Architecture of Distributed Control System for Gearbox-Free More Electric Turbofan Engine
This article presents the development of the electric turbofan engine in distributed architecture with a design thrust in the range of 3 to 7.5 and from 7.5 to 30 kN for small and medium-sized unmanned aerial vehicles. The engine subsystems are considered as separate smart modules with a built-in co...
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| Principais autores: | , , , |
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| Formato: | Artigo |
| Idioma: | Inglês |
| Publicado em: |
MDPI AG
2021-10-01
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| coleção: | Aerospace |
| Assuntos: | |
| Acesso em linha: | https://www.mdpi.com/2226-4310/8/11/316 |
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