My Account Log in

2 options

System-level modeling of the powertrain for an electric aircraft with superconducting components/ Ali Khonya.

DOAB Directory of Open Access Books Available online

View online

OAPEN Available online

View online
Format:
Book
Author/Creator:
Khonya, Ali, author.
Series:
Karlsruher Schriftenreihe zur Supraleitung 39.
Language:
English
Subjects (All):
Electric airplanes--Power supply.
Electric airplanes.
Superconductivity--Technological innovations.
Superconductivity.
Fuel cells--Applications.
Fuel cells.
Hydrogen as fuel--Environmental aspects.
Hydrogen as fuel.
Physical Description:
1 online resource
Place of Publication:
Karlsruhe : KIT Scientific Publishing, 2025.
Summary:
Aviation accounts for approximately 2.4% of global annual carbon emissions, and with an expected passenger traffic growth of 3.6–3.8% per year, CO₂ emissions could double by 2050 without additional mitigation measures. To address this challenge, initiatives such as the EU Flightpath 2050 project promote carbon-free aviation through alternative energy solutions. Among these, sustainable aviation fuel and hydrogen are the most viable options. Liquid hydrogen (LH₂) is particularly attractive due to its high gravimetric energy density, nearly three times that of conventional jet fuel. When used in fuel cell–based electric aircraft, hydrogen offers higher efficiency, quieter operation, and eliminates emissions such as CO₂, NOₓ, and SO₂. As a result, major aerospace companies are exploring fully electric and hybrid-electric aircraft concepts. This work focuses on a fully electric aircraft powered by proton exchange membrane fuel cells (PEMFCs).High power requirements significantly increase system weight, especially hydrogen storage. Therefore, lightweight and efficient powertrain components are essential. Superconducting technologies offer reduced weight, higher efficiency, and compact power transmission, making them promising for aviation electrification. This study presents a MATLAB/Simulink model of a superconducting fuel cell–based electric aircraft powertrain, enabling system-level simulations under various flight scenarios. The proposed fuel cell model captures nonlinear voltage–current behavior and accurately represents resistive, inductive, or combined transient dynamics.
Contents:
Acknowledgments Kurzfassung Abstract List of Figures List of Tables List of Acronyms List of Symbols Introduction Fuel Cell Resistive Superconducting Fault Current Limiter Superconducting Cable Superconducting Motor with DC/AC Inverter Complete Powertrain Simulation Summary, Conclusions, and Outlook Bibliography Appendices.
Notes:
Includes bibliographical references (pages) and index.
Part of the metadata in this record was created with the help of AI Metadata Assistant

The Penn Libraries is committed to describing library materials using current, accurate, and responsible language. If you discover outdated or inaccurate language, please fill out this feedback form to report it and suggest alternative language.

Find

Home Release notes

My Account

Shelf Request an item Bookmarks Fines and fees Settings

Guides

Using the Find catalog Using Articles+ Using your account