Abstract
Based on the newly developed aero-servo-elastic platform containing an external deformable trailing edge flap PID controller, the effect of smart rotor control on blade flap-wise root moment on NREL/Upwind 5 MW reference wind turbine was investigated under extreme wind shear condition in accordance with the IEC standard. Results showed that, not only the blade flap-wise root moment was effectively reduced, but also this system was very helpful for the extreme load reduction of the tower, the drive-chain and the pitch control system etc. Eventually, this paper illustrated the control physics involved in the smart rotor control. Especially, this paper uncovered a phenomenon that the actively deformable trailing edge flap unfastened the strong coupling interactions between flow and blade due to EWS(Extreme Wind Shear).
| Original language | English |
|---|---|
| Pages (from-to) | 1951-1954 |
| Number of pages | 4 |
| Journal | Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics |
| Volume | 35 |
| Issue number | 10 |
| State | Published - 1 Oct 2014 |
| Externally published | Yes |
Keywords
- Control physics
- Deformable trailing edge flap
- Extreme load
- Smart rotor control
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