Wind turbine and device for protecting from lightning

Abstract

A device for protecting from lightning (30) is intended to form at least a portion of an external surface of a structure to be protected and comprises a ground plane (32), a dielectric substrate (34) arranged on the ground plane, and an array of first metal elements (36) arranged on the dielectric substrate (34) and extending substantially parallel to the ground plane (32) in such a way that any pair of consecutive elements from said first metal elements (36) is separated by a distance comprised between 0.01 millimetres and 10 millimetres, said first metal elements being distributed in juxtaposed similar patterns, each of said patterns including first metal elements of different dimensions corresponding respectively to different electromagnetic resonant frequencies the juxtaposition of which defines an electromagnetic absorption band of the pattern.

Claims

1. A wind turbine comprising: a rotor hub; at least one blade supported by the rotor hub; and an earth connection device through which lightning can be carried to the earth, wherein the blade comprises an aerodynamic external skin, wherein said aerodynamic external skin integrates at least one lightning protection device, and wherein said lightning protection device comprises; a ground plane located on an inner side of the blade, a dielectric substrate arranged on the ground plane, and set of first metal elements arranged on the dielectric substrate and located on an outer side of the blade, wherein the set of first metal elements extends substantially parallel to the ground plane in such a way that any pair of consecutive elements of said set of first metal elements is separated by a distance of between 0.01 millimeters and 10 millimeters, said first metal elements being distributed in juxtaposed similar patterns, each of said patterns including first metal elements with different dimensions corresponding to different electromagnetic resonant frequencies, the juxtaposition of which defines an electromagnetic absorption band of the pattern, and wherein first metal elements of said set of first metal elements located at one end of the lightning protection device facing the rotor hub are electrically connected to the earth connection device, and said lighting protection device further comprising a metal grid formed from interlacing of metal strips formed on the dielectric substrate between first metal elements of said set of first metal elements.

2. The wind turbine according to claim 1, in which every pair of consecutive elements among said first metal elements of a same pattern is separated by a distance between 0.3 millimeters and 3 millimeters.

3. The wind turbine according to claim 1, in which said metal strips extend between said patterns.

4. The wind turbine according to claim 1, in which the ground plane is formed from a continuous metal grating.

5. The wind turbine according to claim 1, in which the ground plane is formed from a set of grating portions at a uniform spacing from each other.

6. The wind turbine according to claim 1, in which the ground plane is formed from a plurality of second metal elements at equal spacing from each other.

7. The wind turbine according to claim 1, wherein the metal grid is connected to the earth connection device.

8. The wind turbine according to claim 4, wherein the metal grating forming the ground plane is connected to the earth connection device.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) The invention will be better understood and other details, advantages and characteristics will become clear after reading the following description given as a non-limitative example with reference to the appended drawings among which:

(2) FIG. 1 is a diagrammatic view of a wind turbine according to a preferred embodiment of the invention;

(3) FIG. 2 is a diagrammatic cross-sectional view of a blade of the wind turbine shown in FIG. 1;

(4) FIG. 3 is a diagrammatic perspective view of the blade shown in FIG. 2;

(5) FIG. 4 is a partial diagrammatic sectional view of a lightning protection device integrated into the external skin of the blade in FIG. 2;

(6) FIG. 5 is a partial diagrammatic top view of a ground plane belonging to the device in FIG. 4;

(7) FIGS. 6 and 7 are views similar to FIG. 5 illustrating variants of the ground plane;

(8) FIG. 8 is a partial diagrammatic top view of the device in FIG. 4;

(9) FIG. 9 is a diagrammatic view of an aircraft according to a preferred embodiment of the invention;

(10) In all these figures, identical references can designate identical or similar elements.

DETAILED PRESENTATION OF PREFERRED EMBODIMENTS

(11) FIG. 1 illustrates a wind turbine 10 generally comprising a pole 12, a nacelle 14 supported by the pole and housing a rotor 16 supporting blades 18 and mounted free to rotate about a rotor axis 19. Each blade 18 comprises a base, for example cylindrical in shape, connected to the rotor hub 16, and prolonging a slender aerodynamic profile, in a well-known manner.

