Patent Application
20220065819
The present disclosure relates to a structural web of a wind turbine blade and to a method of forming a structural web. The disclosure also relates to a method of assessing the integrity of adhesive bonds between the structural web and wind turbine blade shell using non-destructive ultrasonic testing techniques.
Typically wind turbine blades are manufactured in two halves, or shells, which are adhesively bonded together along a leading edge and a trailing edge. One or more structural webs are commonly provided between the shell halves.
Adhesive is used to bond the inner surfaces of the shells to the shear web structure, and to bond the outer edges of the shells together. It will be appreciated that the adhesive bonds provide critical connections between the various components of the blade, and that the bonds must therefore have extremely high integrity to withstand the high forces and fatigue loads experienced in operation. To this end, the process of forming and assessing adhesive bonds during production of wind turbine blades must be highly robust.
It will be appreciated that any flaw in an adhesive bond between the component parts of a wind turbine blade is a potential source of crack propagation and/or failure in use. It is therefore desirable that any flaws in the adhesive bonds are detectable using non-destructive analysis techniques so that they may be remedied before the wind turbine blade is put into service.
It is against this background that the present invention has been developed.
An aspect of the invention provides a method of producing a wind turbine blade. The method comprises providing a structural web which comprises a web member having a web portion and a flange portion extending away from the web portion, wherein the web member comprises a heel of substantially curvilinear form located between the web portion and the flange portion; and a flange extender integrated with the flange portion of the web member, wherein a first section of the flange extender overlies the flange portion and a second section of the flange extender extends past the heel and away from the web portion of the web member. The method further comprising bonding the flange extender of the structural web to the inner surface of a windward or leeward wind turbine blade shell using an adhesive to form an adhesive bond; and using non-destructive ultrasonic test equipment to assess the integrity of the adhesive bond, wherein assessing the integrity of the adhesive bond comprises identifying first and second target surfaces of the structural web, wherein the first and second target surfaces are spaced from one another by an intermediate region in which it is not possible to positively identify any surface using the non-destructive ultrasonic test equipment, wherein positive identification of the first and second target surfaces is indicative of a good integrity bond in the intermediate region, and wherein positive identification of only one, or neither, of the target surfaces is indicative of a poor integrity bond in the intermediate region.
The structural web comprises the web member and the flange extender. The flange extender is then bonded to the inner surface of the wind turbine blade shell, and this inner surface may be the inner surface of a spar cap.
The first target surface may preferably be identified as being an inner surface of the flange portion of the web member, and the second target surface may preferably be identified as being an inner surface of the flange extender.
Preferably the intermediate region is identified as corresponding to the vicinity of the heel of the web member.
The flange extender may have a thickness of between 0.5 mm and 1 mm, preferably around 0.8 mm. The flange portion of the web may have a thickness of between 1 mm and 5 mm, preferably between 2 mm and 3 mm. The flange portion of the web may be at least twice as thick as the flange extender. The “thickness” refers to the size of the components between its two major surfaces.
The web member preferably comprises two flange portions and may preferably have a substantially C-shaped cross-section. A flange extender is preferably integrated with each flange portion.
In another aspect the present invention provides a method of using non-destructive ultrasonic test equipment to assess the integrity of an adhesive bond between a flange extender of a structural web assembly of a wind turbine blade and a shell of a wind turbine blade. The method comprises using non-destructive ultrasonic test equipment to identify first and second target surfaces of the structural web assembly, wherein the first and second target surfaces are spaced from one another by an intermediate region in which it is not possible to positively identify any surface using the non-destructive ultrasonic test equipment, wherein positive identification of the first and second target surfaces is indicative of a good integrity bond in the intermediate region, and wherein positive identification of only one, or neither, of the target surfaces is indicative of a poor integrity bond in the intermediate region.
Preferably, the first target surface is identified as being an inner surface of a flange portion of the structural web assembly and the second target surface is identified as being an inner surface of the flange extender.
In a preferred example, the intermediate region is identified as corresponding to the vicinity of a heel of the structural web assembly.
The method may preferably be used to assess the integrity of an adhesive bond between a first flange extender of a structural web assembly of a wind turbine blade and a first shell of a wind turbine blade; and to assess the integrity of an adhesive bond between a second flange extender of a structural web assembly of a wind turbine blade and a second shell of a wind turbine blade.
The present invention will now be described by way of non-limiting examples with reference to the following figures, in which:
Referring now to
The purpose of the glue catcher 6 is to prevent the adhesive 9 from flowing away from the heel 5 as pressure is applied between the web member 2 and the wind turbine blade shell 8. It will be appreciated that it is imperative to have sufficient adhesive 9 in the region of the heel 5 to ensure a good bond between the web 1 and the shell 8. The purpose of the glue catcher 6 is to prevent the adhesive 9 from flowing away from the heel 5 as it is pushed out from between the web member 2 and the wind turbine blade shell 8, and to retain it in the space 13. In this way, enough adhesive 9 is located between the heel 5 of the web member 2 and the wind turbine blade shell 8 to provide sufficient coverage of the heel 5 and to avoid the formation of potentially crack propagating sharp interfaces.
