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...

Descripción completa

Guardado en:

Detalles Bibliográficos
Autores principales:	Viktor Popov, Sergiy Yepifanov, Yevhenii Kononykhyn, Aleksandr Tsaglov
Formato:	article
Lenguaje:	EN
Publicado:	MDPI AG 2021
Materias:	unmanned aerial vehicle more electric aircraft turbofan engine distributed control system Motor vehicles. Aeronautics. Astronautics TL1-4050
Acceso en línea:	https://doaj.org/article/1856eec838da4f09bddc3c4b0073b397
Etiquetas:	Agregar Etiqueta Sin Etiquetas, Sea el primero en etiquetar este registro!

id	oai:doaj.org-article:1856eec838da4f09bddc3c4b0073b397
record_format	dspace
spelling	oai:doaj.org-article:1856eec838da4f09bddc3c4b0073b3972021-11-25T15:57:08ZArchitecture of Distributed Control System for Gearbox-Free More Electric Turbofan Engine10.3390/aerospace81103162226-4310https://doaj.org/article/1856eec838da4f09bddc3c4b0073b3972021-10-01T00:00:00Zhttps://www.mdpi.com/2226-4310/8/11/316https://doaj.org/toc/2226-4310This 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 control system, exchanging data via a digital channel with the central engine control and diagnostics unit. The key smart engine units are combined in the following subsystems: starter and turbine generators, oil pumps, actuator of guide vanes, fuel pumps, fuel metering unit, control and diagnostic unit. All pumps and guide vane actuator are electrically driven. Control and monitoring signals are transmitted via a digital bus. Functional and reliability analysis and the technical configuration design of each subsystem are presented. Based on analysis of the architecture of distributed control systems for a gearbox-free electric engine, different configurations of described subsystems are proposed.Viktor PopovSergiy YepifanovYevhenii KononykhynAleksandr TsaglovMDPI AGarticleunmanned aerial vehiclemore electric aircraftturbofan enginedistributed control systemMotor vehicles. Aeronautics. AstronauticsTL1-4050ENAerospace, Vol 8, Iss 316, p 316 (2021)
institution	DOAJ
collection	DOAJ
language	EN
topic	unmanned aerial vehicle more electric aircraft turbofan engine distributed control system Motor vehicles. Aeronautics. Astronautics TL1-4050
spellingShingle	unmanned aerial vehicle more electric aircraft turbofan engine distributed control system Motor vehicles. Aeronautics. Astronautics TL1-4050 Viktor Popov Sergiy Yepifanov Yevhenii Kononykhyn Aleksandr Tsaglov Architecture of Distributed Control System for Gearbox-Free More Electric Turbofan Engine
description	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 control system, exchanging data via a digital channel with the central engine control and diagnostics unit. The key smart engine units are combined in the following subsystems: starter and turbine generators, oil pumps, actuator of guide vanes, fuel pumps, fuel metering unit, control and diagnostic unit. All pumps and guide vane actuator are electrically driven. Control and monitoring signals are transmitted via a digital bus. Functional and reliability analysis and the technical configuration design of each subsystem are presented. Based on analysis of the architecture of distributed control systems for a gearbox-free electric engine, different configurations of described subsystems are proposed.
format	article
author	Viktor Popov Sergiy Yepifanov Yevhenii Kononykhyn Aleksandr Tsaglov
author_facet	Viktor Popov Sergiy Yepifanov Yevhenii Kononykhyn Aleksandr Tsaglov
author_sort	Viktor Popov
title	Architecture of Distributed Control System for Gearbox-Free More Electric Turbofan Engine
title_short	Architecture of Distributed Control System for Gearbox-Free More Electric Turbofan Engine
title_full	Architecture of Distributed Control System for Gearbox-Free More Electric Turbofan Engine
title_fullStr	Architecture of Distributed Control System for Gearbox-Free More Electric Turbofan Engine
title_full_unstemmed	Architecture of Distributed Control System for Gearbox-Free More Electric Turbofan Engine
title_sort	architecture of distributed control system for gearbox-free more electric turbofan engine
publisher	MDPI AG
publishDate	2021
url	https://doaj.org/article/1856eec838da4f09bddc3c4b0073b397
work_keys_str_mv	AT viktorpopov architectureofdistributedcontrolsystemforgearboxfreemoreelectricturbofanengine AT sergiyyepifanov architectureofdistributedcontrolsystemforgearboxfreemoreelectricturbofanengine AT yevheniikononykhyn architectureofdistributedcontrolsystemforgearboxfreemoreelectricturbofanengine AT aleksandrtsaglov architectureofdistributedcontrolsystemforgearboxfreemoreelectricturbofanengine
_version_	1718413364945747968

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

Ejemplares similares