Wind turbine blade integrating a lightning protection system

Abstract

A wind turbine blade integrating a lightning protection system is provided. The wind turbine blade includes one spar cap formed by carbon plates stacked together; and a first down-conductor placed alongside the tip region of the spar cap, and a second down-conductor placed alongside the root region of the spar cap. The first down-conductor extends from the spar cap's tip end to the mid region, and terminates at a first down-conductor's end adjacent a first region of the spar cap which extends from a cross-sectional area of the spar cap which area is equal or higher than 75% of the maximum cross-sectional area of the spar cap, which is closest to the spar cap's tip end, to a cross-sectional area of the spar cap which is 100% of the cross-sectional area of the spar cap, being 100% of the cross-sectional area the one closest to the spar cap's root end.

Claims

1. A wind turbine blade integrating a lightning protection system, the wind turbine blade including at least one conductive spar cap formed by a stack of carbon plates having a plurality of carbon plates stacked together between a top carbon plate and a bottom carbon plate, and wherein each carbon plate has a root end and a tip end, and wherein the spar cap is an elongated body extending along an axis from a spar cap's root end to a spar cap's tip end, and having a blade tip region, a blade root region and a blade mid region in between the blade tip and root regions, wherein, the wind turbine blade further comprises a first down-conductor placed alongside the tip region of the spar cap, and a plurality of electric conductors connecting the first down-conductor to some of the tip ends of the carbon plates, and a second down-conductor placed alongside the root region of the spar cap, and a plurality of electric conductors connecting the second down-conductor to some of the root ends of the carbon plates, and wherein the first down-conductor extends from the spar cap's tip end towards the spar cap's mid region, and terminates at a first down-conductor's end located adjacent a first region of the spar cap which extends from a cross-sectional area of the spar cap which area is equal or higher than 75% of the maximum cross-sectional area of the spar cap, being that area the one closest to the spar cap's tip end, to a cross-sectional area of the spar cap which area is 100% of the cross-sectional area of the spar cap, being that 100% of the cross-sectional area the one closest to the spar cap's tip end.

2. The wind turbine blade according to claim 1, wherein the second down-conductor extends from the spar cap's root end towards the spar cap's mid region, and terminates at a second down-conductor's end located adjacent a second region of the spar cap which extends from a cross-sectional area of the spar cap which area is equal or higher than 75% of the maximum cross-sectional area of the spar cap, being that area the one closest to the spar cap's root end, to a cross-sectional area of the spar cap which area is 100% of the cross-sectional area of the spar cap, being that 100% of the cross-sectional area the one closest to the spar cap's root end.

3. The wind turbine blade according to claim 1, wherein at least the top carbon plate of the stack of carbon plates, is not electrically connected by an electric conductor to the first or to the second down conductors.

4. The wind turbine blade according to claim 1, wherein the first down-conductor extends from the spar cap's tip end to a plane orthogonal to the spar cap which passes through the end of the top carbon plate which is closest to the spar cap's tip end, and wherein there is an electric conductor connecting the top carbon plate's tip end to the first down-conductor.

5. The wind turbine blade according to claim 4, wherein the second down-conductor extends from the spar cap's root end to a plane orthogonal to the spar cap which passes through the end of the top carbon plate which is closest to the spar cap's root end, and wherein there is an electric conductor connecting the top carbon plate's root end to the second down-conductor.

6. The wind turbine blade according to claim 4, wherein all the carbon plates of the stack of carbon plates, have their tip end connected to the first down-conductor and their root end connected to the second down conductor.

7. The wind turbine blade according to claim 1, wherein the spar cap is an elongated body extending along an axis X, and wherein the first and the second down-conductors, are generally straight conductors running parallel to the axis X.

8. The wind turbine blade comprising two spar caps, namely a first spar cap and a second spar cap, each one constructed as defined in claim 1, the blade further comprising a lightning receptor at the tip of the beam, and a root terminal at the root end, and wherein the down-conductors of the tip region of the spar caps are connected at one end to the lightning receptor, and the down-conductors of the root region of the spar caps are connected at one end to the root terminal.

