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    Numerical Investigation on the Aerodynamic Performance of a Low-Pressure Steam Turbine Exhaust Hood Using Design of Experiment Analysis

    Source: Journal of Engineering for Gas Turbines and Power:;2020:;volume( 142 ):;issue: 011::page 0111006-1
    Author:
    Diurno, Tommaso
    ,
    Fondelli, Tommaso
    ,
    Nettis, Leonardo
    ,
    Maceli, Nicola
    ,
    Arcangeli, Lorenzo
    ,
    Andreini, Antonio
    ,
    Facchini, Bruno
    DOI: 10.1115/1.4048567
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Nowadays, the rising interest in using renewable energy for thermal power generation has led to radical changes in steam turbine design practice and operability. Modern steam turbines are required to operate with greater flexibility due to rapid load changes, fast start-up, and frequent shutdowns. This has given rise to great challenges to the exhaust hood system design, which has a great influence on the overall turbine performance converting the kinetic energy leaving the last stage of low-pressure turbine into static pressure. The radial hoods are characterized by a complex aerodynamic behavior since the flow turns by 90 deg in a very short distance and this generates a highly rotational flow structure within the diffuser and exhaust hood outer casing, moreover, the adverse pressure gradient can promote the flow separation drastically reducing the hood recovery performance. For these reasons, it is fundamental to design the exhaust system in order to ensure a good pressure recovery under all the machine operating conditions. This paper presents a design of experiment (DOE) analysis on a low-pressure steam turbine exhaust hood through computational fluid dynamics (CFD) simulations. A parametric model of an axial-radial exhaust hood was developed, and a sensitivity of exhaust hood performance as a function of key geometrical parameters was carried out, with the aim of optimizing the pressure recovery coefficient and minimizing the overall dimensions of the exhaust casing. Since hood performance strongly depends on a proper coupling with the turbine rear stage, such a stage was modeled using the so-called mixing-plane approach to couple both stator–rotor and rotor-diffuser interfaces. A detailed analysis of the flow field in the exhaust hood in the different configurations was performed, detecting the swirling structures responsible for the energy dissipation in each simulation, as well as correlating the flow field with the pressure recovery coefficient.
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      Numerical Investigation on the Aerodynamic Performance of a Low-Pressure Steam Turbine Exhaust Hood Using Design of Experiment Analysis

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4274727
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    contributor authorDiurno, Tommaso
    contributor authorFondelli, Tommaso
    contributor authorNettis, Leonardo
    contributor authorMaceli, Nicola
    contributor authorArcangeli, Lorenzo
    contributor authorAndreini, Antonio
    contributor authorFacchini, Bruno
    date accessioned2022-02-04T22:01:27Z
    date available2022-02-04T22:01:27Z
    date copyright10/20/2020 12:00:00 AM
    date issued2020
    identifier issn0742-4795
    identifier othergtp_142_11_111006.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4274727
    description abstractNowadays, the rising interest in using renewable energy for thermal power generation has led to radical changes in steam turbine design practice and operability. Modern steam turbines are required to operate with greater flexibility due to rapid load changes, fast start-up, and frequent shutdowns. This has given rise to great challenges to the exhaust hood system design, which has a great influence on the overall turbine performance converting the kinetic energy leaving the last stage of low-pressure turbine into static pressure. The radial hoods are characterized by a complex aerodynamic behavior since the flow turns by 90 deg in a very short distance and this generates a highly rotational flow structure within the diffuser and exhaust hood outer casing, moreover, the adverse pressure gradient can promote the flow separation drastically reducing the hood recovery performance. For these reasons, it is fundamental to design the exhaust system in order to ensure a good pressure recovery under all the machine operating conditions. This paper presents a design of experiment (DOE) analysis on a low-pressure steam turbine exhaust hood through computational fluid dynamics (CFD) simulations. A parametric model of an axial-radial exhaust hood was developed, and a sensitivity of exhaust hood performance as a function of key geometrical parameters was carried out, with the aim of optimizing the pressure recovery coefficient and minimizing the overall dimensions of the exhaust casing. Since hood performance strongly depends on a proper coupling with the turbine rear stage, such a stage was modeled using the so-called mixing-plane approach to couple both stator–rotor and rotor-diffuser interfaces. A detailed analysis of the flow field in the exhaust hood in the different configurations was performed, detecting the swirling structures responsible for the energy dissipation in each simulation, as well as correlating the flow field with the pressure recovery coefficient.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleNumerical Investigation on the Aerodynamic Performance of a Low-Pressure Steam Turbine Exhaust Hood Using Design of Experiment Analysis
    typeJournal Paper
    journal volume142
    journal issue11
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4048567
    journal fristpage0111006-1
    journal lastpage0111006-10
    page10
    treeJournal of Engineering for Gas Turbines and Power:;2020:;volume( 142 ):;issue: 011
    contenttypeFulltext
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