HTS Cable Design for Aircraft Application Considering Fault Conditions
Author:
Affiliation:
1. Graduate School of Frontier Sciences, University of Tokyo, Chiba, Japan
Funder
JST SPRING
Publisher
Institute of Electrical and Electronics Engineers (IEEE)
Link
http://xplorestaging.ieee.org/ielx7/77/10339679/10411069.pdf?arnumber=10411069
Reference13 articles.
1. Lightweight Design of Fully Superconducting Motors for Electrical Aircraft Propulsion Systems
2. An open-source 2D finite difference based transient electro-thermal simulation model for three-phase concentric superconducting power cables
3. High-temperature superconducting tri-axial power cable
4. AmpaCity — Installation of advanced superconducting 10 kV system in city center replaces conventional 110 kV cables
5. Investigation of HTS cable impact on turbo‐electric aircraft performance
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