Wind turbine rotor blade
Wind turbine rotor blade with a longitudinal axis, a blade tip, a blade root, a leading edge, a trailing edge and a cross-section arranged orthogonally to the longitudinal axis and changing from the blade root to the blade tip, is the cross-section being formed at the blade root and in the middle of the rotor blade by an aerodynamic profile, and an imaginary reference plane arranged with respect to the rotor blade which includes the longitudinal axis of the rotor blade, wherein, in a cross-section, an angle α 3 is defined between the reference plane and a straight line, which connects the longitudinal axis with the trailing edge, and describes the position of the trailing edge, wherein the angle α 3 increases with decreasing distance from the blade root in a first longitudinal portion of the rotor blade and decreases with decreasing distance from the blade root in a second longitudinal portion.
1. A wind turbine rotor blade with a longitudinal axis ( 60 ), a blade tip ( 10 ), a blade root ( 12 ), a leading edge ( 16 ), a trailing edge ( 18 ), a pressure side ( 32 ), a suction side ( 30 ) and a cross-section arranged orthogonally to the longitudinal axis ( 60 ) and changing from the blade root ( 12 ) to the blade tip ( 10 ), the cross-section being formed at the blade root ( 12 ) mainly in a circular manner and in the middle ( 14 ) of the rotor blade by an aerodynamic profile, and an imaginary reference plane permanently arranged with respect to the rotor blade and including the longitudinal axis ( 60 ) of the rotor blade, wherein, in a cross-section, an angle α 3 is defined between the reference plane and a straight line ( 62 ), which connects the longitudinal axis ( 60 ) with the trailing edge ( 18 ), and describes the position of the trailing edge ( 18 ), wherein the angle α 3 increases with decreasing distance from the blade root ( 12 ) in a first longitudinal portion of the rotor blade and decreases with decreasing distance from the blade root ( 12 ) in a second longitudinal portion, which is arranged closer to the blade root ( 12 ) than the first longitudinal portion, wherein the first longitudinal portion begins at a first cross-section, which extends over a bulk of a rotor blade length up to a second cross-section ( 52 ), which is spaced from the blade root ( 12 ) by less than 25% of the rotor blade length, and wherein in the second longitudinal portion, a rear portion of the pressure side ( 32 ) is double concavely curved with a first concave curvature in a cross sectional plane and a second concave curvature in a sectional plane being arranged perpendicular to a rotor plane ( 68 ) and parallel to the longitudinal axis ( 60 ).
2. The wind turbine rotor blade according to claim 1 , wherein the angle α 3 increases in a monotonic manner in the first longitudinal portion and/or decreases in a monotonic manner in the second longitudinal portion.
3. The wind turbine rotor blade according to claim 1 , wherein the second longitudinal section at a second cross-section ( 52 ) is directly adjacent to the first longitudinal section, wherein the angle α 3 has a maximum in the second cross-section ( 52 ).
4. The wind turbine rotor blade according to claim 1 , wherein the second longitudinal section extends in the direction of the blade root ( 12 ) up to a third cross-section ( 24 ), which is arranged at a longitudinal position of the rotor blade where the aerodynamically effective profile of the rotor blade ends.
5. The wind turbine rotor blade according to claim 4 , wherein the third cross-section ( 24 ) is arranged at a distance of 0.5 m or more from the blade root ( 12 ).
6. The wind turbine rotor blade according to claim 4 , wherein an angle α 1 is defined in a plane arranged perpendicular to the rotor plane and parallel to the longitudinal axis ( 60 ) of the rotor blade between the rotor plane and a tangential plane on the pressure side ( 32 ) at the trailing edge ( 18 ) at the third cross-section ( 24 ), wherein the angle α 1 lies in the range of 30° to 90°.
7. The wind turbine rotor blade according to claim 4 , wherein an angle α 2 in the rotor plane between the longitudinal axis ( 60 ) of the rotor blade and the projection onto the rotor plane of a tangent to the trailing edge ( 18 ) of the rotor blade is defined at the third cross-section, wherein the angle α 2 lies in the range of 25° to 90°.
8. The wind turbine rotor blade according to claim 4 , wherein an acute angle is formed between a tangential plane on the pressure side ( 32 ) near the trailing edge ( 18 ) at the third cross-section ( 24 ) and a tangential plane on the suction side ( 30 ) near the trailing edge ( 18 ) at the third cross-section ( 24 ).
9. The wind turbine rotor blade according to claim 1 , wherein a rear portion of the suction side ( 30 ) runs in an almost straight line in the second longitudinal portion, which lies opposite the double concavely curved portion of the pressure side ( 32 ), in the cross-sectional direction of the rotor blade.