YaBeSH Engineering and Technology Library

    • Journals
    • PaperQuest
    • YSE Standards
    • YaBeSH
    • Login
    View Item 
    •   YE&T Library
    • ASME
    • Journal of Computing and Information Science in Engineering
    • View Item
    •   YE&T Library
    • ASME
    • Journal of Computing and Information Science in Engineering
    • View Item
    • All Fields
    • Source Title
    • Year
    • Publisher
    • Title
    • Subject
    • Author
    • DOI
    • ISBN
    Advanced Search
    JavaScript is disabled for your browser. Some features of this site may not work without it.

    Archive

    A Finite Element Boundary Condition Setting Method for the Virtual Mounting of Compliant Components

    Source: Journal of Computing and Information Science in Engineering:;2015:;volume( 015 ):;issue: 004::page 41005
    Author:
    Abenhaim, Gad N.
    ,
    Desrochers, Alain
    ,
    Tahan, Antoine S.
    ,
    Bigeon, Jean
    DOI: 10.1115/1.4031152
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Using finiteelement analysis (FEA) to numerically mount compliant components onto their inspection fixture is an approach proposed by researchers in the field of computational metrology. To address the shortcomings of the underlying principle of current methods, this paper presents a boundary displacement constrained (BDC) optimization using FEA. The optimization seeks to minimize the distance between corresponding points, in the scanned manufactured part and the nominal model, that are in unconstrained regions. This is done while maintaining that a distance between corresponding points in constrained regions (i.e., fixing points) remains within a specified contact distance. At the same time, the optimization limits the magnitude and direction of forces on boundary. In contrast to the current methods, postprocessing of the point cloud is not required since the method uses information retrieved from the FEA of the nominal model to estimate the manufactured part’s mechanical behavior. To investigate the performance of the proposed method, it is tested on ten (10) freestate simulated manufactured aerospace panels that differ in their level of induced deformation. Results are then compared to those obtained using the underlying principles of current methods.
    • Download: (1.435Mb)
    • Show Full MetaData Hide Full MetaData
    • Get RIS
    • Item Order
    • Go To Publisher
    • Price: 5000 Rial
    • Statistics

      A Finite Element Boundary Condition Setting Method for the Virtual Mounting of Compliant Components

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/157417
    Collections
    • Journal of Computing and Information Science in Engineering

    Show full item record

    contributor authorAbenhaim, Gad N.
    contributor authorDesrochers, Alain
    contributor authorTahan, Antoine S.
    contributor authorBigeon, Jean
    date accessioned2017-05-09T01:16:08Z
    date available2017-05-09T01:16:08Z
    date issued2015
    identifier issn1530-9827
    identifier otherjcise_015_04_041005.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/157417
    description abstractUsing finiteelement analysis (FEA) to numerically mount compliant components onto their inspection fixture is an approach proposed by researchers in the field of computational metrology. To address the shortcomings of the underlying principle of current methods, this paper presents a boundary displacement constrained (BDC) optimization using FEA. The optimization seeks to minimize the distance between corresponding points, in the scanned manufactured part and the nominal model, that are in unconstrained regions. This is done while maintaining that a distance between corresponding points in constrained regions (i.e., fixing points) remains within a specified contact distance. At the same time, the optimization limits the magnitude and direction of forces on boundary. In contrast to the current methods, postprocessing of the point cloud is not required since the method uses information retrieved from the FEA of the nominal model to estimate the manufactured part’s mechanical behavior. To investigate the performance of the proposed method, it is tested on ten (10) freestate simulated manufactured aerospace panels that differ in their level of induced deformation. Results are then compared to those obtained using the underlying principles of current methods.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleA Finite Element Boundary Condition Setting Method for the Virtual Mounting of Compliant Components
    typeJournal Paper
    journal volume15
    journal issue4
    journal titleJournal of Computing and Information Science in Engineering
    identifier doi10.1115/1.4031152
    journal fristpage41005
    journal lastpage41005
    identifier eissn1530-9827
    treeJournal of Computing and Information Science in Engineering:;2015:;volume( 015 ):;issue: 004
    contenttypeFulltext
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian
     
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian