Diagnostics of aircraft turbine engine using artificial neural networks
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F14%3A%230001729" target="_blank" >RIV/00010669:_____/14:#0001729 - isvavai.cz</a>
Result on the web
<a href="http://www.czaerospace.eu/en/2014-01-49.html" target="_blank" >http://www.czaerospace.eu/en/2014-01-49.html</a>
DOI - Digital Object Identifier
—
Alternative languages
Result language
angličtina
Original language name
Diagnostics of aircraft turbine engine using artificial neural networks
Original language description
The paper deals with composition of an Artificial Neural Network (ANN) applied to technical diagnostics of a small aircraft turboprop engine. A value of thermodynamic parameters describing operating range of the engine are used as an input data further processed to allow optimal training and validation of the Artificial neural network used in diagnostic system of a small aircraft engine. The diagnostic system can be extended by the wear monitoring of the turbine engine parts.
Czech name
—
Czech description
—
Classification
Type
J<sub>x</sub> - Unclassified - Peer-reviewed scientific article (Jimp, Jsc and Jost)
CEP classification
JT - Propulsion, engines and fuels
OECD FORD branch
—
Result continuities
Project
<a href="/en/project/7E12035" target="_blank" >7E12035: Efficient Systems and Propulsion for Small Aircraft</a><br>
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)
Others
Publication year
2014
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Name of the periodical
Czech Aerospace Proceedings / Letecký zpravodaj
ISSN
1211-877X
e-ISSN
—
Volume of the periodical
1/2014
Issue of the periodical within the volume
1
Country of publishing house
CZ - CZECH REPUBLIC
Number of pages
6
Pages from-to
20-25
UT code for WoS article
—
EID of the result in the Scopus database
—