Aircraft turboprop engine vibration monitoring module

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

Title:

Author:

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

Document type:

Conference paper (English)

Source document:

International Conference on Applied Electronics. 2020, vol. 2020-September, p. 33-37

ISSN:

1803-7232 (Sherpa/RoMEO, JCR)

Journal Impact This chart shows the development of journal-level impact metrics in time

JCR	Journal Citation Reports - Impact Factor
SNIP	SCImago Source Normalized Impact per Paper
SJR	SCImago Journal Rank
IPP	SCImago Impact per Publication
CS	Scopus CiteScore

(Note: The metrics are not comparable against one another.)

ISBN:

9788026108917

DOI:

https://doi.org/10.23919/AE49394.2020.9232698

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.

Full text:

https://ieeexplore.ieee.org/document/9232698

Show full item record

Files in this item

Name: Fulltext_1010052.pdf

Size: 420.3Kb

Format: PDF

Description: fulltext

ČSN ISO 690:2011 citation

Citace článku v konferenčním sborníku:
DULÍK, Tomáš, Martin POSPÍŠILÍK, Vladimír OPLUŠTIL a Petr BENEŠ. Aircraft turboprop engine vibration monitoring module. In: International Conference on Applied Electronics [online]. Pilsen: IEEE Computer Society, 2020, s. 33-37. [cit. 2024-12-22]. ISSN 1803-7232. Dostupné z: https://ieeexplore.ieee.org/document/9232698.

These citations are software generated and may contain errors. To verify accuracy, check the appropriate style guide.