• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
  • 法律状态
  • 优先权
    • 专利摘要:
    WIND TURBINE SHOVEL, E, ONE BLADE PRODUCTION METHOD. A wind turbine blade comprising an aerodynamic fairing supported along at least a portion of its axial length by a spar (12). The spar comprises at least two spar segments (12) joined end to end at an interface (9), each spar segment comprising a shear web (3) with a spar cap (4) on each side. The outer face (6) of each spar cap tapers inwardly towards the interface creating a recess on each side of the interface formed by the tapered faces of adjacent spar caps. The respective connecting piece (8) is sized to fit within each recess. Each connecting piece (8) is sized to fit within each recess. Each connecting piece (8) being secured to the tapered faces of adjacent spar caps to form a double snap-in joint.
    公开号:BR112013000158B1
    申请号:R112013000158-5
    申请日:2011-07-08
    公开日:2021-05-11
    发明作者:Paul HAYDEN；Harald Behmer
    申请人:Blade Dynamics Limited；
    IPC主号:
    专利说明:

    FIELD OF THE INVENTION
    [001] The present invention relates to a wind turbine blade. BACKGROUND OF THE INVENTION
    [002] There is a growing trend towards longer and longer wind turbine blades. This has led to a recent development whereby each blade is manufactured in a number of sections which are connected end to end to form the finished blade. The joint between these adjacent sections is critical to blade operation.
    [003] Such wind turbine blades generally comprise an aerodynamic fairing supported by a longitudinally extending spar. On any blade consisting of a number of segments, as noted above, the joint between adjacent spar sections is critical, as it is through this that the vast majority of the load is transmitted.
    [004] US 2008/0069699 exposes a wind turbine blade that is manufactured in two sections that are subsequently joined. In the region adjacent to the joint, the spar is provided with an enlarged portion that has a number of teeth that mesh with corresponding teeth in the adjacent spar section. The surface shell structure can also be provided with reinforcing strips which are similarly provided with intermesh teeth and intermediate connecting devices of various constructions.
    [005] WO 2009/034291 discloses joints between adjacent spar caps where the width of the spar caps is tapered adjacent to the joint. The tapered surfaces are then glued together and additional supports are provided between the shear cores to reinforce the joint.
    [006] Another example of joining adjacent spar sections is shown in US 2009/0162208. The joint between stringer segments exposed in this document is shown in figure 1.
    [007] This comprises a first stringer segment 1 and a second stringer segment 2. Each stringer segment consists of a shear web 3 with a stringer cap 4 on each side. In the first spar segment 1, the shear web 3 stops just before the end of the spar caps. Each of the stringer caps has a tapered end with a tapered, slanted, inwardly facing bottom surface.
    [008] For the second spar segment 2, the shear web and spar caps are confining. In this case, the outer faces of the spar caps taper inwards to provide a thinned surface 6 complementary to the respective thinned surface 5 on the first spar cap 1. The two spar caps are then connected together between the adjacent thinned surfaces 5, 6 to form the complete stringer. By means of the thinning, the depth of the spar caps, rather than the widths in WO 2009/034291, the connection area is greatly increased, thus increasing the strength of the joint.
    [009] However, this project has a number of drawbacks. First, as will be apparent from Figure 1, in the first spar segment 1, the spar caps protrude beyond the edge of the continuous shear band and are long slender components that are not supported, at this point, by the shear web 3 These portions of the stringer cap can extend for several meters. As such, they are highly vulnerable to damage in transit and assembly.
    [0010] Second, the two stringer sections themselves are long components that extend up to 50 meters (but are more typically 20-30 meters). It is difficult in practice to provide stable support for the two segments as the adhesive is applied to the sloped surfaces and then to move relative to each other into the correct alignment and then hold it in position until the lamination process is completed and the resin has cured.
    [0011] Finally, as the direction in which the sloping surfaces 5, 6 extend is close to the direction in which the two components are placed together in view of the shallowness of the thinning, this can cause problems with the adhesive during assembly. In particular, any misalignment in the assembly can scrape the adhesive from surfaces 5, 6, particularly on the leading edge of the stringer caps 4 of the second stringer segment, leading to gaps in the connecting line, which causes problems for the reliability of the joint and finally joint failure. The spar is then surrounded by an F aerodynamic fairing to complete the blade. DESCRIPTION OF THE INVENTION
    [0012] The present invention is directed to the provision of an improvement of such a gasket.
