Small Engine Inlet Distortion Testing Device

Kód výsledku v IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F60162694%3AG43__%2F15%3A00531472" target="_blank" >RIV/60162694:G43__/15:00531472 - isvavai.cz</a>

Výsledek na webu

<a href="http://vavtest.unob.cz/registr" target="_blank" >http://vavtest.unob.cz/registr</a>

DOI - Digital Object Identifier

<a href="http://dx.doi.org/10.1109/MILTECHS.2015.7153691" target="_blank" >10.1109/MILTECHS.2015.7153691</a>

Jazyk výsledku

angličtina

Název v původním jazyce

Small Engine Inlet Distortion Testing Device

Popis výsledku v původním jazyce

A project dealing with small gas turbine engine inlet total pressure distortion testing was solved at the University of Defence. Within this project a new device for creation and measurement of the total pressure inlet distortion was designed. In the early stage of the project there was a need of significant amount of testing for evaluation of newly designed device, foundation of measurement methodology, testing of basic distortion screen designs and their affects. In order to save expanses for the jet engine operation for these initial tests it was replaced by a model device drawing air through the engine inlet. This paper describes design of the measurement device, its initial tests and lessons learned from this development. Difficulties encountered with substitution of the jet engine by standalone compressor are also presented.

Název v anglickém jazyce

Small Engine Inlet Distortion Testing Device

Popis výsledku anglicky

A project dealing with small gas turbine engine inlet total pressure distortion testing was solved at the University of Defence. Within this project a new device for creation and measurement of the total pressure inlet distortion was designed. In the early stage of the project there was a need of significant amount of testing for evaluation of newly designed device, foundation of measurement methodology, testing of basic distortion screen designs and their affects. In order to save expanses for the jet engine operation for these initial tests it was replaced by a model device drawing air through the engine inlet. This paper describes design of the measurement device, its initial tests and lessons learned from this development. Difficulties encountered with substitution of the jet engine by standalone compressor are also presented.

Druh

D - Stať ve sborníku

CEP obor

KA - Vojenství

OECD FORD obor

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Projekt

—

Návaznosti

I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Rok uplatnění

2015

Kód důvěrnosti údajů

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

Název statě ve sborníku

International Conference on Military Technologies 2015

ISBN

978-80-7231-976-3

ISSN

—

e-ISSN

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Počet stran výsledku

6

Strana od-do

455-460

Název nakladatele

University of Defence

Místo vydání

Brno

Místo konání akce

Brno

Datum konání akce

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Typ akce podle státní příslušnosti

WRD - Celosvětová akce

Kód UT WoS článku

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