Patent Application
20130224023
The present invention relates to absorption and shielding of electromagnetic waves. More particularly, the present invention relates to an electromagnetic wave absorber which exhibits a broad absorption bandwidth and has a thin support layer necessary for matching thereof, while retaining the advantage of a Salisbury screen-type absorber in terms of fabrication and structure, and to a method for fabricating the same.
Also, the present invention is concerned with a wind turbine blade having an electromagnetic wave absorption function, and a method for the fabrication thereof, wherein the wind turbine blade having an electromagnetic wave absorption function comprises an electromagnetic wave absorber the dielectric support layer of which employs a part of a composite for a turbine blade.
With the development of various electromagnetic devices operating in a high-frequency band, the wireless communication market has rapidly been expanded in recent years.
Accordingly, there has been much study on the shielding and absorption of electromagnetic waves in order to increase compatibility of electromagnetic devices and reliability of wireless communication in the environment of electromagnetic magnetic pollution.
Electromagnetic wave shielding is the practice of reducing an electromagnetic field in a space across a barrier by reflecting or absorbing electromagnetic waves incident on the barrier, while electromagnetic wave absorption refers to reduction in intensity of electromagnetic waves both reflected by and transmitted through an absorber by transforming the energy of incident electromagnetic waves into thermal energy.
In contrast to electromagnetic shielding, electromagnetic wave absorption does not produce secondary electromagnetic pollution ascribed to reflected electromagnetic waves, and thus may be said to be an advanced technology.
Generally adapted to be added to a preexisting structure, an electromagnetic wave absorber should be thin, low in specific gravity, and wide in absorption bandwidth.
Referring to
As shown in the graph of
The most widely used absorption bandwidth is a −10 dB bandwidth, which means the absorption of 90% of electromagnetic waves as thermal energy.
Resonant electromagnetic wave absorbers are structurally divided into a Dallenbach layer and a Salisbury screen.
With reference to
On the whole, a Dallenbach absorber has an absorption layer as thick as several millimeters which may require a large quantity of materials when it is used over a large area, and the single or composite lossy materials used in the absorption layer are poor in mechanical and chemical properties. Thus, the conventional absorption layer suffers from the disadvantage of increasing the weight of the structure and being vulnerable to mechanical and chemical environments.
The matching thickness (d) of the Dallenbach absorber may be accounted for by the complex permittivity (∈=∈′−j∈″) and complex permeability (μ=μ′−jμ″) of the absorption layer, and can be represented by the following Math Formula 1:
wherein λ is a wavelength of the electromagnetic wave in air, and
is a wavelength of the electromagnetic wave within the absorption layer.
represents a thickness (d) necessary for the electromagnetic wave incident from the air to the absorption layer to show a phase difference of π/2 for the time during which the incident electromagnetic wave propagates to the back layer and is then reflected toward the border between the air and the absorption layer.
When electromagnetic waves are transmitted or reflected at a border between air and an absorption layer, an additional phase difference (θ) occurs due to combinations between the real part (∈′) and the imaginary part (∈″) in the complex permittivity, and between the real part (μ′) and imaginary part (μ″) in the complex permeability.
This phase difference (θ) makes the matching thickness (d) of the Dallenbach absorber smaller than
With reference to
Compared to the Dallenbach layer-type absorber, the Salisbury screen-type absorber is structurally simpler and easier to fabricate.
The matching thickness (d) of the Salisbury screen-type absorber can be accounted for by the dielectric constant (∈) of the dielectric substance, and is represented by the following Math Formula 2:
wherein λ is a wavelength of the electromagnetic wave in air, and
is a wavelength of the electromagnetic was within the absorption layer.
That is, the absorption bandwidth of a Salisbury screen-type absorber is proportional to the thickness of the support layer defined in Math Formula 2.
Referring to
When a glass fiber-reinforced composite (with an absolute value of dielectric constant |∈|=4.7) is used as a material for the support layer, the thickness of the support layer amounts to about 3.47 mm, having a bandwidth of 3.60 GHz.
When used, E-Glass with a dielectric constant of about 6.0 must be fabricated into an absorption layer about 3.06 mm thick with a bandwidth of 3.28 GHz.
As a rule, a Salisbury screen-type absorber is thicker than a Dallenbach layer-type absorber since the dielectric constant (∈) of its absorption layer is smaller than the complex permittivity (∈) and complex permeability (μ) of the absorption layer of the Dallenbach layer-type absorber.
Further, the Salisbury screen-type absorber is narrower in absorption bandwidth per unit thickness than the Dallenbach layer-type absorber.
It is an object of the present invention to provide an electromagnetic wave absorber, comprising a conductive powder-dispersed composite sheet layer having complex permittivity with controlled real and imaginary parts, and a dielectric support layer which is reduced in matching thickness and exhibits a broad absorption bandwidth, and a method for fabricating the same.
It is another object of the present invention to provide a wind turbine blade having an electromagnetic wave absorption function, in which a dielectric material used in a wind turbine blade is employed as a support layer for an electromagnetic wave absorber to allow the avoidance of radar interference.
In accordance with an aspect thereof, the present invention provides an electromagnetic wave absorber, comprising a support layer for providing a resonant space of electromagnetic waves, a highly conductive backing layer assigned to a back surface of the dielectric support layer, and a dielectric lossy composite sheet layer formed on a front surface of the dielectric support layer, said dielectric lossy composite sheet layer having such a dielectric permittivity so as to generate a resonant peak with the electromagnetic waves reflected from the highly conductive backing layer.
According to one embodiment of the electromagnetic wave absorber, the dielectric lossy composite sheet layer comprises a polymer matrix with a conductive powder dispersed therein, and exhibits complex permittivity.
In this regard, the complex permittivity may vary depending on a factor selected from the group consisting of content, morphology, inherent electrical conductivity, and surface condition of the dispersed conductive powder.
In another embodiment of the electromagnetic wave absorber, the complex permittivity may vary depending on a thickness of the composite sheet layer.
In a further embodiment of the electromagnetic wave absorber, the complex permittivity may vary depending on a center frequency of the absorber, and a thickness of the support layer.
In still another embodiment of the electromagnetic wave absorber, the complex permittivity has a real part of greater than 1.
In a still further embodiment of the electromagnetic wave absorber, the composite sheet layer may be formed by applying an epoxy resin in which carbon black, carbon nanofibers, or carbon nanotubes are homogeneously dispersed to a glass fiber fabric.
In yet another embodiment of the electromagnetic wave absorber, the composite sheet layer may comprise a carbon nanomaterial.
In a further embodiment of the electromagnetic wave absorber, the glass fiber fabric is a plain weave fabric which has small cells and is slightly different in fiber count between fill and warp directions, and which is used as a thin PCB insulation mat.
In accordance with another aspect thereof, the present invention provides an electromagnetic wave absorber, comprising: a support layer for providing a resonant space of electromagnetic waves, a highly conductive backing layer assigned to a back surface of the dielectric support layer, and a multi-ply composite sheet layer formed on the dielectric support layer, said multi-ply composite sheet layer having such a dielectric permittivity so as to generate a resonant peak with the electromagnetic waves reflected from the highly conductive backing layer.
In one embodiment of the electromagnetic wave absorber, at least one ply of the multi-ply composite sheet layer is formed by coating a glass fiber fabric with an epoxy resin in which carbon black, carbon nanofibers, or carbon nanotubes are homogenously dispersed.
In accordance with a further aspect thereof, the present invention provides a method for fabricating an electromagnetic wave absorber, comprising providing a dielectric support layer for a resonant space of electromagnetic waves, assigning a highly conductive backing layer to a back surface of the dielectric support layer, and forming a dielectric lossy composite sheet layer on a front surface of the dielectric support layer, said dielectric lossy composite sheet layer having such a complex permittivity so as to generate a resonant peak with an electromagnetic wave reflected from the highly conductive backing layer.
In one embodiment of the method, the dielectric lossy composite sheet layer is formed in such a way that conductive powders are homogenously dispersed in a polymer matrix to endow the dielectric lossy composite sheet layer with complex permittivity.
According to another embodiment of the method, the complex permittivity may vary depending on a factor selected from the group consisting of content, morphology, inherent electrical conductivity, and a surface condition of the dispersed conductive powder.
In a further embodiment of the method, the complex permittivity may vary depending on a thickness of the composite sheet layer.
In still another embodiment of the method, the complex permittivity may vary depending on a center frequency of the absorber and a thickness of the support layer.
In a still further embodiment of the method, the thickness of the composite sheet layer may vary depending on a center frequency of the absorber and a thickness of the support layer.
According to yet another embodiment of the method, the complex permittivity consists of a real part (e′) and an imaginary part (e″), and has a value exceeding 1.
In a yet further embodiment of the method, the composite sheet layer is formed by coating a glass fiber fabric with an epoxy resin in which carbon black, carbon nanofibers, or carbon nanotubes are homogenously dispersed.
In yet another embodiment of the method, the composite sheet layer comprises a carbon nanomaterial.
In a still further embodiment of the method, the glass fiber fabric is a plain weave fabric which has small cells and is slightly different in fiber count between fill and warp directions, and which is used as a thin PCB insulation mat.
In an additional embodiment of the method, the epoxy resin is based on a bisphenol-A type resin with an aromatic amine-type curing agent plus a diluent for easy application to a fabric, and a small amount of a reaction accelerator.
In accordance with a further aspect thereof, the present invention provides a wind turbine blade, comprising a composite in a sandwich structure consisting of an internal face layer, a core, and an external face layer, an electromagnetic wave absorbing screen located below the external face layer, and a resin-permeable, highly conductive backing layer inserted into the sandwich-type composite, functioning to reflect electromagnetic waves.
According to one embodiment of the wind turbine blade, the electromagnetic wave absorbing screen is formed by coating a glass fiber fabric including an epoxy resin in which a carbon nanomaterial is homogeneously dispersed.
In another embodiment of the wind turbine blade, the carbon nanomaterial is selected from the group consisting of carbon black, carbon nanofibers, carbon nanotubes, and a combination thereof.
In a further embodiment of the wind turbine blade, the electromagnetic wave absorbing screen is selected from the group consisting of a dielectric lossy composite sheet, a resistive sheet with sheet resistance of 377 Ω/sq, and a circuit analog.
In still another embodiment of the wind turbine blade, the resin-permeable, highly conductive backing layer is formed by stacking at least one carbon fabric.
In a still further embodiment of the wind turbine blade, the resin-permeable highly conductive backing layer is inserted into the external face layer, between the external face layer and the core, or into the core.
In yet another embodiment of the wind turbine blade, the resin-permeable highly conductive backing layer is located at any position in a thickness direction within the core.
According to a yet further embodiment of the wind turbine blade, the resin-permeable, highly conductive backing layer has a permeability coefficient of 10−6˜10−14 m2 against a flow of a liquid resin in a thickness direction, as calculated according to the following Math Formula.
(U: flow rate [m/s], K: permeability coefficient of medium [m2], δp/δx: pressure gradient in thickness direction [N/m2], μ: viscosity [N·s/m2])
In still another embodiment of the wind turbine blade, the resin-permeable, highly conductive backing layer has electromagnetic wave reflectivity of 95%.
In a still further embodiment of the wind turbine blade, the composite in a sandwich structure comprises an internal face layer, an external face layer, and a core sandwiched therebetween, both said internal face layer and said external face layer being made of a glass fiber-reinforced composite, and said core being made of a non-conductive dielectric selected from the group consisting of a foam and balsa wood.
In accordance with still another aspect thereof, the present invention provides a method for fabricating a wind turbine blade having an electromagnetic wave absorbing function, comprising forming an electromagnetic wave absorbing screen by coating a glass fiber fabric with an epoxy resin in which a carbon nanomaterial is homogeneously dispersed, selecting a position at which a resin-permeable, highly conductive backing layer is to be located, constructing a composite in a sandwich structure with the resin-permeable, highly conductive backing layer located therein by laminating an internal face layer, a core, and an external face layer in that order, and layering the composite on the electromagnetic wave-absorbing screen.
In one embodiment, the method may further comprise placing the electromagnetic wave absorbing screen on a mold.
In another embodiment of the method, the selecting is carried out by inserting the resin-permeable highly conductive backing layer into the external face layer, between the external face layer and the core, or into the core.
In a further embodiment of the method, the resin-permeable highly conductive backing layer is inserted into the core at any position in a thickness direct of the core.
As described above, the electromagnetic wave absorber fabricated using the method of the present invention exhibits a broad absorption bandwidth with a relatively narrow matching thickness of the support layer while retaining the methodological and structural advantages of a conventional Salisbury screen-type absorber.
In addition, the wind turbine blade having an electromagnetic wave absorption function, fabricated using the method of the present invention, utilizes a dielectric material used in a wind turbine blade as a support layer for an electromagnetic wave absorber, thereby avoiding radar interference.
Furthermore, in the present invention, a part of a wind turbine blade is employed as a support layer for an electromagnetic wave absorber to allow the avoidance of radar interference without requiring an additional absorber, thus reducing a burden on production cost, fabrication time, and maintenance.
a to 17c are plots of the complex permittivity of dielectric lossy electromagnetic wave-absorbing screens containing carbon black, carbon nanofibers, and carbon nanotubes as conductive powders, respectively.
a to 18c are reflection loss graphs showing the absorption performance of wind turbine blades fabricated with the dielectric lossy electromagnetic wave absorbing screen.
Reference should now be made to the drawings, throughout which the same reference numerals are used to designate the same or similar components. Below, a description will be given of preferred embodiments of the present invention in conjunction with the accompanying drawings. Throughout the accompanying drawings, the same reference numerals are used to designate the same or similar components. It should be apparent to those skilled in the art that, although many specified elements such as concrete components are elucidated in the following description, they are intended to aid the general understanding of the invention and the present invention can be implemented without the specified elements. Further, in the description of the present invention, when it is determined that the detailed description of the related art would obscure the gist of the present invention, the description thereof will be omitted.
Unless the context clearly requires otherwise, throughout the description and the claims, the words “comprise,” “comprising,” and the like are to be construed in an inclusive sense as opposed to an exclusive or exhaustive sense, that is to say, in the sense of “including, but not limited to.” In addition, the words “˜ part” and “˜ unit” are intended to refer to a unit for processing at least one function or operation and can be realized by hardware, software, or a combination thereof.
In order to fully understand the operational advantages of the present invention and the objects achieved by the embodiment of the present invention, reference must be made to the accompanying drawings illustrating preferred embodiments of the present invention, and the disclosure of the drawings.
Preferred embodiments of the present invention will be explained in detail in conjunction with the accompanying drawings, in which the same reference numerals are used throughout the different drawings to designate the same or similar components.
With reference to
As can be seen in the cross-sectional view of
In the electromagnetic wave absorber, the backing layer 200 serves to provide a space for the resonance of electromagnetic waves.
The highly conductive backing layer 100 may be formed on the back surface of the support layer.
On the front surface of the support layer is assigned the composite sheet layer 300 that has such a complex permittivity so as to generate a resonant peak with an electromagnetic wave reflected from the highly conductive backing layer 100.
The composite sheet layer 300, characteristic of the present invention, is a polymer matrix with a conductive powder dispersed therein, and exhibits various levels of complex permittivity depending on various factors including the dispersed conductive powder's content, morphology, inherent electrical conductivity, and surface condition.
When it is incident on the electromagnetic wave absorber 400, an electromagnetic wave is separated into a wave (s1) transmitted into the absorber and a wave (R) reflected from the surface of the composite sheet layer 300 depending on the properties of the composite sheet layer 300 (e.g., content, morphology, inherent electrical conductivity, and surface condition of the conductive powder dispersed in the sheet layer).
For example, an electromagnetic wave, when incident on the electromagnetic wave absorber 400, is partially absorbed into the support layer 200, working as a first internal wave (s1), while the remnant wave (R) is reflected from the composite sheet layer 300, depending on the property of the composite sheet layer 300.
In addition, the first internal wave (s1) is reflected from the highly conductive backing layer 100 and is then incident on the composite sheet layer 300 to produce a second internal wave (s2), while the remnant wave (e1), which results from the subtraction of the second internal wave from the first internal wave (s1), is transmitted through the composite sheet layer 300 and dissipated into air.
The second internal wave (s2) is again reflected from the highly conductive backing layer 100 and is then incident on the composite sheet layer to produce a third internal wave (s3), while the remnant wave (e2), which results from the subtraction of the third internal wave (s3) from the second internal wave (s2), is transmitted through the composite sheet layer 300 and dissipated into air.
In this manner, an N−1th internal wave (sN−1) is reflected from the highly conductive backing layer 100 and is incident on the composite sheet layer 300 to produce an Nth internal wave (sN), while the remnant wave (eN−1), which results from the subtraction of the Nth internal wave from the N−1th wave (sN−1), is transmitted through the composite sheet layer 300 and dissipated into air.
Accordingly, total reflected wave from the electromagnetic wave absorber 400 can be represented by R−(e1+e2+e3+ . . . +eN−1) (N is a natural number). In the electromagnetic wave absorber, the matching is observed when R−(e1+e2+e3+ . . . +eN−1)=0 (=−∞ dB).
In one embodiment of the present invention, the composite sheet layer 300 may contain a carbon nanomaterial such as carbon black (CB), carbon nanotubes (CNT), or carbon nanofibers (CNF), and may exhibit various complex permittivities depending on the material (J. B. Kim and C. G. Kim, Composite Science and Technology, 70, 2010, 1748-1754). The highly conductive backing layer 100 may be in the form of a metal thin film.
As is understood from the plot of
When the glass fiber/epoxy laminate (dielectric constant: 4.659−j0.171) is applied to a conventional Salisbury screen-type absorber shown in
In consideration of the thickness (0.2 mm) of the composite sheet with a center frequency of 10 GHz, the imaginary part (∈″) of complex permittivity of 22.394 corresponds to a sheet resistance of 377 Ω/sq according to the following Math Formula 3.
R
s=1/(dsheet×σac)=1/(dsheet×2πfcenter∈0∈″) [Math Formula 3]
Rs: sheet resistance [Ω/sq]
dsheet thickness of sheet [m]
σac: alternating current electrical conductivity of sheet [S/m]
fcenter: center frequency of electromagnetic wave absorber [Hz]
∈0: absolute dielectric constant of air (8.854×10−12 F/m)
When recruited in the conventional Salisbury screen type absorber of
As can be seen in
These results indicate that the thickness and complex permittivity of the dielectric lossy composite of the present invention can be properly selected depending on the center frequency of the electromagnetic wave absorber, and the thickness and dielectric constant of the support layer.
In the present invention, test samples made of an epoxy resin with various contents of carbon black (CB), carbon nanofibers (CNF), and carbon nanotubes (MWNT) were evaluated for electromagnetic properties.
In Examples, HG-1P of LINZI HUAGUANG Chemical Ind. (China) was used as carbon black (CB), PYROGRAF III (PR-19-XT-LHT) of APPLIED SCIENCE Inc. (USA) was used as carbon nanofibers (CNF), and CM-95 of ILJIN NANOTECH Co. Ltd. (Korea) was used as carbon nanotubes (MWNT).
The composite 300 is layered on the glass fiber fabric/epoxy laminate.
In detail, the composite 300 is formed by applying an epoxy resin in which carbon black (CB), carbon nanofibers (CNF), or carbon nanotubes (MWNT) are homogenously dispersed to a glass fiber fabric.
The glass fiber fabric may be a plain weave fabric which is slightly different in fiber count between fill and warp directions, and may be, for example, an insulation mat for #110 PCB, manufactured by HANKUK Fiber, which has small cells and is thin.
The epoxy resin is based on a bisphenol-A type resin with an aromatic amine-type curing agent plus a diluent for easy application to a fabric, and a small amount of a reaction accelerator.
As for the weight of the carbon material on the basis of the total weight of the epoxy free of the diluent, it may amount to 5.19 wt % for carbon black, 2.11 wt % for carbon nanofibers, and 4.71 wt % for carbon nanotubes. The composite sheet layer has an R/C (resin content) of about 50%.
In addition, one glass fiber fabric sheet with a dimension of 100 mm in both warp and fill directions, was stacked upon another, and autoclaved for each carbon material.
The absorber 400 may be fabricated with a thermal cycle of 80° C. for 30 min and 125° C. for 90 min under a pressure of 6 Torr. After fabrication, the composite sheet layers containing carbon black (CB), carbon nanofibers (CNF), and carbon nanotubes (MWNT) were measured to be 0.250 mm, 0.275 mm, and 0.252 mm thick, respectively.
Before being applied to the fabrication of the electromagnetic wave absorber 400, the three composite sheet layers 300 were measured for complex permittivity and complex permeability. Because the carbon materials are electrically conductive, the composite sheet layer exhibits a complex permeability of 1. The complex permittivity of the composite was measured using the vector network analyzer Agilent N5230A, and a 7 mm coaxial tube.
In
b shows the complex permittivity of a dielectric lossy composite sheet layer containing carbon nanofibers (CNF) as a function of frequency.
In
In this context, the dielectric lossy composite sheet layer may contain carbon black (CB) in an amount of 5.19 wt %, carbon nanofibers (CNF) in an amount of 2.11 wt %, or carbon nanotubes (MWNT) in an amount of 4.71 wt %, respectively.
Turning to
A glass fiber/epoxy composite laminate (dielectric constant: 4.659−j0.171) was used as a support layer for electromagnetic wave absorbers recruiting one of the three composite sheet layers described above.
a is a plot of the reflection loss of the composite layer containing carbon black against frequency.
b is a plot of the reflection loss of the composite layer containing carbon nanofibers against frequency.
c is a plot of the reflection loss of the composite layer containing carbon nanotubes against frequency.
