Rotor blade assembly for wind turbine having load reduction features
Rotor blade assemblies for wind turbines are provided. In one embodiment, a rotor blade assembly includes a rotor blade having exterior surfaces defining a pressure side, a suction side, a leading edge, and a trailing edge each extending between a tip and a root. The rotor blade further defines a span and a chord. A span-wise portion of the pressure side includes along a chord-wise cross-section a plurality of inflection points. The plurality of inflection points include a first inflection point and a second inflection point, the first and second inflections points positioned within approximately 50% of the chord from the leading edge.
1. A rotor blade assembly for a wind turbine, the rotor blade assembly comprising:
a rotor blade having exterior surfaces defining a pressure side, a suction side, a leading edge, and a trailing edge each extending between a tip and a root, the rotor blade further defining a span and a chord,
wherein a span-wise portion of the pressure side comprises a tab mounted along a chord-wise cross-section, the tab comprising a plurality of inflection points, the plurality of inflection points comprising a first inflection point, a second inflection point, and a third inflection point, the first and second inflections points positioned within 40% of the chord from the leading edge, and the third inflection point positioned between 50% and 100% of the chord from the leading edge, the tab comprising a first end and an opposing, second end that define an overall length therebetween, the first end corresponding to the first inflection point, the second end corresponding to the third inflection point, the second inflection point configured between the first and third inflection points,
wherein the tab comprises a continuously curved profile along its entire length that tapers towards the pressure side of the rotor blade from the second inflection point to the third inflection point.
2. The rotor blade assembly of claim 1 , wherein the span-wise portion is positioned between a span-wise location of a maximum local chord of the rotor blade and the tip of the rotor blade.
3. The rotor blade assembly of claim 1 , wherein the span-wise portion is positioned between a span-wise location of a maximum local chord of the rotor blade and 90% of the span.
4. The rotor blade assembly of claim 1 , wherein an inner surface of the tab has a curvature that corresponds to a curvature of an exterior surface of the rotor blade.
5. The rotor blade assembly of claim 1 , wherein the tab is passive.
6. The rotor blade assembly of claim 1 , wherein the tab comprises a plurality of tabs.
7. The rotor blade assembly of claim 1 , wherein the tab tapers continuously away from the pressure side of the rotor blade from the first inflection point to the second inflection point and also tapers continuously towards the pressure side of the rotor blade from the second inflection point to the third inflection point.
8. A wind turbine, comprising:
a tower;
a nacelle mounted on the tower; and
a plurality of rotor blades, each of the plurality of rotor blades having exterior surfaces defining a pressure side, a suction side, a leading edge, and a trailing edge each extending between a tip and a root, each of the plurality of rotor blades further defining a span and a chord,
wherein a span-wise portion of the pressure side of at least one of the plurality of rotor blades comprises a tab mounted along a chord-wise cross-section, the tab comprising a plurality of inflection points, the plurality of inflection points comprising a first inflection point, a second inflection point, and a third inflection point, the first and second inflections points positioned within 40% of the chord from the leading edge, and the third inflection point positioned between 50% and 100% of the chord from the leading edge, the tab comprising first end and an opposing, second end that define an overall length therebetween, the first end corresponding to the first inflection point, the second end corresponding to the third inflection point, the second inflection point configured between the first and third inflection points,
wherein the tab comprises a continuously curved profile along its entire length that tapers towards the pressure side of the rotor blade from the second inflection point to the third inflection point.
9. The wind turbine of claim 8 , wherein the span-wise portion is positioned between a span-wise location of a maximum local chord of the rotor blade and the tip of the rotor blade.
10. The wind turbine of claim 8 , wherein the span-wise portion is positioned between a span-wise location of a maximum local chord of the rotor blade and 90% of the span.
11. The wind turbine of claim 8 , wherein an inner surface of the tab has a curvature that corresponds to a curvature of an exterior surface of the rotor blade.
12. The wind turbine of claim 8 , wherein the tab is passive.
13. The wind turbine of claim 8 , wherein the tab comprises a plurality of tabs.
14. The rotor blade assembly of claim 8 , wherein the tab tapers continuously away from the pressure side of the rotor blade from the first inflection point to the second inflection point and also tapers continuously towards the pressure side of the rotor blade from the second inflection point to the third inflection point.