9. The wind turbine blade comprising two main spar caps and two secondary spar caps, each one of the spar caps constructed as defined in claim 1, and wherein the secondary spar caps are shorter than the main spar caps and extend parallel to the main spar caps, and wherein the distance between the tip end of a secondary spar caps to the tip of the a main spar caps is equal or longer than a length, wherein the length starts at the tip end of the main spar cap and terminates at a main spar cap position or radius where the cross-sectional area in that radius of the spar cap is equal or larger than 75% of the maximum cross-sectional area of the spar cap.

10. The wind turbine blade comprising two main spar caps and two secondary spar caps, each one of the spar caps constructed as defined in claim 1, and wherein the secondary spar caps are shorter than the main spar caps and extend parallel to the main spar caps, and wherein the distance between the tip end of a secondary spar caps to the tip end of the main spar caps is shorter than the a length, wherein the length starts at the tip end of the main spar cap and terminates at a main spar cap position or radius where the cross-sectional area in that radius of the spar cap is equal or larger than 75% of the maximum cross-sectional area of the spar cap.

11. The wind turbine blade according to claim 1, wherein the first and the second down-conductors) are made of copper, aluminum, or other conductive material.

12. The wind turbine blade according to claim 11, wherein the cross-sectional area of the first and the second down-conductors is between 25 mm.sup.2 and 50 mm.sup.2.

Description

BRIEF DESCRIPTION

(1) Some of the embodiments will be described in detail, with references to the following Figures, wherein like designations denote like members.

(2) FIG. 1A shows a perspective view of a conventional wind turbine of the conventional art;

(3) FIG. 1B shows a cross-sectional view of one of the blades;

(4) FIG. 2 shows a schematic representation of a longitudinal cross-sectional view of a spar cap of a wind turbine blade according to the conventional art;

(5) FIG. 3 shows a schematic representation of a longitudinal cross-sectional view of a spar cap of a wind turbine blade according to the conventional art;

(6) FIG. 4 shows a schematic representation of a longitudinal cross-sectional view of a spar cap of a wind turbine blade according to embodiments of the invention;

(7) FIG. 5 shows a schematic representation of a longitudinal cross-sectional view of a spar cap of a wind turbine blade according to embodiments of the invention;

(8) FIG. 6 shows a schematic representation of a longitudinal cross-sectional view of a spar cap of a wind turbine blade according to embodiments of the invention;

(9) FIG. 7 shows a schematic representation of a longitudinal cross-sectional view of a spar cap of a wind turbine blade according to embodiments of the invention;

(10) FIG. 8 shows in a schematic representation, an embodiment of the invention including the whole beam having two spar caps, and the complete Lightning Protection System of the embodiments of the invention;

(11) FIG. 9 shows an electric diagram representing the electric impedances involved in the electric circuit integrated in a blade according to embodiments of the invention;

(12) FIG. 10 shows an electric diagram representing the electric impedances involved in the electric circuit integrated in a blade according to embodiments of the invention;

(13) FIG. 11 shows a graph representing the linear impedance of the carbon beam material, against blade radius of a beam according to embodiments of the invention. The blade radius is the distance from the rotating point about which the blade rotates, to a particular point in the blade;

(14) FIG. 12 shows a graph representing the linear impedance of the carbon beam material, against blade radius of a beam according to embodiments of the invention. The blade radius is the distance from the rotating point about which the blade rotates, to a particular point in the blade;

(15) FIG. 13 shows an exemplary embodiment of the invention including four spar caps; and

(16) FIG. 14 shows an exemplary embodiment of the invention including four spar caps.

DETAILED DESCRIPTION

(17) FIG. 4 shows an embodiment of the invention, in particular a spar cap (7) of a wind turbine blade, wherein the spar cap (7) conventionally extends from a spar cap's root end (15) to a spar cap's tip end (14), and it is formed by a plurality of carbon plates stacked together, each carbon plate having a tapered root end and a tapered tip end.

(18) The stack (11) of carbon plates has a top plate (11a), a bottom plate (11b) and a plurality of intermediate plates (11c) stacked in between the top and bottom plates (11a,11b).

(19) The spar cap (7) is an elongated body that extends along an axis (X), wherein conventionally a blade tip region, a blade root region and a blade mid region in between the blade tip and root regions, are defined.

(20) In an embodiment, the wind turbine blade comprises a first down-conductor (12) placed alongside the tip region of the spar cap, and a first set of electric conductors (10) connecting the first down-conductor (12) to some of the tip ends of the carbon plates (11a, 11b,11c), and a second down-conductor (13) placed alongside the root region of the spar cap, and a second set of electric conductors (10) connecting the second down-conductor (13) to some of the roots ends of the carbon plates (11a, 11b,11c).

(21) As represented in FIG. 4, the first down-conductor (12) extends from the tip end (14) of the spar cap (7) towards the spar cap's mid region, and it has a length which is longer or equal than a length (L1) and which is equal or shorter than a length (L2). The length (L1) starts at the tip end (14) of the spar cap and terminates at a spar cap position or radius where the cross-sectional area in that radius of the spar cap (7) is equal or larger than 75% of the maximum cross-sectional area of the spar cap (7). The length (L2) also starts at the tip end (14) and terminates at a spar cap position or radius where the cross-sectional area is 100% of the maximum cross-sectional area of the spar cap (7) and which is closer to the blade's tip end (14).

(22) In an embodiment, the second down-conductor (13) extends from the root end (15) of the spar cap towards the spar cap's mid region, and it has as length equal or longer than (L1) and equal or shorter than a length (L2). The length (L1) starts at the root end (15) and terminates at a carbon spar cap position or radius where the cross-sectional area in that radius of the spar cap is equal or larger than 75% of the maximum cross-sectional area of the spar cap (7). The length (L2) also starts at the root end (15) and terminates at the carbon spar cap position or radius, where the cross-sectional area is 100% of the maximum cross-sectional area of the spar cap, and which is closer to the root end (15).

(23) The first and second down-conductors (12,13) are made of cooper having a 50 mm.sup.2 cross-sectional area. With the above-described range of length of the first and second down-conductor (12,13), the electrical impedance of a region of the spar cap for which no down-conductor is provided, must be lower than the impedance of a 50 mm.sup.2 copper conductor, which is the impedance of the first and second down-conductors (12,13).

(24) The first and second down-conductors (12,13) are straight conductors that are arranged parallel to the axis (X), and are electrically connected respectively to all or some of the tip ends of the carbon plates (11a,11b, 11c) by the first set of conductors (10), and to all or some of the root ends of the carbon plates (11a,11b,11c) by the second set of conductors (10).

(25) In an embodiment in view of FIG. 4, is that first down-conductor (12) extends from the spar cap's tip end (14) towards the spar cap's mid region, and terminates at a first down-conductor's end (12a) located adjacent or within a first region (R1) of the spar cap (7). This first region (R1) is a region of the spar cap that extends between a first plane (P1) and a second plane (P2), wherein the first plane (P1) is a plane orthogonal to the axis (X) at which the cross-sectional area of the spar cap (7) at this first plane (P1) is equal or higher than 75% of the maximum cross-sectional area of the spar cap and which is the one closest to the spar cap's tip end (14). The second plane (P2) is a plane orthogonal to the axis (X), and at which the cross-sectional area of the spar cap at this second plane (P2) is 100% of the cross-sectional area of the spar cap, and which area is closest to the spar cap's tip end (14).

(26) Similarly, the second down-conductor (13) extends from the spar cap's root end (15) towards the spar cap's mid region and terminates at a second down-conductor's end (13a) located adjacent or within a second region (R2) of the spar cap (7). This second region (R2) is a region of the spar cap that extends between a third plane (P3) and a fourth plane (P4), wherein the third plane (P3) is orthogonal to the axis (X) at which the cross-sectional area of the spar cap (7) at this third plane (P3) is equal or higher than 75% of the maximum cross-sectional area of the spar cap and which is the one closest to the spar cap's root end (15). The fourth plane (P4) is a plane orthogonal to the axis (X), and at which the cross-sectional area of the par cap at this fourth plane (P4) is 100% of the cross-sectional area of the spar cap and which is the one closest to the spar cap's root end (15).

(27) In an embodiment shown in FIG. 5, the first down-conductor (12) extends from the spar cap's tip end (14) to a plane (P5) orthogonal to the spar cap's axis (X), which passes through the end of the top carbon plate (11a) which is closest to the spar cap's tip end (14).

