[HTML][HTML] High temperature superconducting rotating electrical machines: An overview

CCT Chow, MD Ainslie, KT Chau - Energy Reports, 2023 - Elsevier
Superconducting rotating machines are more efficient, smaller and lighter than conventional
ones. Thus, they can reduce energy consumption and can be an enabling technology in …

[HTML][HTML] A review of liquid hydrogen aircraft and propulsion technologies

S Tiwari, MJ Pekris, JJ Doherty - International Journal of Hydrogen Energy, 2024 - Elsevier
Sustainable aviation is a key part of achieving Net Zero by 2050, and is arguably one of the
most challenging sectors to decarbonise. Hydrogen has gained unprecedented attention as …

[HTML][HTML] Thermal management challenges in hybrid-electric propulsion aircraft

M Asli, P König, D Sharma, E Pontika, J Huete… - Progress in Aerospace …, 2024 - Elsevier
The utilization of hybrid electric propulsion concept in aviation offers a viable solution to
address the limitations posed by the relatively low energy density of batteries in fully electric …

Challenges for developing high temperature superconducting ring magnets for rotating electric machine applications in future electric aircrafts

M Yazdani-Asrami, M Zhang, W Yuan - Journal of Magnetism and Magnetic …, 2021 - Elsevier
One of the most promising applications for high temperature superconducting (HTS) material
is magnet. HTS magnet is considered to be used in a wide range of applications including …

Experimental evaluation of 1 kW-class prototype REBCO fully superconducting synchronous motor cooled by subcooled liquid nitrogen for E-aircraft

H Sasa, M Iwakuma, K Yoshida, S Sato… - IEEE Transactions …, 2021 - ieeexplore.ieee.org
For the development of electric propulsion aircrafts with light weight, low emission and high
efficiency, MW-class fully superconducting synchronous machines operating at liquid …

Impact of LH2 Fuel Cell-Electric Propulsion on Aircraft Configuration and Integration

E Waddington, JM Merret, PJ Ansell - AIAA Aviation 2021 Forum, 2021 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2021-2409. vid This study considers the
aircraft configuration impact of a liquid hydrogen/fuel cell electric propulsion system when …

Impact of liquid-hydrogen fuel-cell electric propulsion on aircraft configuration and integration

E Waddington, JM Merret, PJ Ansell - Journal of Aircraft, 2023 - arc.aiaa.org
This study considers the aircraft configuration impacts of a liquid-hydrogen fuel-cell electric
propulsion system when integrated into a single-aisle, transport-class aircraft having …

A Double Rotor Flux Switching Machine With HTS Field Coils for All Electric Aircraft Applications

S Saeidabadi, L Parsa, K Corzine… - IEEE Transactions …, 2023 - ieeexplore.ieee.org
The increasing demand for high-power density motors in electric transport industries opens
a new research opportunity to develop motor topologies with less weight and high efficiency …

Conceptual design of distributed electrified boundary layer ingesting propulsors for the cheeta aircraft concept

D Chandel, JD Reband, DK Hall… - 2021 AIAA/IEEE …, 2021 - ieeexplore.ieee.org
This paper describes the conceptual design of a boundary layer ingesting, distributed
electric propulsor system for civil aircraft, supported through NASA's CHEETA (Center for …

Electromagnetic-thermal coupled analysis considering AC losses in REBCO windings of 10 MW fully superconducting synchronous generators cooled by subcooled …

H Sasa, S Miura, H Miyazaki… - IEEE Transactions …, 2022 - ieeexplore.ieee.org
A large AC loss is generated in armature windings composed of a REBa 2 Cu 3 O y
(REBCO, RE= rare earth, Eu, Gd, etc.) wire in a fully superconducting synchronous …