LIGHTNING PROTECTION OF A SECTIONED WIND TURBINE BLADE
20210381494 · 2021-12-09
Inventors
Cpc classification
F05B2240/302
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D80/30
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05B2280/2006
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D1/0675
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05B2280/6003
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
Disclosed is a spar beam and a wind turbine blade comprising a spar beam. The wind turbine blade comprising a first blade section extending along a longitudinal axis from a root to a first end and a second blade section extending along the longitudinal axis from a second end to a tip. The spar beam comprises a conductive beam sheath circumscribing at least a beam sheath angular distance of the spar beam about the spar beam axis and longitudinally extending from a fourth beam axis position to a fifth beam axis position.
Claims
1. A wind turbine blade extending along a longitudinal axis from a root through a first airfoil region and a second airfoil region to a tip, the wind turbine blade comprising a first blade section extending along the longitudinal axis to a first end and a second blade section extending along the longitudinal axis from a second end towards the tip, the first blade section comprising the first airfoil region, the second blade section comprising the second airfoil region, the wind turbine blade comprising a spar beam structurally connecting the first blade section and the second blade section, the spar beam longitudinally extending along a spar beam axis from a first beam end at a first beam axis position to a second beam end at a second beam axis position and being positioned such that the first beam axis position is located in the first airfoil region and the second beam axis position is located in the second airfoil region and a third beam axis position, between the first beam axis position and the second beam axis position, is aligned with the second end of the second blade section, and wherein the spar beam comprises a conductive beam sheath circumscribing at least a beam sheath angular distance of the spar beam about the spar beam axis and longitudinally extending along the spar beam axis from a fourth beam axis position to a fifth beam axis position.
2. Wind turbine blade according to claim 1, wherein the fourth beam axis position and the fifth beam axis position are between the first beam axis position and the second beam axis position.
3. Wind turbine blade according to claim 1, wherein the conductive beam sheath is a mesh of electrically conductive material.
4. Wind turbine blade according to claim 1, wherein the beam sheath angular distance is more than 90 degrees, such as more than 180 degrees, such as more than 270 degrees, such as 360 degrees.
5. Wind turbine blade according to claim 1, wherein the fifth beam axis position is the second beam axis position.
6. Wind turbine blade according to claim 1, wherein the fifth beam axis position is between the fourth beam axis position and the second beam axis position.
7. Wind turbine blade according to claim 1, wherein the fourth beam axis position is between the third beam axis position and the fifth beam axis position.
8. Wind turbine blade according to claim 1, wherein the fourth beam axis position and the third beam axis position is separated by a first distance, the first distance being more than 10 mm.
9. Wind turbine blade according to claim 1, wherein the spar beam comprises carbon fibre with a fibre volume ratio of more than 40%, such as more than 50%, such as more than 60%.
10. Wind turbine blade according to claim 1, wherein a first shell part of the first blade section comprises a first conductive shell sheath circumscribing at least a first sheath angular distance about the longitudinal axis from a first primary sheath angular position to a first secondary sheath angular position and longitudinally extending from a first sheath position to a second sheath position, e.g. wherein the first shell part comprises a first spar cap, and wherein the first conductive shell sheath is positioned such that the first spar cap is located between the first primary sheath angular position and the first secondary sheath angular position, and/or wherein a second shell part of the first blade section comprises a second conductive shell sheath circumscribing at least a second sheath angular distance about the longitudinal axis from a second primary sheath angular position to a second secondary sheath angular position and longitudinally extending from the first sheath position to the second sheath position, optionally wherein the second shell part comprises a second spar cap, and wherein the second conductive shell sheath is positioned such that the second spar cap is located between the second primary sheath angular position and the second secondary sheath angular position, and/or wherein the first conductive shell sheath and/or the second conductive shell sheath is a mesh of electrically conductive material.
11. Wind turbine blade according to claim 1, wherein the first blade section comprises a first down conductor configured for conducting lightning current to ground.
12. Wind turbine blade according to claim 11, wherein the first down conductor is electrically connected to the first conductive shell sheath and/or the second conductive shell sheath.
13. Wind turbine blade according to claim 12, wherein the second blade section comprises a second down conductor being connected to the first down conductor of the first blade section.
14. Wind turbine blade according to claim 13, wherein the second down conductor is electrically connected to the conductive beam sheath at a sixth beam axis position, wherein the sixth beam axis position is between the fourth beam axis position and the fifth beam axis position, and wherein the sixth beam axis position and the fifth beam axis position is separated by a second distance, the second distance being less than 100 mm, such as less than 50 mm, e.g. the sixth beam axis position may be the fifth beam axis position.
15. Wind turbine blade according to claim 1, wherein the second blade section comprises a first lightning receptor at or in proximity of the external surface of the blade, wherein the first lightning receptor is positioned at or in proximity of the tip.
16. Wind turbine blade according to claim 15, wherein the second down conductor is electrically connected to the first lightning receptor.
17. Spar beam for structurally connecting a first blade section and a second blade section of a wind turbine blade, wherein the wind turbine blade extends along a longitudinal axis from a root through a first airfoil region and a second airfoil region to a tip, wherein the first blade section extends along the longitudinal axis to a first end and the second blade section extends along the longitudinal axis from a second end towards the tip, the first blade section comprising the first airfoil region, the second blade section comprising the second airfoil region, the spar beam longitudinally extending along a spar beam axis from a first beam end at a first beam axis position to a second beam end at a second beam axis position and being configured to be positioned such that the first beam axis position is located in the first airfoil region and the second beam axis position is located in the second airfoil region and a third beam axis position between the first beam axis position and the second beam axis position is aligned with the second end of the second blade section, and wherein the spar beam comprises a conductive beam sheath circumscribing at least a beam sheath angular distance about the spar beam axis and longitudinally extending along the spar beam axis from a fourth beam axis position to a fifth beam axis position.
18. A method for structurally connecting a first blade section with a second blade section of a wind turbine blade, the method comprising: providing a spar beam according to claim 17 and the first and second blade section of the wind turbine blade; positioning the spar beam such that the first beam axis position is located in the first airfoil region of the first blade section and the second beam axis position is located in the second airfoil region of the second blade section and the third beam axis position is aligned with the second end of the second blade section; and structurally connecting the first blade section and the second blade section via the spar beam.
19. Use of a spar beam according to claim 17 for structurally connecting a first blade section and a second blade section to form a wind turbine blade, wherein the wind turbine blade extends along a longitudinal axis from a root through a first airfoil region and a second airfoil region to a tip, wherein the first blade section extends along the longitudinal axis to a first end and the second blade section extends along the longitudinal axis from a second end towards the tip, the first blade section comprising the first airfoil region, the second blade section comprising the second airfoil region.
Description
BRIEF DESCRIPTION OF THE FIGURES
[0052] Embodiments of the disclosure will be described in more detail in the following with regard to the accompanying figures. The figures show one way of implementing the present invention and are not to be construed as being limiting to other possible embodiments falling within the scope of the attached claim set.
[0053]
[0054]
[0055]
[0056]
[0057]
[0058]
[0059]
[0060]
DETAILED DESCRIPTION
[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 area 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 r 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 r from the hub.
[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 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 may comprise two blade shell parts, a first blade shell part 24 and a second blade shell part 26, typically made of fibre-reinforced polymer. The first blade shell part 24 is typically a pressure side or upwind blade shell part. The second blade shell part 26 is typically a suction side or downwind blade shell part. The first blade shell part 24 and the second blade shell part are typically glued together along bond lines or glue joints 28 extending along the trailing edge 20 and the leading edge 18 of the blade 10. Typically, the root ends of the blade shell parts 24, 26 has a semi-circular or semi-oval outer cross-sectional shape.
[0067] The wind turbine blade 10 extends along a longitudinal axis L. The root end 17 extends in a root end plane, substantially perpendicular to the longitudinal axis L.
[0068]
[0069] The wind turbine blade 10 comprises a chord line 38 between the leading edge 18 and the trailing edge 20.
[0070] The wind turbine blade 10 comprises shear webs 42, such as a leading edge shear web and a trailing edge shear web. The shear webs 42 could alternatively be a spar box with spar sides, such as a trailing edge spar side and a leading edge spar side.
[0071]
[0072] The wind turbine blade 10 is a so-called split blade, or two-part blade, or segmented blade. The wind turbine blade 10 comprises a first blade section 44 and a second blade section 46. The first blade section 44 extends along the longitudinal axis L from a root, such as the root end 17, to a first end 50. The second blade section 46 extends along the longitudinal axis L from a second end 52 to a tip, such as the tip end 15. The first blade section comprises 44 a root region 30, a first airfoil region 34a and a transition region 32 between the root region 30 and the first airfoil region 34a. The second blade section 46 comprises a second airfoil region 34b with the tip, such as the tip end 15. The first blade section 44 and the second blade section 46 may be connected with a spar beam (see following figures).
