A Concept Plane using electric distributed propulsion Evaluation of advanced power architecture
| Autor: | 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. |
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| Přispěvatelé: | 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 |
| Jazyk: | angličtina |
| Rok vydání: | 2015 |
| Předmět: | |
| Zdroj: | More Electric Aircraft-MEA 2015 More Electric Aircraft-MEA 2015, Feb 2015, TOULOUSE, France |
| Popis: | 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. |
| Databáze: | OpenAIRE |
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