Transformation of an aviation turboshaft engine into a experimental jet engine for laboratory testing unstable radial compressor work

Kód výsledku v IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F49777513%3A23210%2F14%3A43927764" target="_blank" >RIV/49777513:23210/14:43927764 - isvavai.cz</a>

Výsledek na webu

<a href="http://dx.doi.org/10.1115/IMECE2014-37298" target="_blank" >http://dx.doi.org/10.1115/IMECE2014-37298</a>

DOI - Digital Object Identifier

<a href="http://dx.doi.org/10.1115/IMECE2014-37298" target="_blank" >10.1115/IMECE2014-37298</a>

Jazyk výsledku

angličtina

Název v původním jazyce

Transformation of an aviation turboshaft engine into a experimental jet engine for laboratory testing unstable radial compressor work

Popis výsledku v původním jazyce

The article deals with the use of a small aviation turboshaft engine for laboratory purposes. This study describes its transformation into an experimental device for research and education. Various constructional, technological and controlling modifications and settings of the gas turbine test stand were carried out and tested on a stationary configuration. The stationary system can be used as a small backup power generator or as a drive unit for a compressor, pump, etc. New control systems, electronicelements and methods of measuring rotations, pressure and temperature are tested for educational and research purposes. The study includes a schematic description of modelling measurements and subsequent numerical evaluation of the thermodynamic characteristics of the cycle in an experimental gas turbine. The laboratory device presented here is, thanks to technological, material and thermodynamic research, suitable for educating and testing the knowledge of future aviation and mechanical

Název v anglickém jazyce

Transformation of an aviation turboshaft engine into a experimental jet engine for laboratory testing unstable radial compressor work

Popis výsledku anglicky

The article deals with the use of a small aviation turboshaft engine for laboratory purposes. This study describes its transformation into an experimental device for research and education. Various constructional, technological and controlling modifications and settings of the gas turbine test stand were carried out and tested on a stationary configuration. The stationary system can be used as a small backup power generator or as a drive unit for a compressor, pump, etc. New control systems, electronicelements and methods of measuring rotations, pressure and temperature are tested for educational and research purposes. The study includes a schematic description of modelling measurements and subsequent numerical evaluation of the thermodynamic characteristics of the cycle in an experimental gas turbine. The laboratory device presented here is, thanks to technological, material and thermodynamic research, suitable for educating and testing the knowledge of future aviation and mechanical

Druh

D - Stať ve sborníku

CEP obor

JE - Nejaderná energetika, spotřeba a užití energie

OECD FORD obor

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Projekt

<a href="/cs/project/EE2.3.20.0139" target="_blank" >EE2.3.20.0139: Budování excelentního vědeckého týmu pro experimentální a numerické modelování v mechanice tekutin a termodynamice</a><br>

Návaznosti

P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Rok uplatnění

2014

Kód důvěrnosti údajů

S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Název statě ve sborníku

ASME International Mechanical Engineering Congress and Exposition

ISBN

978-0-7918-4950-7

ISSN

—

e-ISSN

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Počet stran výsledku

7

Strana od-do

1-7

Název nakladatele

ASME

Místo vydání

Montreál

Místo konání akce

Montreal, Canada

Datum konání akce

14. 11. 2014

Typ akce podle státní příslušnosti

WRD - Celosvětová akce

Kód UT WoS článku

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