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    Gas Turbine Fouling Tests: Review, Critical Analysis, and Particle Impact Behavior Map

    Source: Journal of Engineering for Gas Turbines and Power:;2019:;volume( 141 ):;issue: 003::page 32601
    Author:
    Suman, Alessio
    ,
    Casari, Nicola
    ,
    Fabbri, Elettra
    ,
    Pinelli, Michele
    ,
    di Mare, Luca
    ,
    Montomoli, Francesco
    DOI: 10.1115/1.4041282
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Fouling affects gas turbine operation, and airborne or fuel contaminants, under certain conditions, become very likely to adhere to surfaces if impact takes place. Particle sticking implies the change in shape in terms of roughness of the impinged surface. The consequences of these deposits could be dramatic: these effects can shut an aircraft engine down or derate a land-based power unit. This occurrence may happen due to the reduction of the compressor flow rate and the turbine capacity, caused by a variation in the HPT nozzle throat area (geometric blockage due to the thickness of the deposited layer and the aerodynamic blockage due to the increased roughness, and in turn boundary layer). Several methods to quantify particle sticking have been proposed in literature so far, and the experimental data used for their validation vary in a wide range of materials and conditions. The experimental analyzes have been supported by (and have given inspiration to) increasingly realistic mathematical models. Experimental tests have been carried out on (i) a full scale gas turbine unit, (ii) wind tunnel testing or hot gas facilities using stationary cascades, able to reproduce the same conditions of gas turbine nozzle operation and finally, (iii) wind tunnel testing or hot gas facilities using a coupon as the target. In this review, the whole variety of experimental tests performed are gathered and classified according to composition, size, temperature, and particle impact velocity. Using particle viscosity and sticking prediction models, over seventy (70) tests are compared with each other and with the model previsions providing a useful starting point for a comprehensive critical analysis. Due to the variety of test conditions, the related results are difficult to be pieced together due to differences in particle material and properties. The historical data of particle deposition obtained over thirty (30) years are classified using particle kinetic energy and the ratio between particle temperature and its softening temperature. Qualitative thresholds for the distinction between particle deposition, surface erosion, and particle break-up, based on particle properties and impact conditions, are identified. The outcome of this paper can be used for further development of sticking models or as a starting point for new insight into the problem.
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      Gas Turbine Fouling Tests: Review, Critical Analysis, and Particle Impact Behavior Map

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    contributor authorSuman, Alessio
    contributor authorCasari, Nicola
    contributor authorFabbri, Elettra
    contributor authorPinelli, Michele
    contributor authordi Mare, Luca
    contributor authorMontomoli, Francesco
    date accessioned2019-03-17T10:59:01Z
    date available2019-03-17T10:59:01Z
    date copyright11/29/2018 12:00:00 AM
    date issued2019
    identifier issn0742-4795
    identifier othergtp_141_03_032601.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4256486
    description abstractFouling affects gas turbine operation, and airborne or fuel contaminants, under certain conditions, become very likely to adhere to surfaces if impact takes place. Particle sticking implies the change in shape in terms of roughness of the impinged surface. The consequences of these deposits could be dramatic: these effects can shut an aircraft engine down or derate a land-based power unit. This occurrence may happen due to the reduction of the compressor flow rate and the turbine capacity, caused by a variation in the HPT nozzle throat area (geometric blockage due to the thickness of the deposited layer and the aerodynamic blockage due to the increased roughness, and in turn boundary layer). Several methods to quantify particle sticking have been proposed in literature so far, and the experimental data used for their validation vary in a wide range of materials and conditions. The experimental analyzes have been supported by (and have given inspiration to) increasingly realistic mathematical models. Experimental tests have been carried out on (i) a full scale gas turbine unit, (ii) wind tunnel testing or hot gas facilities using stationary cascades, able to reproduce the same conditions of gas turbine nozzle operation and finally, (iii) wind tunnel testing or hot gas facilities using a coupon as the target. In this review, the whole variety of experimental tests performed are gathered and classified according to composition, size, temperature, and particle impact velocity. Using particle viscosity and sticking prediction models, over seventy (70) tests are compared with each other and with the model previsions providing a useful starting point for a comprehensive critical analysis. Due to the variety of test conditions, the related results are difficult to be pieced together due to differences in particle material and properties. The historical data of particle deposition obtained over thirty (30) years are classified using particle kinetic energy and the ratio between particle temperature and its softening temperature. Qualitative thresholds for the distinction between particle deposition, surface erosion, and particle break-up, based on particle properties and impact conditions, are identified. The outcome of this paper can be used for further development of sticking models or as a starting point for new insight into the problem.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleGas Turbine Fouling Tests: Review, Critical Analysis, and Particle Impact Behavior Map
    typeJournal Paper
    journal volume141
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4041282
    journal fristpage32601
    journal lastpage032601-18
    treeJournal of Engineering for Gas Turbines and Power:;2019:;volume( 141 ):;issue: 003
    contenttypeFulltext
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