| 摘要 |
The rotor blade (10) has an aerodynamic profile with a rotor blade leading edge (18) and a rotor blade trailing edge (20), the tip region (12) of the rotor blade curved or bent at an angle of between 1 and 45 degrees in the direction of the trailing edge of the rotor blade and/or the cross-section of the tip region of the rotor blade is reduced. Also included are Independent claims for the following: (a) a rotor blade tip; (b) a wind-powered energy plant. |
