The aviation industry has been challenged to increase the sustainability of its technologies, which is the main driving force in research and exploration of fully electrified propulsion. This paper presents the initial steps in the design and modeling of the Cryogenic High-Eﬃciency Electrical Technologies for Aircraft (CHEETA) that would form the basis for hybrid-electric aircraft power systems. To this end, different power system configurations for fully electrified propulsion are proposed and analyzed. Novel, multi-domain components used in both the power system model and the cryogenic thermal system model are introduced and explained in detail. This paper also presents initial results for the different power system configurations under steady-state conditions.
|Original language||English (US)|
|Title of host publication||AIAA Propulsion and Energy 2020 Forum|
|Publisher||American Institute of Aeronautics and Astronautics|
|State||Published - Aug 17 2020|
Bibliographical noteKAUST Repository Item: Exported on 2022-06-30
Acknowledged KAUST grant number(s): OSR-2019-CoE-NEOM-4178.12
Acknowledgements: This work was supported in part by NASA under award number 80NSSC19M0125 as part of the Center for High-Efficiency Electrical Technologies for Aircraft (CHEETA), by the Engineering Research Center Program of the National Science Foundation and the Department of Energy under Award EEC-1041877, by the CURENT Industry Partnership Program, and by the Center of Excellence for NEOM Research at the King Abdullah University of Science and Technology under grant OSR-2019-CoE-NEOM-4178.12. The first author is supported through a Rensselaer Graduate Fellowship and through the National Science Foundation through a Graduate Research Fellowship.
This publication acknowledges KAUST support, but has no KAUST affiliated authors.