MOULD FOR MOULDING WIND TURBINE BLADE AND ASSEMBLY OF MOULD

Abstract

A mould for moulding a wind turbine blade or an elongate structural part thereof, the mould comprising a plurality of longitudinal elongate mould sections adapted to be fitted together in an end-to-end relationship to form a unitary mould, each mould section having a central mould portion between opposite end portions, each mould section being composed of a fibre reinforced resin matrix composite material, at least one end portion of each mould section forming an integral flange oriented substantially orthogonally downwardly with respect to an upper surface of the mould section, and the upper surface including a moulding surface and a recess located between the flange and the moulding surface, the recess extending across a transverse width of the mould section whereby when the flanges of adjacent mould sections are fitted together in an abutting relationship, the adjacent recesses form a combined recess separating the moulding surfaces of the adjacent mould sections.

Claims

1. A mould for moulding a wind turbine blade or an elongate structural part thereof, the mould comprising a plurality of longitudinal elongate mould sections adapted to be fitted together in an end-to-end relationship to form a unitary mould, each mould section having a central mould portion between opposite end portions, each mould section being composed of a fibre reinforced resin matrix composite material, at least one end portion of each mould section forming an integral flange oriented substantially orthogonally downwardly with respect to an upper surface of the mould section, and the upper surface including a moulding surface and a recess located between the flange and the moulding surface, the recess extending across a transverse width of the mould section whereby when the flanges of adjacent mould sections are fitted together in an abutting relationship, the adjacent recesses form a combined recess separating the moulding surfaces of the adjacent mould sections.

2. A mould according to claim 1 wherein the central mould portion and the flange are connected by a curved region of the fibre reinforced resin matrix composite material forming a continuously curved upper surface from the recess to the flange.

3. A mould according to claim 1 further comprising heating wires within each mould section, the heating wires extending from the central mould portion into the flange.

4. A mould according to claim 1 further comprising an alignment device fitted to each mould section for longitudinally aligning the mould sections to form the unitary mould, the alignment device including a guide element including a notch or opening for aligning a laser beam.

5. A mould according to claim 1 further comprising a plurality of assembly devices for assembling together the mould sections to form the unitary mould.

6. A mould according to claim 1 wherein the unitary mould has a length of at least 50 metres and at least some of the mould sections have a length of at least 8 metres.

7. A mould according to claim 6 wherein the unitary mould has a length of at least 50 metres and the maximum length of each mould section is less than 11.8 metres.

8. A method of assembling a mould for moulding a wind turbine blade or an elongate structural part thereof, the method comprising the steps of: a. providing a plurality of longitudinal elongate mould sections adapted to be fitted together in an end-to-end relationship to form a unitary mould, each mould section having a central mould portion between opposite end portions, each mould section being composed of a fibre reinforced resin matrix composite material, at least one end portion of each mould section forming an integral flange oriented substantially orthogonally downwardly with respect to an upper surface of the mould section, and the upper surface including a moulding surface and a recess located between the flange and the moulding surface, the recess extending across a transverse width of the mould section; b. fitting together the flanges of adjacent mould sections in an abutting relationship, the adjacent recesses form a combined recess separating the moulding surfaces of the adjacent mould sections; c. filling the combined recess with a lamination of fibrous material; d. locating a mould tool over the fibrous material to define a mould cavity having an upper surface substantially aligned with the moulding surfaces of the adjacent mould sections; e. infusing a curable resin into the fibrous material; and f. curing the resin to form a fibre reinforced resin matrix composite material bonded to the adjacent mould sections and defining an interconnecting mould surface therebetween.

9. A method according to claim 8 further comprising the step, before step c, of disposing a curable resin paste in a vertical gap between the adjacent flanges and wherein the curable resin paste is cured during the curing step f.

10. A method according to claim 9 wherein the curable resin paste includes metallic particles to provide a thermally conductive material between the adjacent flanges.

11. A method according to claim 8 further comprising the step, before step e, of laminating a strap of fibrous material across a lower edge of the adjacent flanges.

12. A method according to claim 8 wherein the central mould portion and the flange are connected by a curved region of the fibre reinforced resin matrix composite material forming a continuously curved upper surface from the recess to the flange.

13. A method according to claim 8 further comprising the step of disposing heating wires within each mould section, the heating wires extending from the central mould portion into the flange.

14. A method according to claim 8 further comprising the step of longitudinally aligning the mould sections to form the unitary mould using alignment devices fitted to the mould sections, the alignment devices each including a guide element including an opening for aligning a laser beam.

15. A method according to claim 8 wherein the unitary mould has a length of at least 50 metres and at least some of the mould sections have a length of at least 8 metres.

16. A method according to claim 15 wherein the unitary mould has a length of at least 50 metres and the maximum length of each mould section is less than 11.8 metres.

17. A mould for moulding a wind turbine blade or an elongate structural part thereof, the mould being assembled by the method according to claim 8.

18. A method of molding a wind turbine blade or an elongate structural part thereof using the mould of claim 1.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0036] Embodiements of the present invention will now be described by way of example only, with reference to the accompanying drawings, in which:

[0037] FIG. 1 is a schematic plan view of a wind turbine blade mould according to a first embodiment of the present invention.

[0038] FIG. 2 is a schematic plan view of a mould for moulding a spar cap of a wind turbine blade according to a second embodiment of the present invention.

[0039] FIG. 3 is a schematic plan view of a mould for moulding a shear web of a wind turbine blade according to a third embodiment of the present invention.

[0040] FIG. 4 is a schematic side view of two mould sections of a wind turbine blade mould according to a fourth embodiment of the present invention, the two sections abutting during an initial step of an assembly process for assembling a wind turbine blade mould according to this embodiment of the present invention.

[0041] FIG. 5 is a schematic side view of the two mould sections of FIG. 4 after disposing a curable resin paste between the two abutting sections during a subsequent step of the assembly process according to this embodiment of the present invention.

[0042] FIG. 6 is a schematic side view of the two mould sections of FIG. 5 after partly filling a combined recess between the lower curved portions of the two abutting sections with a first lamination of fibrous material and curable resin during a subsequent step of the assembly process according to this embodiment of the present invention.

[0043] FIG. 7 is a schematic side view of the two mould sections of FIG. 6 after completing the filling of the combined recess between the upper portions of the two abutting sections with a second lamination of fibrous material during a subsequent step of the assembly process according to this embodiment of the present invention.

[0044] FIG. 8 is a schematic side view of the two mould sections of FIG. 7 after locating a mould tool over the fibrous material to define a mould cavity having an upper surface substantially aligned with the moulding surfaces of the two abutting sections and during resin infusion into the fibrous material in a subsequent step of the assembly process according to this embodiment of the present invention.

[0045] FIG. 9 is a schematic side view of the two mould sections of FIG. 8 after resin infusion, resin curing and removal of the mould tool during a subsequent step of the assembly process according to this embodiment of the present invention.

[0046] FIG. 10 is a schematic side view of the two mould sections of FIG. 9 with a strap of fibrous material laminated across a lower edge of adjacent flanges of the two abutting sections, which may be applied prior to resin infusion, according to a modified embodiment of the present invention.

[0047] FIG. 11 is a schematic perspective view of a mould section of the mould of FIG. 1 showing an alignment device of a frame carrying a mould section according to a further embodiment of the present invention.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS

[0048] Referring to FIG. 1, there is shown a wind turbine blade mould 2 according to a first embodiment of the present invention. The mould 2 is for moulding an entire wind turbine blade having a length of greater than 60 metres. The mould 2 includes a first section 4, including the blade root 6, a second central section 8 and a third tip section 10. The first and second sections 4, 8 are each less than 25 metres in length whereas the third tip section 10 is less than 11.8 metres in length. Each mould section 4, 6, 10 includes a respective frame section 12, 14, 16 and an associated respective moulding surface 18, 20, 22. Each frame section 12, 14, 16 is constructed of a welded steel structure, with the steel structure being provided with connecting mechanisms, such as bolts, for securely connecting the frame sections 12, 14, 16 together to form a unitary mould 2. FIG. 11 shows, as an example, the mould section 6 carried on the frame section 14.

[0049] The length of the sections was selected to facilitate shipping by land by trucks. The tip section 10 could be incorporated into a conventional shipping container.

[0050] Referring to FIG. 2, there is shown a wind turbine blade mould 32 according to a second embodiment of the present invention. The mould 32 is for moulding a spar cap of a wind turbine blade. The entire spar cap has a length of less than greater than 47.2 metres. The mould 32 includes four sections 34, 36, 38, 40, each less than 11.8 metres in length so that each section 34, 36, 38, 40 can be fitted into a conventional shipping container. Each mould section 34, 36, 38, 40 includes, as described above for the first embodiment, a respective frame section (not shown) and an associated respective moulding surface.

[0051] Referring to FIG. 3, there is shown a wind turbine blade mould 42 according to a third embodiment of the present invention. The mould 42 is for moulding a shear web of a wind turbine blade. The entire shear web cap has a length of less than greater than 50 metres. The mould 42 includes four short sequentially adjacent sections 44, 46, 48, 50, to be located at the root end 52, each less than 2 metres in length so that each section 44, 46, 48, 50 can be fitted into a conventional shipping container. The mould 42 also includes four longer sections 54, 56, 58, 60, each less than 11.8 metres in length so that each section 54, 56, 58, 60 can be fitted into a conventional shipping container. Each mould section 44, 46, 48, 50, 54, 56, 58, 60 includes, as described above for the first embodiment, a respective frame section (not shown) and an associated respective moulding surface.

[0052] For each of the moulds 2, 32, 42 of FIGS. 1, 2 and 3, the adjacent ends of the abutting mould sections can be assembled and fitted together as described hereinbelow with reference to FIGS. 4 to 11 in order to assemble a unitary mould from the various respective mould sections.

[0053] Referring to FIG. 4, there is shown two mould sections of a wind turbine blade mould according to an embodiment of the present invention, the two sections abutting during an initial step of an assembly process for assembling a wind turbine blade mould. The mould 62 is for moulding a wind turbine blade or an elongate structural part thereof. The mould 62 comprises a plurality of longitudinal elongate mould sections 64, 66 fitted together in an end-to-end relationship to form a unitary mould, such as moulds 2, 32 or 42, or any other such mould. Only two such mould sections 64, 66 are shown, but more may be provided as shown in FIGS. 1 to 3.

[0054] The mould 62 comprises a plurality of assembly devices, such as bolts (not shown) for assembling together the mould sections 64, 66, for example by bolting together the frame sections as shown in FIG. 1, to form the unitary mould 62. Typically, as shown in FIG. 11, the mould 62 further comprises an alignment device 63 fitted to each mould section 64, 66 for longitudinally aligning the mould sections 64, 66 to form the unitary mould 62. The alignment device 63 includes a guide element 65 including a notch or opening 67 for aligning a laser beam 69.

[0055] Each mould section 64, 66 has a central mould portion 68 between opposite end portions 70. Each mould section 64, 66 is composed of a fibre reinforced resin matrix composite material 72 which forms the moulding surface 74, for example glass fibre reinforced epoxy resin. At least one end portion 70 of each mould section 64, 66 forms an integral flange 76 oriented substantially orthogonally downwardly with respect to the upper surface 78 of the mould section 64, 66.

[0056] The upper surface 78 includes the moulding surface 74 and a recess 80 located between the flange 76 and the moulding surface 74. The recess 80 extends in a longitudinal direction and also across a transverse width of the mould section 64, 66 whereby when the flanges 76a, 76b of adjacent mould sections 64, 66 are fitted together in a substantially abutting relationship, with typically a vertical gap 81 therebetween, the adjacent recesses 80 form a combined recess 82 separating the moulding surfaces 74 of the adjacent mould sections 64, 66.

[0057] The central mould portion 68 and the flange 76 are connected by a curved region 84 of the fibre reinforced resin matrix composite material 72. The curved region 84 forms a continuously curved upper surface 86 from the recess 80 to the flange 76.

