Abstract
In a recent joint research project, a new FLOX®-combustion system was developed to couple a fixed-bed gasifier with a micro gas turbine (MGT). Product gases from biomass gasification exhibit low calorific values and varying compositions of mainly H2, CO, CO2, N2, and CH4. Furthermore, combustion characteristics differ significantly compared to the commonly used natural gas. As the FLOX-technology is considered as efficient and fuel-flexible featuring low emissions of hazardous pollutants, the design of the lower calorific value (LCV) combustor is based on it. It contains a two-staged combustor consisting of a jet-stabilized main stage adapted from the FLOX-concept combined with a swirl stabilized pilot stage. The combustor was operated in a Turbec T100 test rig using an optically accessible combustion chamber, which allowed OH*-chemiluminescence and OH-PLIF measurements for various fuel compositions. In particular, the hydrogen content in the synthetically mixed fuel gas was varied from 0% to 30%. The exhaust gas composition was additionally analyzed regarding CO, NOx, and unburned hydrocarbons. The results provide a comprehensive insight into the flame behavior during turbine operation. Efficient combustion and stable operation of the MGT was observed for all fuel compositions, while the hydrogen showed a strong influence. It is remarkable that with hydrogen contents higher than 9%, no OH radicals were detected within the inner recirculation zone, while they were increasingly entrained below hydrogen contents of 9%. Without hydrogen, the inner recirculation zone was completely filled with OH radicals and the highest concentrations were detected there. Therefore, the results indicate a different flame behavior with low and high hydrogen contents. Although the flame shape and position were affected, pollutant emissions remained consistently below 10 ppm based on 15% O2. Only in the case of 0% hydrogen, CO-emissions increased to 43 ppm, which are still meeting the emission limits. Thus, the combustor allows operation with syngases having hydrogen contents from 0% to 30%.
Highlights
Micro gas turbines (MGT) constitute an upcoming technology in the field of decentralized combined heat and power (CHP) production [1]
SUMMARY AND CONCLUSIONS The fuel-flexibility of a lower calorific values (LCV)-combustor consisting of a FLOX® adopted main stage and a swirl stabilized pilot stage was analysed and demonstrated in this work by varying the hydrogen concentration in the fuel
Stable operation of the Turbec T100 was observed in all cases the OH*-chemiluminescence and the OH-PLIF measurements showed different flame behaviour depending on high and low hydrogen contents
Summary
Micro gas turbines (MGT) constitute an upcoming technology in the field of decentralized combined heat and power (CHP) production [1]. It offers various advantages such as low maintenance requirements, low vibrations, high fuelflexibility as well as low emissions [2]. The combustors of most commercial MGTs are designed for conventional fuels like natural gas, which exhibit high calorific values. The FLOX®-combustor, which was designed for LCV fuels and successfully operated in the micro gas turbine by Zornek et al [5], was implemented into an optical accessible combustion chamber in order to analyse the influence of the hydrogen contained in the fuel. An exhaust gas analysis system delivered the concentrations of pollutant emissions and information about combustion efficiency
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Disclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.