[0073]
[0074] The spar beam 60 extends along a spar beam axis B. The spar beam axis B may be coinciding and/or parallel with the longitudinal axis of the wind turbine blade 10. The spar beam 60 extends from a first beam axis position pb1 in the first airfoil region 34a to a second beam axis position pb2 in the second airfoil region 34b.
[0075] A third beam axis position pb3 is between the first beam axis position pb1 and second beam axis position pb2. The third beam axis position pb3 is aligned with the second end 52 of the second blade section 46.
[0076] The spar beam 60 comprises a conductive beam sheath 62. The conductive beam sheath 62 circumscribes at least a beam sheath angular distance 68 (see, e.g.
[0077] Also illustrated are a fourteenth beam axis position pb14 and a fifteenth beam axis position pb15. These positions may denote a part of the spar beam 60 comprising electrically conductive fibres, such as carbon fibres. For example, the spar beam 60 may comprise carbon fibres between the fourteenth beam axis position pb14 and a fifteenth beam axis position pb15. For example, the spar beam may comprise pultruded fibre reinforced elements 110, 112 comprising carbon fibres between the fourteenth beam axis position pb14 and the fifteenth beam axis position pb15. Alternatively or additionally, the pultruded fibre reinforced element 110, 112, e.g. being pultruded carbon fibre reinforced elements may extend between the fourteenth beam axis position pb14 and the fifteenth beam axis position pb15.
[0078] The fifteenth beam axis position pb15 is between the fifth beam axis position pb5 and the fourth beam axis position pb4. The fifteenth beam axis position pb15 and the fifth beam axis position pb5 is separated by a fourth distance D4. The fourth distance D4 may be more than 10 mm, such as more than 20 mm, such as more than 30 mm, such as 50 mm. By terminating the content of conductive fibres prior to the end of the conductive beam sheath 62, lightning protection of the spar beam 60 may be enhanced.
[0079]
[0080] The wind turbine blade 10 comprises a spar beam 60. The spar beam 60 comprises a conductive beam sheath 62 circumscribing at least a beam sheath angular distance 68 about the spar beam axis B. The beam sheath angular distance 68 is more than 90 degrees, such as more than 180 degrees, such as more than 270 degrees, such as 360 degrees. For example, the beam sheath 62 may circumscribe the entire spar beam axis B, e.g. the beam sheath angular distance 68 may be 360 degrees, such as illustrated. The cross section of the spar beam 60 is substantially rectangular. However, alternatively the cross section of the spar beam 60 may be circular or oval.
[0081]
[0082] The first blade section 44 comprises a first down conductor 80 configured for conducting lightning current to ground. The first down conductor 80 is electrically connected to the first conductive shell sheath 64 and/or the second conductive shell sheath 66. The second blade section 46 comprises a second down conductor 82. The second down conductor 82 is configured for being connected to the first down conductor 80 of the first blade section 44.
[0083] The second down conductor 82 is electrically connected to the conductive beam sheath 62 at a sixth beam axis position pb6. The sixth beam axis position pb6 is between the fourth beam axis position pb4 and the fifth beam axis position pb5. The sixth beam axis position pb6 and the fifth beam axis position pb5 is separated by a second distance D2. The second distance D2 may be less than 150 mm, such as less than 100 mm, such as less than 50 mm. In an alternative exemplary wind turbine blade, the sixth beam axis position pb6 may be the fifth beam axis position pb5. For example, the second distance D2 may be 0 mm. The second down conductor 82 may be electrically connected to the conductive beam sheath at a plurality of beam axis positions, e.g. including the sixth beam axis position pb6 and a seventh beam axis position pb7.
[0084] The wind turbine blade 10 comprises a plurality of lightning receptors 86 at or in proximity of the external surface of the wind turbine blade 10. The plurality of lightning receptors 86 are electrically connected to the first down conductor 80 and/or the second down conductor 82. The second blade section 46 comprises a first lightning receptor 84. The first lightning receptor 84 is positioned at or in proximity of the tip end 15. The second down conductor 82 is electrically connected to the first lightning receptor 84.
