Investigation of methane oxy-fuel combustion in a swirl-stabilised gas turbine model combustor
(2017) In Energies 10(5).- Abstract
CO2 has a strong impact on both operability and emission behaviours in gas turbine combustors. In the present study, an atmospheric, preheated, swirl-stabilised optical gas turbine model combustor rig was employed. The primary objectives were to analyse the influence of CO2 on the fundamental characteristics of combustion, lean blowout (LBO) limits, CO emission and flame structures. CO2 dilution effects were examined with three preheating temperatures (396.15, 431.15, and 466.15 K). The fundamental combustion characteristics were studied utilising chemical kinetic simulations. To study the influence of CO2 on the operational range of the combustor, equivalence ratio (Φ) was varied from... (More)
CO2 has a strong impact on both operability and emission behaviours in gas turbine combustors. In the present study, an atmospheric, preheated, swirl-stabilised optical gas turbine model combustor rig was employed. The primary objectives were to analyse the influence of CO2 on the fundamental characteristics of combustion, lean blowout (LBO) limits, CO emission and flame structures. CO2 dilution effects were examined with three preheating temperatures (396.15, 431.15, and 466.15 K). The fundamental combustion characteristics were studied utilising chemical kinetic simulations. To study the influence of CO2 on the operational range of the combustor, equivalence ratio (Φ) was varied from stoichiometric conditions to the LBO limits. CO emissions were measured at the exit of the combustor using a water-cooled probe over the entire operational range. The flame structures and locations were characterised by performing CH chemiluminescence imaging. The inverse Abel transformation was used to analyse the CH distribution on the axisymmetric plane of the combustor. Chemical kinetic modelling indicated that the CO2 resulted in a lower reaction rate compared with the CH4/air flame. Fundamental combustion properties such as laminar flame speed, ignition delay time and blowout residence time were found to be affected by CO2. The experimental results revealed that CO2 dilution resulted in a narrower operational range for the equivalence ratio. It was also found that CO2 had a strong inhibiting effect on CO burnout, which led to a higher concentration of CO in the combustion exhaust. CH chemiluminescence showed that the CO2 dilution did not have a significant impact on the flame structure.
(Less)
- author
- Li, Mao LU ; Tong, Yiheng LU ; Thern, Marcus LU and Klingmann, Jens LU
- organization
- publishing date
- 2017
- type
- Contribution to journal
- publication status
- published
- subject
- keywords
- CO emission, Gas turbine combustion, Lean blowout, Methane flame, Oxy-fuel
- in
- Energies
- volume
- 10
- issue
- 5
- article number
- 648
- publisher
- MDPI AG
- external identifiers
-
- wos:000403048400067
- scopus:85035135237
- ISSN
- 1996-1073
- DOI
- 10.3390/en10050648
- language
- English
- LU publication?
- yes
- id
- 6a1fa93f-496c-41c4-9fc1-d152205898a6
- date added to LUP
- 2017-12-11 07:55:34
- date last changed
- 2024-06-10 05:34:12
@article{6a1fa93f-496c-41c4-9fc1-d152205898a6,
abstract = {{<p>CO<sub>2</sub> has a strong impact on both operability and emission behaviours in gas turbine combustors. In the present study, an atmospheric, preheated, swirl-stabilised optical gas turbine model combustor rig was employed. The primary objectives were to analyse the influence of CO<sub>2</sub> on the fundamental characteristics of combustion, lean blowout (LBO) limits, CO emission and flame structures. CO<sub>2</sub> dilution effects were examined with three preheating temperatures (396.15, 431.15, and 466.15 K). The fundamental combustion characteristics were studied utilising chemical kinetic simulations. To study the influence of CO<sub>2</sub> on the operational range of the combustor, equivalence ratio (Φ) was varied from stoichiometric conditions to the LBO limits. CO emissions were measured at the exit of the combustor using a water-cooled probe over the entire operational range. The flame structures and locations were characterised by performing CH chemiluminescence imaging. The inverse Abel transformation was used to analyse the CH distribution on the axisymmetric plane of the combustor. Chemical kinetic modelling indicated that the CO<sub>2</sub> resulted in a lower reaction rate compared with the CH<sub>4</sub>/air flame. Fundamental combustion properties such as laminar flame speed, ignition delay time and blowout residence time were found to be affected by CO<sub>2</sub>. The experimental results revealed that CO<sub>2</sub> dilution resulted in a narrower operational range for the equivalence ratio. It was also found that CO<sub>2</sub> had a strong inhibiting effect on CO burnout, which led to a higher concentration of CO in the combustion exhaust. CH chemiluminescence showed that the CO<sub>2</sub> dilution did not have a significant impact on the flame structure.</p>}},
author = {{Li, Mao and Tong, Yiheng and Thern, Marcus and Klingmann, Jens}},
issn = {{1996-1073}},
keywords = {{CO emission; Gas turbine combustion; Lean blowout; Methane flame; Oxy-fuel}},
language = {{eng}},
number = {{5}},
publisher = {{MDPI AG}},
series = {{Energies}},
title = {{Investigation of methane oxy-fuel combustion in a swirl-stabilised gas turbine model combustor}},
url = {{http://dx.doi.org/10.3390/en10050648}},
doi = {{10.3390/en10050648}},
volume = {{10}},
year = {{2017}},
}