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Author | dc.contributor.author | Ahumada, Constanza | |
Author | dc.contributor.author | Wheeler, Pat | |
Admission date | dc.date.accessioned | 2019-10-11T17:30:10Z | |
Available date | dc.date.available | 2019-10-11T17:30:10Z | |
Publication date | dc.date.issued | 2019 | |
Cita de ítem | dc.identifier.citation | IET Electric Power Applications, Volumen 13, Issue 7, 2019, Pages 1061-1070 | |
Identifier | dc.identifier.issn | 17518679 | |
Identifier | dc.identifier.issn | 17518660 | |
Identifier | dc.identifier.other | 10.1049/iet-epa.2019.0122 | |
Identifier | dc.identifier.uri | https://repositorio.uchile.cl/handle/2250/171273 | |
Abstract | dc.description.abstract | © 2019 Institution of Engineering and Technology. All rights reserved.Rotational systems such as aircraft engine drivetrains are subject to vibrations that can damage shafts. Torsional vibrations in drivetrains can be excited by the connection of loads to the generator due to electromechanical interaction. This problem is particularly relevant in new aircraft because the drivetrain is flexible and the electrical power system (EPS) load is high. To extend the lifespan of the aircraft engine, the electromechanical interaction must be considered. Since real-time constants of the electrical and mechanical systems have very different magnitudes, the simulation time can be high. Furthermore, highly detailed models of the electrical system have unnecessary complexity for the study of electromechanical interactions. For these reasons, modelling using reduced order systems is fundamental. Past studies of electromechanical interaction in aircraft engines developed models that allow the analysis | |
Lenguage | dc.language.iso | en | |
Publisher | dc.publisher | Institution of Engineering and Technology | |
Type of license | dc.rights | Attribution-NonCommercial-NoDerivs 3.0 Chile | |
Link to License | dc.rights.uri | http://creativecommons.org/licenses/by-nc-nd/3.0/cl/ | |
Source | dc.source | IET Electric Power Applications | |
Keywords | dc.subject | Electrical and Electronic Engineering | |
Título | dc.title | Modelling of reduced electromechanical interaction system for aircraft applications | |
Document type | dc.type | Artículo de revista | |
dcterms.accessRights | dcterms.accessRights | Acceso Abierto | |
Cataloguer | uchile.catalogador | SCOPUS | |
Indexation | uchile.index | Artículo de publicación SCOPUS | |
uchile.cosecha | uchile.cosecha | SI | |
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