TY  - JOUR
VL  - 90
UR  - https://www.scopus.com/inward/record.uri?eid=2-s2.0-85016084804&doi=10.1016%2fj.joei.2015.09.003&partnerID=40&md5=16884b5e7f48246b42023251cdc392f5
JF  - Journal of the Energy Institute
A1  - Sadig, H.
A1  - Sulaiman, S.A.
A1  - Said, M.A.
Y1  - 2017///
KW  - Biomass; Carbon dioxide; Combustion; Combustors; Computational fluid dynamics; Energy resources; Exhaust gases; Fossil fuels; Fuels; Gas fuels; Gas turbines; Gases; Liquefied petroleum gas; Particulate emissions; Turbine components; Waste disposal; Waste incineration
KW  -  Emission characteristics; Entrance Temperature; Liquefied petroleum gas (LPG); Micro gas turbine systems; Performance; Performance and emissions; Producer gas; Staged combustion
KW  -  Gas emissions
ID  - scholars9343
N2  - Producer gas from biomass gasification has a potential to cover a considerable part of power production in the future, the availability and variety of biomass put it as the fourth energy resource. The use of producer gas fuels in gas turbine engines can help mitigating problems related to fossil fuels depletion, emissions and biomass waste disposal. In this work, the effect of the staged combustion of a simulated low calorific value producer gas fuels on the performance and emissions of a single shaft micro gas turbine was investigated experimentally. In order to perform the experiments, the micro gas turbine system was characterized first with the liquefied petroleum gas (LPG) and then tested with two producer gas fuels, producer gas1 (10.53 H2, 24.94 CO, 2.03 CH4, 12.80 CO2, and 49.70 N2) and producer gas2 (21.62 H2, 32.48 CO, 3.72 CH4, 19.69 CO2, and 22.49 N2) in a dual fuel mode. Two injection methods were proposed and tested for producer gases including radially and axially injection. The tests were examined in terms of LPG fuel replacement, turbine entrance temperature, combustor efficiency, turbine efficiency, and emission characteristics at different LPG fuel replacement ratios. The study showed stable operation with a maximum LPG replacement of 42 and 56 for the radially injected producer gas1 and producer gas2, respectively. While for the axially injected producer gas fuels, the maximum achieved LPG replacement ratio was 38 and 52 for producer gas1 and producer gas2, respectively. A relatively higher efficiencies for the combustor and turbine with a remarkable reduction in NOx emissions were achieved when LPG fuel was replaced with producer gas fuels. On the other hand CO emissions were increased for both injection methods. © 2015 Energy Institute
IS  - 1
EP  - 144
SN  - 17439671
PB  - Elsevier B.V.
TI  - Effect of producer gas staged combustion on the performance and emissions of a single shaft micro-gas turbine running in a dual fuel mode
SP  - 132
N1  - cited By 11
AV  - none
ER  -