• Login
    View Item 
    •   DSpace Home
    • ASME
    • Journal of Dynamic Systems, Measurement, and Control
    • View Item
    •   DSpace Home
    • ASME
    • Journal of Dynamic Systems, Measurement, and Control
    • View Item
    JavaScript is disabled for your browser. Some features of this site may not work without it.

    Control Framework and Integrative Design Method for an Adaptive Wind Turbine Blade

    Thumbnail
    View/Open
    ds_142_10_101001.pdf (1.951Mb)
    Date
    2020
    Author
    Khakpour Nejadkhaki, Hamid
    Hall, John F.
    Metadata
    Show full item record
    Abstract
    A control framework and integrative design method for an adaptive wind turbine blade is presented. The blade is adapted by actively transforming the twist angle distribution (TAD) along the blade. This can alleviate fatigue loads and improve wind capture. In this paper, we focus on wind capture. The proposed design concept consists of a rigid spar that is surrounded by a series of flexible blade sections. Each section has two zones of stiffness. The sections are actuated at each end to deform the TAD. A quasi-static control technique is proposed for the TAD. The controller sets the position of the blade actuators that shape the TAD during steady-state operation. A design procedure is used to define the required TAD as a function of the wind speed. This is based on an optimization procedure that minimizes the deviation between the actual TAD and that found in the aerodynamic design. The design inputs for this optimization problem include the stiffness for each zone of the section, and the actuator locations along the blade. Given the optimal TAD at each wind speed, the free position of the blade is established using a dynamic programming technique. The position is selected based on minimal actuation energy according to wind conditions at any installation site. The proposed framework is demonstrated using a National Renewable Energy Laboratory (NREL) certified wind turbine model with recorded wind data. An increase in efficiency of 3.8% with only a deviation of 0.34% from the aerodynamic TAD is observed.
    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/4274546
    Collections
    • Journal of Dynamic Systems, Measurement, and Control

    DSpace software copyright © 2002-2015  DuraSpace
    Contact Us | Send Feedback
    Theme by 
    @mire NV
     

     

    Browse

    All of DSpaceCommunities & CollectionsBy Issue DateAuthorsTitlesSubjectsThis CollectionBy Issue DateAuthorsTitlesSubjects

    My Account

    LoginRegister

    Statistics

    View Usage Statistics

    DSpace software copyright © 2002-2015  DuraSpace
    Contact Us | Send Feedback
    Theme by 
    @mire NV