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Architecture of Distributed Control System for Gearbox-Free More Electric Turbofan Engine

2021-09-02

Abstract excerpt

The article presents development of the more electric turbofan engine in distributed architecture with a design thrust in the range from 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 control system, exchanging data via a digital channel with the central engine control and diagnostics unit. The key s...

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Literature Corpus work
bf45f516-2780-5044-b550-a4b8346afaaa
DOI
10.20944/preprints202109.0042.v1
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Architecture of Distributed Control System for Gearbox-Free More Electric Turbofan EngineDOI 10.20944/preprints202109.0042.v1
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