High-power density electric motors for regional aircraft propulsion.
This Master's thesis project aims, firstly, to evaluate the current state of the art in aeronautical propulsion technology using electric machines. Once the state of the art has been studied, a tool for the design and calculation of electric motors with superconducting windings is developed i...
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Format: | info:eu-repo/semantics/masterThesis |
Language: | eng |
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Servicio de Publicaciones. Universidad de Navarra
2021
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Online Access: | https://hdl.handle.net/10171/61869 |
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author | Alvarez-Santos, P. (Pablo) Satrústegui-de-Legarra, M. (Marco) |
author_facet | Alvarez-Santos, P. (Pablo) Satrústegui-de-Legarra, M. (Marco) |
author_sort | Alvarez-Santos, P. (Pablo) |
collection | DSpace |
description | This Master's thesis project aims, firstly, to evaluate the current state of the art in aeronautical
propulsion technology using electric machines. Once the state of the art has been studied, a tool
for the design and calculation of electric motors with superconducting windings is developed in
order to present a pre-design that meets the established objectives.
The analysis carried out on the state of the art will provide information on the design guidelines
that have been taken in recent years, as well as the different projects and studies that are
planned for the medium-term future. Thanks to this framework, geometric and performance
requirements of the motor are defined together with the objectives to be met.
In order to achieve this goal, a superconducting motor design module is implemented in Matlab
and FEMM, which helps to develop the selected motor efficiently, rapidly and accurately. The
IPED electric machine design tool is described, and the different stages in the calculation of the
motor are explained in detail.
Finally, the conclusions drawn from the different chapters are summarised, which will serve as
a guideline for the continuation of the HIVOMOT project, in which this Master's thesis is framed. |
format | info:eu-repo/semantics/masterThesis |
id | oai:dadun.unav.edu:10171-61869 |
institution | Universidad de Navarra |
language | eng |
publishDate | 2021 |
publisher | Servicio de Publicaciones. Universidad de Navarra |
record_format | dspace |
spelling | oai:dadun.unav.edu:10171-618692023-02-09T11:11:20Z High-power density electric motors for regional aircraft propulsion. Alvarez-Santos, P. (Pablo) Satrústegui-de-Legarra, M. (Marco) Electric motor. High voltage. Aeronautics. High-temperature superconductors. High power. This Master's thesis project aims, firstly, to evaluate the current state of the art in aeronautical propulsion technology using electric machines. Once the state of the art has been studied, a tool for the design and calculation of electric motors with superconducting windings is developed in order to present a pre-design that meets the established objectives. The analysis carried out on the state of the art will provide information on the design guidelines that have been taken in recent years, as well as the different projects and studies that are planned for the medium-term future. Thanks to this framework, geometric and performance requirements of the motor are defined together with the objectives to be met. In order to achieve this goal, a superconducting motor design module is implemented in Matlab and FEMM, which helps to develop the selected motor efficiently, rapidly and accurately. The IPED electric machine design tool is described, and the different stages in the calculation of the motor are explained in detail. Finally, the conclusions drawn from the different chapters are summarised, which will serve as a guideline for the continuation of the HIVOMOT project, in which this Master's thesis is framed. El presente proyecto de fin de Máster trata, en primer lugar, de realizar una evaluación sobre el estado actual de la tecnología de la propulsión aeronáutica mediante máquinas eléctricas. Una vez estudiado el estado del arte, se desarrolla una herramienta de diseño y cálculo de motores eléctricos con devanados superconductores con el fin de presentar un prediseño que cumpla con los objetivos establecidos. El análisis realizado sobre el estado de la tecnología permitirá conocer las líneas de diseño que se han tomado en los últimos años, así como los diferentes proyectos y estudios que están previstos en un futuro a medio plazo. Gracias a este marco de trabajo se definen unos requerimientos geométricos y de prestaciones del motor junto con unos objetivos a cumplir. Para poder alcanzar esta meta se implementa un módulo de diseño de motores superconductores en Matlab y FEMM que ayuda a desarrollar el motor seleccionado de forma eficaz, rápida y precisa. Se describe la herramienta de diseño de máquinas eléctricas IPED, y se explica de forma detallada las diferentes etapas en el cálculo del motor. Por último, se resumen las conclusiones extrapoladas en los diferentes capítulos y que servirán como pauta de cara a la continuación del proyecto HIVOMOT, en el que se encuentra enmarcado este proyecto de Fin de Máster. 2021-08-30T08:02:58Z 2021-08-30T08:02:58Z 2021-08-30 2021-05 info:eu-repo/semantics/masterThesis https://hdl.handle.net/10171/61869 eng info:eu-repo/semantics/openAccess application/pdf Servicio de Publicaciones. Universidad de Navarra |
spellingShingle | Electric motor. High voltage. Aeronautics. High-temperature superconductors. High power. Alvarez-Santos, P. (Pablo) Satrústegui-de-Legarra, M. (Marco) High-power density electric motors for regional aircraft propulsion. |
title | High-power density electric motors for regional aircraft propulsion. |
title_full | High-power density electric motors for regional aircraft propulsion. |
title_fullStr | High-power density electric motors for regional aircraft propulsion. |
title_full_unstemmed | High-power density electric motors for regional aircraft propulsion. |
title_short | High-power density electric motors for regional aircraft propulsion. |
title_sort | high-power density electric motors for regional aircraft propulsion. |
topic | Electric motor. High voltage. Aeronautics. High-temperature superconductors. High power. |
url | https://hdl.handle.net/10171/61869 |
work_keys_str_mv | AT alvarezsantosppablo highpowerdensityelectricmotorsforregionalaircraftpropulsion AT satrusteguidelegarrammarco highpowerdensityelectricmotorsforregionalaircraftpropulsion |