A LOW-IMPACT HIGH-EFFICIENCY BRAYTON CYCLE CONCEPT WITH EVAPORATIVE COOLING DURING THE COMPRESSION PROCESS USING H2/CH4 FUEL BLENDS
DOI:
https://doi.org/10.59277/CLC.2024.37Keywords:
Evaporative cooling, Hydrogen, Brayton cycle, Entropy generation, Constructal LawAbstract
Towards a low-impact, high-efficiency Brayton cycle concept, a gas generator system including a compressor with evaporative cooling, a combustion chamber using H2/CH4 fuel blends, and a gas turbine is being analyzed at this preliminary stage. The Constructal approach on the effectiveness of compressed air temperature control by evaporative cooling, previously carried out by the authors, shed some light on the potential growth of mechanical power provided by gas turbine power plants of 45.81% and a simultaneous reduction of 2.26% in specific fuel consumption.
The current study carried out on the combustion chamber reveals that increasing the H2 fraction in the fuel blend results in a direct reduction in carbon dioxide production and a decrease in CO and NOx emissions when the temperature of the flue gas is maintained at 1450 K. Meanwhile, the exergy efficiency of the combustion chamber remains almost constant at 39.3%. Studying the two components already analyzed, the compressor and the combustion chamber, allows us to move towards a low-impact, high-efficiency Brayton cycle concept as close as possible to its technical implementation.
References
(1) Barigozzi G. et al., Techno-economic analysis of gas turbine inlet air cooling for combined cycle power plant for different climatic conditions, Applied Thermal Engineering, 82, 57–67 (2015).
(2) Ibrahim M. A., Varnham A., A review of inlet air-cooling technologies for enhancing the performance of combustion turbines in Saudi Arabia, Applied Thermal Engineering, 30, 1879–1888 (2010).
(3) Bhargava et al., Gas turbine compressor performance characteristics during wet compression – influence of polydisperse spray, Proceedings of ASME Turbo Expo 2009: Power for Land, Sea and Air (GT2009), June 8–12, 2009, Orlando, FL USA.
(4) Stanescu G., Ene B., Vilag V., Andreescu T., Constructal approach on the feasibility of compressed air temperature control by evaporative cooling in gas turbine power plants, Proceedings of the Romanian Academy, Series A, Special Issue,/ 2018, pp. 201–206
(5) Gordon S. and McBride B.J., Computer Program for Calculation of Complex Chemical Equilibrium Compositions and Applications, NASA Reference Publication, 1311, 1996.
(6) Barbu E. et al., The influence of inlet air cooling and afterburning on gas turbine cogeneration groups performance, Gas Turbines – Materials, Modeling and Performance, Dr. Gurrappa Injeti (Ed.), InTech, 2015.
(7) Stanescu G., Barbu E., Vilag V. and Vilag J., Achieving Temperature Control by Direct Injection of Liquid Water in Axial Compressors of “in-service” Gas Turbine Engines, Proceedings of the 16th International Conference on Heat Transfer, Fluid Mechanics and Thermodynamics, 2022.
(8) Lopez-Ruiz G., Castresana-Larrauri J., Blanco Ilzarbe, J.M, Thermodynamic Analysis of a Regenerative Brayton Cycle Using H2, CH4 and H2/CH4 Blends as Fuel, Energies, 15, p. 1508 (2022), https://doi.org/10.3390/en15041508
(9) Petrescu S. et al., Advanced Thermodynamics of Irreversible Processes with Finite Speed and Finite Dimensions, Edit. AGIR, 2015.