Preliminary sizing methodologies for regional aircraft with liquid hydrogen fuel and SOFC-GT-Battery hybrid-electric powertrains

Solid Oxide Fuel Cell (SOFC) systems for aviation applications have been considered for their use as APUs or powertrains, as standalone systems or in combination with gas turbines, and both fueled by reformed Jet-A or by hydrogen. Most existing studies focus on powertrain performance modelling. In this work, traditional tube-and-wing regional...

Efficient Modeling of Hybrid-Electric Aircraft for Design and Performance Optimization Studies

The world is faced with two concurrent trends. The first is the growing demand for air travel in the long term. The second is the need to cut aircraft emissions due to environmental goals and ambitions set by authorities. Fully-electric aircraft are currently infeasible due to the limited battery specific energy and power. Hybrid-electric...

A coupled propulsion and thermal management system for hybrid electric aircraft design: A case study

Air transport is facing an important challenge when it comes to the reduction of its environmental footprint. Hybrid electric aircraft offer a potential solution to reduce in-flight emissions. The essence of hybrid electric aircraft is to combine multiple energy sources and energy conversion systems, in order to improve the overall energy...

Redesign of a Hybrid Electric General Aviation Aircraft: A case study

The aviation sector and its associated activities contribute to climate change, damage to the environment, community noise, and local air pollution. As a consequence it affects the health and quality of life of citizens that live close to airports, and through climate change every person on earth. To reduce the impact of air travel and thereby...