Power Balance of a Hybrid Power Source in a Power Plant for a Small Propulsion Aircraft

Bataller Planes, Elena and Lapena Rey, Nieves and Mosquera, Jonay and Ortí, Fortunato and Oliver Ramírez, Jesús Angel and García Suárez, Oscar and Moreno González, Félix Antonio and Portilla Berrueco, Jorge and Torroja Fungairiño, Yago and Vasic, Miroslav and Huerta Oliveres, Santa Concepción and Trocki, M. and Zumel Vaquero, Pablo and Cobos Márquez, José Antonio (2008). Power Balance of a Hybrid Power Source in a Power Plant for a Small Propulsion Aircraft. In: "IEEE Power Electronics Specialists Conference (PESC)", 15/06/2008-19/06/2008, Rodas (Grecia). ISBN 978-14-2441-668-4. pp. 704-710.

Description

Title: Power Balance of a Hybrid Power Source in a Power Plant for a Small Propulsion Aircraft
Author/s:
  • Bataller Planes, Elena
  • Lapena Rey, Nieves
  • Mosquera, Jonay
  • Ortí, Fortunato
  • Oliver Ramírez, Jesús Angel
  • García Suárez, Oscar
  • Moreno González, Félix Antonio
  • Portilla Berrueco, Jorge
  • Torroja Fungairiño, Yago
  • Vasic, Miroslav
  • Huerta Oliveres, Santa Concepción
  • Trocki, M.
  • Zumel Vaquero, Pablo
  • Cobos Márquez, José Antonio
Contributor/s:
  • Ortí, F.
  • Mosquera, J.
  • Trocki, M.
  • Lapena, N.
  • Zumel, P.
Item Type: Presentation at Congress or Conference (Article)
Event Title: IEEE Power Electronics Specialists Conference (PESC)
Event Dates: 15/06/2008-19/06/2008
Event Location: Rodas (Grecia)
Title of Book: Power Electronics Specialists Conference, 2008. PESC 2008. IEEE
Date: 2008
ISBN: 978-14-2441-668-4
Subjects:
Faculty: E.T.S.I. Industriales (UPM)
Department: Automática, Ingeniería Electrónica e Informática Industrial [hasta 2014]
Creative Commons Licenses: Recognition - No derivative works - Non commercial

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Abstract

This paper analyzes two different architectures for a hybrid power source comprising a PEM (Polymer Electrolyte Membrane) fuel cell and a Li ion battery. The hybrid power source feeds the propulsion motor of an all electrical aircraft, the Boeing Fuel Cell Demonstrator. The architectures are an unregulated and a regulated hybrid power source. The regulation is achieved by means of a controllable series boost converter (SBC) connected in series with the fuel cell. Both architectures have been simulated, implemented and tested in the Boeing Fuel Cell Demonstrator Airplane.

More information

Item ID: 3434
DC Identifier: http://oa.upm.es/3434/
OAI Identifier: oai:oa.upm.es:3434
Official URL: http://ieeexplore.ieee.org/xpl/mostRecentIssue.jsp?punumber=4578427
Deposited by: Memoria Investigacion
Deposited on: 28 Jun 2010 09:00
Last Modified: 23 Feb 2017 17:47
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