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Prediction of non-stationary deformation of gas turbine using machine learning approach coupling between CFD and FEM model

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F24%3A00375067" target="_blank" >RIV/68407700:21220/24:00375067 - isvavai.cz</a>

  • Result on the web

    <a href="https://doi.org/10.21495/em2024-226" target="_blank" >https://doi.org/10.21495/em2024-226</a>

  • DOI - Digital Object Identifier

    <a href="http://dx.doi.org/10.21495/em2024-226" target="_blank" >10.21495/em2024-226</a>

Alternative languages

  • Result language

    angličtina

  • Original language name

    Prediction of non-stationary deformation of gas turbine using machine learning approach coupling between CFD and FEM model

  • Original language description

    After shutdown, the gas turbine rotor system cooling primarily through natural convection and radiation. It is presenting a common engineering challenge prevalent across various applications. In power engineering, this phenomenon has long been acknowledged and addressed through gradual startup and shutdown procedures of the rotor system. However, within the aircraft engine domain, this issue is more necessary due to the variable operating conditions and temperatures changes by flight modes or engine shutdown events. Moreover, engine aftercooling proves particularly arduous owing to the intricate geometry and equipment constraints. This paper delves into the application of a developed Finite Element Method (FEM) tool for predicting rotor thermal bow induced by temperature discrepancies between the upper and lower sides of the rotor. The paper meticulously elucidates the mathematical model of the FEM tool and expounds upon the calculation methodology for rotor deflection based on the selected geometry.

  • 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/EF16_019%2F0000826" target="_blank" >EF16_019/0000826: Center of Advanced Aerospace Technology</a><br>

  • Continuities

    P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)<br>S - Specificky vyzkum na vysokych skolach

Others

  • Publication year

    2024

  • Confidentiality

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

Data specific for result type

  • Article name in the collection

    Engineering Mechanics 2024: Book of full texts

  • ISBN

    978-80-214-6235-9

  • ISSN

    1805-8248

  • e-ISSN

  • Number of pages

    4

  • Pages from-to

    226-229

  • Publisher name

    Institute of Thermomechanics, AS CR, v.v.i.

  • Place of publication

    Prague

  • Event location

    Milovy

  • Event date

    May 14, 2024

  • Type of event by nationality

    WRD - Celosvětová akce

  • UT code for WoS article