Number of the records: 1  

Turbine Cascades of Last Stage Blades for Wide Range of Operating Conditions

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    SYSNO ASEP0508969
    Document TypeC - Proceedings Paper (int. conf.)
    R&D Document TypeThe record was not marked in the RIV
    TitleTurbine Cascades of Last Stage Blades for Wide Range of Operating Conditions
    Author(s) Novák, O. (CZ)
    Bobčík, M. (CZ)
    Luxa, Martin (UT-L) RID, ORCID
    Fořt, J. (CZ)
    Rudas, B. (CZ)
    Synáč, J. (CZ)
    Šimurda, David (UT-L) RID, ORCID
    Fürst, J. (CZ)
    Halama, J. (CZ)
    Hric, V. (CZ)
    Příhoda, Jaromír (UT-L) RID, ORCID
    Šimka, Z. (CZ)
    Source Title13th European Turbomachinery Conference on Turbomachinery Fluid Dynamics and Thermodynamics. - Lausanne : European Turbomachinery Society, 2019
    Number of pages10 s.
    ActionEuropean Turbomachinery Conference on Turbomachinery Fluid Dynamics and Thermodynamics, ETC 2019 /13./
    Event date08.04.2019 - 12.04.2019
    VEvent locationLausanne
    CountryCH - Switzerland
    Event typeWRD
    Languageeng - English
    CountryCH - Switzerland
    Keywordsturbine ; cascade ; last stage blad ; CFD ; experimental validation
    Subject RIVBK - Fluid Dynamics
    OECD categoryApplied mechanics
    R&D ProjectsTH02020057 GA TA ČR - Technology Agency of the Czech Republic (TA ČR)
    Institutional supportUT-L - RVO:61388998
    EID SCOPUS85065992569
    AnnotationRecent trends in the electric energy market such as biomass, waste incineration or combined cycle power plants require innovative solutions in steam turbine design. Variable operating conditions cause significant changes in flow field surrounding the steam turbine last stage blades. Therefore, the enlargement of operating range for last stage blades presents new challenges in design of turbine cascades. Several turbine cascades were designed and analyzed by commercial and in-house software of CTU Prague. Selected profiles were experimentally validated in the high-speed wind tunnel for 2D cascade measurements of the Institute of Thermomechanics of the Czech Academy of Sciences which is equipped by an adjustable supersonic inlet nozzle, perforated inserts at side walls and adjustable perforated tailboard. Comparisons are presented of numerical results with optical and pneumatic measurements for a wide range of inlet and outlet Mach numbers for optimized hub and tip profile cascades.
    WorkplaceInstitute of Thermomechanics
    ContactMarie Kajprová, kajprova@it.cas.cz, Tel.: 266 053 154 ; Jana Lahovská, jaja@it.cas.cz, Tel.: 266 053 823
    Year of Publishing2020
Number of the records: 1  

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