| 摘要 |
The rotor blade has a 2-part construction with its aerodynamic profile having a maximum profile thickness lying at a point between 15 and 40 % of its overall length, the maximum profile thickness corresponding to between 20 and 45 % of the overall length, with the cross-section of the rotor blade defined by a curvature line with a maximum curvature of between 50 and 70 degrees. An independent claim for a wind-turbine power plant is also included. |
