Method of repairing a wind turbine blade

1. A method of repairing a wind turbine blade ( 100 ) while mounted on a tower ( 500 ) without removing the blade ( 100 ) from the tower ( 500 ), comprising:

positioning the blade ( 100 ) in a substantially vertical orientation;

suspending a blade reinforcement structure ( 600 ) from a nacelle ( 400 ) via a hoisting system ( 1600 ) including a sinistral cable ( 1610 ), a dextral cable ( 1620 ), a sinistral hoist ( 1630 ), and a dextral hoist ( 1640 ), and further including the step of operating the sinistral hoist ( 1630 ) and the dextral hoist ( 1640 ) to raise the blade reinforcement structure ( 600 ) to the damaged portion ( 230 );

securing the blade reinforcement structure ( 600 ) to the blade ( 100 ) to reduce stress on a portion of the blade ( 100 ) further including the step of securing a clamping structure ( 700 ) to the blade ( 100 ) including securing a primary proximal clamp ( 800 ) and a primary distal clamp ( 1000 ) to the blade ( 100 ), and further includes the step of rigidly interlocking the primary proximal clamp ( 800 ) and the primary distal clamp ( 1000 ) with a clamp interlock structure ( 1200 ) so that the blade reinforcement structure ( 600 ) applies a load to the blade ( 100 ) in at least two locations, wherein the damaged portion ( 230 ) is located between the primary proximal clamp ( 800 ) and the primary distal clamp ( 1000 );

removing a damaged portion ( 230 ) of the blade ( 100 );

installing a repair portion ( 240 ) to the blade ( 100 ) where the damaged portion ( 230 ) was removed; and

removing the blade reinforcement structure ( 600 ) from the blade ( 100 ).

2. The method of claim 1 , further including the step of positioning the blade ( 100 ) so that a blade leading-to-trailing edge axis ( 150 ) is substantially parallel to a wind direction.

3. The method of claim 1 , wherein the clamp interlock structure ( 1200 ) includes at least a compressive side interlock structure ( 1202 ), and further including the step of applying force to the primary proximal clamp ( 800 ) and the primary distal clamp ( 1000 ) with the compressive side interlock structure ( 1202 ) thereby reducing stress on a portion of the blade ( 100 ) located between the primary proximal clamp ( 800 ) and the primary distal clamp ( 1000 ).

4. The method of claim 1 , wherein the clamp interlock structure ( 1200 ) includes at least a tensile side interlock structure ( 1204 ), and further including the step of applying force to the primary proximal clamp ( 800 ) and the primary distal clamp ( 1000 ) with the tensile side interlock structure ( 1204 ) thereby reducing stress on a portion of the blade ( 100 ) located between the primary proximal clamp ( 800 ) and the primary distal clamp ( 1000 ).

5. The method of claim 1 , wherein the clamp interlock structure ( 1200 ) includes at least a compressive side interlock structure ( 1202 ) and a tensile side interlock structure ( 1204 ), and further including the step of applying force to the primary proximal clamp ( 800 ) and the primary distal clamp ( 1000 ) with the compressive side interlock structure ( 1202 ) and the tensile side interlock structure ( 1204 ) thereby reducing stress on a portion of the blade ( 100 ) located between the primary proximal clamp ( 800 ) and the primary distal clamp ( 1000 ).

6. The method of claim 1 , further including the steps of securing a secondary proximal clamp ( 900 ) above the primary proximal clamp ( 800 ), securing a secondary distal clamp ( 1100 ) below the primary distal clamp ( 1000 ), interlocking the primary proximal clamp ( 800 ) and the secondary proximal clamp ( 900 ) with a secondary proximal clamp interlock structure ( 1210 ), and interlocking the primary distal clamp ( 1000 ) and the secondary distal clamp ( 1100 ) with a secondary distal clamp interlock structure ( 1220 ).

7. The method of claim 1 , wherein the primary proximal clamp ( 800 ) is secured above a max chord location ( 180 ) and the primary distal clamp ( 1000 ) is secured below the max chord location ( 180 ).

8. The method of claim 7 , wherein the secured primary proximal clamp ( 800 ) cannot pass the max chord location ( 180 ).

9. The method of claim 1 , further including the step of securing a reinforcement structure work platform ( 610 ) to the blade reinforcement structure ( 600 ).

10. The method of claim 1 , further including the step of enclosing the damaged portion ( 230 ) of the blade ( 100 ) within a containment structure ( 620 ).

11. The method of claim 10 , further including the step of controlling the temperature of the air within the containment structure ( 620 ).

12. The method of claim 11 , further including the step of controlling the humidity of the air within the containment structure ( 620 ).

13. The method of claim 1 , wherein the damaged portion ( 230 ) includes at least a portion of a spar cap ( 210 ) of the blade ( 100 ).

14. The method of claim 1 , wherein the step of securing the blade reinforcement structure ( 600 ) to the blade ( 100 ) further includes the step of stabilizing the blade ( 100 ) from the tower ( 500 ) by securing a load transfer structure ( 1300 ) to the blade ( 100 ) and the tower ( 500 ), wherein the load transfer structure ( 1300 ) includes an adjustable blade-to-tower support ( 1400 ) having a blade attachment device ( 1410 ), a longitudinally adjustable device ( 1420 ), and a tower attachment device ( 1430 ).

15. The method of claim 14 , further including the step of applying a force to the blade ( 100 ) with the load transfer structure ( 1300 ).

16. The method of claim 14 , wherein the blade attachment device ( 1410 ) includes a blade attachment vacuum device ( 1412 ) and the tower attachment device ( 1430 ) includes a tower attachment vacuum device ( 1432 ).

17. The method of claim 14 , wherein the blade attachment device ( 1410 ) includes a primary proximal clamp ( 800 ) applying a clamping force to the blade ( 100 ).

18. The method of claim 14 , wherein the load transfer structure ( 1300 ) is secured to the blade ( 100 ) below the damaged portion ( 230 ).

19. The method of claim 1 , wherein the primary proximal clamp ( 800 ) includes a proximal reinforced vacuum blanket including a flexible material and a plurality of reinforcement devices, and further including the step of vacuum attaching the reinforced vacuum blanket against the blade ( 100 ).

20. A method of repairing a wind turbine blade ( 100 ) while mounted on a tower ( 500 ) without removing the blade ( 100 ) from the tower ( 500 ), comprising:

positioning the blade ( 100 ) in a substantially vertical orientation;

securing a blade reinforcement structure ( 600 ) to the blade ( 100 ) to reduce stress on a portion of the blade ( 100 );

enclosing a damaged portion ( 230 ) of the blade ( 100 ) within a containment structure ( 620 ) and controlling the temperature of the air within the containment structure ( 620 );

removing the damaged portion ( 230 ) of the blade ( 100 );

installing a repair portion ( 240 ) to the blade ( 100 ) where the damaged portion ( 230 ) was removed; and

removing the blade reinforcement structure ( 600 ) and the containment structure ( 620 ) from the blade ( 100 ).

21. The method of claim 20 , further including the step of controlling the humidity of the air within the containment structure ( 620 ).

22. The method of claim 20 , wherein the step of securing a blade reinforcement structure ( 600 ) to the blade ( 100 ) further includes the step of securing a clamping structure ( 700 ) to the blade ( 100 ) including securing a primary proximal clamp ( 800 ) and a primary distal clamp ( 1000 ) to the blade ( 100 ), and further includes the step of interlocking the primary proximal clamp ( 800 ) and the primary distal clamp ( 1000 ) with a clamp interlock structure ( 1200 ), wherein the damaged portion ( 230 ) is located between the primary proximal clamp ( 800 ) and the primary distal clamp ( 1000 ).

23. The method of claim 22 , wherein the clamp interlock structure ( 1200 ) includes at least a compressive side interlock structure ( 1202 ), and further including the step of applying force to the primary proximal clamp ( 800 ) and the primary distal clamp ( 1000 ) with the compressive side interlock structure ( 1202 ) thereby reducing stress on a portion of the blade ( 100 ) located between the primary proximal clamp ( 800 ) and the primary distal clamp ( 1000 ).

24. The method of claim 22 , wherein the clamp interlock structure ( 1200 ) includes at least a tensile side interlock structure ( 1204 ), and further including the step of applying force to the primary proximal clamp ( 800 ) and the primary distal clamp ( 1000 ) with the tensile side interlock structure ( 1204 ) thereby reducing stress on a portion of the blade ( 100 ) located between the primary proximal clamp ( 800 ) and the primary distal clamp ( 1000 ).

25. The method of claim 22 , wherein the clamp interlock structure ( 1200 ) includes at least a compressive side interlock structure ( 1202 ) and a tensile side interlock structure ( 1204 ), and further including the step of applying force to the primary proximal clamp ( 800 ) and the primary distal clamp ( 1000 ) with the compressive side interlock structure ( 1202 ) and the tensile side interlock structure ( 1204 ) thereby reducing stress on a portion of the blade ( 100 ) located between the primary proximal clamp ( 800 ) and the primary distal clamp ( 1000 ).

26. A method of repairing a wind turbine blade ( 100 ) while mounted on a tower ( 500 ) without removing the blade ( 100 ) from the tower ( 500 ), comprising:

positioning the blade ( 100 ) in a substantially vertical orientation;

securing a blade reinforcement structure ( 600 ) to the blade ( 100 ) to reduce stress on a portion of the blade ( 100 ) wherein the step of securing a blade reinforcement structure ( 600 ) to the blade ( 100 ) further includes the step of securing a clamping structure ( 700 ) to the blade ( 100 ) including securing a primary proximal clamp ( 800 ) and a primary distal clamp ( 1000 ) to the blade ( 100 ), and further includes the step of interlocking the primary proximal clamp ( 800 ) and the primary distal clamp ( 1000 ) with a clamp interlock structure ( 1200 ), wherein the damaged portion ( 230 ) is located between the primary proximal clamp ( 800 ) and the primary distal clamp ( 1000 ), and wherein the clamp interlock structure ( 1200 ) includes at least a compressive side interlock structure ( 1202 ), and further including the step of applying force to the primary proximal clamp ( 800 ) and the primary distal clamp ( 1000 ) with the compressive side interlock structure ( 1202 ) thereby reducing stress on a portion of the blade ( 100 ) located between the primary proximal clamp ( 800 ) and the primary distal clamp ( 1000 );

removing a damaged portion ( 230 ) of the blade ( 100 );

installing a repair portion ( 240 ) to the blade ( 100 ) where the damaged portion ( 230 ) was removed; and

removing the blade reinforcement structure ( 600 ) from the blade ( 100 ).

27. The method of claim 26 , wherein the clamp interlock structure ( 1200 ) includes at least a tensile side interlock structure ( 1204 ), and further including the step of applying force to the primary proximal clamp ( 800 ) and the primary distal clamp ( 1000 ) with the tensile side interlock structure ( 1204 ) thereby reducing stress on a portion of the blade ( 100 ) located between the primary proximal clamp ( 800 ) and the primary distal clamp ( 1000 ).

28. The method of claim 26 , wherein the clamp interlock structure ( 1200 ) includes at least a compressive side interlock structure ( 1202 ) and a tensile side interlock structure ( 1204 ), and further including the step of applying force to the primary proximal clamp ( 800 ) and the primary distal clamp ( 1000 ) with the compressive side interlock structure ( 1202 ) and the tensile side interlock structure ( 1204 ) thereby reducing stress on a portion of the blade ( 100 ) located between the primary proximal clamp ( 800 ) and the primary distal clamp ( 1000 ).

