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    Numerical Experimental Confrontation in the Simulation of Tool/Abradable Material Interaction

    Source: Journal of Engineering for Gas Turbines and Power:;2013:;volume( 135 ):;issue: 006::page 62102
    Author:
    Batailly, Alain
    ,
    Cuny, Marion
    ,
    Legrand, Mathias
    ,
    Philippon, Sylvain
    DOI: 10.1115/1.4023262
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In turbomachinery, depositing abradable coatings along the circonference of casings is recognized as a robust solution which combines the adjustment of operating clearances with the reduction of nonrepairable damages potentially affecting the rotating blades. Accordingly, the modeling of the removal process experienced by these materials is of growing industrial importance. Based on a numerical strategy detailed in a previous publication by the authors, the present study aims at describing the mechanical behavior of abradable coatings used within turbomachines in the context of translational highspeed interactions with a rigid tool. The developed plastic constitutive law macroscopically capturing the abradable material removal is first enriched to account for its strain rate dependence. Then, a sensitivity analysis with respect to a few parameters of interest is conducted and calibration of the numerical investigation with existing experimental data validates the proposed approach. Finally, the strainrate dependence of the viscoplastic law implemented within a full numerical threedimensional rotor/stator interaction is addressed. Results reveal that viscoplastic terms have minor effects in turbomachinery interactions.
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      Numerical Experimental Confrontation in the Simulation of Tool/Abradable Material Interaction

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    http://yetl.yabesh.ir/yetl1/handle/yetl/151630
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    contributor authorBatailly, Alain
    contributor authorCuny, Marion
    contributor authorLegrand, Mathias
    contributor authorPhilippon, Sylvain
    date accessioned2017-05-09T00:58:18Z
    date available2017-05-09T00:58:18Z
    date issued2013
    identifier issn1528-8919
    identifier othergtp_135_6_062102.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/151630
    description abstractIn turbomachinery, depositing abradable coatings along the circonference of casings is recognized as a robust solution which combines the adjustment of operating clearances with the reduction of nonrepairable damages potentially affecting the rotating blades. Accordingly, the modeling of the removal process experienced by these materials is of growing industrial importance. Based on a numerical strategy detailed in a previous publication by the authors, the present study aims at describing the mechanical behavior of abradable coatings used within turbomachines in the context of translational highspeed interactions with a rigid tool. The developed plastic constitutive law macroscopically capturing the abradable material removal is first enriched to account for its strain rate dependence. Then, a sensitivity analysis with respect to a few parameters of interest is conducted and calibration of the numerical investigation with existing experimental data validates the proposed approach. Finally, the strainrate dependence of the viscoplastic law implemented within a full numerical threedimensional rotor/stator interaction is addressed. Results reveal that viscoplastic terms have minor effects in turbomachinery interactions.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleNumerical Experimental Confrontation in the Simulation of Tool/Abradable Material Interaction
    typeJournal Paper
    journal volume135
    journal issue6
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4023262
    journal fristpage62102
    journal lastpage62102
    identifier eissn0742-4795
    treeJournal of Engineering for Gas Turbines and Power:;2013:;volume( 135 ):;issue: 006
    contenttypeFulltext
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