Strength analysis of AL-7F-1 engine turbine rotor blade

Kód výsledku v IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F49777513%3A23210%2F16%3A43932251" target="_blank" >RIV/49777513:23210/16:43932251 - isvavai.cz</a>

Výsledek na webu

<a href="http://proceedings.asmedigitalcollection.asme.org/proceeding.aspx?articleid=2602658" target="_blank" >http://proceedings.asmedigitalcollection.asme.org/proceeding.aspx?articleid=2602658</a>

DOI - Digital Object Identifier

<a href="http://dx.doi.org/10.1115/IMECE201665251" target="_blank" >10.1115/IMECE201665251</a>

Jazyk výsledku

angličtina

Název v původním jazyce

Strength analysis of AL-7F-1 engine turbine rotor blade

Popis výsledku v původním jazyce

The key intent of the article is to describe clearly the strength issue of blades for aircraft engines, on the basis of which to create a calculation algorithm and apply it to a particular blade. The work then deals with a strength analysis of a rotor blade used in the gas turbine of an AL-7F-1 turbocharger aircraft engine. The article describes comprehensively in terms of strength the influences which act on the blade during operation. Generally, these loads can be divided into static load, which includes the tensile stress generated by the rotating mass of the blades, bending and torsion moments caused by the kinetic energy of the flowing gas. The last part of the article is dedicated to the issue of compensation of the bending moments acting on the turbine blades, resulting in analytical calculation of the blade inclination angles in the critical cross section.

Název v anglickém jazyce

Strength analysis of AL-7F-1 engine turbine rotor blade

Popis výsledku anglicky

The key intent of the article is to describe clearly the strength issue of blades for aircraft engines, on the basis of which to create a calculation algorithm and apply it to a particular blade. The work then deals with a strength analysis of a rotor blade used in the gas turbine of an AL-7F-1 turbocharger aircraft engine. The article describes comprehensively in terms of strength the influences which act on the blade during operation. Generally, these loads can be divided into static load, which includes the tensile stress generated by the rotating mass of the blades, bending and torsion moments caused by the kinetic energy of the flowing gas. The last part of the article is dedicated to the issue of compensation of the bending moments acting on the turbine blades, resulting in analytical calculation of the blade inclination angles in the critical cross section.

Druh

D - Stať ve sborníku

CEP obor

—

OECD FORD obor

20304 - Aerospace engineering

Projekt

<a href="/cs/project/LQ1603" target="_blank" >LQ1603: Výzkum pro SUSEN</a><br>

Návaznosti

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

Rok uplatnění

2016

Kód důvěrnosti údajů

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

Název statě ve sborníku

ASME 2016 International Mechanical Engineering Congress and Exposition (IMECE 2016)

ISBN

978-0-7918-5063-3

ISSN

—

e-ISSN

neuvedeno

Počet stran výsledku

8

Strana od-do

1-8

Název nakladatele

American Society of Mechanical Engineers

Místo vydání

New York

Místo konání akce

Phoenix, Arizona (USA)

Datum konání akce

11. 11. 2016

Typ akce podle státní příslušnosti

WRD - Celosvětová akce

Kód UT WoS článku

—