    [0013] According to a first embodiment of the present invention, there is provided a wind turbine blade comprising an aerodynamic fairing supported along at least a portion of its axial length by a spar, the spar comprising at least two joined spar segments end to end at an interface, each spar segment comprising a shear core with a spar cap on each side; wherein the outer face of each spar cap tapers inwardly towards the interface such that its depth is reduced towards the interface creating a recess on each side of the interface formed by the tapered faces of adjacent spar caps; and a respective connecting piece sized to fit within each recess, each connecting piece being secured to the tapered faces of adjacent spar caps to form a double fit joint.
    [0014] The present invention therefore offers a number of benefits over the prior art gasket.
    [0015] In particular, none of the spar segments have the protruding spar caps which are susceptible to damage during transport. Second, the two spar segments or the two spar caps can be precisely aligned with each other in their final position before the connecting piece is assembled. This simplifies the assembly process and joint reliability. The connecting piece is a small component that is easy to manipulate. It is placed in place in a direction that is close to being orthogonal to the direction in which the tapered surfaces extend. Therefore, any scraping between adjacent thinned surfaces caused by slight misalignments of components is much less likely to occur. Even if it does, the orientation of the surfaces means that the touch that occurs will have a significantly reduced effect. This greatly increases the reliability of the link.
    [0016] Similar joint configurations are disclosed in WO 2009/077192 for joining solid blocks of wood and in FR 2710871 in shipbuilding applications.
    [0017] EP 2186622 discloses a gasket for aircraft wings. This uses a splice joint on all parts of the beam section, more specifically the webs and flanges. The techniques described in this patent are techniques that are only suitable for a high-cost application, such as in aircraft construction. The assembly process requires a complex assembly installation that requires a sophisticated vacuum bag arrangement and an associated heating and cooling system. Such an installation is entirely unsuitable for the fabrication of a wind turbine blade, where the blade segments are often required to be mounted in a location close to the region where the wind turbine is to be erected. Even if they are mounted in a factory environment, the mounting installation cost shown in EP 2186622 is simply not justifiable in the wind turbine industry.
    [0018] Preferably, the end of each shear web is substantially perpendicular (when viewed in cross section in an axial plane running parallel to the spar caps) in the axial direction so that the ends of the shear webs support each other. Also, preferably, there is no double socket joint between the shear webs. This provides a simplified but robust construction in which the connecting pieces are confined only to the spar caps and the webs are mutually supportive.
    [0019] The connecting piece can be fixed in place by glueing. In this case, the connecting piece is provided as a single piece. This is preferably a pre-cured part. For the reasons mentioned above, the ease of handling of the connecting piece and the direction of movement will not unduly disturb the adhesive in the joint.
    [0020] Alternatively, the connecting piece can be formed "in situ" as a number of laminations. In this case, the laminated connecting piece can be formed in a very controlled and accessible location. This ensures that the surface can be prepared well and that the quality of the laminate can be high, thus greatly increasing the reliability of the connection.
    [0021] Another benefit provided by the present invention is its versatility in that it can be assembled using different methods, depending on whether it is required to be assembled in the field, because transportation issues mean that a full-length spar cannot be transported to the site of the wind turbine, or if it is to be assembled at the factory. For field assembly, separate spar segments comprising their own spar caps and at least one shear web are assembled and transported to the field assembly site. Each segment is then connected end-to-end together.
    [0022] Preferably, a support member receives and aligns the shear webs with respect to one another. This support member can be a separate component, or it can take the form of one or more projections that are part of one or both of the shear webs. If the support member is a separate component, the shear webs continue to support each other, albeit indirectly through the support member.
