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Comparison of Three-phase Active Rectifier Solutions for Avionic Applications: Impact of the Avionic Standard DO-160 F and Failure Modes
Citation
Borovic, Uros, Zhao, Sisi, Silva Fernández, Marcelo Alexis, Bouvier Rescalvo, Yann, Vasic, Miroslav 
ORCID: https://orcid.org/0000-0001-9597-6409, Oliver Ramírez, Jesús Angel ORCID: https://orcid.org/0000-0002-5286-5378, Alou Cervera, Pedro ORCID: https://orcid.org/0000-0002-2985-1330, Cobos Marquez, Jose Antonio ORCID: https://orcid.org/0000-0003-4542-2656, Arévalo, F., García-Tembleque, J. C., Carmena, J., García, C. and Pejovic, P.
(2016).
Comparison of Three-phase Active Rectifier Solutions for Avionic Applications: Impact of the Avionic Standard DO-160 F and Failure Modes.
In: "2016 IEEE Energy Conversion Congress and Exposition (ECCE)", Sept. 18–22, 2016, Milwaukee, WI. pp. 1-8.
https://doi.org/10.1109/ECCE.2016.7854943.
Description
| Title: | Comparison of Three-phase Active Rectifier Solutions for Avionic Applications: Impact of the Avionic Standard DO-160 F and Failure Modes |
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| Author/s: |
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| Item Type: | Presentation at Congress or Conference (Article) |
| Event Title: | 2016 IEEE Energy Conversion Congress and Exposition (ECCE) |
| Event Dates: | Sept. 18–22, 2016 |
| Event Location: | Milwaukee, WI |
| Title of Book: | 2016 IEEE Energy Conversion Congress and Exposition (ECCE) Proceedings |
| Date: | 2016 |
| Subjects: | |
| Faculty: | E.T.S.I. Industriales (UPM) |
| Department: | Automática, Ingeniería Eléctrica y Electrónica e Informática Industrial |
| Creative Commons Licenses: | Recognition - No derivative works - Non commercial |
Abstract
In aircraft applications, there has been an increasing trend related with the More Electric Aircraft (MEA), which results in rapid rise in the electrical power demand on-board. One of its goals lies in minimizing weight and volume of the electrical subsystem while maintaining good power quality and efficiency. The main purpose of this paper is to present and analyze an electrical design of a three-phase Boost rectifier, a three-phase Buck rectifier and a three-phase Vienna rectifier for output power level of 10 kW and compare them in terms of weight, volume, efficiency etc. Moreover, the design is obliged to comply with specific sections of DO-160 standard for avionic equipment with 230 VAC, 360-800 Hz grid conditions. Even though all proposed solutions satisfy the standard requirements, it will be shown that the Vienna rectifier has the lowest volume and not considering failure modes, the better solution overall. However, due to increased number of semiconductors and additional circuitry required for soft start-up, the Buck rectifier would prove to be the more robust solution failure-wise.
More information
| Item ID: | 46881 |
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| DC Identifier: | https://oa.upm.es/46881/ |
| OAI Identifier: | oai:oa.upm.es:46881 |
| DOI: | 10.1109/ECCE.2016.7854943 |
| Official URL: | http://ieeexplore.ieee.org/document/7854943/ |
| Deposited by: | Memoria Investigacion |
| Deposited on: | 20 Jun 2017 16:19 |
| Last Modified: | 20 Jun 2017 16:19 |
