Moving towards a more electric aircraft

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dc.contributor	Universitat Politècnica de Catalunya. Departament d'Enginyeria Electrònica
dc.contributor	Universitat Politècnica de Catalunya. Departament d'Enginyeria Elèctrica
dc.contributor	Universitat Politècnica de Catalunya. MCIA - Motion Control and Industrial Applications Research Group
dc.contributor	Universitat Politècnica de Catalunya. SEER - Sistemes Elèctrics d'Energia Renovable
dc.contributor.author	Rosero García, Javier Alveiro
dc.contributor.author	Ortega Redondo, Juan Antonio
dc.contributor.author	Aldabas Rubira, Emiliano
dc.contributor.author	Romeral Martínez, José Luis
dc.date	2007-03
dc.identifier.citation	Rosero, J. [et al.]. Moving towards a more electric aircraft. "IEEE aerospace and electronic systems magazine", Març 2007, vol. 22, núm. 3, p. 3-9.
dc.identifier.citation	0885-8985
dc.identifier.citation	10.1109/MAES.2007.340500
dc.identifier.uri	http://hdl.handle.net/2117/20075
dc.language.iso	eng
dc.rights	Attribution-NonCommercial-NoDerivs 3.0 Spain
dc.rights	info:eu-repo/semantics/openAccess
dc.rights	http://creativecommons.org/licenses/by-nc-nd/3.0/es/
dc.subject	Àrees temàtiques de la UPC::Aeronàutica i espai::Aeronaus::Avions
dc.subject	Àrees temàtiques de la UPC::Energies::Energia elèctrica
dc.subject	Aircraft power systems
dc.subject	Aeronàutica -- Aparells i instruments
dc.title	Moving towards a more electric aircraft
dc.type	info:eu-repo/semantics/publishedVersion
dc.type	info:eu-repo/semantics/article
dc.description.abstract	Harry Rowe Mimno Award for the March 2007 AESS Magazine Paper: “Moving Towards A More Electric Aircraft”
dc.description.abstract	The latest advances in electric and electronic aircraft technologies from the point of view of an "all-electric" aircraft are presented herein. Specifically, we describe the concept of a "more electric aircraft" (MEA), which involves removing the need for on-engine hydraulic power generation and bleed air off-takes, and the increasing use of power electronics in the starter/generation system of the main engine. Removal of the engine hydraulic pumps requires fully-operative electrical power actuators and mastery of the flight control architecture. The paper presents a general overview of the electrical power generation system and electric drives for the MEA, with special regard to the flight controls. Some discussion regarding the interconnection of nodes and safety of buses and protocols in distributed systems is also presented.
dc.description.abstract	Peer Reviewed
dc.description.abstract	Award-winning

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