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Development of a MW scale wind turbine for high wind complex terrain sites the MEGAWIND project

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Title: Development of a MW scale wind turbine for high wind complex terrain sites the MEGAWIND project


1
Development of a MW scale wind turbine for high
wind complex terrain sites the MEGAWIND project
European Wind Energy Conference 2006 Athens,
Greece, 27/2/2006-2/3/2006 Technical
TrackSession CT3 Innovative turbines,
components, systems and techniques
  • P. Vionis, D. Lekou, F. Gonzalez, J. Mieres,T.
    Kossivas, E. Soria,
  • E. Gutierrez, C. Galiotis, T. P. Philippidis, S.
    Voutsinas, D. Hofmann

2
The Partners
  • Industrial (3)
  • NECSO (ES), MADE (ES) and
  • GEOBIOLOGIKI SA (GR)
  • Research Organisations (4)
  • CRES (GR), EC-JRC-IPCS (IT),
  • CIEMAT (ES) and ICE/HT (GR)
  • Universities (3)
  • UP (GR), NTUA (GR) and
  • DU/NU (UK)

3
Project Background
Some of the most promising areas for wind energy
development are in high wind mountainous sites of
poor infrastructure High transportation and
erection costs are discouraging the installation
of MW size WTs in such areas
Strategic aim To develop procedures to
circumvent the barriers hindering the deployment
of large wind turbines in such sites
4
Project objectives
  • The development of critical components of a 1.3
    MW WT focusing on the following aspects
  • an alternative tower allowing for on-site
    manufacturing
  • high wind speed optimised blades featuring
    splitting parts
  • advanced geabox aiming at high reliability, easy
    maintenance and low noise

5
Advanced Composite Tower
  • Extensive research has been carried out with
    regard to
  • composite materials suitable for composite
    structures
  • alternative joining designs
  • alternative tower designs
  • Environmental effects on selected materials
  • Design focused on 2 alternative concepts
  • Monolithic (GFRP)
  • Hybrid (GFRP high strength concrete)
  • Design is strongly influenced by manufacturing
    processes and relevant costs
  • Large scale structural tests on ½ length
    1/3-scale prototypes of both designs have been
    carried out

6
Monolithic Tower test configuration in
7
During test and final failure
8
Monolithic Tower final test in
Base Moment N?m versus Curvature m-1
1.8 MNm
9
Sandwich Tower test configuration in
10
Sandwich Tower test configuration in
Base Moment N?m versus Curvature m-1
11
Performance of H. Tower
12
Comparison between M. H. Towers
13
Advanced Composite Tower Conclusions from 1/3
scale tests
  • The monolithic tower meets all the serviceability
    and safety criteria
  • The equivalent peak bending moment at the 1/3
    scale was 0.72 MNm, while the tower failure
    occurred at 1.8 MNm (SF2.3)
  • SF could be improved to 3.2 with better quality
    assurance on the filament winding lay-up
  • The hybrid tower meets all the serviceability and
    safety criteria, although the production quality
    assurance lower than ordered
  • Tower base moment at failure 1.17 MNm (SF1.6)
  • SF could be improved to 2.5 had the FRP material
    modulus been only equal to the monolithic tower
    tested.

14
Advanced Composite Tower- Final Design
  • Total tower length 40.8 m
  • Diameter varying from 3.14 m (bottom) to 2.40 m
    (top)
  • 17 parts 2.4 m each
  • 8 parts carbon fibre skins and polyurethane core
  • 1 part hybrid glass/carbon fibre skins and high
    strength concrete core
  • 8 parts glass fibre skins and polyurethane core

15
Advanced Composite Tower- Constructed
16
Advanced Composite Tower- Test preparations
17
Split Rotor Blade Aerodynamic Design
Guidelines
  • Optimize the blade for maximum Energy Production.
  • Design a blade to produce a rated power of 1300
    KW.
  • Design new optimised airfoils.
  • No use of external aerodynamic reinforcements.
  • Design of the Airfoil sections
  • Generate a database of airfoils, optimized for
    maximum energy production over the whole range of
    their operation
  • Design airfoils insensitive to the transition of
    their boundary layer.
  • Select airfoils exhibiting a flat top CL and a
    smooth post stall drop of CL in order to
    reduce/avoid stall induced vibrations.

