Title: Development of a MW scale wind turbine for high wind complex terrain sites the MEGAWIND project
1Development 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
2The 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)
3Project 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
4Project 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
5Advanced 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
6Monolithic Tower test configuration in
7During test and final failure
8Monolithic Tower final test in
Base Moment N?m versus Curvature m-1
1.8 MNm
9Sandwich Tower test configuration in
10Sandwich Tower test configuration in
Base Moment N?m versus Curvature m-1
11Performance of H. Tower
12Comparison between M. H. Towers
13Advanced 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.
14Advanced 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
15Advanced Composite Tower- Constructed
16Advanced Composite Tower- Test preparations
17Split 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.
18Split Rotor Blade Designed profile CL-CD
characteristics
19Split Rotor Blade Structural design
T-Bolt concept was selected for the intermediate
joint
20Split 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
21Split Rotor Blade - Structural Design FEM model
of blade 30_1(GRP) Tsai-Wu failure criterion
IEC 61400-1 Class I
22Split 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
23Split Rotor Blade
Manufacturing
Blade inner part - 4595 kg - 12.4 m
Blade outer part - 1828 kg - 17.25 m
ready for transportation
24Split Rotor Blade Blade assembly
25Split Rotor Blade Full scale Testing (edgewis
e)
26Split Rotor Blade Full scale Testing (flapwis
e)
Max test load 4.3 MNm at root
Max test load 4.3 MNm at root
27Advanced 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
28Advanced Transmission System 3 Stage, Dual Load
Path, Balance Beam
29Advanced 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
30Measurement 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
31Sensor installation
32Measurement campaign
33Conclusions
- 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
34Conclusions
- 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
35Conclusions
- 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
36The happy team in front of the tower
37The happy team in front of the blade