Method for establishing a blade connection of a rotor blade, a blade connection and a securing element for a blade connection
The invention relates to a process for manufacturing a blade connection of a rotor blade for a wind energy system which comprises fastening elements for fastening the blade connection to a hub, which fastening elements are provided on a circular arc, preferably equidistant from each other. Furthermore, the invention relates to a blade connection and a fastening element for a blade connection. The invention is based on the problem of improving the fastening of a rotor blade on the hub of a wind energy system as well as improving the manufacture and/or making a suitable blade connection available. The invention solves this problem as regards the process in that fastening elements formed in pieces are arranged on the circular arc and spaced from each other with spacer elements.
1. A process for manufacturing a blade connection of a rotor blade for a wind energy system which comprises fastening elements for fastening the blade connection to a hub, which fastening elements are provided on a circular arc, and the fastening elements formed in pieces are arranged on the circular arc and spaced from each other with spacer elements,
characterized in that a fastening element is used that has a substantially square, cross section in a connection plane or parallel to it or has a trapezoidal cross section, and in that a substantially strip-shaped spacer element is used that is oriented approximately vertically to a connection plane and has a T-shaped, horseshoe-shaped or trapezoidal cross section.
2. The process according to claim 1 , characterized in that each two fastening elements adjacent to one another are spaced from each other by at least one spacer element.
3. The process according to claim 2 , characterized in that a fastening element is used that has a trapezoidal cross section with a side tapering radially inward to the circular arc.
4. The process according to claim 2 , characterized in that the arrangement of fastening elements and spacer elements are connected to each other by lamination and are arranged only on the radially inner side and on the radially outer side of the arrangement.
5. The process according to claim 2 , characterized in that at least one fastening element and at least one spacer element are connected to each other with a resin filling in an intermediate space formed by them.
6. The process according to claim 1 , characterized in that a closed circle or a segment of it is selected as circular arc for the blade connection and that the rotor blade receives a blade connection or several such blade connections as a function of the circular arc of the blade connection in such a manner that the finished rotor blade has a full-circle connection root for the connection to a hub.
7. The process according to claim 6 , characterized in that the blade connection is designed asymmetrically from a connection plane in the direction of the tip of the rotor blade relative to an axis of a circular arc and that the mounted part or added-on part already makes a part of a carrying surface form or wing form available in its free end area.
8. The process according to claim 1 , characterized in that the blade connection is provided with a tear-off foil at least in a partial area during its manufacture, which foil leaves a continuous but rough surface after it has been torn off that can be further treated.
9. A blade connection of a rotor blade for a wind energy system which comprises fastening elements for fastening the blade connection to a hub, which fastening elements are provided on a circular arc characterized in that fastening elements formed in pieces are arranged on the circular arc and spaced from each other with substantially strip shaped spacer elements and at least one fastening element has a substantially square, cross section in a connection plane or parallel to it or has at least one trapezoidal cross section and at least one strip-shaped spacer element is oriented approximately vertically to a connection plane and has an approximately T-shaped or horseshoe-shaped or approximately trapezoidal cross section.
10. The blade connection according to claim 9 , characterized in that each two fastening elements adjacent to one another are spaced from each other by at least one spacer element.
11. The blade connection according to claim 9 , characterized in that at least one fastening element has a rectangular cross section in a connection plane or parallel to it.
12. The blade connection according to claim 11 , characterized in that at least one fastening element has a substantially quadratic cross section.
13. The blade connection according to claim 11 , characterized in that at least one fastening means has at least one trapezoidal cross section with a side that tapers radially inward to the circular arc.
14. The blade connection according to claim 9 , characterized in that the arrangement of fastening elements and spacer elements are connected to each other by lamination and that a laminate is arranged only on the radially inner side and on the radially outer side of the arrangement.
15. The blade connection according to claim 9 , characterized in that at least one fastening element and at least one spacer element are connected to each other with a resin filling in an intermediate space formed by them.
16. The blade connection according to claim 9 , characterized in that the blade connection is constructed in the shape of a circular arc as a closed circle or a segment of it, and that a rotor blade comprises a blade connection or several such blade connections as a function of the circular arc of the blade connection in such a manner that the finished rotor blade has a full-circle connection root for the connection to a hub.
17. The blade connection according to claim 16 , characterized in that the blade connection is designed asymmetrically from a connection plane in the direction of the tip of the rotor blade relative to an axis of a circular arc and that the mounted part or added-on part already makes a part of a carrying surface form or wing form available in its free end area.
18. The blade connection according to claim 9 , characterized in that the blade connection has a tear-off foil at least in a partial area during its manufacture, which foil leaves a continuous but rough surface after it has been torn off that can be further treated.
19. A fastening element of a blade connection of a rotor blade for a wind energy system, characterized by a substantially approximately square or trapezoidal cross section in a connection plane or parallel to it.
20. The fastening element according to claim 19 , characterized in that it tapers in a direction toward the tip of a rotor blade.