Stability limits for a full wind turbine equipped with trailing edge systems - PowerPoint PPT Presentation

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Stability limits for a full wind turbine equipped with trailing edge systems

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Stability limits for a full wind turbine equipped with trailing edge systems by Thomas Buhl, Mac Gaunaa, Leonardo Bergami and Peter B. Andersen – PowerPoint PPT presentation

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Title: Stability limits for a full wind turbine equipped with trailing edge systems


1
Stability limits for a full wind turbine equipped
with trailing edge systems
  • by Thomas Buhl, Mac Gaunaa, Leonardo Bergami and
    Peter B. Andersen

2
Outline
  • Motivation
  • 2D stability
  • 3D stability
  • Results
  • Conclusion

3
Motivation
Complex terrain CFD by Dr. Bechmann Risø
Siemens Wind power
4
Motivation
5
Adaptive trailing edges
From 2003 to today three large research
projects involving more than 10 researchers, 6
master thesis and 3 Ph.ds
Inspiration
Not applicable!
6
Typical turbine layout
7
Controller
aerodynamic controller part
elastic controller part
pitch controller part
power controller part
8
Motivation
Load reduction on Upwind turbine by P. B.
Andersen
9
Wind tunnel results
10
2D stability
2D stability results from L. Bergami and M. Gaunaa
11
Full turbine stability Results -Original turbine
no flaps
12
Full turbine stability Results -Original turbine
with and without flaps
13
Moving the center of gravity
Figures made by Li Na in ADAPWING2 project funded
by Danish Research Council
14
Moving the center of gravity
15
2D Stability -Moving the center of gravity
From Hansen, M.H., Aeroelastic instability
problems for wind turbines. Wind Energy (2007)
10 , 551-577
16
Moving the center of mass
17
Full turbine stability Results -Moving the
center of gravity
18
Full turbine stability Results -Moving the
center of gravity
19
Conclusions
  • Results from 2D studies show that adding flap
    control generally lowers the stability limits
  • Results from 2D show that the effects of adding
    elastic trailing edges are not trivial.
    Possibility of drastically lowered flutter
    velocities.
  • The reference turbine is very stable.
  • The full turbine results show that the critical
    tip speed for which instability occurs is lower
    for turbines equipped with trailing edge flaps
    compared to the turbine without.
  • In most of the instability cases found an
    artificial propeller mode (large forward blade
    deflections) occurs.

20
Future work
  • Emergency stop
  • future extensions to this work should focused
    also on the controller parameters and the
    influence of these on the stability limits
  • Elastic flaps
  • Aggresivily tuned flap control
  • Less stable reference turbine
  • This work is partially funded by

Acknowledgement
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