Wind Turbine Flap Technology Development from laboratory to … · 2018-09-26 · DTU Wind Energy,...

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Wind Turbine Flap Technology Development – from laboratory to full scale H Aa Madsen [email protected] In cooperation with

Transcript of Wind Turbine Flap Technology Development from laboratory to … · 2018-09-26 · DTU Wind Energy,...

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Wind Turbine Flap Technology Development

– from laboratory to full scale

H Aa Madsen [email protected]

In cooperation with

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Flap or morphing airfoil

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Morphing trailing edge counteract disturbances from turbulent inflow

Flaps add a third control option to the traditional rotor speed and pitch control

Sandia Blade Workshop 2018 Helge Aagaard Madsen DTU, Denmark

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Ideally flap control can be very efficient and counteract most of the inflow disturbances

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Sandia Blade Workshop 2018 Helge Aagaard Madsen DTU, Denmark

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But limitations in the real world

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bandwidth of the flap actuation

amplitude limits

non-optimal control inputs

cost of the technology

robustness

Sandia Blade Workshop 2018 Helge Aagaard Madsen DTU, Denmark

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Example of a flap system used in a steady position

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The negative flap deflection decreases most extreme loads and reduces blade tip deflection - SWT-4.0-130 turbine

Ref. Alejandro 2018

Sandia Blade Workshop 2018 Helge Aagaard Madsen DTU, Denmark

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Example of a flap system used in a dynamic control

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Ref. Barlas 2016

Case: - DTU 10MW rotor stretched 5% in radius

- Increase in AEP of 3.4%

- Flap system included to reduce the increase in loads

- 30% of the blade length, starting from the tip, with 10% chordwise length, flap angles range between -15/+15 degrees.

Sandia Blade Workshop 2018 Helge Aagaard Madsen DTU, Denmark

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The flap technology

Sandia Blade Workshop 2018 Helge Aagaard Madsen DTU, Denmark

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Use flap technology from aircraft ?

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Too complex

Sandia Blade Workshop 2018 Helge Aagaard Madsen DTU, Denmark

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Strong requirements from the wind turbine industry to the technology

robust and reliable (25 years lifetime)

no metal parts

no electronics

no mechanical parts

scalable to large blade sizes (+100m)

piezzo electric actuators in

wind tunnel exp. 2007

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Helge Aagaard Madsen DTU, Denmark

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Basic flap design that full-fills these requirements

a flap in an elastic material

pneumatically activated

two main concepts

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internal voids

full morphing TE separate hose add/on flap

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The development stages

CAD version

FEM simulations

Design iterations – FSI based optimization

Lab model – simplified manufacturing

Lab testing – performance - fatigue

Wind tunnel tests (typical leading to new design iteration)

Lightning testing

Final prototype manufacturing – co-extrusion

Testing functionality and performance on an outdoor rotating test rig in atmospheric flow

Full scale testing

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FEM – FSI optimization

• Design variables: voids position/size

• Response: Cl, Cd, safety factor

• Optimization with Multi-Objective Genetic Algorithm (max(Cl), min(Cd), SF≥1.5

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Lab models – simplified testing

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Wind tunnel tests – CFD computations

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Final prototype manufacturing - co-extrusion

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Allows designs with optimal combination of soft and stiff material

Solve gluing problems with Santoprene as the surface can be covered with a layer suited for gluing

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One flap system tested for lightning damage

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The Santoprene flap material showed a higher withstand voltage in tracking tests than GFRP

Sandia Blade Workshop 2018 Helge Aagaard Madsen DTU, Denmark

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Pitch actuator

Pressure measurements

Sketch of the rotating test rig

- Intended to close the gap between wind tunnel and full scale testing

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Test rig based on a 100 kW turbine. Rotation of a 10m long boom with an airfoil section of 2x1m

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Blade section for rotating test rig

Blade section mounted on the 10m long boom in the workshop - instrumentation

2x1 m blade section + end caps

Pressure taps in chordwise and spanwise direction

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Flap testing on the rotating rig

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Flap design from the Innwind.EU project

Example of measured flap performance on the rotating rig

ΔCL @ 8o

Case +ΔCL -ΔCL

CFD +0.21 -0.25

Wind tunnel* +0.18 -0.24

Rotating rig +0.18 -0.20

* Poul La Cour wind

tunnel - DTU (!) 20

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Full-scale tests

• Testing on a multi-MW turbine in Denmark since Dec 2017

• Test and validation under real weather conditions

• Testing planned until end of 2018

• For further information: http://www.induflap.dk/

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Conclusions

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a complete development line for flap technology from prototype to full scale has been developed in cooperation with two industrial partners

A considerable amount of testing in wind tunnels and on a rotating rig has been conducted

Full scale testing of first prototypes initiated and will contribute with new important information about a possible commercialization of the technology

Sandia Blade Workshop 2018 Helge Aagaard Madsen DTU, Denmark

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Thank you

for your attention