(28) In an embodiment, the second down-conductor (13) extends from the spar cap's root end (15) to a plane (P6) orthogonal to the spar cap's axis (X), which passes through the end of the top carbon plate (11a) which is closest to the spar cap's root end (15).

(29) In the embodiment of FIG. 5, all the carbon plates (11a,11b,11c) have their tip end connected to the first down-conductor (12), and their root end connected to the second down conductor (13), respectively by first and second sets (10,10) of electric conductors.

(30) There is no down conductor at a mid-region of the spar cap (7) between planes (P5, P6).

(31) In the alternative embodiment of FIG. 6, at least the top carbon plate (11a), and optionally one or more of the intermediate plates (11c), are not connected by a conductor to the first or to the second down-conductors (12,13). In this embodiment, the length of the first and the second down-conductors (12,13), comply with the definition given above in relation to FIG. 4.

(32) FIG. 8 shows an embodiment of the invention applied to a full blade, that is, having one carbon beam comprising a pressure spar cap and a suction spar cap. In this particular embodiment comprising two spar caps, namely a first spar cap (7) and a second spar cap (7), each spar cap constructed as shown in any of the FIGS. 4, 5 and 6 and as described above in relation to any of those figures or any combination thereof. In the particular embodiment of FIG. 8, the first spar cap (7) is constructed as shown in FIG. 5 and as described above in relation to FIG. 5, and the second spar cap (7) is constructed as shown in FIG. 6 and as described above in relation to FIG. 6.

(33) The embodiment of FIG. 8 includes a lightning receptor (16) installed nearby the blade tip from the beam tip end, and a root terminal (17) installed nearby the blade root from the beam root end. The two down-conductors (12,12) of the tip region of the spar caps (7,7) are connected at one end to the lightning receptor (16) by additional metallic conductors (19,19), and the two down-conductors (13,13) of the root region of the spar caps (7,7) are connected at one end to the root terminal (17) by additional metallic conductors (20,20), as shown in FIG. 8. A lightning strike would penetrate through the lightning receptor (16), and would circulate through the down-conductors, mid region of the spar caps (7,7), and through the root terminal (17).

(34) FIG. 7, in combination with Tables 1 and 2 below, provide some figures on the dimensions in which the cross-sectional area of the spar cap reaches 75%, and 100% from the tip and from the root, as defined above.

(35) TABLE-US-00001 TABLE 1 Cross-section respect maximum carbon spar cap Radius: cross-section [%] R0 & R6 0% R1 85% R2 100% R3 100% R4 85% R5 28.5%

(36) TABLE-US-00002 TABLE 2 Radius: Length [m] Percentage of the carbon spar cap length [%] R0-R1 3-10 5-10% R0-R2 10-15 10-15% R2-R3 30-60 50-60% R6-R5 2-6 3-7% R6-R4 15-30 25-35% R6-R3 20-40 35-50%

(37) As an example, and in order to describe the effect of parallel impedances using different materials and cross-sections, it may be supposed that a metallic main down-conductor has a cross-section of 50 mm.sup.2, and the carbon plates as described above, specially at tip region have a total cross-section of about 1000 mm.sup.2 multiplied by the number of carbon plates. As the resistivities of both materials are approximately: Cu: 1.66E-08 Ohm.Math.m, and Carbon: 2.30E-05 Ohm.Math.m, it leads to a resistance (R) per meter in each case for a 50 mm.sup.2 Copper cable and 1000 mm.sup.2 carbon plate of about:

(38) TABLE-US-00003 R Cu 0.000333 Ohm/m R Carbon 0.02300 Ohm/m

(39) This means that 69 carbon plates in parallel are needed to get the same voltage drop per meter or the same resistance per meter, than for a copper conductor. The explanation above applies to low frequencies. In high frequencies this ratio is reduced because of skin effect affecting more the metallic conductor because its geometry (smaller cross-section). For first positive short stroke at 25 kHz, this ratio is reduced at around 15, meaning that a cross-section of 15 carbon plates would have same resistance per meter of a 50 mm.sup.2 copper cable. In an embodiment of the invention, 15 carbon plates are accumulated far from the tip region, so, a down-conductor is needed a certain length from the start of the carbon spar cap at the tip, whereas at the root the increase on number of carbon plates is faster (larger spar cap slope).

