YaBeSH Engineering and Technology Library

    • Journals
    • PaperQuest
    • YSE Standards
    • YaBeSH
    • Login
    View Item 
    •   YE&T Library
    • ASCE
    • Journal of Aerospace Engineering
    • View Item
    •   YE&T Library
    • ASCE
    • Journal of Aerospace 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

    Research on Key Technology of Hydraulic Impulse Testing Equipment

    Source: Journal of Aerospace Engineering:;2011:;Volume ( 024 ):;issue: 004
    Author:
    Kang Song
    ,
    Shipin Zhao
    ,
    Junbi Liao
    ,
    Yitong Dou
    ,
    Xia Zhao
    DOI: 10.1061/(ASCE)AS.1943-5525.0000086
    Publisher: American Society of Civil Engineers
    Abstract: Aiming at the ability of the key technology problem of hydraulic impulse-testing equipment to reliably and controllably produce standard hydraulic pulse, on the basis of the pipe-cubage model, a ramp model has been established for the first time, and the response expression of ramp input has been deduced. The computation results indicate that the maximum adjustable excess of a ramp-input model is 67.7%. According to the step-input and the ramp-input models, theoretical analysis shows that the ramp-input signal can be treated as a step-input signal when the time of ramp input is less than one-tenth of system oscillation periods, and the simulation results indicate that the difference of the maximal excess of both ramp and step models is no more than 7%. Both the step-input and ramp-input models have carried out digital simulations using software and the electrohydraulic assimilation method. The simulation results show that by adjusting pipe-cubage model system parameters, such as cubage, length of pipe, and diameter of pipe, the standard pulse can be produced.
    • Download: (673.2Kb)
    • Show Full MetaData Hide Full MetaData
    • Get RIS
    • Item Order
    • Go To Publisher
    • Price: 5000 Rial
    • Statistics

      Research on Key Technology of Hydraulic Impulse Testing Equipment

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/56229
    Collections
    • Journal of Aerospace Engineering

    Show full item record

    contributor authorKang Song
    contributor authorShipin Zhao
    contributor authorJunbi Liao
    contributor authorYitong Dou
    contributor authorXia Zhao
    date accessioned2017-05-08T21:33:47Z
    date available2017-05-08T21:33:47Z
    date copyrightOctober 2011
    date issued2011
    identifier other%28asce%29as%2E1943-5525%2E0000086.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/56229
    description abstractAiming at the ability of the key technology problem of hydraulic impulse-testing equipment to reliably and controllably produce standard hydraulic pulse, on the basis of the pipe-cubage model, a ramp model has been established for the first time, and the response expression of ramp input has been deduced. The computation results indicate that the maximum adjustable excess of a ramp-input model is 67.7%. According to the step-input and the ramp-input models, theoretical analysis shows that the ramp-input signal can be treated as a step-input signal when the time of ramp input is less than one-tenth of system oscillation periods, and the simulation results indicate that the difference of the maximal excess of both ramp and step models is no more than 7%. Both the step-input and ramp-input models have carried out digital simulations using software and the electrohydraulic assimilation method. The simulation results show that by adjusting pipe-cubage model system parameters, such as cubage, length of pipe, and diameter of pipe, the standard pulse can be produced.
    publisherAmerican Society of Civil Engineers
    titleResearch on Key Technology of Hydraulic Impulse Testing Equipment
    typeJournal Paper
    journal volume24
    journal issue4
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)AS.1943-5525.0000086
    treeJournal of Aerospace Engineering:;2011:;Volume ( 024 ):;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