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    Piezohydraulic Actuator Development for Microjet Flow Control

    Source: Journal of Mechanical Design:;2009:;volume( 131 ):;issue: 009::page 91001
    Author:
    William S. Oates
    ,
    Fei Liu
    DOI: 10.1115/1.3158986
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes the development of a piezohydraulic actuator for broadband microjet flow control applications. The actuator utilizes a lead zirconate titanate (PZT) stack actuator and a hydraulic amplification design to achieve relatively large displacements in a compact actuator to control flow through a microjet orifice. Displacement amplification of 81 times the stack actuator displacement was achieved using a new dual-diaphragm design. The nonlinear and hysteretic field-coupled material behavior, structural dynamics, and fluid dynamics of the actuator are modeled using a system dynamic model and compared with experimental results. The nonlinear and hysteretic piezohydraulic actuator characteristics are shown to be strongly dependent on the nonlinear deformation of the rubber diaphragm and minor loop hysteresis of the PZT stack actuator. The modeling technique provides a design tool for broadband performance predictions and system optimization to facilitate implementation of the actuator in a flow environment.
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      Piezohydraulic Actuator Development for Microjet Flow Control

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    http://yetl.yabesh.ir/yetl1/handle/yetl/141323
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    contributor authorWilliam S. Oates
    contributor authorFei Liu
    date accessioned2017-05-09T00:34:16Z
    date available2017-05-09T00:34:16Z
    date copyrightSeptember, 2009
    date issued2009
    identifier issn1050-0472
    identifier otherJMDEDB-27907#091001_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/141323
    description abstractThis paper describes the development of a piezohydraulic actuator for broadband microjet flow control applications. The actuator utilizes a lead zirconate titanate (PZT) stack actuator and a hydraulic amplification design to achieve relatively large displacements in a compact actuator to control flow through a microjet orifice. Displacement amplification of 81 times the stack actuator displacement was achieved using a new dual-diaphragm design. The nonlinear and hysteretic field-coupled material behavior, structural dynamics, and fluid dynamics of the actuator are modeled using a system dynamic model and compared with experimental results. The nonlinear and hysteretic piezohydraulic actuator characteristics are shown to be strongly dependent on the nonlinear deformation of the rubber diaphragm and minor loop hysteresis of the PZT stack actuator. The modeling technique provides a design tool for broadband performance predictions and system optimization to facilitate implementation of the actuator in a flow environment.
    publisherThe American Society of Mechanical Engineers (ASME)
    titlePiezohydraulic Actuator Development for Microjet Flow Control
    typeJournal Paper
    journal volume131
    journal issue9
    journal titleJournal of Mechanical Design
    identifier doi10.1115/1.3158986
    journal fristpage91001
    identifier eissn1528-9001
    treeJournal of Mechanical Design:;2009:;volume( 131 ):;issue: 009
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian