Anti-ovalization tool for introduction into a wind turbine blade root and method of reducing ovalization of a wind turbine blade root
View Patent ↗Anti-ovalization tool for introduction into a wind turbine blade root comprising two or more rigid bodies connected to one another along their side edges with distances in between them and together forming a substantially cylindrical body, wherein the distances between the rigid bodies are adjustable. The invention is further related to the method of reducing ovalization of a wind turbine blade root and to the use of a tool comprising two or more rigid bodies as an anti-ovalization tool.
1. An anti-ovalization tool for introduction into a wind turbine blade root comprising two or more rigid bodies connected to one another along their side edges with distances in between them and together forming a substantially cylindrical body, wherein the rigid bodies are connected to each other by one or more turnbuckles, and wherein the turnbuckles are controllable to adjust the distance between the rigid bodies.
2. The anti-ovalization tool according to claim 1 , wherein the cylindrical body has a central axis and the side edges of the rigid bodies extend substantially parallel to said central axis.
3. The anti-ovalization tool according to claim 1 , wherein the rigid bodies are two semi-cylindrical rigid bodies.
4. The anti-ovalization tool according to claim 1 , wherein one or more rigid bodies comprise a curved wall comprising one or more weight-saving holes.
5. The anti-ovalization tool according to claim 1 , wherein the rigid bodies are made of steel or a composite material.
6. The anti-ovalization tool according to claim 1 , wherein an external surface of one or more of the rigid bodies comprises a layer of a deformable material for cushioning roughness's of an inner wall of a wind turbine blade root.
7. A wind turbine blade comprising a blade root portion for coupling to a hub or extender of a wind turbine, the blade root portion comprising an anti-ovalization tool having two or more rigid bodies connected to one another along their side edges with distances in between them and together forming a substantially cylindrical body, wherein the tool is adjusted such that the rigid bodies exert pressure against a blade root inner wall.
8. The wind turbine blade according to claim 7 , the blade being manufactured from two longitudinal blade halves, wherein the blade halves are joined together such that, when being manufactured, the joints between the two blade halves are in a first plane and the anti-ovalization tool is arranged such that the side edges of the rigid bodies do not coincide with said first plane.
9. A wind turbine blade for a wind turbine comprising a blade root portion for coupling to a hub or extender of the wind turbine, the blade root portion comprising an anti-ovalization tool according to claim 3 and the blade being manufactured from two longitudinal blade halves, wherein the blade halves are joined together such that, when being manufactured, the joints between the two blade halves are in a first plane and the anti-ovalization tool is arranged such that the side edges of the two substantially semi-cylindrical bodies are arranged in a plane substantially perpendicular to that of the joints between the two blades halves.
10. A wind turbine comprising a blade according to claim 7 .
11. A method of reducing ovalization of a wind turbine blade root of a blade manufactured from two longitudinal blade halves being joined together, the method comprising the step of introducing an anti-ovalization tool having two or more rigid bodies connected to one another along their side edges with distances in between them and together forming a substantially cylindrical body inside the blade root and adjusting the distances in between the rigid bodies of the anti-ovalization tool so as to position the rigid bodies against a blade root inner wall.
12. The method according to claim 11 , wherein the step of introducing the anti-ovalization tool inside the blade root is carried out substantially directly after joining the two blade halves together.
13. The method according to claim 11 , wherein the step of introducing the anti-ovalization tool inside the blade root is carried out substantially directly before joining the two blade halves together.
14. The method according to claim 11 , wherein the anti-ovalization tool is arranged such that the side edges of the rigid bodies are arranged in planes that do not coincide with a plane of the joint between the two blade halves.