    [0023] Preferably, however, the stringer segments are connected together through their shear webs. Such a joint between shear cores can take the form of mechanical fasteners and/or adhesive (which can be applied through the support) and can be temporary and/or permanent. It should be noted that the joint is primarily required to be sufficient to retain the two segments adjacent to each other, while the connection is made between the spar caps and the connecting piece. This joint also forms the shear connection through the two spar segments. This provides a simple way of positioning and joining segments for “in-the-field” assembly.
    [0024] For a factory assembly, a different proposal may be taken. This time, the full length spar caps are first assembled before affixing the or each shear web. In this case, according to a second aspect of the present invention, there is preferably provided a method of producing a blade according to the first aspect of the invention comprising the steps of inserting spar caps of adjacent segments into a U-shaped channel with its tapered surface to the uppermost one, and mount the connecting piece on the tapered surfaces on the adjacent spar caps.
    [0025] Additional stringer caps can be added where necessary with the addition of connecting pieces to complete the full length stringer cap.
    [0026] A second spar cap is then formed in the same way and the two spar caps are joined with at least one shear core to form a first spar beam.
    [0027] This first spar beam can then be joined side by side to a second spar beam formed in the same way. Three or more beams can be joined in this way.
    [0028] This provides a method that is extremely versatile, yet has a relatively small number of component parts and assembly jigs. The stringer caps have the same external shape and size to be mounted in the same U-shaped channel. This can (if required) be the channel in which the stringer caps are initially formed, thus further reducing the tooling required. However, the process remains versatile in that the web depth can be varied to create beams of different heights, and even to create beams with heights that vary along their length. Also, by displacing the first and second spar beams when they are joined side by side, a virtual “twist” can be incorporated into the beam. Thus, from a very small set of component parts and simple tooling, complex beam shapes can be produced.
    [0029] Stringer segments can be any beam section that has a shear web with a stringer cap on each side, such as an I-beam, C-beam or box beam. The invention can also be applied to spar segments made up of two or more beam sections connected side by side. BRIEF DESCRIPTION OF THE DRAWINGS
    [0030] An example of a spar for a wind turbine blade will now be described with reference to the attached drawings, in which: - figure 1 is a cross section through two spar covers according to the state of the art; Figure 2 is a cross section through the top of two segments of spar cap and connecting piece of the present invention before assembly; figure 3 is a perspective view of the joint in figure 2, before assembly; - figure 4 is a cross section of the joint complete with assembled components; figure 5 is a perspective view of a second joint before assembly; figure 6 is a perspective view of a third joint before assembly; figures 7A and 7B are views similar to figure 2 showing a fourth joint, with figure 7A showing the joint in a partially assembled condition; - figures 8A-8D are schematic representations of a second assembly process for a stringer; figure 9 is a schematic view showing the jig used to assemble the complete spar caps as shown in figures 8A-8D; and - figures 9A-9C are cross sections of lines AA, BB and CC in figure 9 respectively. DESCRIPTION OF ACHIEVEMENTS OF THE INVENTION
    [0031] The spar comprises two spar segments 7 which have essentially the same structure as the second spar segment 2 shown in figure 1. Each has a shear core 3, made of the multiaxial material, and spar caps 4 are provided on either side, which are formed predominantly of a uniaxial material which are preferably formed as pultrusions, but could also be made from prepregs, laminations or other preforms known in the art which form cost effective spar caps. and good mechanical properties.
    [0032] Further details of the construction and materials of the stringer sections are set out in our own earlier application WO 2009/034291.
    [0033] At the end adjacent to the gasket, each of the spar caps 4 has a tapered surface 6, as described above in relation to figure 1.
    [0034] A pair of connecting pieces 8 has a width and depth corresponding to the width and depth of the adjacent spar caps 4 and has slanted faces 9 corresponding to the slanted faces 6 of the spar caps 6, so that in use , as shown in figure 3, connecting pieces 8 are flush with adjacent spar caps 4.
    [0035] The assembly process for the joint in the field is as follows.
    [0036] As an initial step, the stringer segments 7 are supported by a jig through holes 10 and are placed together end to end so that the shear webs 3 meet at interface 9. They can be supported in this position by a support 11, preferably made of multiaxial material (figure 3), which receives and aligns the two shear webs 3. This support 11 fits exactly between the spar caps 4 so as to align the two segments 7 vertically. They are then bonded together or fixed using mechanical fasteners, the union being either temporary or permanent. Although this involves handling two large components, this operation should be contrasted with the gluing operation described above in relation to figure 1. The gluing operation just described is simply to position the two joint parts in which the gluing operation main gluing is carried out. In relation to figure 1, the operation being performed was the main gluing operation between the two components. In the case of figure 1, any difficulties in handling two large components directly affect the quality of the joint for reasons explained above.
    [0037] Once the two segments have been positioned with respect to each other, adhesive can be applied to the sloping surfaces 6, 9 when the connecting piece is then moved into place in a direction orthogonal to the longitudinal dimension of the spar.
    [0038] Rather than gluing two large components together, this operation simply requires gluing two small connecting pieces 8 to a larger underlying structure. The handling of the connecting pieces 8 is therefore much simpler than trying to glue or connect two spar segments together. As a result, the connecting piece 7 can be handled with greater stability. Even better, any misalignment of the connecting piece that would tend to disturb adhesive from one of the surfaces will not move the adhesive a significant distance, as the connecting piece 7 itself only moves over a very small distance. to their gluing positions, compared to gluing the two stringer segments together where the greater distances involved introduce much greater potentials for scraping adhesive from the larger areas.
    [0039] A second joint is shown in figure 5. This is the same in most respects as the first joint and the same reference numbers were used to designate the same components. The difference is that the joint is being applied to the box beam, rather than the I-beam of the first joint. Thus, each spar segment 7' has a pair of shear webs 3', one on each side of a respective spar cap. The joint is the same except that two supports 10 are used, one for each 3’ shear web.
    [0040] A third joint is shown in figure 6. This is simply a double version of the joint in figure 5. It will be appreciated from this that the joint can be applied to beams connected side by side with a small gap between adjacent shear webs to receive supports 11. The two beams, as shown in figure 6, are slightly offset. By constructing multiple beams in this way, a spar with a more complex shape can be formed.
    [0041] A fourth joint is shown in figures 7A and 7B. In this case, a connector piece is laminated 'in situ'. This could be achieved using any composite lamination techniques (or combinations) that are well known in the art, such as wet lamination, resin infusion and prepreg, for example. The 'laminate stack' will predominantly consist of unidirectional fibers with the main direction along the beam axis and a small percentage of multiaxial fibers to stabilize the structure and assist in the lamination (typically around 10¬20%). The fibers can be glass, carbon, aramid or fiber of another structure, and the resin can be epoxy, vinyl ester, polyester or polyurethane, for example. The stack is created by placing every 12 into the undercut created by the two stringer ends, starting with the small lengths of laminate over the first layers (figure 7A) and then increasing to longer lengths over the last laminate as the undercut size increases , as is well known in the art. Once the laminate pile has been created (including the resin) it will then be heated to cure the laminate 'in situ', this is also typically done under light vacuum. This method can be applied to any of the beam types in the preceding examples.
    [0042] An example of the stringer assembly in the factories shown in figures 8 and 9.
    [0043] Unlike the previous examples where beam sections are made and then joined end to end, if the joint is made in a factory, full length components can be made from scratch. Initially, two stringer caps 4 (as shown in figure 8A) are inserted into a jig, as shown in figure 9. As shown, the jig is a main jig 20 with two end sections 21, in which the stringer caps are fixed, for example, using a G-clamp. A very simple vacuum bag can also be used for this purpose. The jig and end sections 20, 21 all have a U-shaped cross section as in figures 9A-C. In place of the jig and end sections 20, 21, the same process can be performed using the tool that was initially used to form the spar caps. If the spar is made of more than one section, the sections can be made at the same time in additional jigs arranged next to the jig illustrated. Alternatively, a section can be made as shown in figure 9 and then the joined subset can be moved across to allow the next section to be joined. Once in place, the connecting piece 8 is added using one of the methods described above as shown in figure 8B. The joint is then cured at a curing temperature of 50-120°C (which temperature range is appropriate to cure all of the examples set out above). Additional connections can be made until the full length of the stringer cap is made. This process is repeated, producing a second stringer cap. These two spar caps are then joined by a pair of webs 3, as shown in figure 8C. To produce a more complex spar shape, two beams are then joined side by side as shown in figure 8D. As mentioned previously, the two beams can be offset and can be of different depths to allow complex beam sections to be produced.