In
One of the problems of the prior art method of manufacture is that it is not possible to know if there is sufficient adhesive 9 in the space 13 to ensure that a robust bond has been formed. The glue catcher 6 is very flexible and the scrivets 7 are relatively weak. Because of this, it may be that the adhesive 9 has pushed the glue catcher 6 out of the way, and/or that the scrivets 7 have broken under the tensile loads caused by the adhesive 9 pushing against the glue catcher 6 as it is pushed out from between the web member 2 and the wind turbine blade shell 8.
Once the structural web assembly 1 is bonded between the wind turbine blade shells, it is not possible to visually inspect the adhesive bond. Furthermore, it is also not possible to interrogate the integrity of the adhesive bond in the region of the heel 5 using ultrasonic non-destructive testing (NDT) equipment as there is no internal feature in this region which may be reliably identified by ultrasonic NDT examination.
Referring to
In an NDT process, an ultrasonic transducer is positioned outside of the blade shell 8 (i.e. below the blade shells in the orientation of
Referring to
In contrast to this, in the region 17 extending from the position 19, immediately before the beginning of the heel 5, to the free end 18 of the glue catcher 6, there are no internal surfaces which may be positively identified by ultrasonic NDT analysis. Because of the curved shape of the heel 5 and the glue catcher 6, as well as the flexibility of the glue catcher 6 and the unpredictable formation of the accumulation of adhesive 12, it is not possible to positively identify any part of the interior blade structure in the region 17. For an NDT technician, the good adhesive bond of
Referring now to
The structural web 20 comprises a web member 2 having a web portion 3 and two flange portions 4 located on either side of the web portion 3. The flange portions 4 extend transversely from the web portion 3. A heel 5 is located between each of the flange portions 4 and the web portion 3. Two flange extenders 21 are integrated with the flange portions 4 by means of an adhesive bond. In this example, adhesive 9 is located between the flange extenders 21 and the flange portions 4.
The web portion 3 and two flange portions 4 together form a ‘C’ shaped web. With the addition of the flange extenders 21 this results in an ‘I’ shaped web assembly. The heel 5 is the transition between the web portion 3 and the flange portion 4 and is curved, such that it has a radius. To ensure a good load path between the web portion 3 and the flange portion 4, the radius of curvature of the heel 5 may be 20 mm for example.
The web member 2 is placed on a mould (not shown) and a bead 24 of adhesive 9 is applied to an outer surface of each of the flange portions 4. The flange extenders 21 are positioned adjacent to the flange portions 4 such that a portion 22 of the flange extenders 21 project past the heels 5 and away from the web portion 3. Pressure is applied to bring the flange extenders 21 into contact with the adhesive 9 and to force the adhesive 9 to flow along the breadth of the flange portions 4 so that a layer of adhesive 9 is formed between the flange extenders 21 and the flange portions 4.
As shown in
Once the adhesive has a suitable profile 23, it is cured so that the flange extenders 21 become integrated with the flange portions 4 of the web member 2 to form the structural web 20. The pressure applied between the flange extenders 21 and the flange portions 4 of the web member 2 is maintained for the duration of the adhesive cure to better ensure the integrity of the adhesive bond.
The adhesive bond between the flange portions 4 and the flange extenders 21 can be visually inspected. As can be seen there is an accumulation 10 of adhesive 9 at the free edge 11 of the flange portion 4 and an accumulation of adhesive 12 in the region of the heel 5 between the web member 2 and the flange extenders 21. This indicates that there will be adhesive across the full width of the flange portion 4. In addition, where the flange extender 21 is formed from glass fibre reinforced plastic it will be translucent, so a visual inspection of the adhesive bond can also be carried out simply by looking through the flange extender 21. These simple visual inspections can be used to qualify the use of the structural web 20 in the wind turbine blade manufacturing process. The adhesive 9 that forms in the region of the heel 5 between the web member 2 and the flange extenders 21 (e.g. 12 in
Heel coverage 14 is provided between the web member 2 and the flange extenders 21 in the region of the heel 5 to provide a suitable load transfer path without sharp edges or transitions.
In the example of
If the web member 2 comprises a lay-up of dry fibre material, the assembly is enclosed in a vacuum bag and resin is infused into the fibre lay-up prior to curing in a vacuum assisted resin transfer moulding technique (VARTM). If the web member 2 comprises a lay-up of pre-impregnated fibre material, the resin infusion step is not required and the resin is cured in a conventional pre-preg process. During the resin cure, the flange extenders 21 become integrated with the flange portions 4 of the web member 2 to form the structural web 20.
In the example of
For example, when the heel coverage 14 is a bead of adhesive, the adhesive 9 may be applied before the resin is cured (in the VARTM or pre-preg process) such that the adhesive 9 is in place and is cured along with the resin. Alternatively, the adhesive 9 may be applied after the resin is cured. The adhesive 9 is then cured in a separate step. A combination of these two methods may be used such that some of the adhesive 9 is applied before the resin cure, and a subsequent application of adhesive 9 is made after the resin cure. In either case, the adhesive 9 is preferably shaped with a filet profile 23 to ensure no sharp transitions between the adhesive 9 and the web member 2 or flange extenders 21.
