Webinars
Upcoming
Tuesday, September 15, 11 am CST (Click to Join)
by Ethan Pesterfield, PhD Student, Tennessee Tech University, ecpesterfi42@tntech.edu
Commercial aviation currently accounts for approximately 3% of global carbon emissions, a share that is expected to increase as air travel continues to grow. Solid Oxide Fuel Cell–Gas Turbine (SOFC-GT) hybrid systems offer a promising alternative propulsion technology for reducing aviation emissions through increased energy-conversion efficiency. Computational studies have predicted overall system efficiencies approaching 70%, potentially reducing fuel consumption and operating costs for commercial aviation. However, experimental validation under simulated flight-relevant conditions is necessary before SOFC-GT systems can be considered for aircraft applications.
This work presents the development and commissioning of the Electrochemical And Gas-turbine Laboratory for Energy (EAGLE Lab), a demonstration-scale facility designed to investigate fuel cell–gas turbine hybrid systems by coupling a SOFC bundle with a micro gas turbine. The current status of the facility, recent updates, and planned future capabilities will be presented. Experimental data generated by the EAGLE Lab will support the refinement and validation of computational models, evaluation of system-level control strategies, and characterization of overall hybrid-system performance under representative operating conditions.
Archived
A CFD–LES Framework for Simulating Contrail Formation from Ammonia Aviation Fuels
Aerodynamic Study of Boeing 737-800 and Truss-Braced Wing Aircrafts Using CFD Techniques
A Comprehensive Optimizer for Multi-Objective and Multidisciplinary Applications
Axial Fan Optimization for High-Bypass SOFC-C-GT Hybrid System
An Exploration of Ammonia NOx Emissions Using CFD
Tennessee Tech
University’s Pressurized SOFC Test Stand Updates and Progress Through 2024
Investigation of Ammonia Fed SOFCC-GT Hybrid System for Commercial Aviation
Design and Manufacture of an Anode Ejector to Boost System Efficiency of a 1kW SOFC
Zero/Low Emission Commercial Aircraft Powered by Solid Oxide Fuel Cell Turbogenerator Hybrid
Design and Operation of Solid Oxide Electrochemical Cell Systems for Space Applications
SWaP Analysis and Optimization for SOFC-C Hybrid System for Commercial Aviation
Modeling of a SOFC Combustor Hybrid Cycle for Commercial Electric Aviation