    权利要求:
    Claims (15)
    [0001]
    1. WIND TURBINE BLADE, comprising an aerodynamic fairing (F) supported along at least a portion of its axial length by a stringer, the stringer comprising at least two stringer segments (1, 2) joined end to end in one interface (9), each spar segment (1, 2) comprising a shear core (3) with a spar cap (4) on each side; characterized in that an outer face (6) of each spar cap (4) thins inwards towards the interface (9) so that its depth is reduced towards the interface (9) creating a recess on each side of the interface (9) formed by the thinned faces of adjacent spar caps (4); and a respective connecting piece (8) sized to fit within each recess, each connecting piece (8) being secured to the tapered faces of adjacent spar caps (4) to form a double snap-in joint.
    [0002]
    2. Blade, according to claim 1, characterized in that the end of each shear web (3) is perpendicular to the axial direction so that the ends of the shear webs (3) support each other.
    [0003]
    Blade, according to any one of claims 1 to 2, characterized in that there is no double socket joint between the shear cores (3).
    [0004]
    Blade according to any one of claims 1 to 3, characterized in that the connecting piece (8) is connected to the thinned faces of adjacent spar caps (4).
    [0005]
    Blade according to claim 4, characterized in that the connecting piece (8) is a precured component.
    [0006]
    Blade, according to any one of claims 1 to 4, characterized in that the connecting piece (8) is formed "in situ" from a plurality of laminations.
    [0007]
    Blade according to any one of claims 1 to 6, characterized in that the shear webs (3) of adjacent spar segments (1, 2) are connected together.
    [0008]
    Blade according to claim 7, characterized in that shear cores (3) of adjacent spar segments (1, 2) are bonded together with adhesive.
    [0009]
    Blade according to any one of claims 1 to 8, characterized in that it additionally comprises a support member which receives and aligns the shear webs (3) with respect to one another.
    [0010]
    Blade according to any one of claims 6 to 7, characterized in that adjacent spar segments (1, 2) are bonded together with adhesive which is applied to the support member.
    [0011]
    11. METHOD OF PRODUCING A SHOVEL as defined in any one of claims 1 to 8, characterized in that it comprises the steps of inserting stringer caps (4) of adjacent segments into a U-shaped channel with its surface thinned to the most superior; and mounting the connecting piece (8) on the tapered surfaces of adjacent spar caps (4) to form a subassembly.
    [0012]
    12. The METHOD according to claim 11, characterized in that it further comprises subsequently joining additional spar caps (4) with additional connecting pieces (8) to the sub-assembly to form a first spar cap (4).
    [0013]
    13. METHOD according to claim 12, characterized in that it further comprises forming a second spar cap (4), and joining the first and second spar cap (4) with at least one shear core (3) to form a first stringer beam.
    [0014]
    The METHOD of claim 13, further comprising forming a second spar beam and joining the first and second beams side by side to form a spar.
    [0015]
    15. METHOD according to any one of claims 11 to 14, characterized in that the U-shaped channel is the channel used to form the stringer caps (4).
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    法律状态:
    2018-03-13| B25G| Requested change of headquarter approved|Owner name: BLADE DYNAMICS LIMITED (GB) |
    2018-12-26| B06F| Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]|
    2019-11-12| B06U| Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette]|
    2021-03-30| B09A| Decision: intention to grant [chapter 9.1 patent gazette]|
    2021-05-11| B16A| Patent or certificate of addition of invention granted|Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 08/07/2011, OBSERVADAS AS CONDICOES LEGAIS. |
    优先权:
    申请号 | 申请日 | 专利标题
    GBGB1011539.2A|GB201011539D0|2010-07-08|2010-07-08|A wind turbine blade|
    GB1011539.2|2010-07-08|
    PCT/GB2011/001035|WO2012004571A2|2010-07-08|2011-07-08|A wind turbine blade|
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