ASSEMBLY, TRANSPORTATION AND INSTALLATION OF FLOATING WIND TURBINES

20250376248 ยท 2025-12-11

    Inventors

    Cpc classification

    International classification

    Abstract

    A spar-type floating offshore wind turbine assembly is assembled and then supported in a transport configuration with its longitudinal axis substantially horizontal or inclined at a shallow acute angle to the horizontal. The assembly is upended during installation to bring the longitudinal axis to a substantially vertical orientation. In a transport configuration, buoyant upthrust is applied to the assembly by immersion of a spar buoy at a lower end of the assembly and of at least one discrete support buoy that is attached to the spar buoy at a position offset longitudinally from the lower end. A brace acts between the spar buoy and an upper structure of the assembly, that structure comprising a mast that is cantilevered from an upper end of the spar buoy. The brace may be attached to the or each support buoy.

    Claims

    1. A method of supporting a spar-type floating offshore wind turbine assembly in a transport configuration, the method comprising: applying buoyant upthrust to the assembly by partial immersion of a spar buoy at a lower end of the assembly and at least partial immersion of at least one discrete support buoy that is attached to the spar buoy at a position offset longitudinally from the lower end; and bracing an upper structure of the assembly with a brace that acts between the spar buoy and the upper structure, the upper structure comprising a mast that is cantilevered from an upper end of the spar buoy.

    2. The method of claim 1, wherein a longitudinal axis of the assembly is inclined at an acute angle to the horizontal.

    3. The method of claim 1, wherein the aggregate upthrust acting on the spar buoy and the at least one support buoy substantially equates to the entire weight of the assembly.

    4. The method of claim 1, comprising supporting the brace on the or each support buoy.

    5. The method of claim 1, comprising placing one or more members of the brace under tension, the or each of the members being anchored to the spar buoy and/or to the upper structure.

    6. The method of claim 1, comprising applying suspension force to the upper structure through the brace from above the upper structure.

    7. The method of claim 1, comprising applying supporting force to the upper structure through the brace from beneath the upper structure.

    8. The method of claim 1, wherein the assembly has a centre of gravity disposed at a longitudinal position between the or each support buoy and the lower end of the assembly.

    9. The method of claim 1, further comprising upending the assembly from the transport configuration by ballasting the spar buoy and rotating the assembly about the or each support buoy as the longitudinal axis approaches an upright orientation.

    10. The method of claim 9, comprising separating the upper structure from the brace before or during rotation of the assembly.

    11. The method of claim 9, comprising separating the brace from the or each support buoy before rotation of the assembly.

    12. The method of claim 9, comprising rotating the or each support buoy with the assembly.

    13. The method of claim 9, comprising rotating the assembly relative to the or each support buoy.

    14. The method of claim 1, comprising cradling the spar buoy with the support buoy or between two or more of the support buoys.

    15. A method of assembling a spar-type floating offshore wind turbine assembly, the method comprising: attaching a discrete support buoy to a spar buoy at a position offset longitudinally from a lower end of the spar buoy; joining an upper structure of the assembly to the spar buoy along a common longitudinal axis, the upper structure comprising a mast that is cantilevered from an end of the spar buoy; and bracing the upper structure of the assembly with a brace that acts between the spar buoy and the upper structure.

    16. The method of claim 15, wherein the longitudinal axis is inclined at an acute angle to the horizontal.

    17. The method of claim 15, comprising positioning the support buoy or buoys beneath and/or to opposed sides of the spar buoy.

    18. The method of claim 15, comprising attaching the brace to the or each support buoy.

    19. The method of claim 15, comprising preliminarily assembling the spar buoy from two or more sections that are moved onto, and united on, a launch axis that is aligned with the longitudinal axis of the assembly.

    20. The method of claim 19, comprising moving one or more sections of the spar buoy along the launch axis as another section is moved onto the launch axis.

    21. The method of claim 19, comprising moving each section of the spar buoy onto the launch axis from a direction transverse to the launch axis.

    22. The method of claim 19, further comprising launching the assembly into water to be supported by buoyant upthrust arising from partial immersion of the spar buoy and at least partial immersion of the at least one support buoy.

    23. The method of claim 21, comprising supporting the assembly on the at least one support buoy during launch movement of the assembly.

    24. A spar-type offshore wind turbine assembly floating on water in a transport configuration, the assembly comprising: a partially immersed spar buoy at a lower end of the assembly; an upper structure comprising a mast that is cantilevered from an upper end of the spar buoy; at least one discrete support buoy that is attached to the spar buoy at a position offset longitudinally from the lower end, the or each support buoy being at least partially immersed; and a brace that acts between the spar buoy and the upper structure.

    25. The assembly of claim 24, wherein a longitudinal axis of the assembly is inclined at an acute angle to the horizontal.

    26. The assembly of claim 24, wherein aggregate upthrust acting on the spar buoy and the at least one support buoy substantially equates to the entire weight of the assembly.

    27. The assembly of claim 24, wherein the brace acts between the spar buoy and the upper structure via the or each support buoy.

    28. The assembly of claim 24, where the brace is supported on the or each support buoy.

    29. The assembly of claim 28, wherein the brace is cantilevered from the support buoy.

    30. The assembly of claim 24, wherein the brace comprises one or more members under tension, the or each of those members being anchored to the spar buoy and/or to the upper structure.

    31. The assembly of claim 24, wherein the brace suspends the upper structure from above.

    32. The assembly of claim 31, wherein the brace comprises at least one upright that supports at least one tensile member extending longitudinally and downwardly from the upright to the spar buoy and/or to the upper structure.

    33. The assembly of claim 32, wherein tensile members extend downwardly in opposite longitudinal directions from the upright to the spar buoy and the upper structure.

    34. The assembly of claim 24, wherein the brace supports the upper structure from beneath.

    35. The assembly of claim 24, having a centre of gravity disposed at a longitudinal position between the or each support buoy and the lower end of the spar buoy.

    36. The assembly of claim 24, wherein the spar buoy is cradled by or between the or each support buoy.

    37. The assembly of claim 24, wherein the brace is negatively or neutrally buoyant.

    38. The assembly of claim 24, wherein the or each support buoy is offset transversely to beneath the longitudinal axis.

    39. The assembly of claim 24, wherein the or each support buoy extends to, or is positioned at, laterally offset locations on opposed sides of the spar buoy.

    40. The assembly of claim 39, wherein said laterally offset locations are spaced apart by a distance greater than a length of the or each support buoy in a direction parallel to the longitudinal axis.

    41. The assembly of claim 24, wherein the or each support buoy is at a longitudinal position wholly within the length of the spar buoy.

    Description

    [0049] In order that the invention may be more readily understood, reference will now be made, by way of example, to the accompanying drawings in which:

    [0050] FIG. 1 is a schematic side view of a wind turbine assembly floating on water in a transport configuration of the invention;

    [0051] FIG. 2 is a cross section on line II-II of FIG. 1;

    [0052] FIG. 3 is a cross section on line III-III of FIG. 1;

    [0053] FIGS. 4a to 4j are a sequence of schematic side views showing construction, launching, transportation and installation of a wind turbine assembly in accordance with the invention;

    [0054] FIG. 5 is a schematic side view showing a variant of the installation step shown in FIG. 4i;

    [0055] FIG. 6 is a schematic side view showing a second embodiment of the invention;

    [0056] FIG. 7 is a cross section on line VII-VII of FIG. 6;

    [0057] FIG. 8 is a schematic side view showing a variant of the second embodiment shown in FIGS. 6 and 7; and

    [0058] FIGS. 9 and 10 are cross-sectional views corresponding to FIG. 2 but showing other possible support buoy arrangements.

    [0059] Referring firstly to FIG. 1 of the drawings, a floating offshore wind turbine assembly 10 is shown here floating on the surface 12 of a body of water in a transport configuration in accordance with the invention.

    [0060] The wind turbine assembly 10 comprises a spar buoy 14 surmounted by a conventional upper turbine structure 16 that comprises a mast 18 extending upwardly to a nacelle 20. The spar buoy 14 and the mast 18 are in substantially coaxial alignment in series along a common longitudinal axis 22. In the transport configuration, the assembly 10 is in a near-horizontal orientation in which the longitudinal axis 22 is inclined at a shallow angle of less than about thirty degrees to the horizontal, for example ten degrees as shown. Thus, the mast 18 extends from the top of the spar buoy 14 in the manner of a cantilever arm.

    [0061] The nacelle 20 supports a rotor 24 comprising a set of blades 26 extending radially from a hub 28. Typically, the rotor 24 comprises three blades 26; in the transport configuration, one of the blades 26 is held substantially parallel to the longitudinal axis 22 so that the other two blades 26 balance each other about that axis 22.

    [0062] Toward the lower end of the assembly 10, the spar buoy 14 is partially immersed in the water but at this stage is deballasted to contribute buoyant upthrust, with its internal buoyancy tank 30 substantially filled with air. Toward the upper end of the assembly 10, the upper structure 16 is held clear of the surface 12.

    [0063] In accordance with the invention, the assembly 10 also receives buoyant upthrust from a discrete support buoy 32. The support buoy 32 is situated beneath the assembly 10 at an intermediate longitudinal position between the upper and lower ends of the assembly 10. In this example, the support buoy 32 is located beneath the spar buoy 14 near an upper end of the spar buoy 14, close to the interface between the spar buoy 14 and the mast 18.

    [0064] Conveniently, the support buoy 32 is positioned at or close to the surface 12 of the water when the assembly 10 is in the transport configuration. In this example, the support buoy 32 is at the surface 12, hence partially immersed, and is at a longitudinal position aligned with where the inclined assembly 10 intersects the generally horizontal level of the surface 12.

    [0065] The centre of buoyancy 34 and the centre of gravity 36 of the system comprising the assembly 10 and the support buoy 32 are at respective locations between the support buoy 32 and the immersed part of the spar buoy 14. In the meta-stable system of the transport configuration, the centre of gravity 36 is, nominally, directly above the centre of buoyancy 34 and both are in a vertical plane containing the longitudinal axis 22. Of course, there will be some relative lateral movement between the centre of buoyancy 34 and the centre of gravity 36 during pitching or rolling motions of the assembly 10. However, these transient offsets between the centre of buoyancy 34 and the centre of gravity 36 will produce self-righting moments when the assembly 10 is in the transport configuration.

    [0066] As will be apparent from the cross-sectional views of FIGS. 2 and 3, the support buoy 32 lies beneath, and extends laterally beyond, the spar buoy 14, hence retaining and supporting the spar buoy 14 in the manner of a cradle. For this purpose, the top of the support buoy 32 is traversed by a longitudinal groove 38 whose upwardly concave curvature complements the convex external curvature of the spar buoy 14.

    [0067] In this example, the buoyancy of the support buoy 32 is offset transversely to beneath the longitudinal axis 22 at the longitudinal location of the support buoy 32. Indeed, in this example, the buoyancy of the support buoy 32 is entirely beneath the longitudinal axis 22.

    [0068] FIG. 2 shows that the support buoy 32 contains at least one hollow air-filled chamber 40 positioned or extending to each side of the assembly 10. The support buoy 32 is compact longitudinally but relatively large laterally, being substantially wider than it is long. This spreads substantial buoyancy laterally outboard of the spar buoy 14 on opposite sides of the longitudinal axis 22, to the benefit of stability of the assembly 10 against rolling motion. Conversely, the relative shortness of the support buoy 32 in the longitudinal direction makes the support buoy 32 easy to turn or pitch about a transverse horizontal axis. This makes it simple to control the inclination of the assembly 10 via the buoyancy tank 30 during transportation and to initiate and control upending of the assembly 10 when the buoyancy tank 30 is flooded during installation.

    [0069] In addition to providing a seat for the spar buoy 14, the groove 34 maximises the depth and therefore the volume and buoyancy of the lateral portions of the support buoy 32. This is achieved without correspondingly elevating the centre of gravity 36 of the assembly 10, which is also to the benefit of stability and simplifies attachment of the support buoy 32 to the assembly 10 during construction. In this respect, the support buoy 32 may be positioned relative to the assembly 10 as a unit or could be assembled around the assembly 10 before launching and transportation.

    [0070] FIGS. 1 and 3 show a brace structure 42 that extends longitudinally from the support buoy 32 as an outrigger to support the upper structure 16 of the assembly 10 against transverse bending loads. The brace structure 42 may be tuned to give minimal resistance to pitching motions and thus a more constant support against bending moments.

    [0071] In this example, the brace structure 42 is a strut arrangement that comprises a pair of rigid arms 44, each of which may take the form of a lattice frame as shown. The arms 44 converge from respective sides of the support buoy 32 around the top of the spar buoy 14 to hold a cradle 46 between them that receives and supports the mast 18. Thus, the cradle 46 has upwardly concave curvature that complements the convex external curvature of the mast 18.

    [0072] The cradle 46 supports the mast 18 at an intermediate location along the length of the mast 18, in this example about halfway along the mast 18. More generally, the cradle 46 could be positioned at between one quarter and three quarters of the length of the mast 18 away from the spar buoy 14. There could also be more than one cradle 46, the cradles 46 then being spaced longitudinally at different respective locations along the mast 18.

    [0073] Whilst a minor portion of the brace structure 42 could be submerged below the surface 12, the brace structure 42 contributes no buoyancy, or at most negligible buoyancy, to the system. Indeed, the brace structure 42 itself can be negatively buoyant. For example, members of the brace structure 42 could be flooded even if they are hollow.

    [0074] Turning now to FIGS. 4a to 4j, these drawings exemplify steps of construction, launching, transportation and installation of a floating offshore wind turbine assembly 10 in accordance with the invention. With initial reference to FIGS. 4a to 4f, construction of the assembly 10 is performed in a yard 48 onshore at a coastal location with ready access to the sea.

    [0075] In this case, the yard 48 comprises an inclined slipway 50 that slopes down into the water and so extends beneath the surface 12. Conveniently, the inclination of the slipway 50 approximately corresponds to the desired inclination of the assembly 10 in the transport configuration shown in FIG. 1, but this is not essential. However, it is preferred to launch the assembly 10 with the spar buoy 14 leading the upper structure 16 into the water. Thus, the spar buoy 14 will be at a lower end of the assembly 10 extending down the incline of the slipway 50, with the longitudinal axis 22 of the assembly 10 coincident with a launch axis 52 that is generally orthogonal to the edge of the water at the end of the slipway 50. The direction of the launch axis 52 may, for example, be defined by rails extending down the slipway 50.

    [0076] The bulk and weight of the spar buoy 14 makes it convenient to assemble the spar buoy 14 from a series of prefabricated sections 54. Those sections 54 can be maneuvered onto the launch axis 52 carried by respective trolleys 56, which may be self-propelled or towed to a desired position on the slipway 50. For this purpose, the slipway 50 comprises a substantially horizontal roadway 58 that extends across the slope of the slipway 50, parallel to the edge of the surface 12. Sections 54 of the spar buoy 14 can thereby be introduced to the launch axis 52 on respective trolleys 56. turned off the roadway 58 and then moved down the slipway 50 in alignment with the launch axis 52.

    [0077] In FIG. 4a, a first section 54 of the spar buoy 14 and its trolley 56 are already on the launch axis 52 on the slipway 50. The second section 54 and its trolley 56 are moving along the roadway 58 toward the launch axis 52. FIG. 4b then shows the second section 54 joined to the first section 54 on the slipway 50 and the third section 54 and its trolley 56 moving along the roadway 58 toward the launch axis 52. It will be noted that the first section 54 has moved down the slipway 50 to accommodate the second section 54. FIG. 4c then shows the third section 54 united with the first two sections 54 on the slipway 50 to complete the spar buoy 14.

    [0078] Up to this stage, the three sections 54 remain supported on the slipway 50 by their respective trolleys 56. The trolleys 56 may, however, be supplemented or replaced by fixed temporary supports 60 as shown in FIG. 4d, which also shows the complete upper section 16 of the assembly 10 being lifted as a unit via lifting cables 62 to be joined to the top of the spar buoy 14. Parts of the upper structure 16, such as the nacelle 20 or sections of the mast 18, could be lifted separately. In principle, parts of the upper structure 16 could also be introduced onto the slipway 50 and maneuvered on trolleys 56 via the roadway 58.

    [0079] FIG. 4e shows the support buoy 32 and the brace structure 42 positioned beneath and fixed temporarily to the spar buoy 14 and the mast 18 while the upper structure 16 remains supported by the lifting cables 62. FIG. 4f then shows the lifting cables 62 removed and the assembly 10, with the support buoy 32 and the brace structure 42, being launched down the slipway 50 into the water. The assembly 10 is shown here being pulled into the water by one or more lines 64 attached to the spar buoy 14.

    [0080] Conveniently, the support buoy 32 can serve as a skid to support movement of the assembly 10 along the launch axis 52. The assembly 10 can also remain supported by at least some of the trolleys 56 and/or temporary supports 60 during that movement. The trolleys 56 and/or the temporary supports 60 can move down the slipway 50 with the assembly 10 or the assembly 10 can slide relative to the trolleys 56 and/or the temporary supports 60. The trolleys 56 and/or the temporary supports 60 are removed in turn as the weight of the assembly 10 is progressively transferred to the water.

    [0081] With the launch operation now complete, FIG. 4g shows the assembly 10, with the support buoy 32 and the brace structure 42 attached, now inclined in the transport configuration as shown in FIG. 1. Lines 64 couple the assembly 10 to tugs 66 that are shown here towing the assembly 10 between them across the surface 12 toward an installation site.

    [0082] Once at the installation site as shown in FIG. 4h, the brace structure 42 can be removed from the support buoy 32 in preparation for upending the assembly 10. The tugs 66 then act in opposition about the assembly 10 to control upending using their winches 68, with the line 64 of one tug 66 being connected to the spar buoy 14 and the line 64 of the other tug 66 being connected to the support buoy 32.