(40) In wind turbine blades a copper lightning conductor is always used as main down-conductor. A 50 mm.sup.2 cable is commonly used in all blades, either fiberglass or carbon blades. The impedance is an electrical parameter which depends on the frequency. Basically, in lightning frequencies (up to 1 MHZ) the impedance is mainly affected by the contribution of the resistance and the self-inductance of the conductors.

(41) As shown in FIG. 9, in a carbon blade with two carbon spar cap, there are in general three impedances in parallel; one of the metallic cable and two of the carbon spar caps (pressure and suction caps), wherein Z1 and Z3 are the impedances of the carbon spar caps, and Z2 is the impedance of the metallic cable which is used as main down-conductor.

(42) These three impedances Z1, Z2 and Z3 may be split into multiple impedances because Z1 and Z3 are not constant along the spar cap axis (X) whereas Z2 is constant (cable cross-section is constant). Therefore, in a general case, the three branches of the circuit of FIG. 9 can be discretized as shown in FIG. 10.

(43) In FIG. 10, Z2 is a constant impedance [/m], while the different longitudinal segments of impedances Z1 and Z3 change along the blade. Therefore, in general for standard carbon blades, it leads to the condition shown in FIG. 11 of the impedance for a reference frequency of 25 kHz.

(44) In the graph of FIG. 11, at blade mid-span regions, as soon as the cross-section of the blade spar caps is increased, the linear impedance of the carbon beam is lower than the one of the down-conductor, which means that most of the lightning current flows through the carbon beam, and the down-conductor may be removed at the mid-span region, in particular at a region between X1 and X2.

(45) The scenario for frequencies higher than 25 kHz is shown in FIG. 12.

(46) The graphs of FIGS. 11 and 12 demonstrate that even as a single conductor carbon fibers are worst conductors of electrical currents than copper conductors, when having much higher cross-sectional area, and taking into account the reduced self-inductance of the spar caps respect to copper cables used in blades, the total linear impedance of the spar caps is lower than the one for the copper cables. It should be emphasized that this is feasible due to the high frequency nature of lightning strikes, and that low frequency lightning events are not compromising the circuit as the values of lightning currents at low frequencies, are much lower than at 25 kHz (values of 2 kA are maximum for low frequencies, which produce a lower voltage drop and Joule heating lower than the maximum 200 kA with 10 MJ/ at 25 kHz).

(47) It has been described above that the linear impedance of the carbon spar cap is lower in mid-span regions, so it happens physically when the cross-section of each spar cap is higher than 75% of its maximum cross-section. In this scenario, it may be defined that the metallic cable to inject the lightning current into the carbon spar cap may have a length L1 and L2 being L1 the length in which the carbon spar cap has a cross-section of 75% of the maximum spar cap cross-section and L1 a value of 100%, or have a length L1 and L2 being L1 the length in which the carbon spar cap has a cross-section of 75% of the maximum spar cap cross-section and L1 a value of 100%, as defined above in relation to FIG. 4.

(48) The embodiment of FIG. 4 includes only one main spar cap (7) which may comprise several parallel stacks or just a single stack of carbon plates. However, other embodiments may include a second parallel carbon spar cap with different length and starting and ending radius than the main spar cap. This is for example when using a rear cap, in some blades, in which a shorter cap is needed for structural reasons at the trailing edge of the blade's shell.

(49) FIG. 13 shows an embodiment having two main spar caps (7,7) and two secondary spar caps (7a,7a) shorter than the main spar caps and parallel to them. In this embodiment, the distance between the tip end of a secondary beam (7a,7a) to the tip end of the main beam (7,7) is equal or longer than the distance (L1) defined above in relation with FIG. 4.

(50) FIG. 14 shows another embodiment also having two main spar caps (7,7) and two secondary spar caps (7a,7a) shorter than the main spar caps and parallel to them. In this embodiment, the distance between the root end of the secondary beams (7a,7a) to the root end of the main beam (7,7) is shorter than the distance (L1) defined above in relation with FIG. 4.

(51) Although the present invention has been disclosed in the form of embodiments and variations thereon, it will be understood that numerous additional modifications and variations could be made thereto without departing from the scope of the invention.

(52) For the sake of clarity, it is to be understood that the use of a or an throughout this application does not exclude a plurality, and comprising does not exclude other steps or elements.