All

What are you looking for?

All
Projects
Results
Organizations

Quick search

  • Projects supported by TA ČR
  • Excellent projects
  • Projects with the highest public support
  • Current projects

Smart search

  • That is how I find a specific +word
  • That is how I leave the -word out of the results
  • “That is how I can find the whole phrase”

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

The result's identifiers

  • Result code in 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>

  • Result on the web

    <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>

Alternative languages

  • Result language

    angličtina

  • Original language name

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

  • Original language description

    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.

  • Czech name

  • Czech description

Classification

  • Type

    D - Article in proceedings

  • CEP classification

  • OECD FORD branch

    20304 - Aerospace engineering

Result continuities

  • Project

    <a href="/en/project/LQ1603" target="_blank" >LQ1603: Research for SUSEN</a><br>

  • Continuities

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

Others

  • Publication year

    2016

  • Confidentiality

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

Data specific for result type

  • Article name in the collection

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

  • ISBN

    978-0-7918-5063-3

  • ISSN

  • e-ISSN

    neuvedeno

  • Number of pages

    8

  • Pages from-to

    1-8

  • Publisher name

    American Society of Mechanical Engineers

  • Place of publication

    New York

  • Event location

    Phoenix, Arizona (USA)

  • Event date

    Nov 11, 2016

  • Type of event by nationality

    WRD - Celosvětová akce

  • UT code for WoS article