The present invention concerns a tower-like structure for a wind turbine, a method for manufacturing such a structure, and a wind turbine.
EP 3 443 224 B1 discloses generic objects. The tower-like structure or supporting structure for a wind turbine connects the nacelle carrying the rotor to the substrate, in particular the sea bed. In a generic structure, the connecting or overlap region of the slip joint is restricted to a respective conical region of the lower and upper components. Accordingly, the load is dissipated via the conical connecting region. This must be designed large according to the bending and support loads to be tolerated, which leads to costly structures.
It is an object of the present invention to improve the support structure provided for the expected loads such that the manufacture of the structure as a whole is more favorable.
This object is achieved by a structure in which the upper and the lower component each have at least one further component portion which co-forms the slip joint and which, when viewed transversely to a central longitudinal axis of the structure, is arranged above and/or below the conical component portion, and the surface perpendiculars of which intersect the longitudinal axis at a greater angle than the surface perpendiculars of the conical component portion. In the case of two further component portions of the upper and lower component, co-forming the slip joint, preferably one component is arranged above and the other below the respective conical component portion, and the surface perpendiculars of both the one and the other component portion intersect the central longitudinal axis of the structure at a greater angle than the surface perpendiculars of the conical component portion. The surface perpendiculars are here viewed in a vertical longitudinal section of the structure, i.e. at an identical circumferential angle relative to the central longitudinal axis of the structure which stands perpendicularly on a substrate when the structure is oriented vertically. The surface perpendiculars of the respective component portions run perpendicularly from the surfaces in the direction of the longitudinal center axis of the respective component, i.e. one surface perpendicular for example runs on an outside of the lower component, perpendicularly from its surface, through the wall of the component towards the longitudinal central axis. The surface of a conical component portion corresponds at least substantially, in particular completely to that of a truncated cone, disregarding production-induced tolerances or e.g. necessary beads of weld seams.
To form the slip joint with the at least one further component portion of the upper component, the at least one further component portion of the lower component lies at a height with respect to the longitudinal center axis. For the two further component portions per component, the two (second) further component portions also again lie at a height to one another. Preferably, the surface perpendiculars of this pair of component portions intersect the longitudinal axis-disregarding production-induced tolerances-at the same angle so that the component portions run in parallel.
In the prior art, load transitions occurring were calculated exclusively for the conical component portions to be dimensioned accordingly. The greater the overlap region, the lower the load or the greater the bending moments which can be absorbed. As structures become larger, the conical portions of the structure or supporting structure become ever larger and hence more costly. The invention uses the knowledge that the load transfers occurring can be at least partially separated or divided. For purely axial loads, for the same angles of the cone, a significantly shorter overlap length would suffice. According to the invention therefore, there is an at least partial separation of the axial forces which in particular are determined by the own weight of the upper component and wind turbine parts attached thereto, and the bending load caused for example by wind and waves. Whereas the axial force is still absorbed by the cone, the bending load is now at least partially co-absorbed by the additional component portion. The loads on the slip joint connection which result from the axial load and bending load then occur at different locations, and a stress superposition is at least partially avoided. The slip joint connection is thus formed by the regions of the components lying against one another and serving for load transmission, including any connecting elements arranged between the components.
This applies in particular to a variant of the invention in which, as well as the conical component portion, additional upper and lower component portions are present, and in which then the connecting region continues both upward and downward from a central conical region. In this case, the bending loads would be at least substantially dissipated, preferably to at least 80%, more preferably to at least 90% in these additional component portions.
Preferably, the surface perpendiculars of the further component portion of the upper and lower component are configured such that they intersect the longitudinal axis at a same angle. The course of the components in the in particular three-part connecting region is thus parallel, at least in the regions outside the transitions between the component portions. Both the lower and the upper component form three component portions forming the slip joint, wherein a respective one of the further component portions is formed above the conical component portion and the respective other of the two below the conical component portion.
Preferably, the angle at which the surface perpendiculars of the further component portion or portions intersect the central longitudinal axis differs from that of the conical component portion by at least 2°.
Preferably, the at least one further component portion of the lower and/or upper component is hollow cylindrical, and in particular formed by straight tube segments. The surface perpendiculars of the further component portion or portions then stand in particular perpendicularly to the central longitudinal axis. An in particular middle conical part (in the case of two further component portions) adjoining the at least one hollow cylindrical component portion may be designed significantly smaller and hence more cheaply. In particular as dimensions and loads become ever larger, because of the smaller dimensioning of the middle conical component portion, substantial cost advantages result for the manufacture of the structure according to the invention and a corresponding wind turbine.
In a variant of the invention which is particularly advantageous for load dissipation during operation, an upper and a lower component each have a conical component portion, wherein the further component portions are hollow cylindrical. The conical component portion is preferably adjoined upward and downward (relative to the central longitudinal axis in the operating position of the component) by a respective one of these further component portions.