29. The method of claim 26 , further including the step of securing a reinforcement structure work platform ( 610 ) to the blade reinforcement structure ( 600 ).

30. The method of claim 26 , further including the step of enclosing the damaged portion ( 230 ) of the blade ( 100 ) within a containment structure ( 620 ).

31. The method of claim 30 , further including the step of controlling the temperature of the air within the containment structure ( 620 ).

32. The method of claim 31 , further including the step of controlling the humidity of the air within the containment structure ( 620 ).

33. A method of repairing a wind turbine blade ( 100 ) while mounted on a tower ( 500 ) without removing the blade ( 100 ) from the tower ( 500 ), comprising:

positioning the blade ( 100 ) in a substantially vertical orientation;

securing a blade reinforcement structure ( 600 ) to the blade ( 100 ) to reduce stress on a portion of the blade ( 100 );

stabilizing the blade ( 100 ) from the tower ( 500 ) by securing a load transfer structure ( 1300 ) to the blade ( 100 ) and the tower ( 500 ), wherein the load transfer structure ( 1300 ) includes an adjustable blade-to-tower support ( 1400 ) having a blade attachment device ( 1410 ), a longitudinally adjustable device ( 1420 ), and a tower attachment device ( 1430 ), wherein the blade attachment device ( 1410 ) includes a blade attachment vacuum device ( 1412 ) and the tower attachment device ( 1430 ) includes a tower attachment vacuum device ( 1432 );

applying a force to the blade ( 100 ) with the load transfer structure ( 1300 );

removing a damaged portion ( 230 ) of the blade ( 100 );

installing a repair portion ( 240 ) to the blade ( 100 ) where the damaged portion ( 230 ) was removed; and

removing the blade reinforcement structure ( 600 ) from the blade ( 100 ).

34. The method of claim 33 , wherein the step of securing a blade reinforcement structure ( 600 ) to the blade ( 100 ) further includes the step of securing a clamping structure ( 700 ) to the blade ( 100 ) including securing a primary proximal clamp ( 800 ) and a primary distal clamp ( 1000 ) to the blade ( 100 ), and further includes the step of interlocking the primary proximal clamp ( 800 ) and the primary distal clamp ( 1000 ) with a clamp interlock structure ( 1200 ), wherein the damaged portion ( 230 ) is located between the primary proximal clamp ( 800 ) and the primary distal clamp ( 1000 ).

35. The method of claim 34 , wherein the clamp interlock structure ( 1200 ) includes at least a compressive side interlock structure ( 1202 ), and further including the step of applying force to the primary proximal clamp ( 800 ) and the primary distal clamp ( 1000 ) with the compressive side interlock structure ( 1202 ) thereby reducing stress on a portion of the blade ( 100 ) located between the primary proximal clamp ( 800 ) and the primary distal clamp ( 1000 ).

36. The method of claim 34 , wherein the clamp interlock structure ( 1200 ) includes at least a tensile side interlock structure ( 1204 ), and further including the step of applying force to the primary proximal clamp ( 800 ) and the primary distal clamp ( 1000 ) with the tensile side interlock structure ( 1204 ) thereby reducing stress on a portion of the blade ( 100 ) located between the primary proximal clamp ( 800 ) and the primary distal clamp ( 1000 ).

37. The method of claim 33 , further including the step of securing a reinforcement structure work platform ( 610 ) to the blade reinforcement structure ( 600 ).

38. The method of claim 33 , further including the step of enclosing the damaged portion ( 230 ) of the blade ( 100 ) within a containment structure ( 620 ).

39. The method of claim 38 , further including the step of controlling the temperature of the air within the containment structure ( 620 ).

40. The method of claim 39 , further including the step of controlling the humidity of the air within the containment structure ( 620 ).