VORTEX GENERATOR TAPE FOR A WIND TURBINE BLADE AND METHOD OF MANUFACTURE AND ATTACHMENT THEREOF
20230265825 · 2023-08-24
Inventors
Cpc classification
F03D1/0633
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05B2240/3062
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y02P70/50
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
F05B2230/90
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y02E10/72
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
International classification
Abstract
A vortex generator tape for installation on an outer surface of a wind turbine blade, the vortex generator comprising an elongate base part comprising an inner side configured for being adhered to the outer surface of the wind turbine blade, and an outer side arranged opposite to the inner side; and a plurality of protrusions each for generating vortices during the operation of the wind turbine blade, wherein each protrusion protrudes from the outer side of the base part and is spaced apart from every other protrusion along the base part; wherein the plurality of protrusions is formed integrally with the base part.
Claims
1. A vortex generator tape for installation on an outer surface of a wind turbine blade, the vortex generator comprising: an elongate base part comprising an inner side configured for being adhered to the outer surface of the wind turbine blade, and an outer side arranged opposite to the inner side; and a plurality of protrusions for generating vortices during the operation of the wind turbine blade, wherein each protrusion protrudes from the outer side of the base part; wherein the plurality of protrusions is formed integrally with the base part.
2. A vortex generator tape according to claim 1, wherein the plurality of protrusions and the base part are formed of the same material, preferably from a single mass of material.
3. A vortex generator tape according claim 1, wherein the vortex generator tape comprises a supply state and an uncoiled state and wherein the base part is flexible so that the base part is coiled up in a roll in the supply state, and so that the base part is uncoiled and substantially flat in the uncoiled state, wherein the vortex generator tape is configured for being installed on the outer surface of the wind turbine blade when in the uncoiled state.
4. A vortex generator tape according to claim 1, wherein each protrusion has a maximum protrusion height, the maximum protrusion height of each protrusion being between 0.1 mm and 20 mm, preferably between 0.5 mm and 15 mm, more preferably between 1 mm and 10 mm, or even more preferably between 2 mm and 5 mm.
5. A vortex generator tape according to claim 1, wherein each protrusion of the plurality of protrusions have substantially equal maximum protrusion height.
6. A vortex generator tape according to claim 1, wherein each protrusion has a protrusion thickness, such as a fin thickness, wherein the protrusion thickness of each protrusion is less than 5 mm, preferably less than 1 mm.
7. A vortex generator tape according to claim 1, wherein the plurality of protrusions comprises one or more protrusion pairs, such as fin pairs, wherein each protrusion pair comprising a left protrusion and a right protrusion having different shapes and being mirror symmetrical shape with respect to each other.
8. A vortex generator tape according to claim 1, comprising at least two protrusions, preferably at least four protrusions, more preferably at least eight protrusions, or even more preferably at least sixteen protrusions.
9. A vortex generator tape according to claim 1, wherein at least the plurality of protrusions of the vortex generator tape, preferably the entire vortex generator tape, is obtained by additive manufacturing, such as 3D-printing.
10. A wind turbine blade comprising an outer surface and a vortex generator tape according claim 1 adhered to the outer surface.
11. A method for manufacturing a vortex generator tape for a tip of a wind turbine blade, comprising the steps of: providing an elongate base part comprising an inner side and an outer side opposite the inner side; integrally forming a plurality of protrusions on the base part so that each protrusion protrudes from the outer side of the base part; and applying an adhesive layer to the inner side of the base part.
12. A method according to claim 11, wherein the step of integrally forming the plurality of protrusions on the base part is performed by additive manufacturing, such as 3D-printing.
13. A method according to claim 11, wherein the base part is provided by an extrusion process and wherein the plurality of protrusions is integrally formed on the base part by a thermoforming process, e.g. vacuum thermoforming process.
14. A method for attaching a vortex generator tape to an outer surface of a wind turbine blade, the method comprising the steps of: providing a vortex generator tape according to claim 1 or performing a method of manufacturing a vortex performing a method of manufacturing a vortex generator tape for a tip of a wind turbine blade; providing a wind turbine blade having an outer surface; and adhering the inner side of the vortex generator to the outer surface of the wind turbine blade.