Preferably, a connecting device, comprising a plurality of in particular annular, plate-like and/or layer-like and preferably elastic, in particular viscoelastic and/or compressible connecting elements, is arranged between the lower and upper components for the purpose of transmitting load between the upper and lower components. This connecting device may be arranged at least in one of the two or three portions of the connecting region of the slip joint which runs fully around a central longitudinal axis in the circumferential direction and thereby forms a sealing level. However, the connecting elements may also be arranged at a distance from one another, spaced apart from one another over the height of the structure along the central longitudinal axis and/or in the circumferential direction. In particular, no connecting element is arranged in the transitional regions between an e.g. hollow cylindrical tube or component portion and a conical component portion, which improves the arrangement of the respective connecting elements and increases the precision of fit. Preferably, at least with respect to the longitudinal direction, a plurality of connecting elements is arranged on each component portion, evenly distributed about the longitudinal axis in the circumferential direction.
In particular, in the conical middle component portion of the structure, the connecting device forms a circumferential seal. The arrangement of the seal in this region is particularly advantageous since any movements of the lower and upper components relative to one another in this component portion, resulting from the occurring bending loads, have only a negligible effect if the main bending loads are absorbed by a lower and an upper component portion.
In particular, the connecting elements are made at least largely from polyurethane. For example, these are polyurethane panels which have a coating of a slip lacquer or another friction-reducing coating on their surface to facilitate installation of the lower and upper components.
Depending on orientation of the component portions of the lower and upper component to be connected, the connecting elements which are arranged between connecting portions situated above one another with respect to the longitudinal axis have surface normals which are angled relative to one another. This again applies to observation of the vertical longitudinal section through the central longitudinal axis. Advantageously, the at least one connecting element arranged between the conical component portions has a different thickness than the adjacent connecting element, viewed in the direction transversely to the longitudinal axis. This takes account of the loads usually occurring there. Also, a connecting element may be provided with a thickness which varies in the direction of the superficial extent.
According to a further exemplary embodiment of a structure according to the invention, of the connecting elements which are arranged next to one another in the circumferential direction about the longitudinal axis, at least one has a greater thickness than a neighboring connecting element or one arranged above it with respect to the longitudinal axis. Thus tolerances occurring on one component can be compensated. For example, a connecting element may also have chamfered edges in order, during installation of the structure when the upper component is placed over the lower component, to allow the components to slide on one another more safely. This applies in particular for connecting elements arranged between upper and lower hollow cylindrical component portions.
Advantageously, at least some of the connecting elements are at least partially elastically, in particular viscoelastically, deformable. This may be utilized in targeted fashion for adapting the connecting elements to inaccuracies and unevennesses of the lower and upper components, e.g. in the form of weld seams, so that these can for example be securely embedded in a sealing level, or gaps formed by inaccurate arrangement of connecting elements can be closed. Also, the damping and hence the long-term stability of the structure may be increased. It may also help adaptation to the components if some of the connecting elements, at least therefore one connecting element, are provided with a varying thickness and thereby compensate e.g. for tolerances of a component or for weld seam elevations. The individual connecting elements may thus have a varying thickness in order to take account of any deviations on the component from a nominal dimension, for example in the form of weld seams. Similarly, the connecting elements may be provided with chamfers e.g. for the purpose of improved installation, or be at least partially wedge-shaped in cross-section.
The connecting elements of the connecting device are preferably at least largely, with the exception of any coatings or external glue layers, preferably made completely from a compact polyurethane which may be provided with openings. In the context of the invention, a compact polyurethane or a solid polyurethane means a solid body which is substantially free from gaseous inclusions. “Substantially free from gaseous inclusions” in this case means that the polyurethane contains gaseous inclusions to preferably less than 20 volume percent, particularly preferably less than 10 volume percent, in particular less than 5 volume percent, and quite particularly less than 2 volume percent.
In addition to the use of load-dissipating, at least partially elastic connecting elements, the thickness of which, viewed transversely to any superficial extent, may in particular lie between 2 and 10 cm, at least some of the connecting elements may be at least partially compressible, wherein the compressibility of the respective connecting element is formed in particular by a structuring of the surface, by openings in the material and/or by the material of at least one layer of the in particular multilayer connecting element. For example, this may be a foamed polyurethane connection which forms a plate-like connecting element.
Because of the compressible and/or at least partially elastic connecting element, as well as load transmission between the lower and upper components of the tower-like structure, also any forces occurring are damped, which improves the integrity of the structure in comparison with previously known connections using mortar or bolts.
The object cited initially is also achieved by a method for manufacturing a tower-like structure formed as described above and below, and wherein at least some of the connecting elements are molded and/or cast onto the lower and/or the upper component. Advantageously, the connecting elements are arranged on the transition piece independently of the production process. The application of a casting compound, e.g. in the form of polyurethane, may be improved by adhesion-promoting agents or primers, and the arrangement of plate-like connecting elements may be improved by adhesives.
In particular, one or more magnet holders are used which hold the connecting elements in position until they are securely fixed, e.g. by hardening of the adhesive.
