Shear web for a wind turbine rotor blade

1. A rotor blade for a wind turbine, the rotor blade comprising:

an upper shell member having a spar cap configured on an internal face thereof;

a lower shell member having a spar cap configured on an internal face thereof; and,

a shear web assembly extending between the spar caps along a span of the rotor blade, the shear web assembly comprising, at least, a first shear web and a second shear web, the first shear web starting at a blade root of the rotor blade and extending to a first intermediate span location, the second shear web starting at a second intermediate span location, the second intermediate span location being closer to the blade root than the first intermediate span location, the second shear web overlapping the first shear web between the first and second intermediate span locations and extending towards a blade tip of the rotor blade.

2. The rotor blade of claim 1 , wherein the shear web assembly further comprises a third shear web overlapping the first shear web.

3. The rotor blade of claim 2 , wherein the second and third shear webs overlap opposing sides of the first shear web.

4. The rotor blade of claim 3 , wherein the first, second, and third shear webs are equally spaced in a chord-wise direction of the rotor blade.

5. The rotor blade of claim 1 , wherein the first shear web is longer than the second shear web.

6. The rotor blade of claim 1 , wherein the first and second shear web overlap at a location from about 40% span to about 60% span of the rotor blade.

7. The rotor blade of claim 1 , wherein at least one of the first shear web, the second shear web, or the third shear web comprises one or more cut-outs configured to provide stress relief to the respective shear web.

8. The rotor blade of claim 1 , wherein the shear web assembly further comprises an additional shear web at a different chord location than the first and second shear webs.

9. A rotor blade for a wind turbine, the rotor blade comprising:

an upper shell member having a spar cap configured on an internal face thereof;

a lower shell member having a spar cap configured on an internal face thereof; and,

a shear web assembly extending between the spar caps along a span of the rotor blade, the shear web assembly comprising, at least, a first shear web and a second shear web, the first shear web starting at a blade root of the rotor blade and extending toward a blade tip of the rotor blade to a first intermediate span location, the second shear web starting at a second intermediate span location, the second intermediate span location being closer to the blade root than the first intermediate span location, the second shear web overlapping the first shear web between the first and second intermediate span locations.

10. The rotor blade of claim 9 , wherein the shear web assembly further comprises a third shear web overlapping the first shear web.

11. The rotor blade of claim 10 , wherein the second and third shear webs overlap opposing sides of the first shear web.

12. The rotor blade of claim 10 , wherein the first, second, and third shear webs are equally spaced in a chord-wise direction of the rotor blade.

13. The rotor blade of claim 9 , wherein the first shear web is longer than the second shear web.

14. The rotor blade of claim 9 , wherein the first and second shear web overlap at a location from about 40% span to about 60% span of the rotor blade.

15. The rotor blade of claim 9 , wherein at least one of the first shear web, the second shear web, or the third shear web comprises one or more cut-outs configured to provide stress relief to the respective shear web.

16. The rotor blade of claim 9 , wherein the shear web assembly further comprises an additional shear web at a different chord location than the first and second shear webs.

17. A method for manufacturing a rotor blade having increased torsional rigidity, the method comprising:

providing upper and lower shell members with spar caps configured on respective internal faces thereof;

placing a first shear web along a span of the rotor blade from a blade root towards a blade tip thereof between the spar caps to a first intermediate span location;

placing a second shear web along the span of the rotor blade starting at a second intermediate span location, the second intermediate span location being closer to the blade root than the first intermediate span location such that a portion of the second shear web overlaps the first shear web between the first and second intermediate span locations; and,

joining the upper and lower shell members.

18. The method of claim 17 , further comprising determining a location of the portion of overlap between the first and second shear webs as a function of a desired twist of the rotor blade.

19. The method of claim 18 , further comprising determining the desired twist of the rotor blade as a function of one or more wind conditions at a site of the wind turbine.