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01 Introduction GvK

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    Challenge the future

    DelftUniversity ofTechnology

    Wind TurbineDesign

    AE4-W09

    5 ECTS

    2010

    Prof. Dr. Ir. G.A.M van Kuik, Gijs

    and many other DUWIND experts

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    General Course Information

    All communication through Blackboard. Allsheets and material are available at Blackboard

    There is no hard-copy binder The course has a little overlap with:

    1. AE4-W012: Rotor Aerodynamics(now running)

    2. AE4-W013: Wind and Site Conditions, first semester

    so here only: the use of , and no detailed background

    AE3W02: Introduction to wind energy, is

    mandatory as preceding course. Testing of thisknowledge is done by homework assignments.

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    Set-up of the course

    Lectures, homework and group assignment

    Attendance of lectures not mandatory but strongly

    advised. Examination is by the group assignment

    Admission to group assignment requires satisfactory

    execution of the homework assignments

    Feed-back on course is highly appreciated

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    The planning

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    Background Material for this hour

    Volume 1: Turbine Technology, from WindEnergy, the Facts

    Available at Blackboard and

    http://www.ewea.org/index.php?id=91

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    The design process, starting freshMany classificationsand/ or terminologyexist. Here:

    Conceptual design

    Preliminary design

    Detailed design

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    The design process

    Conceptual design

    Preliminary design

    Detailed design

    All choicesdepend on each other

    Each solution/param. to be detailed

    independent of others

    Turbine concept (e.g. const/var. ,number of blades, gearbox or not, )

    Main parameters (e.g. diameter, hubheight, wind class, eigenfrequencies)

    Main operational aspects (e.g. safety,

    control, maintenance, grid aspects)

    Main materials (tower & bladematerial, casted or welded bedplate)

    Targeted weights, annual yield, ex-factory costs

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    The design process

    Conceptual design

    Preliminary design

    Detailed design

    Main component/systemis detailed to subcomponent level

    Subcomponents to be detailed

    independent of others

    Rotor: blade geometry andconstruction, specs of pitch bearing

    Nacelle: dimensions, weights, specsof axes, bearings, couplings, gearbox, yaw drives, bedplate, housing

    Tower: wall thickness, access,elevator, installation process

    Electric: specs of generator, power

    electronics, trafo

    Control: soft- & hardware

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    The design process

    Conceptual design

    Preliminary design

    Detailed design

    All components aredetailed to sufficient level

    All is ready for manufacturing

    or ordering

    Rotor: sheet lay-out, resindistribution, curing times, details of

    hub, actuators, bearings, battery andcontrol back-up equipment

    Nacelle: drawings and detailed specs

    of axes, bearings, couplings, gearbox, yaw drives, bedplate, housing

    Etcetera

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    The design process

    Conceptual design

    Preliminary design

    Detailed design

    Driven by market developments,accumulated experience,manufacturing capabilities, new

    applications e.g. deep wateroffshore. Usually: carefulupscaling of previous version

    Here the research & engineeringknowledge is used to fullextend. This design phase is the

    area of this course, with someexcursions to conceptual design

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    Concept development: scaling

    effects

    Rated Power Diameter2.155

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    Concept development: scaling

    effects

    Hub height Diameter-0.3

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    Concept development: scaling

    effects

    Rotor mass Diameter2.6

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    Concept development: scaling

    effects

    All trends show an exponent < 3 which would follow

    from straightforward upscaling (square cube law) Due to

    increased hub height higher wind speeds

    improved technology

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    Scaling effects in case of unchanged

    design

    Enercon main shaft mass follows square cube law

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    Main pin (it is stationairy)

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    Some

    abandonedconcepts

    Darrieus turbine

    - Lower Cp

    - Guy wires

    Revival for use inbuilt environment:

    BUT:

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    Some

    abandonedconcepts

    Single bladed

    Turbine

    - High tip loss- High noise

    level

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    Some

    abandonedconcepts

    Flexible, passivelycontrolled(downwind)turbines

    - Difficulttechnology

    - Most suited for 2-bladers

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    Modern turbines are common in:

    Number of blades: 3

    Collective pitch controlVariable speed operation

    and differ in:Gearbox or direct drive or mixed

    Rotor support (main bearing / axis)

    Nacelle frame

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    Schematic

    Conceptual

    Preliminary

    Detailed

    DISAS

    TER

    !

    Example: soil stiffness / foundationresults in wrong support structurefrequency

    turbine

    tower

    soil

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    Schematic

    Conceptual

    Preliminary

    Detailed

    Major

    proble

    m

    Example: many gearbox problems,control problems

    turbine

    gearbox

    bear-ing

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    The design process, starting fromprevious experience

    Preceding, usuallysmaller, turbine

    Conceptual design

    Preliminary design

    Detailed design Series productionprototype

    measurements

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    Design is part of prototype

    developmentConcept, wind class, grid

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    Survey of simplifying design

    assumptions (1)

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    assumptions (2)


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