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Steam Turbine Axial Exhaust Diffuser Investigation Using a Test Rig and its Numerical Model

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F49193864%3A_____%2F19%3AN0000001" target="_blank" >RIV/49193864:_____/19:N0000001 - isvavai.cz</a>

  • Alternative codes found

    RIV/49193864:_____/19:N0000006

  • Result on the web

    <a href="https://asmedigitalcollection.asme.org/IMECE/proceedings-abstract/IMECE2019/59438/V006T06A033/1073159" target="_blank" >https://asmedigitalcollection.asme.org/IMECE/proceedings-abstract/IMECE2019/59438/V006T06A033/1073159</a>

  • DOI - Digital Object Identifier

    <a href="http://dx.doi.org/10.1115/IMECE2019-10267" target="_blank" >10.1115/IMECE2019-10267</a>

Alternative languages

  • Result language

    angličtina

  • Original language name

    Steam Turbine Axial Exhaust Diffuser Investigation Using a Test Rig and its Numerical Model

  • Original language description

    Exhaust casings are one of the most important steam turbine components. The main purpose of the exhaust casing is to increase the last stage enthalpy drop, which results in an increase of the whole turbine output. It plays a significant role especially in turbines with lower outputs and in turbines whose condenser is cooled by air. In such cases, the exhaust casings with an axial diffuser is usually used. This paper deals with the investigation of the axial diffuser outlet part based on experimental measurements performed on a test rig installed in a wind tunnel in the Doosan Skoda Power laboratories and numerical simulations. The first part of the paper is about the general issues appearing the exhaust diffusers. Then, the design of the experimental test rig which aim is to simulate the flow conditions in real turbines is described. The last part of the paper is about experimental measurement as well as numerical results. The main observed phenomenon which is the effect of the circumferential angle on the inlet of the diffuser is described on different designs which were tested from the static pressure recovery factor point of view. For measuring flow parameters, a static wall pressure measurement was used together with multi-hole pneumatic probes. For numerical simulations, the commercial code ANSYS CFX 18.2 was used.

  • Czech name

  • Czech description

Classification

  • Type

    D - Article in proceedings

  • CEP classification

  • OECD FORD branch

    20302 - Applied mechanics

Result continuities

  • Project

    <a href="/en/project/TJ01000048" target="_blank" >TJ01000048: Decreasing of Exhaust Loss in Modern Design Steam Turbines</a><br>

  • Continuities

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

Others

  • Publication year

    2019

  • 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 2019 International Mechanical Engineering Congress and Exposition

  • ISBN

    978-0-7918-5943-8

  • ISSN

  • e-ISSN

  • Number of pages

    9

  • Pages from-to

  • Publisher name

    ASME

  • Place of publication

    Salt Lake City, Utah, USA

  • Event location

    Salt Lake City, Utah, USA

  • Event date

    Jan 1, 2019

  • Type of event by nationality

    WRD - Celosvětová akce

  • UT code for WoS article