(12) FIGS. 2 and 3 illustrate the general outlines of a blade 18 of a wind turbine 10, in cross-sectional and perspective views respectively. The blade 18 is generally in the form of a structural member 20 and an aerodynamic external skin 22 fixed to the structural member 20 (FIG. 2). Obviously, the structural member 20 can be made as a single piece or can be formed from several sections assembled end to end. Furthermore, the invention is not limited to a blade comprising a single structural member. Thus, the blade 18 may include several, for example two, parallel structural members.

(13) The outer skin 22 of the blade includes a lightning protection device 30, formed from a stack that can be seen on FIG. 4, including a ground plane 32, a dielectric substrate 34 placed on the ground plane 32, and a set of first metal elements 36 and a metal grid 38 placed on the dielectric substrate. The ground plane 32 is located at the inner side of the blade 22 while all the first metal elements 36 are located at the outer side of the blade.

(14) In the example illustrated, the ground plane 32 is in the form of a grating made from a metal material such as copper, and extending continuously in a known manner as shown on FIG. 5. The dimension of the meshes of this grating are preferably less than 3 mm. The fact that the ground plane 32 is this fine makes reflection of electromagnetic radiation with a frequency of less than about 10 GHz possible.

(15) As a variant, the ground plane 32 may be formed from a sheet of expanded metal.

(16) The surface density of the grating or expanded metal sheet forming the ground plane 32 may for example be about 80 g/m.sup.2.

(17) In the example illustrated on FIG. 5, the ground plane 32 is continuous.

(18) As a variant, this ground plane may be discontinuous. In this case, the ground plane 32 may be formed from a set of grating portions 32A, for example square or rectangular in shape, at a uniform spacing from each other, as shown on FIG. 6.

(19) In another variant, the discontinuous ground plane may be formed from a plurality of second metal elements 32B, for example square or rectangular in shape, at uniform spacing, as shown on FIG. 7.

(20) If the ground plane is discontinuous, the ground plane preferably has a shape complementary to the shape of the metal grid 38, in other words the shape of each of the grating portions 32A or each of the second metal elements 32B corresponds to the space delimited by a mesh of the metal grid 38.

(21) As another variant, the ground plane may be composed of a layer of composite Carbon Fibre Reinforced Plastic (CFRP) material. The lightning protection device can thus may good use of the electrical conducting properties of carbon fibres possibly included in the outer skin 22 of the turbine blade, particularly when the wind turbine considered includes large blades, in other words more than 60 metres long.

(22) In all cases, the ground plane is provided with a structure in which openings are formed to allow resin to diffuse through the structure, which is advantageous for fabrication of the protection device 30 and the part on which this device is located, as will become clearer from the following description.

(23) Furthermore, the dielectric substrate 34 may for example be composed of a layer of composite glass fibre reinforced plastic (GFRP) material, for example with a thickness equal to about 1 mm. For example, the matrix of the composite material may be composed of epoxy resin.

(24) Moreover, the external skin 22 of the blade preferably comprises a relatively thick layer of composite material 40, for example glass fibre or carbon fibre reinforced plastic on which the lighting protection layer 30 is placed.

(25) Finally, the lightning protection device 30 is advantageously covered with a protective coating such as a coat of paint 42, for example with a thickness of about 300 m. This paint coat is preferably provided with openings (not shown on FIG. 3) leaving some of the first metal elements 36 exposed so as to improve lighting attachment on these metal elements.

(26) For example, the first metal elements 36 are made of copper and for example they are in the form of relatively thin platelets, with a thickness preferably equal to between 15 m and 70 m, and for example equal to 35 m. Each metal element 36 may have an arbitrary shape, for example polygonal or circular, and is preferably rectangular or square.

(27) As shown in FIG. 7, the first metal elements 36 are arranged in the form of similar approximately square patterns 44, each pattern extending in the space corresponding to a mesh of the metal grid 38 and being centred in said space. In other words, the metal grid 38 is formed by interlacing of metal tracks 46 and 48 arranged on the dielectric substrate and routed between the patterns 44 formed by the first metal elements 36. For example, the width of each of the metal tracks 46 and 48 may be about 1 mm.

(28) Each metal element 36 is at a spacing from each of its neighbours equal to a distance of between 0.01 mm and 10 mm, as will become clearer in the following. This distance appeared to be optimal for lightning to slip from one of the first metal elements 36 to the next. Lightning can thus be transferred as far as an appropriate receptor device, without damaging the external skin 22 of the blade.

(29) In the example illustrated on the figures, the metal grid 38 is electrically connected to an earth connection device integrated into the rotor hub 16 and to the wind turbine pole 12 (this earth connection device not being visible on the figures). For example, the metal grill 38 may be connected to the earth connection device by a down cable 49 located in the base of the blade (FIG. 3).

(30) Furthermore, first metal elements 36 located at one end of the blade lightning protection device 30 facing the rotor hub 16 are also electrically connected to the earth connection device. The earth connection device thus forms the above-mentioned receptor device through which lightning can be carried to the earth.

(31) Preferably, the ground plane 32 is also connected to the earth connection device, for example through the down cable 49.

(32) Thus, when lightning strikes the protection device 30, several electric current passage channels can be used, firstly within the metal grid 38 and secondly from one metal element 36 to the next among the first metal elements, as far as the earth connection device. Instead of penetrating into the outer skin 22 of the blade, lightning slides on the protection device 30 until it reaches the earth connection device. The risk of damage to the outer skin 22 is thus reduced. Furthermore, the protection device 30 does not include any electrical conducting element inside the blade, which prevents risks of electric arcs as with wind turbine blades of prior art.

(33) Furthermore, due to its structure, the lightning protection device 30 provides an effect by which electromagnetic waves are absorbed in a determined frequency band.

(34) Each metal element 36 acts like a passive polar antenna.

(35) Thus, a metal element with a rectangular shape has an electromagnetic resonant frequency f.sub.r that, as a first order approximation, is approximately equal to:

(36) $f_r=\frac{c_0}{2\sqrt{L^2+W^2}\sqrt{{}_r{\mathrm{.Math.}}_r}}$

(37) in which: f.sub.r is the zero order resonant frequency of the metal element 36, c.sub.0 is the speed of light in vacuum, L is the length of the metal element 36, W is the width of the metal element 36, .sub.r is the relative permeability of the dielectric substrate 34, .sub.r is the relative permittivity of the dielectric substrate 34.

(38) According to one principle of the invention, each of the patterns 44 formed by the first metal elements 36 comprises first metal elements with different dimensions each corresponding to a different electromagnetic resonant frequency. The set of these resonant frequencies defines of widened electromagnetic absorption band of the pattern.

(39) In the particularly efficient example illustrated on FIG. 8, each pattern 44 is generally square and is composed of four elementary sub-patterns 50 distributed uniformly around a centre C of the pattern 44, such that the pattern 44 is symmetric about said centre. Each elementary sub-pattern 50 is thus similar to the other elementary sub-patterns and is the result of a 90 rotation of each of the two elementary sub-patterns adjacent to it within the pattern 44.

(40) In each pattern 44, one of the elementary sub-patterns 50 comprises seven metal elements arranged as follows, with reference to the X and Y directions in FIG. 8: a first metal element 36a, with a square shape, located in the corner of the elementary sub-pattern close to the centre of the pattern 44, the side length of which is equal to 5.25 mm; a second metal element 36b, with a rectangular shape, extending adjacent to the first metal element 36a towards increasing X dimensions, at a spacing from the first element equal to 0.6 mm along the X direction, with an extent 10.55 mm along the X direction and 5.25 mm along the Y direction; a third metal element 36c, with a rectangular shape, extending adjacent to the first metal element 36a towards increasing Y dimensions, at a spacing from the first element equal to 0.6 mm along the Y direction, with an extent 5.25 mm along the X direction and 10.55 mm along the Y direction; a fourth metal element 36d, with a square shape extending adjacent to the second metal element 36b towards increasing Y dimensions, at a spacing from the second metal element equal to 0.6 mm along the Y direction, and extending adjacent to the third metal element 36c towards increasing X dimensions, at a spacing from the third metal element equal to 0.6 mm along the X direction, the side length of which is equal to 10.55 mm; a fifth metal element 36e, with a rectangular shape, extending adjacent to the second metal element 36b and to the fourth metal element 36d towards increasing X dimensions, at a spacing from these elements equal to 2.4 mm along the X direction, with an extent 10.60 mm along the X direction and 15.83 mm along the Y direction; a sixth metal element 36f, with a rectangular shape, extending adjacent to the third metal element 36c and to the fourth metal element 36d towards increasing Y dimensions, at a spacing from these elements equal to 2.4 mm along the Y direction, with an extent 15.83 mm along the X direction and 10.60 mm along the Y direction; a seventh metal element 36g, with a square shape extending adjacent to the fifth metal element 36e towards increasing Y dimensions, at a spacing from the fifth metal element equal to 2.4 mm along the Y direction, and extending adjacent to the sixth metal element 36f towards increasing X dimensions, at a spacing from the sixth metal element equal to 2.4 mm along the X direction, the side length of which is equal to 10.60 mm;

(41) Furthermore, the fourth metal element 36d and the seventh metal element 36g are at a spacing from the closest track 48 forming part of the metal grid 38 and parallel to the Y direction by a distance equal to 2.4 mm. Similarly, the sixth metal element 36f and the seventh metal element 36g are at a spacing from the closest track 46 forming part of the metal grid 38 and parallel to the X direction by a distance equal to 2.4 mm.

(42) The other three elementary sub-patterns 50 of the pattern 44 are deduced from the elementary sub-pattern described above by successive 90 rotations in the anti-clockwise direction.

(43) The first metal elements 36a, 36b and 36e of each elementary sub-pattern are separated from the first adjacent metal elements 36a, 36d and 36f of another elementary sub-pattern by a distance equal to 0.6 mm.

(44) The layout of the first metal elements 36 described above can for example result in an attenuation of more than 20 dB in the electromagnetic waves in a frequency band centred on a frequency of about 5.7 GHz and with a width of about 1 GHz.

(45) The wind turbine blade 18 can be made using a method including steps consisting of: successively stacking fibres of the dielectric substrate 34, the ground plane 32, and fibres of the composite material layer 40, on the set of first metal elements 36 and the metal grid 38, and then infuse the resin through the assembly thus formed, and then polymerise the resin so as to solidify the assembly, then apply finish coats (typically paint) on the assembly thus formed.

(46) The perforated nature of the ground plane thus contributes to making the protection device 32 jointly with the layer of composite material 40 on which the device is placed, in a particularly simple manner.

(47) FIG. 9 illustrates an aircraft 60 for which the outside skin of the fuselage and the wing is covered with a lightning protection device 61 similar to the device mentioned above. In particular, this device extends from the aircraft nose 62 to the tips 64 of the wings and to the aft tip 66 of the aircraft. These zones form preferred entry and exit points for lightning. In the same way as described above for the wind turbine 10, the ground plane 32 is located inside the aircraft 60 while all the first metal elements 36 are located on the outside of the aircraft 60.

(48) The lightning protection device 61 enables lightning 68 to slide on the first metal elements of the device from one element to the next, from a preferred entry point such as the nose 62 of the aircraft to a preferred exit point such as the aft tip 66 of the aircraft, without damaging the structure of the aircraft, while reducing the RADAR signature of the aircraft.