When the heel coverage 14 is a filler material this may be incorporated as part of a VARTM process. A filler material, such as a fibrous rope, is placed between the web member 2 and the flange extender 21 in the region of the heel 5. During the resin infusion step, resin will infuse into the filler material to provide the heel coverage 14.
Regardless of whether the heel coverage 14 is a bead of adhesive or a filler material infused with resin, the end result is the same. Namely, a region of adhesive or resin which covers the radius of the heel 5 and ensures a good adhesive bond between the heel 5 and the flange extender 21.
After curing of the adhesive bond between the structural web 20 and the first wind turbine blade shell 30, a bead 36 of adhesive 9 is applied to the outermost surface of the remaining un-bonded flange extender 21. The second wind turbine blade shell 31 is placed on top of the adhesive 9 and pressure is applied to cause the adhesive 9 to flow between the flange extender 21 and the inner surface of the second wind turbine blade 31. Under the action of the applied pressure the adhesive 9 forms a layer 35 between the flange extender 21 and the inner surface of the second wind turbine blade 31 and forms accumulations 32, 33 at each free end of the flange extender 21. The adhesive 9 is cured with the pressure being maintained throughout the duration of the cure.
Similarly, in region 42 extending from a free edge 43 of the heel coverage 14 to a second free edge 44 of the flange extender 21, an inner surface 45 of the flange extender 21 may be identified by N DT analysis as the ultrasonic signal reflects off the interface between the inner surface 45 of the flange extender and the air filled space in the interior of the blade. Once again, this occurs at a predictable/consistent depth (corresponding to a signal return time) so that the surface 45 may be positively identified. As before, positive identification of this surface provides a strong indication that the region 42 between the flange extender 21 and the inner surface of the first wind turbine blade shell 30 is filled with adhesive and that therefore a good bond exists. If there is any portion of the region 42 in which there is an anomalous signal return at a lower depth (or a shorter signal return time), this indicates the existence of an air pocket somewhere below the surface 45 and hence a poor adhesive bond.
In contrast to the above, in the region 46 extending from the position 19 at the beginning of the heel 5 to the free edge 43 of the heel coverage 14, there are no internal surfaces which may be positively identified by ultrasonic NDT analysis. Because of the curved shape of the heel 5 and the heel coverage 14 in this region, it is not possible to positively identify any part of the interior blade structure in region 46. However, in view of the fact that it has been possible to ascertain that there is a good adhesive bond in the neighbouring regions 40 and 42, it is possible to surmise that, in all probability, the bond is also good in region 46.
By way of contrast,
As a result of the configuration of the structural web 20 and the manufacturing process described above, it is possible to have a high level of certainty that the adhesive bonds in the wind turbine blade between the structural web 20 and the wind turbine blade shells 30, 31 are robust. This is because the adhesive bonds in the structural web 20 are either visible or suitable for ultrasonic NDT analysis before the structural web 20 is bonded into the wind turbine blade, and because the adhesive bond between the structural member 20 and the wind turbine blade shells 30, 31 may be interrogated by ultrasonic NDT analysis in such a way as to provide a sufficient level of certainty that the bond is robust across its entire breadth.
In the examples described the web 20 is formed from glass fibre reinforced plastic (GFRP). The plastic matrix may be an epoxy matrix, for example. The adhesive used to bond the flange portion 4 to the flange extender 21 may be an epoxy or a polyurethane adhesive, for example. The adhesive used to bond the flange extender 21 to the blade shells may also be an epoxy or a polyurethane adhesive, for example. The wind turbine blade shells may be formed from GFRP and may also include carbon fibre reinforced plastic (CFRP).
In the examples described above the structural web 20 is formed first as a ‘C’ shaped web, and then the addition of the flange extenders results in an ‘I’ shaped web. However, it would also be possible to use the flange extender 21 on a single side of the web, rather than on both sides as shown in the Figures.
As described the flange extender 21 is a pre-cured composite component that is attached to the flange portions 4 of the web. The flange extender may have a thickness of between 0.5 mm and 1 mm, preferably around 0.8 mm. The flange portions 4 of the web may have a thickness of between 1 mm and 5 mm, preferably between 2 mm and 3 mm. Therefore, it can be seen that the flange extender 21 is a relatively thin component that is attached to the flange portion 4 as a process aid for adhesively bonding the structural web 20 to the blade shell. In other words, the flange extender does not contribute to the structural strength of the web, other than by ensuring a robust bond between the web and the shell.
| Number | Date | Country | Kind |
|---|---|---|---|
| PA 2018 70834 | Dec 2018 | DK | national |
| Filing Document | Filing Date | Country | Kind |
|---|---|---|---|
| PCT/DK2019/050407 | 12/18/2019 | WO | 00 |
