Comparison of Three-phase Active Rectifier Solutions for Avionic Applications: Impact of the Avionic Standard DO-160 F and Failure Modes

Borovic, Uros; Zhao, Sisi; Silva Fernández, Marcelo Alexis; Bouvier Rescalvo, Yann; Vasic, Miroslav; Oliver Ramírez, Jesús Angel; Alou Cervera, Pedro; Cobos Marquez, Jose Antonio; Arévalo, F.; García-Tembleque, J. C.; Carmena, J.; García, C. y Pejovic, P. (2016). Comparison of Three-phase Active Rectifier Solutions for Avionic Applications: Impact of the Avionic Standard DO-160 F and Failure Modes. En: "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.

Descripción

Título: Comparison of Three-phase Active Rectifier Solutions for Avionic Applications: Impact of the Avionic Standard DO-160 F and Failure Modes
Autor/es:
  • Borovic, Uros
  • Zhao, Sisi
  • Silva Fernández, Marcelo Alexis
  • Bouvier Rescalvo, Yann
  • Vasic, Miroslav
  • Oliver Ramírez, Jesús Angel
  • Alou Cervera, Pedro
  • Cobos Marquez, Jose Antonio
  • Arévalo, F.
  • García-Tembleque, J. C.
  • Carmena, J.
  • García, C.
  • Pejovic, P.
Tipo de Documento: Ponencia en Congreso o Jornada (Artículo)
Título del Evento: 2016 IEEE Energy Conversion Congress and Exposition (ECCE)
Fechas del Evento: Sept. 18–22, 2016
Lugar del Evento: Milwaukee, WI
Título del Libro: 2016 IEEE Energy Conversion Congress and Exposition (ECCE) Proceedings
Fecha: 2016
Materias:
Escuela: E.T.S.I. Industriales (UPM)
Departamento: Automática, Ingeniería Eléctrica y Electrónica e Informática Industrial
Licencias Creative Commons: Reconocimiento - Sin obra derivada - No comercial

Texto completo

[img]
Vista Previa
PDF (Document Portable Format) - Se necesita un visor de ficheros PDF, como GSview, Xpdf o Adobe Acrobat Reader
Descargar (1MB) | Vista Previa

Resumen

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.

Más información

ID de Registro: 46881
Identificador DC: http://oa.upm.es/46881/
Identificador OAI: oai:oa.upm.es:46881
Identificador DOI: 10.1109/ECCE.2016.7854943
URL Oficial: http://ieeexplore.ieee.org/document/7854943/
Depositado por: Memoria Investigacion
Depositado el: 20 Jun 2017 16:19
Ultima Modificación: 20 Jun 2017 16:19
  • Open Access
  • Open Access
  • Sherpa-Romeo
    Compruebe si la revista anglosajona en la que ha publicado un artículo permite también su publicación en abierto.
  • Dulcinea
    Compruebe si la revista española en la que ha publicado un artículo permite también su publicación en abierto.
  • Recolecta
  • e-ciencia
  • Observatorio I+D+i UPM
  • OpenCourseWare UPM