Aircraft turboprop engine vibration monitoring module

Dulík, Tomáš; Pospíšilík, Martin; Opluštil, Vladimír; Beneš, Petr

dc.title	Aircraft turboprop engine vibration monitoring module	en
dc.contributor.author	Dulík, Tomáš
dc.contributor.author	Pospíšilík, Martin
dc.contributor.author	Opluštil, Vladimír
dc.contributor.author	Beneš, Petr
dc.relation.ispartof	International Conference on Applied Electronics
dc.identifier.issn	1803-7232 Scopus Sources, Sherpa/RoMEO, JCR
dc.identifier.isbn	9788026108917
dc.date.issued	2020
utb.relation.volume	2020-September
dc.citation.spage	33
dc.citation.epage	37
dc.event.title	25th International Conference on Applied Electronics, AE 2020
dc.event.location	Pilsen
utb.event.state-en	Czech Republic
utb.event.state-cs	Česká republika
dc.event.sdate	2020-09-08
dc.event.edate	2020-09-09
dc.type	conferenceObject
dc.language.iso	en
dc.publisher	IEEE Computer Society
dc.identifier.doi	10.23919/AE49394.2020.9232698
dc.relation.uri	https://ieeexplore.ieee.org/document/9232698
dc.subject	in flight vibration monitoring	en
dc.subject	turboprop engine vibrations	en
dc.subject	vibration monitoring system	en
dc.subject	signal processing algorithm	en
dc.description.abstract	The paper describes electronic vibration monitoring module (EVM) that can be used as standalone diagnostic system or as a part of a complex modular concept of engine electronic control (EEC/FADEC) with aircraft health monitoring system. We present a new generation of EVM for modern small turboprop engines and their vibration diagnostics which has been developed by Unis, a.s. in cooperation with Brno University of Technology and Tomas Bata University in Zlin. © 2020 University of West Bohemia.	en
utb.faculty	Faculty of Applied Informatics
dc.identifier.uri	http://hdl.handle.net/10563/1010052
utb.identifier.scopus	2-s2.0-85096357497
utb.identifier.wok	000659296200008
utb.source	d-scopus
dc.date.accessioned	2020-12-09T01:52:46Z
dc.date.available	2020-12-09T01:52:46Z
dc.description.sponsorship	Ministry of Industry and Business (MPO) by the grant "Advanced Technology of Modular Control and Diagnostics Systems for Aircraft Engines" ("Pokrocile technologie modularnich ridicich a diagnostickych systemu") [FV20043]
utb.contributor.internalauthor	Dulík, Tomáš
utb.contributor.internalauthor	Pospíšilík, Martin
utb.fulltext.affiliation	Tomas Dulík, Martin Pospíšilík, Vladimír Opluštil, Petr Beneš Faculty of Applied Informatics Tomas Bata University in Zlin Zlin, Czech Republic dulik@utb.cz Division Aerospace and Advanced Control, UNIS, a.s. Brno, Czech Republic oplustil@unis.cz Faculty of Electrical Engineering and Communication Brno University of Technology Brno, Czech Republic benesp@feec.vutbr.cz
utb.fulltext.dates	-
utb.fulltext.sponsorship	This project was supported by Ministry of Industry and Business (MPO) by the grant “Advanced Technology of Modular Control and Diagnostics Systems for Aircraft Engines” (“Pokročilé technologie modulárních řídicích a diagnostických systémů”), project number: FV20043.
utb.wos.affiliation	[Dulik, Tomas; Pospisilik, Martin] Tomas Bata Univ Zlin, Fac Appl Informat, Zlin, Czech Republic; [Oplustil, Vladimir] UNIS As, Div Aerosp & Adv Control, Brno, Czech Republic; [Benes, Petr] Brno Univ Technol, Fac Elect Engn & Commun, Brno, Czech Republic
utb.scopus.affiliation	Tomas Bata University in Zlin, Faculty of Applied Informatics, Zlin, Czech Republic; UNIS, Division Aerospace and Advanced Control, a.s. Brno, Czech Republic; Brno University of Technology, Faculty of Electrical Engineering and Communication, Brno, Czech Republic
utb.fulltext.projects	FV20043
utb.fulltext.faculty	Faculty of Applied Informatics
utb.fulltext.faculty	Faculty of Applied Informatics