15. A method according to claim 14, wherein the vortex generator tape is provided as a coiled-up roll in a supply state, the method further comprises uncoiling at least a portion of the vortex generator tape to an uncoiled state, and optionally cutting the uncoiled portion of the vortex generator tape, preferably prior to adhering the vortex generator tape to the outer surface of the wind turbine blade.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0052] Embodiments of the present disclosure will be described in more detail in the following with regard to the accompanying figures. Like reference numerals refer to like elements throughout. Like elements may, thus, not be described in detail with respect to the description of each figure. The figures show one way of implementing embodiments of the present disclosure and are not to be construed as being limiting to other possible embodiments falling within the scope of the attached claim set. In addition, an illustrated embodiment needs not have all the aspects or advantages shown. An aspect or an advantage described in conjunction with a particular embodiment is not necessarily limited to that embodiment and can be practiced in any other embodiments even if not so illustrated, or if not so explicitly described.
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DETAILED DESCRIPTION
[0060] In the following figure description, the same reference numbers refer to the same elements and may thus not be described in relation to all figures.
[0061]
[0062]
[0063] The airfoil region 34 (also called the profiled region) has an ideal or almost ideal blade shape with respect to generating lift, whereas the root region 30 due to structural considerations has a substantially circular or elliptical cross-section, which for instance makes it easier and safer to mount the blade 10 to the hub. The diameter (or the chord) of the root region 30 may be constant along the entire root region 30. The transition region 32 has a transitional profile gradually changing from the circular or elliptical shape of the root region 30 to the airfoil profile of the airfoil region 34. The chord length of the transition region 32 typically increases with increasing distance from the hub. The airfoil region 34 has an airfoil profile with a chord extending between the leading edge 18 and the trailing edge 20 of the blade 10. The width of the chord decreases with increasing distance from the root end 17.
[0064] A shoulder 40 of the blade 10 is defined as the position, where the blade 10 has its largest chord length. The shoulder 40 is typically provided at the boundary between the transition region 32 and the airfoil region 34.
[0065] It should be noted that the chords of different sections of the blade 10 normally do not lie in a common plane, since the blade may be twisted and/or curved (i.e. pre-bent), thus providing the chord plane with a correspondingly twisted and/or curved course, this being most often the case in order to compensate for the local velocity of the blade being dependent on the radius from the hub.
[0066] The wind turbine blade 10 comprises a blade shell 13 typically comprising an outer surface 22 and two blade shell parts or half shells: a first blade shell part 24 and a second blade shell part 26, typically made of fibre-reinforced polymer. The wind turbine blade 10 may comprise additional shell parts, such as a third shell part and/or a fourth shell part. The first blade shell part 24 is a suction side or downwind blade shell part. The second blade shell part 26 is a pressure side or upwind blade shell part. The first blade shell part 24 and the second blade shell part 26 are fastened together with adhesive, such as glue, along bond lines or glue joints extending along the trailing edge 20 and the leading edge 18 of the blade 10 typically via a glue flange.
[0067] The performance of the tip region 36 of the blade 10 can be optimised by installing a vortex generator tape 50 on an outer surface 22 of the wind turbine blade 10 near the leading edge 18 as shown in
[0068] As best seen in
[0069] In each embodiment, the protrusions have the same shape, but the protrusion shape varies between embodiments. A first embodiment is shown in
[0070] Prior to installing the vortex generator tape 50 on the wind turbine blade 10, the vortex generator tape 50 is advantageously provided in a supply state wherein the base part 60 is coiled up around a paperboard roll core 64 as is shown for the third embodiment in
[0071] The polymer material of the base part 60 is flexible enough to allow the installer to uncoil the base part 60 and bring it to an uncoiled state in which the base part is substantially flat and allows it to conform to the outer surface 22 of the blade 10 as shown in
[0072] The protrusions may have many different shapes.
TABLE-US-00001 LIST OF REFERENCES 2 wind turbine 4 tower 6 nacelle 8 hub 10 blade 13 shell 14 blade tip 15 tip end 16 blade root 17 root end 18 leading edge 20 trailing edge 22 outer surface 24 first blade shell part 26 second blade shell part 30 root region 32 transition region 34 airfoil region 36 tip region 40 shoulder 50 vortex generator tape 51 wind direction 60 base part 61 inner side 62 outer side 63 inner diameter 64 roll core 70 protrusion 70a left protrusion 70b right protrusion 71 protrusion height direction