less)
Please use this url to cite or link to this publication:
https://lup.lub.lu.se/record/778156
- author
- Li, Guoqiang ; Gutmark, Ephraim J. ; Stankovic, Dragan LU ; Overman, Nick ; Cornwell, Michael ; Fuchs, Laszlo LU and Milosavljevic, Vladimir LU
- organization
- publishing date
- 2006
- type
- Chapter in Book/Report/Conference proceeding
- publication status
- published
- subject
- host publication
- [Host publication title missing]
- publisher
- American Institute of Aeronautics and Astronautics
- conference name
- 44th AIAA Aerospace Sciences Meeting and Exhibit, 2006
- conference location
- Reno, Nevada, United States
- conference dates
- 2006-01-09 - 2006-09-12
- external identifiers
-
- other:AIAA paper no. 2006-546
- scopus:34250761522
- language
- English
- LU publication?
- yes
- id
- 5d84cad7-a22f-4b26-b222-05d998f045c2 (old id 778156)
- date added to LUP
- 2016-04-04 12:02:06
- date last changed
- 2022-01-29 22:47:16
@inproceedings{5d84cad7-a22f-4b26-b222-05d998f045c2,
abstract = {{This paper presents experimental data on investigation of novel flameless combustors in<br/><br>
application of gas turbine engines at atmospheric conditions. Flameless combustion is<br/><br>
characterized by distributed flame and even temperature distribution under the conditions<br/><br>
of high preheat air temperature and sufficient large amount of recirculating low oxygen<br/><br>
concentration exhaust gas. Extremely low emissions of NOx, CO, and UHC are reported in<br/><br>
this paper for flameless combustion in a multiple jets premixed gas turbine combustor and a<br/><br>
swirling jet combustor. Measurements on the flame chemiluminescence, CO and NOx<br/><br>
emissions, acoustic pressure, temperature field, and velocity field reveal the influence of<br/><br>
preheat temperature, inlet air mass flow rate, combustor exhaust nozzle contraction ratio,<br/><br>
and combustor chamber diameter on emissions and combustion dynamics. The data indicate<br/><br>
that greater air mass flow rate, thus larger pressure drop, promotes the formation of<br/><br>
flameless combustion and lower NOx emissions for the same flame temperature. This<br/><br>
flameless combustor is in nature a premixed combustion which NOx emission is an<br/><br>
exponential function of the flame temperature regardless of different preheated<br/><br>
temperature. High preheated temperature and flow rate also helps in forming stable<br/><br>
combustion therefore are favorable for flameless combustion. The effects on emissions and<br/><br>
combustion dynamics from the combustor exhaust contraction and the combustion chamber diameter are also discussed.}},
author = {{Li, Guoqiang and Gutmark, Ephraim J. and Stankovic, Dragan and Overman, Nick and Cornwell, Michael and Fuchs, Laszlo and Milosavljevic, Vladimir}},
booktitle = {{[Host publication title missing]}},
language = {{eng}},
publisher = {{American Institute of Aeronautics and Astronautics}},
title = {{Experimental Study of Flameless Combustion in Gas Turbine Combustors}},
year = {{2006}},
}