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A Concept Plane using electric distributed propulsion Evaluation of advanced power architecture

Authors :
Ridel, M.
Paluch, B.
Doll, C.
Donjat, D.
Hermetz, J.
Guigon, A.
Schmollgruber, P.
Atinault, O.
Choy, P.
Le Tallec, P.
Dessornes, O.
Lefebvre, T.
ONERA - The French Aerospace Lab [Toulouse]
ONERA
ONERA - The French Aerospace Lab [Lille]
ONERA - The French Aerospace Lab [Palaiseau]
ONERA-Université Paris Saclay (COmUE)
ONERA - The French Aerospace Lab [Meudon]
André, Cécile
Source :
More Electric Aircraft-MEA 2015, More Electric Aircraft-MEA 2015, Feb 2015, TOULOUSE, France
Publication Year :
2015
Publisher :
HAL CCSD, 2015.

Abstract

International audience; Starting from electrical distributed propulsion system concept, the ONERA’s engineers demonstrated the viability of an all electrical aircraft for a small business aircraft. This paper describes the advanced power architecture considering energy conversion and power distribution. The design of this advanced power architecture requires the multi-physic integration of different domains as flight performances, safety and environmental requirements (thermal, electric, electromagnetic). From this analysis, all components of this advanced power architecture have been identified and evaluated.

Details

Language :
English
Database :
OpenAIRE
Journal :
More Electric Aircraft-MEA 2015, More Electric Aircraft-MEA 2015, Feb 2015, TOULOUSE, France
Accession number :
edsair.dedup.wf.001..1a407327405b1c5e308e565fc127fae5