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    Design Considerations of Rotor Cone Angle for Downwind Wind Turbines

    Source: Journal of Engineering for Gas Turbines and Power:;2016:;volume( 138 ):;issue: 005::page 52602
    Author:
    Kress, Christian
    ,
    Chokani, Ndaona
    ,
    Abhari, Reza S.
    DOI: 10.1115/1.4031604
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Due to their potential to use light, flexible blades, downwind turbines are well suited for offshore floating platforms, for which there is a need to substantially lower the cost of windgenerated electricity. However, downwind rotors must operate in the presence of the tower's wakes with which are associated strong changes in flow incidence, and thus high fatigue loads. In order to guide the development of design rules for multimegawatt downwind turbines, a comprehensive experimental study has been conducted to better understand the characteristics of the unsteady rotor torque on downwind turbines. Highfrequency measurements of the unsteady rotor torque on a model turbine that can be configured with rotors of different cone angles and operated either downwind or upwind in wellcontrolled flow conditions are conducted. The measurements show that in the case of the downwind turbine, the blade's passage through the tower's wake accounts for 56% to 61% of the variance of the rotor torque; the proportion of this unsteadiness is independent of the cone angle. For nonoptimum tip speed ratios (TSRs), the increase in unsteadiness is consistently less for downwind configurations than for upwind configurations. For the 5 degcone downwind configuration, the increase in rotor torque unsteadiness is 13–18% of the increase observed for the 5degcone upwind configuration for nonoptimum TSRs. Thus from a design perspective, downwind rotor configurations offer above or below rated wind speed, a smaller increase in unsteadiness of the rotor torque compared to upwind turbine configurations. These characteristics differ from upwind turbines, on which broadband vortex shedding from the blade is the primary source of the unsteadiness, which may be reduced by increasing the rotortower clearance. It is suggested that given the strong periodic character of the blade's passage through the tower's wake, the turbine control system may be designed to reduce fatigue loads and there is a broader design space on downwind turbines that can be exploited for peak load mitigation by moderately adjusting the blade's stiffness.
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      Design Considerations of Rotor Cone Angle for Downwind Wind Turbines

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    http://yetl.yabesh.ir/yetl1/handle/yetl/161077
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorKress, Christian
    contributor authorChokani, Ndaona
    contributor authorAbhari, Reza S.
    date accessioned2017-05-09T01:28:26Z
    date available2017-05-09T01:28:26Z
    date issued2016
    identifier issn1528-8919
    identifier othergtp_138_05_052602.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/161077
    description abstractDue to their potential to use light, flexible blades, downwind turbines are well suited for offshore floating platforms, for which there is a need to substantially lower the cost of windgenerated electricity. However, downwind rotors must operate in the presence of the tower's wakes with which are associated strong changes in flow incidence, and thus high fatigue loads. In order to guide the development of design rules for multimegawatt downwind turbines, a comprehensive experimental study has been conducted to better understand the characteristics of the unsteady rotor torque on downwind turbines. Highfrequency measurements of the unsteady rotor torque on a model turbine that can be configured with rotors of different cone angles and operated either downwind or upwind in wellcontrolled flow conditions are conducted. The measurements show that in the case of the downwind turbine, the blade's passage through the tower's wake accounts for 56% to 61% of the variance of the rotor torque; the proportion of this unsteadiness is independent of the cone angle. For nonoptimum tip speed ratios (TSRs), the increase in unsteadiness is consistently less for downwind configurations than for upwind configurations. For the 5 degcone downwind configuration, the increase in rotor torque unsteadiness is 13–18% of the increase observed for the 5degcone upwind configuration for nonoptimum TSRs. Thus from a design perspective, downwind rotor configurations offer above or below rated wind speed, a smaller increase in unsteadiness of the rotor torque compared to upwind turbine configurations. These characteristics differ from upwind turbines, on which broadband vortex shedding from the blade is the primary source of the unsteadiness, which may be reduced by increasing the rotortower clearance. It is suggested that given the strong periodic character of the blade's passage through the tower's wake, the turbine control system may be designed to reduce fatigue loads and there is a broader design space on downwind turbines that can be exploited for peak load mitigation by moderately adjusting the blade's stiffness.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleDesign Considerations of Rotor Cone Angle for Downwind Wind Turbines
    typeJournal Paper
    journal volume138
    journal issue5
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4031604
    journal fristpage52602
    journal lastpage52602
    identifier eissn0742-4795
    treeJournal of Engineering for Gas Turbines and Power:;2016:;volume( 138 ):;issue: 005
    contenttypeFulltext
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