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Journal ArticleDOI

HTS machines as enabling technology for all-electric airborne vehicles

TLDR
This paper investigates the feasibility of all-electric aircraft based on currently available technology by investigating the development of high power density superconducting motors for aircraft propulsion and fuel cell based power systems for aircraft.
Abstract
Environmental protection has now become paramount as evidence mounts to support the thesis of human activity-driven global warming. A global reduction of the emissions of pollutants into the atmosphere is therefore needed and new technologies have to be considered. A large part of the emissions come from transportation vehicles, including cars, trucks and airplanes, due to the nature of their combustion-based propulsion systems. Our team has been working for several years on the development of high power density superconducting motors for aircraft propulsion and fuel cell based power systems for aircraft. This paper investigates the feasibility of all-electric aircraft based on currently available technology. Electric propulsion would require the development of high power density electric propulsion motors, generators, power management and distribution systems. The requirements in terms of weight and volume of these components cannot be achieved with conventional technologies; however, the use of superconductors associated with hydrogen-based power plants makes possible the design of a reasonably light power system and would therefore enable the development of all-electric aero-vehicles. A system sizing has been performed both for actuators and for primary propulsion. Many advantages would come from electrical propulsion such as better controllability of the propulsion, higher efficiency, higher availability and less maintenance needs. Superconducting machines may very well be the enabling technology for all-electric aircraft development.

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Citations
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Journal ArticleDOI

Next Generation More-Electric Aircraft: A Potential Application for HTS Superconductors

TL;DR: In this paper, the main issues involved in using superconductors for aeropropulsion are discussed. And the feasibility of superconducting electric propulsion is investigated for turbo-electric aircraft of the future.

Turboelectric Distributed Propulsion Engine Cycle Analysis for Hybrid-Wing-Body Aircraft

TL;DR: In this paper, a propulsion system which transmits power from the turbine to the fan electrically rather than mechanically was presented, and the performance of the fan inlet was evaluated.
Journal ArticleDOI

Modelling of bulk superconductor magnetization

TL;DR: In this paper, the authors present a topical review of the current state of the art in modelling the magnetization of bulk superconductors, including both (RE)BCO (where RE?=?rare earth or Y) and MgB2 materials.
Proceedings ArticleDOI

Turboelectric Distributed Propulsion Engine Cycle Analysis for Hybrid-Wing-Body Aircraft

TL;DR: In this article, a propulsion system which transmits power from the turbine to the fan electrically rather than mechanically was presented, and the performance of the fan inlet was evaluated.
Journal ArticleDOI

Overview of H -Formulation: A Versatile Tool for Modeling Electromagnetics in High-Temperature Superconductor Applications

TL;DR: The basics of the finite-element method (FEM) based on theinline-formula, its evolution from 2D to 3D, its application for calculating critical currents and AC losses as well as magnetization of HTS bulks and tape stacks, and its application to study the dynamic resistance of superconductors and flux pumps are reviewed.
References
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Journal ArticleDOI

High power density superconducting motor for all-electric aircraft propulsion

TL;DR: A preliminary electromagnetic design of a 200 HP high temperature superconducting motor optimized in terms of power density targets the Cessna 172 propulsion requirements that are 200 HP at 2700 RPM.
Journal ArticleDOI

HTS motors in aircraft propulsion: design considerations

TL;DR: In this paper, a specific sizing model of superconducting propulsion motors for aircraft design is presented, and the requirements for this application are presented in terms of power and dynamics as well as a load profile corresponding to a typical mission.
Journal ArticleDOI

A novel approach to power quality assessment: real time hardware-in-the-loop test bed

TL;DR: In this paper, a real-time hardware-in-the-loop (RT-HIL) platform is used for power quality assessment of all-electric ships in the US Navy.
Journal ArticleDOI

Design and Testing of a Superconducting Rotating Machine

TL;DR: In this article, an eight-pole superconducting rotating machine was designed, constructed and tested based on an unconventional topology that could potentially lead to a significant increase in power density.
Journal ArticleDOI

Improving performance of cryogenic power electronics

TL;DR: This paper aims to review the present status of CPE and to provide an outlook on emerging device technologies that are gaining in interest and advanced power electronic packaging/interconnect methods that adapt well to cryogenics and help further improve system performance is discussed.
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