Flatback slat for wind turbine
View Patent ↗An aerodynamic slat ( 30 F) having a flatback trailing edge ( 44 F) extending along and spaced proximate an inboard portion of a wind turbine blade ( 22 ). At least the leading edge ( 42 F) of the slat may be disposed within a zone ( 48 ) of airflow that is generally parallel to the suction side ( 40 ) of the wind turbine blade over a range of air inflow angles. A splitter plate ( 52 ) may extend aft from the flatback trailing edge to reduce vortex shedding and extend the effective chord length of the slat. Vortex generators ( 60 ) may be attached to the slat. Flatback slats may be retrofitted to a wind turbine rotor ( 20 ) by attaching them to the spar caps ( 56 ) of the blades or to the hub spinner ( 28 ). The flatback slat provides lift on low-lift inboard portions of the wind turbine blade over a range of angles of attack of the inboard portion.
1. A wind turbine blade comprising:
a main blade element comprising a radially inboard portion; and
a flatback slat comprising a flatback trailing edge spaced proximate the main blade element along a radial span of the inboard portion in a transverse sectional view thereof;
wherein at least a portion of a leading edge of the slat is disposed within a zone of parallel flow wherein an operational airflow flows parallel ±6° to a suction side of the main blade element throughout a variation of at least 8° in an inflow angle to the primary blade element.
2. The wind turbine blade of claim 1 , wherein the flatback trailing edge comprises a generally flat surface that is normal ±30° to a mean camber line of the slat or to a chord line of the slat, and has a thickness of 5% to 30% of a chord length of the slat.
3. The wind turbine blade of claim 1 , wherein the thickness of the flatback trailing edge decreases along a radial extent of the slat with increasing distance from a root of the main blade element.
4. The wind turbine blade of claim 1 , wherein a line is defined perpendicular to a mean camber line of the main blade element at a leading edge of the main blade element, and the slat is disposed behind said line and spaced from a suction side of the inboard portion of the main blade element throughout a radial span of the slat.
5. The wind turbine blade of claim 1 , wherein the slat is disposed within the zone of parallel flow throughout a radial span of the slat.
6. The wind turbine blade of claim 1 , wherein at least a leading edge of the slat is disposed within a zone of reduced inflow angle variation, wherein, when an angle of an operational air inflow to the main blade element changes by N degrees relative to a chord line of the main blade element, an angle of a resultant air inflow to the slat changes by only up to N/2 degrees relative to a chord line of the slat throughout a variation of at least 8° in an inflow angle to the primary blade element.
7. The wind turbine blade of claim 6 , wherein the slat is spaced from a suction side of the main blade element by distance of 5% to 10% of a selected chord length of the main blade element along a radial span of the slat, and the slat is disposed within the zone of reduced inflow angle variation throughout the radial span of the slat.
8. The wind turbine blade of claim 1 , further wherein the slat is attached to a spinner of a hub of the main blade element.
9. The wind turbine blade of claim 1 , wherein, for each transverse section through the slat and main blade element, a chord line of the slat forms an angle with a respective chord line of the main blade element of 10 to 30 degrees.
10. The wind turbine blade of claim 9 , wherein said angle decreases with increasing distance from a root of the main blade element via a twist in the slat that exceeds a corresponding twist in the main blade element along a radial span of the slat.
11. The wind turbine blade of claim 1 , further comprising a splitter plate extending aft from the flatback trailing edge by a distance of at least 5% of a chord length of the slat.
12. The wind turbine blade of claim 11 , wherein the splitter plate extends aft from the flatback trailing edge from a midpoint in the thickness of the flatback trailing edge.
13. The wind turbine blade of claim 11 , wherein the splitter plate is oriented normally ±20° to the flatback trailing edge.
14. The wind turbine blade of claim 11 , wherein the splitter plate is angled toward the main blade element at an angle of up to 30 degrees relative to a camber line of the flatback slat.
15. The wind turbine blade of claim 11 , wherein the splitter plate extends aft from the flatback trailing edge flush with a suction side of the slat, and forms an aft extension of the suction side of the slat.
16. The wind turbine blade of claim 11 , wherein the splitter plate migrates from a midpoint on the thickness of the flatback trailing edge at an inboard end of the slat to an upper part of the flatback trailing edge at an outboard end of the slat.
17. The wind turbine blade of claim 1 , further comprising a support structure attaching the slat to a suction side spar cap of the main blade element.
18. A wind turbine blade comprising:
a main blade element comprising a radially inboard portion; and
a flatback slat comprising a flatback trailing edge, wherein the flatback slat is spaced proximate the main blade element along a radial span of the inboard portion in a transverse sectional view thereof;
wherein at least a leading edge of the slat is disposed within a zone of reduced inflow angle variation, wherein, when an angle of an operational air inflow to the main blade element changes by N degrees relative to a chord line of the main blade element, an angle of a resultant air inflow to the slat changes by only up to N/2 degrees relative to a chord line of the slat throughout a variation of at least 8° in an inflow angle to the primary blade element.
19. A wind turbine blade comprising:
a main blade element comprising a radially inboard portion;
a flatback slat comprising a flatback trailing edge, wherein the flatback slat is spaced proximate the main blade element along a radial span of the inboard portion in a transverse sectional view thereof; and
a splitter plate extending aft from the flatback trailing edge by a distance of at least 5% of a chord length of the slat.
20. The wind turbine blade of claim 19 , wherein the splitter plate extends aft from the flatback trailing edge from a midpoint in the thickness of the flatback trailing edge.