[0085]
[0086] The first shell part 24 comprises a first conductive shell sheath 64 circumscribing at least a first sheath angular distance 70 about the longitudinal axis L from a first primary sheath angular position pall to a first secondary sheath angular position pa12. The first conductive shell sheath 64 may longitudinally extend from a first sheath position psi. (see
[0087] The second shell part 26 comprises a second conductive shell sheath 66 circumscribing at least a second sheath angular distance 72 about the longitudinal axis L from a second primary sheath angular position pa21 to a second secondary sheath angular position pa22. The second conductive shell sheath 66 may longitudinally extend from a first sheath position psi. (see
[0088] The first conductive shell sheath 64 and/or the second conductive shell sheath 66 may be a mesh or partly a mesh. The first conductive shell sheath 64 and/or the second conductive shell sheath 66 may be of an electrically conductive material, such as carbon fiber reinforced polymer or metals, such as copper, or alloy of metals.
[0089] For illustrative purposes, the spar caps 74, 76 and the conductive shell sheaths 64, 66 are shown separately from the shells 24, 26 of the wind turbine blade 10. However, the spar caps 74, 76 and/or the conductive shell sheaths 64, 66 may be integral parts of the shell parts 24, 26.
[0090] A first down conductor 80, runs in a longitudinal direction of the blade 10 along the shear web 42, e.g. along the trailing edge shear web. The first down conductor 80 may alternatively run along the leading edge shear web. The first down conductor 80 is electrically connected to a plurality of lightning receptors 86. The lightning receptors 86 may be supported by a receptor bracket 90. The receptor bracket 90 may be of an electrically conductive material, such as a carbon fiber reinforced polymer or metal. Alternatively, the receptor bracket 90 may be of a non-electrically-conductive material, in which case, the receptors 86 may be electrically connected to the first down conductor 80 with cables or other conductive means. The lightning receptors 86 may be located at or in the proximity of the external surface of the wind turbine blade 10.
[0091] The term “receptor” is to be understood as an electrically conductive object being configured with a view to capturing and conducting a lightning current.
[0092] Throughout the disclosure, the term “conductive”, if not specified otherwise, is to be understood as electrically conductive.
[0093] Numbered elements are provided purely for naming purposes to allow distinguishing between elements. Hence, numbering does not imply any order of importance, and the presence of a numbered element is not to be construed as implying the presence of any lower numbered elements. For example, a fourth element may be present without a corresponding first, second or third element.
[0094] The invention has been described with reference to preferred embodiments. However, the scope of the invention is not limited to the illustrated embodiments, and alterations and modifications can be carried out without deviating from the scope of the invention.
LIST OF REFERENCES
[0095] 2 wind turbine
[0096] 4 tower
[0097] 6 nacelle
[0098] 8 hub
[0099] 10 blade
[0100] 14 blade tip
[0101] 15 tip end
[0102] 16 blade root
[0103] 17 root end
[0104] 18 leading edge
[0105] 20 trailing edge
[0106] 24 first blade shell part (pressure side)
[0107] 26 second blade shell part (suction side)
[0108] 28 bond lines/glue joints
[0109] 30 root region
[0110] 32 transition region
[0111] 34 airfoil region
[0112] 34a first airfoil region
[0113] 34b second airfoil region
[0114] 36 tip region
[0115] 38 chord line
[0116] 40 shoulder
[0117] 42 shear web or spar side
[0118] 44 first blade section
[0119] 46 second blade section
[0120] 50 first end
[0121] 52 second end
[0122] 60 spar beam
[0123] 62 beam sheath
[0124] 64 first conductive shell sheath
[0125] 66 second conductive shell sheath
[0126] 68 beam sheath angular distance
[0127] 70 first sheath angular distance
[0128] 72 second sheath angular distance
[0129] 74 first spar cap
[0130] 76 second spar cap
[0131] 80 first down conductor
[0132] 82 second down conductor
[0133] 84 first lightning receptor
[0134] 86 lightning receptor
[0135] 90 receptor bracket
[0136] B spar beam axis
[0137] D1 first distance
[0138] D2 second distance
[0139] D3 third distance
[0140] D4 fourth distance
[0141] L longitudinal axis
[0142] pa11 first primary sheath angular position
[0143] pa12 first secondary sheath angular position
[0144] pa21 second primary sheath angular position
[0145] pa22 second secondary sheath angular position
[0146] pb1 first beam axis position
[0147] pb2 second beam axis position
[0148] pb3 third beam axis position
[0149] pb4 fourth beam axis position
[0150] pb5 fifth beam axis position
[0151] pb6 sixth beam axis position
[0152] pb7 seventh beam axis position
[0153] pb14 fourteenth beam axis position
[0154] pb15 fifteenth beam axis position
[0155] ps1 first sheath position
[0156] ps2 second sheath position