Advantageously, at least some of the connecting elements are prefabricated and then attached to the lower and/or upper component. Preferably, all connecting elements are precast, e.g. in the form of plates, and then attached in particular to the upper component. One option, which is advantageous because easy to implement, for fixing the connecting elements lies in the use of a magnet holder, via which a connecting element can be held in the desired position on the upper or lower component at least until the connecting element is adequately secured.
The upper and/or lower component may be measured after manufacture to establish any deviations of the components from a predefined form due to production tolerances or e.g. weld seams, giving a deviation dimension arising from deviations from the nominal shape, which is then taken into account by a different thickness and/or superficial extent of the connecting elements. This can be taken into account during manufacture of the connecting elements. Preferably, the deviation dimension is however taken into account by after-machining of at least one of the connecting elements, which may take place e.g. by material removal by milling.
The object cited initially is also achieved by a wind turbine, in particular an offshore wind turbine, which has a structure as described above or below.
Reference is now made more particularly to the drawings, which illustrate the best presently known mode of carrying out the invention and wherein similar reference characters indicate the same parts throughout the views.
Individual technical features of the exemplary embodiments described below, also in combination with the features of the claims, at least one of the independent claims, may lead to further refinements according to the invention. Where suitable, functionally equivalent parts carry identical reference signs.
A wind turbine according to the invention is preferably configured as an offshore wind turbine with a lower component 2, over which an upper component 4 is placed. The lower component 2 is in this case (
The wind turbine comprises a structure according to the invention, consisting of the lower and upper parts 2, 4 and any connecting device arranged in between. The lower component 4 is arranged standing vertically on the sea bed or substrate 10 and protrudes above the water surface 12. The loads acting on the connection between the lower and upper components arise firstly from the weight load of the transition piece, directed vertically down to the substrate 10, and the nacelle 8 arranged thereon. Wind and waves cause additional loads running horizontally to the substrate, which also act on the transition piece and hence must be dissipated via the connection to the monopile. Any vibrations or impacts acting on the monopile may be additionally transmitted in the direction of the transition piece.
A design and connection according to the invention, in the manner of a slip joint for the structure or wind turbine according to
The component portions of the lower component or monopile can be defined similarly to the component portions 22, 24 and 26 of the transition piece. A lower hollow cylindrical part 32 of the lower component 2 constitutes a lower component portion. This transforms upward into a middle conical component portion 32, which is formed by the conical region of the lower component 2 and at the top adjoins another hollow cylindrical component portion 36, the diameter of which both externally and internally is smaller than the diameter of the also hollow cylindrical component portion 32 situated further down. All component portions 22, 24, 26, 32, 34, 36 run circumferentially around the central longitudinal axis 28. In the drawings, for reasons of simplicity, arrows with curly brackets instead refer to component portions 22, 24, 26, 32, 34, 36.
In the exemplary embodiment of
In the detail view of
The component portions of the lower and upper component together form three connecting portions of the connecting region 14. The first connecting portion comprises the lower component portions 22 and 32. The middle connecting portion is that with the conical component portions of the lower and upper components 2, 4. The third portion comprises the region of the upper hollow cylindrical component portions 26 and 36. Each of these connecting portions may comprise one or more parts of the connecting device.
In the exemplary embodiment of
The thickness of the connecting elements 18 varies preferably at least over 30% of the thickness, further preferably over at least 80% of the thickness and up to 90% of the thickness, wherein when the connecting elements 18 are attached to the upper component 4, the end of the connecting elements 18 with narrower cross-section is at the bottom. If the connecting elements 18 are attached to the monopile or lower component 2 before the two components are interconnected, the narrower end of the connecting elements 18 is at the top.
Instead of two rows of connecting elements 18, each connecting portion may have merely one connecting segment 18 wherein, as in the exemplary embodiment of
In the exemplary embodiment of
As an alternative to the plate-like connecting elements, the connecting device may also have rounded connecting elements. This may run circumferentially fully around the longitudinal axis and hence form a seal. Alternatively, they may also be provided solely for support purposes and for example be fixed on the transition piece in particular remotely and then placed over the monopile.
In general, the lower component need not be a monopile. It is also conceivable to configure a tower-like structure with a plurality of slip joint connections and for example as a tripod, so that the three legs of the wind turbine are each formed by means of a slip joint connection.
Preferably, the dimensions of the connecting elements 18 are dependent on the loads occurring in the regions concerned.
Whereas in
Number | Date | Country | Kind |
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BE2021/5506 | Jun 2021 | BE | national |
This application claims priority to PCT Application No. PCT/EP2022/067914, filed Jun. 29, 2022, which itself claims priority to Belgian Patent Application No. BE2021/5506, filed Jun. 29, 2021, the entireties of both of which are hereby incorporated by reference.
Filing Document | Filing Date | Country | Kind |
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PCT/EP2022/067914 | 6/29/2022 | WO |