18
Split Rotor Blade Designed profile CL-CD
characteristics
19
Split Rotor Blade Structural design
T-Bolt concept was selected for the intermediate
joint
20
Split Rotor Blade Intermediate Joint Design
  • Designed According to VDI 2230
  • 45 necked-down bolts (M24x2)
  • Bolt Length 453mm
  • Design Load (ECDneg)
  • F 85.878 kN

21
Split Rotor Blade - Structural Design FEM model
of blade 30_1(GRP) Tsai-Wu failure criterion
IEC 61400-1 Class I
22
Split Rotor Blade Component testing
  • Full-scale specimen
  • study the behaviour of the intermediate joint
  • Bolt preloading
  • Estimation of joint constant,F
  • Separation Load
  • Static and fatigue strength of joint

23
Split Rotor Blade
Manufacturing
Blade inner part - 4595 kg - 12.4 m
Blade outer part - 1828 kg - 17.25 m
ready for transportation
24
Split Rotor Blade Blade assembly
25
Split Rotor Blade Full scale Testing (edgewis
e)
26
Split Rotor Blade Full scale Testing (flapwis
e)
Max test load 4.3 MNm at root
Max test load 4.3 MNm at root
27
Advanced Transmission System
  • Feasibility Studies of Alternative Gearbox
    Concepts
  • 4 Epicyclic Gearboxes
  • 5 Parallel Axis Gearboxes
  • Selected Gearbox 3 Stage Single Helical, Dual
    Load Path with Balance Beam Load Equalisation
  • Advantages - Lowest Part Count - 8 Gears
  • 12 Bearings
  • - Low cost
  • - No Significant Weight or Size Penalty

28
Advanced Transmission System 3 Stage, Dual Load
Path, Balance Beam
29
Advanced Transmission System 3 Stage, Dual Load
Path, Balance Beam
  • PROS
  • Simple load path balancing technique
  • Very compact overall design (40 smaller than
    standard dual path parallel axis gearbox)
  • Small number of Gear elements
  • Small number of Bearings
  • Good access to both gear elements and bearings
  • Potential to design very quiet gearbox
  • CONS
  • Slightly higher and wider than reference
    Epicyclic 2 Helical stage arrangement

30
Measurement campaign
  • Since the prototype gearbox could not be
    manufactured in time, the dynamic behaviour of a
    gearbox of similar concept (3 stage, duplex load
    path) operating on a MADE 1.3 MW WT was
    investigated
  • An advanced measuring system was implemented on
    the refitted gearbox components
  • Measurements included
  • bending moments and torsion on the main shaft,
  • intermediate shaft torque
  • axial load on the low speed shaft
  • movement of the gearbox
  • Power data, rotor speed and azimuthal position
  • Meteorological data

31
Sensor installation
32
Measurement campaign
33
Conclusions
  • Innovative solutions have been pursued for the
    major WT components tower, rotor gearbox
  • TOWER
  • A 40 m composite tower was for the first time
    manufactured and full scale tested
  • Extensive RD work on alternative tower designs,
    suitable composite materials, joining systems and
    manufacturing methods
  • Joining of the shell rings can be carried out
    on-site
  • FRP towers offer new possibilities for the
    on-site logistics and assembly
  • Further effort is needed in the fatigue
    verification of the tower concept and the design
    of special tower details

34
Conclusions
  • SPLIT BLADE
  • The 30 m blade is the biggest split blade built
    and full-scale tested to date
  • The prototype blade was manufactured using low
    cost material and simple production methods. If
    more advanced production methods and materials
    are used, bigger split blades could be
    efficiently implemented
  • The blade sustained successfully static test
    loading. Failure of a number of bolts of the
    blade joint during fatigue testing lead to joint
    design refinement
  • The advantages of the split blade concept were
    demonstrated also in practice, when the blade was
    transported from Greece to Denmark by truck for
    testing in 3 days

35
Conclusions
  • TRANSMISSION SYSTEM
  • A number of alternative gearbox arrangements has
    been investigated
  • An optimal gearbox for wind turbines has been
    designed, having the novel arrangement of a three
    stage, duplex load path with single helical gears
    and a balance beam to equalise torque on the
    intermediate gear shafts
  • The assessment of the proposed gearbox design in
    service is an issue for further investigation
  • The created measurement database from the
    operation of a similar concept gearbox is a
    valuable tool for getting a better insight in the
    loading of this type of gearbox

36
The happy team in front of the tower
37
The happy team in front of the blade
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