ROTOR BLADE FOR A WIND TURBINE
20200392937 ยท 2020-12-17
Inventors
Cpc classification
F05B2240/302
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05B2250/292
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D1/0675
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y02E10/72
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
International classification
Abstract
Provide is a rotor blade for a wind turbine, including a hollow blade body with a root and a tip, wherein the blade body is split along a split plane into two body parts, one extending from the root to a first connection section and the other extending from a second connection section to the tip, wherein the first and the second connection sections are adapted to overlap each other in the connected position.
Claims
1. A rotor blade for a wind turbine, comprising a hollow blade body with a root and a tip wherein the hollow blade body is split along a split plane into two body parts, one body part extending from the root to a first connection section and the other body part extending from a second connection section to the tip; wherein the first connection section and the second connection section are configured to overlap each other in a connected position.
2. The rotor blade according to claim 1, wherein the split plane is in an area where the rotor blade has a convex peripheral geometry.
3. The rotor blade according to claim 1, wherein the split plane is in an area where the rotor blade has a single curved cross section seen in a direction from the root to the tip.
4. The rotor blade according to claim 1, wherein the split plane is in an area where the rotor blade has a convex peripheral geometry and where the rotor blade has a single curved cross section seen in a direction from the root to the tip.
5. The rotor blade according to claim 3, wherein the single curved cross section is circular, oval or egg-shaped.
6. The rotor blade according to claim 1, wherein the first connection section and the second connection section have a conical geometry configured to insert one connection section into the other connection section.
7. The rotor blade according to claim 1, wherein at least one connection section of the first connection section and the second connection section has a stepped geometry.
8. The rotor blade according to claim 6, wherein the first connection section and the second connection section are interlocked with a form fit.
9. The rotor blade according to claim 6, wherein the first connection section is inserted into the second connection section.
10. The rotor blade according to claim 6, further comprising, at the first connection section and/or at the second connection section, one or more slits extending from an end edge over at least a part of a length of the first connection section and/or the second connection section.
11. The rotor blade according to claim 1, further comprising a connection or a stiffening means extending at inner surfaces and bridging a transition region from the first connection section to the second connection section.
12. The rotor blade according to claim 11, wherein the connection or the stiffening means comprises one or more webs or sheets attached to the inner surfaces.
13. The rotor blade according to claim 12, wherein the connection or the stiffening means comprises at least one web or sheet extending along an inner circumference for at least 360 degrees.
14. The rotor blade according to claim 12, wherein the connection or the stiffening means comprises several band- or strip-like webs or sheets extending in a longitudinal direction over the transition region and being distanced to each other along the inner circumference.
15. The rotor blade according to claim 12, wherein the webs or sheets are attached by means of a hardened bonding agent, by lamination or by vacuum assisted resin transfer molding.
16. The rotor blade according to claim 1, wherein the split plane is at an inboard section of the hollow blade body.
17. A wind turbine, comprising a rotor with at least one rotor blade according to claim 1.
Description
BRIEF DESCRIPTION
[0022] Some of the embodiments will be described in detail, with references to the following Figures, wherein like designations denote like members, wherein:
[0023]
[0024]
[0025]
[0026]
[0027]
DETAILED DESCRIPTION
[0028]
[0029]
[0030] The rotor blade 5 as shown in
[0031] In the connected position, as shown in
[0032] The split plane 7 is arranged in an area of the rotor blade 5, where the blade has, as shown in
[0033] Furthermore, the split plane 7 is arranged in an area where the blade has a single curved cross section, as is shown in the exploded view in
[0034]
[0035]
[0036] Certainly, additional fixation mean may be used for fixing the body parts 8, 9 to each other in the overlapping connection sections, for example bolt-nut-connections or the like, which are not shown in detail. It is clear that the connection of the body parts 8, 9 needs to be as firm as possible due to the forces acting on the rotor blade and thus on the connection area when in motion.
[0037] Finally
[0038] In this embodiment the connection section 11 shows several slits 19 extending from the end edge 20 over at least a part of the length of the connection section 11. These slits 19 are preferably equally distributed around the circumference and define respective flexible fingers 21. These flexible fingers 21 enhance the flexibility of the connection section 11 which is advantageous for the good form fit of the connection sections 11, 12.
[0039] While the fingers 21 are only provided at the first connection section 11, it is also possible to provide the second connection 12 with the respective fingers 21 or to provide both connections 11, 12 with fingers 21.
[0040] Although the present invention has been disclosed in the form of preferred embodiments and variations thereon, it will be understood that numerous additional modifications and variations could be made thereto without departing from the scope of the invention.
[0041] For the sake of clarity, it is to be understood that the use of a or an throughout this application does not exclude a plurality, and comprising does not exclude other steps or elements.