    [0083] FIG. 4i shows the assembly 10 during upending, with its internal buoyancy tank 30 now partially flooded with ballast water 70. This causes the centre of gravity 36 to migrate toward the lower end of the spar buoy 14 and so causes the assembly 10 to pivot about the support buoy 32. The support buoy 32 is held in a desired position by tension in the line 64 that couples the support buoy 32 to the associated tug 66. Nevertheless, it will be noted that the support buoy 32 remains attached to the assembly 10 and so tilts with the assembly 10 during upending.

    [0084] FIG. 4j then shows the assembly 10 fully upended and coupled to catenary moorings 72 that extend from the spar buoy 14 toward respective anchors in the seabed beneath. It will be noted that the centre of gravity 36 is now beneath the centre of buoyancy 34 in a fully stable configuration. The support buoy 32 can now be detached from the assembly 10 and towed away by the associated tug 66, as shown, for re-use to install another floating wind turbine offshore. The other tug 66 has also detached from the spar buoy 14 and is shown sailing away to perform other operations.

    [0085] As noted above with reference to FIG. 4h and FIG. 4i, the brace structure 42 may be removed from the support buoy 32 before upending and the support buoy 32 can remain attached to the assembly 10 to tilt with the assembly 10 during upending. However, as illustrated in FIG. 5, this is not essential. Here, the brace structure 42 remains attached to the support buoy 32 but the support buoy 32 is detached from the assembly 10. In that case, the orientation of the support buoy 32 and the brace structure 42 need not change during upending of the assembly 10. However, the support buoy 32 can be held by one or more additional lines 64 to serve as a fulcrum about which the assembly 10 pivots during upending.

    [0086] FIGS. 6 to 8 show variants of the brace structure 42 of FIGS. 1 and 3. Specifically, FIGS. 6 and 7 show a variant in which a brace structure 74 comprises one or more uprights 76 beside the assembly 10 extending upwardly from the support buoy 32 to a level above the assembly 10. The upright 76 supports the upper ends of cables 78 that diverge downwardly from the upright 76 to respective anchor points 80 on an upper side of the spar buoy 14 and the mast 18. The cables 78 may be separate cables 78 that are attached to the upright 76 individually or opposed end portions of one cable 78 that extends through or over the upright 76.

    [0087] As best appreciated in the cross-sectional view of FIG. 7, there is a pair of uprights 76 in this example, one to each side of the assembly 10 and therefore straddling the assembly 10 between them. The uprights 76 may converge upwardly as shown and could join each other at their upper ends but here they are joined by a transverse cross-member or bridge structure 82 to which the cables 78 are attached or over which one cable 78 extends as shown. Thus, the arrangement of the cables 78 shown in FIGS. 6 and 7 is akin to that of a cable-stayed bridge.

    [0088] The dotted lines in FIG. 8 show that multiple cables 78 could extend from the or each upright 76 to respective anchor points 80 that are spaced longitudinally along the assembly 10 on the spar buoy 14 and/or the mast 18. Additional cables are shown here in a parallel arrangement 84 and a downwardly divergent arrangement 86, and another cable 88 suspended vertically from a main inclined cable 78 in an arrangement akin to a suspension bridge.

    [0089] Referring finally to FIGS. 9 and 10, these drawings show that a support buoy 32 could also comprise buoyant elements 90 that may or may not be conjoined or linked to each other, other than via the assembly 10. For example, there could be separate buoyant elements 90 to each side of the assembly 10 mounted on or linked to the assembly 10 individually or directly as shown in FIG. 9. Alternatively, the buoyant elements 90 could be buoyancy modules attached to respective spigots or other mountings on or attached to the assembly 10, for example the ends of a cross-member 92 extending beneath or cradling the assembly 10 as shown in FIG. 10. Such buoyancy elements 90 may be mounted on or linked to the assembly 10 rigidly as shown in FIG. 9 or via pliant links 94 such as wires as shown in FIG. 10. At least one of such buoyancy elements 90 may be located on each respective side of the assembly 10.

    [0090] Many other variations are possible within the inventive concept. For example, the support buoy could comprise buoyancy aligned laterally with the longitudinal axis, hence being positioned above or below the floating wind turbine assembly.

    [0091] Whilst use of a slipway is preferred, another inclined surface such as a beach, or indeed a substantially horizontal surface, could be used for constructing and launching a floating wind turbine assembly instead.

    [0092] A support buoy could remain attached to a floating wind turbine assembly after installation, for example for use in relocating or decommissioning the assembly.