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