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    Simulation of Particle Trajectories and Erosion in a Centrifugal Compressor

    Source: Journal of Turbomachinery:;2012:;volume( 134 ):;issue: 005::page 51022
    Author:
    Adel Ghenaiet
    DOI: 10.1115/1.4004448
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Turbocompressors manipulating particle-laden airflows suffer from severe erosion damages which affect their operating performance and lifetime. This paper presents the results of a numerical investigation of the dynamics of sand particles and the subsequent erosion in a centrifugal compressor. The particle trajectories simulations used a developed code based on a stochastic Lagrangian model, which solves the equations of motion separately from the airflow, whereas the tracking of particles in different computational cells used the finite element method. The number of particles, sizes, and initial positions were specified, conformed to a sand particle size distribution AC_coarse (0–200 μm), and a given concentration profile. The obtained results show that the speed of rotation and particle size strongly affect the trajectories of particles and their locations of impact. Erosion is spreading over the pressure side of the main blade. Regions of high erosion rates are seen over the leading edge, at the inducer top corner and along the blade tip. Over the splitter pressure side erosion wear is much less than the main blade. The suction sides are almost without erosion except near the leading edge, and the casing is mainly affected over the inducer and tips of the blades.
    keyword(s): Sands , Particulate matter , Compressors , Impellers , Erosion , Blades , Flow (Dynamics) AND Pressure ,
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      Simulation of Particle Trajectories and Erosion in a Centrifugal Compressor

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    http://yetl.yabesh.ir/yetl1/handle/yetl/150459
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    contributor authorAdel Ghenaiet
    date accessioned2017-05-09T00:55:04Z
    date available2017-05-09T00:55:04Z
    date copyrightSeptember, 2012
    date issued2012
    identifier issn0889-504X
    identifier otherJOTUEI-926079#051022_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/150459
    description abstractTurbocompressors manipulating particle-laden airflows suffer from severe erosion damages which affect their operating performance and lifetime. This paper presents the results of a numerical investigation of the dynamics of sand particles and the subsequent erosion in a centrifugal compressor. The particle trajectories simulations used a developed code based on a stochastic Lagrangian model, which solves the equations of motion separately from the airflow, whereas the tracking of particles in different computational cells used the finite element method. The number of particles, sizes, and initial positions were specified, conformed to a sand particle size distribution AC_coarse (0–200 μm), and a given concentration profile. The obtained results show that the speed of rotation and particle size strongly affect the trajectories of particles and their locations of impact. Erosion is spreading over the pressure side of the main blade. Regions of high erosion rates are seen over the leading edge, at the inducer top corner and along the blade tip. Over the splitter pressure side erosion wear is much less than the main blade. The suction sides are almost without erosion except near the leading edge, and the casing is mainly affected over the inducer and tips of the blades.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleSimulation of Particle Trajectories and Erosion in a Centrifugal Compressor
    typeJournal Paper
    journal volume134
    journal issue5
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4004448
    journal fristpage51022
    identifier eissn1528-8900
    keywordsSands
    keywordsParticulate matter
    keywordsCompressors
    keywordsImpellers
    keywordsErosion
    keywordsBlades
    keywordsFlow (Dynamics) AND Pressure
    treeJournal of Turbomachinery:;2012:;volume( 134 ):;issue: 005
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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