Energy-Exergy Analysis and Optimal Design of a Hydrogen Turbofan Engine
Mohammadreza Sabzehali, Somayeh Davoodabadi Farahani, Amir Mosavi

TL;DR
This paper analyzes the impact of inlet air cooling and fuel type on a jet engine's performance and optimizes its cycle using genetic algorithms and TOPSIS for economic and environmental benefits.
Contribution
It introduces a comprehensive energy-exergy analysis and applies multi-objective optimization to improve engine performance with hydrogen fuel and inlet cooling.
Findings
Inlet air cooling improves thermal efficiency and reduces emissions.
Hydrogen fuel cycle optimization enhances environmental performance.
Optimal engine cycle varies based on economic and environmental criteria.
Abstract
In this study, the effect of inlet air cooling and fuel type on the performance parameters of thrust-specific fuel consumption (TSFC), thermal and exergetic efficiencies, entropy generation rate, and Nitrogen oxide emission intensity index (SNOx) of the GENX 1B70 engine is analyzed in two states of take-off and on design. The results show that with a 20-degree delicious reduction in inlet air temperature on design conditions and JP10 fuel usage, the thermal efficiency and entropy generation rate, thrust and fuel mass flow rate, and TSFC of the engine increase by 1.85 percent, 16.51 percent, 11.76 percent, 10.53 percent, and 2.15 percent and SNOx and exergetic efficiency decrease by 2.11 percent and 26.60 percent, respectively. Also, optimization of the GENX 1B70 engine cycle as hydrogen fuel usage with three separate objective functions: thrust maximization, thermal efficiency…
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Taxonomy
MethodsBalanced Selection