[0058] The mould further comprises heating wires 90 within each mould section 64, 66. The heating wires 90 extend from the central mould portion 68 into the flange 76 so as to provide substantially uniform heating across the surface area of the unitary moulding surface. The heating wires 4 are preferably located close to the moulding surface 74, for example the embedded wires being from 1 mm to 20 mm, typically from 2 to 10 mm from the moulding surface 74.

[0059] In typical preferred embodiments, the unitary mould has a length of at least 50 metres and at least some of the mould sections have a length of at least 8 metres, and/or the maximum length of each mould section is less than 11.8 metres.

[0060] Optionally, as shown in FIG. 10, a strap 120 of fibrous material, for example of glass fibre impregnated with a curable resin such as epoxy resin, is laminated across a lower edge 122 of the adjacent flanges 76. This seals the lower edge of any gap between the flanges 76.

[0061] Referirng to FIG. 5, in a next step a curable resin paste 92, for example including a curable epoxy resin and filler material such as silica particles to provide a high paste viscosity, is disposed in the vertical gap 81 between the flanges 76a, 76b of the two abutting sections 64, 66. The resin paste 92 may include metallic particles to provide a thermally conductive material between the adjacent flanges 76a, 76b and thereby increase the thermal conductivity of the connection between the flanges 76a, 76b. The provision of such a thermally conductive material enhances the uniformity of the thermal properties of the mould 62, so that even though the heating wires 90 are longitudinally spaced at the adjacent flanges 76a, 76b the presence of the thermally conductive material conducts heat from the heating wires toward the moulding surface above the cured resin paste, the curing being as discussed below, so as to compensate for the discontinuity of the heating wires at the connections between the mould sections. The delivery of heat to thermally cure the resin material of the wind blade during manufacture is substantially uniform over the surface area of the mould at the connections between the mould sections.

[0062] Subsequently, as shown in FIG. 6, the portion 94 of the combined recess 82 between the lower curved regions 84 above the resin paste 92 is filled with a first lamination of fibrous material 96 and curable resin 98. The fibrous material 96 is typically composed of glass fibres and the curable resin 98 is typically an epoxy resin. This first lamination acts provides a level upper surface and as a plug seal for a subsequent vacuum infusion process, as described below. As shown in FIG. 7, the combined recess 82 between the upper portions of the two abutting sections 64, 66 is then completely filled with a second lamination 100 of fibrous material. Dry fibre mats 102, for example of glass fibre, are laid up into the combined recess 82, so as to level with the moulding surfaces 74. The mats 102 may comprise stitched or woven fabric.

[0063] Then, as shown in FIG. 8, a mould tool 104 is located over the fibrous material 100 to define a mould cavity 105 containing the dry fibre lamination 100 having an upper surface 106 substantially aligned with the moulding surfaces 74 of the two abutting sections 64, 66. Then a curable resin 108, such as epoxy resin, is infused under vacuum into the fibrous material 100. Typically the infusion point for the resin 108 is at the longitudinal centre of the combined recess 82, so that the resin 108 flows outwardly towards the longitudinal ends 110, 112 of the combined recess 82, and the infusion point may be located at the transverse centre or at a lateral side of the combined recess 82.

[0064] The curable resins 98, 108 and in the resin paste 92 are then cured at elevated temperature and under vacuum to form a unitary fibre reinforced matrix resin material plug 111 intimately bonded to, and composed substantially of a similar fibre reinforced matrix resin composite material as, the mould sections 64, 66. The resultant plug 111 is shown in FIG. 9. The plug 111 has low surface roughness, which does not require finish sanding because the upper surface 114 of the plug 111 is defined by the mould tool 104, so that the two mould sections 64, 66 are assembled together with a substantially uniform interconnecting moulding surface 114 of the plug 111 substantially indistinguishable from the moulding surfaces 74 of the two mould sections 64, 66.

[0065] Although the illustrated embodiment of the present invention employs a wind turbine blade mould, the present invention may be implemented in moulds for moulding other large articles of composite material.