Considering the data given in
With reference to the reflection loss graph of
With reference to the reflection loss graph of
With reference to the reflection loss graph of
As can be seen in
In full consideration of the data shown in
In addition, the electromagnetic wave absorber of the present invention comprises a dielectric support layer for providing a resonant space of electromagnetic waves, a highly conductive backing layer assigned to a back surface of the dielectric support layer, and a dielectric lossy composite sheet layer formed on a front surface of the dielectric support layer, said dielectric lossy composite sheet layer having such a dielectric permittivity so as to generate a resonant peak with the electromagnetic waves reflected from the highly conductive backing layer.
If a structure has as its surface a material that reflects more than 90% of electromagnetic waves incident thereon, like a metal or a carbon fiber-reinforced composite, the surface may be used as the backing layer 100 of the electromagnetic wave absorber of the present invention. When the surface of a certain structure reflects electromagnetic waves at a rate of less than 90%, a thin metal film may be employed as a highly conductive backing layer 100 between the surface of the structure and the support layer 200.
As shown in
Therefore, the electromagnetic wave absorber of the present invention finds applications in various structures having a highly conductive surface, such as a car, an aircraft, a ship, a wireless communication device, a railroad train, a wind turbine, a mobile communication device, etc.
Further, the electromagnetic wave absorber of the present invention may be fabricated into a form which is readily attachable to a preexisting structure. For example, the electromagnetic wave absorber, when applied to a ship, may be in a rectangular form (e.g., tile form).
In the case of large vessels or aircrafts, which are typically manufactured using an assembly process, their surface designed to absorb electromagnetic waves requires an additional process in the manufacture, giving rise to an increase in production cost.
However, the electromagnetic wave absorber of the present invention allows a process for electromagnetic wave shielding or absorption, which has been incorporated into the manufacture of a structure, to be separated from the manufacture process, and can be readily applied to a ready-made structure having a highly conductive surface, thus exerting an excellent effect in terms of production cost.
The structure to which the electromagnetic wave absorber of the present invention is applied increases biocompatibility between electromagnetic devices in high-frequency bands, and enhances the reliability of wireless communication against electromagnetic wave environments.
Embodiments described above are only exemplary of the technical spirit of the present invention, and thus, those skilled in the art can make selective modifications on conditions for fabrication processes, such as temperatures, time, polymer resin, and kind and volume fraction of conductive powders (inclusive of fibers).
As shown in
The composite is a sandwich structure composed of an internal face layer 110′, a core 130′, and an external face layer 120′. In the sandwich structure, the internal face layer and the external face layer may be made of a glass fiber-reinforced composite, while the core may consist of a non-conductive dielectric, such as a foam or balsa wood.
In detail, the glass fiber-reinforced composite used for both the internal and external face layers was a 4-ply laminate of the [±45] bi-axial NCF fabric (SAERTEX GmbH & Co. of German) reinforced with SE1500 glass fibers (OWENS CORNING), while the non-conductive dielectric used as the core was AIREX PVC foam (ALCAN, USA). When a 4-ply laminate of the [±45] bi-axial NCF fabric manufactured by SAERTEX GmbH & Co. is used as each of the internal and external face layers, it may have a thickness of 2.15 mm.
The electromagnetic wave-absorbing screen 150′ is located below the external face layer 120′, and may be in a form selected from the group consisting of a dielectric lossy composite sheet, a resistive sheet with a sheet resistance of 377 Ω/sq, or a circuit analog.
An epoxy resin in which a carbon nanomaterial is homogenously dispersed may be applied to a glass fiber fabric to form the electromagnetic screen. The carbon nanomaterial may be selected from carbon black, carbon nanofibers, carbon nanotubes, and a combination thereof.
In detail, the electromagnetic wave absorbing screen of the present invention may be made of an epoxy resin with various contents of carbon black (CB), carbon nanofibers (CNF), or carbon nanotubes (MWNT), and may be evaluated for electromagnetic properties. In the present invention, HG-1P of LINZI HUAGUANG Chemical Ind. (China) was used as carbon black (CB), PYROGRAF III (PR-19-XT-LHT) of APPLIED SCIENCE Inc. (USA) was used as carbon nanofibers (CNF), and CM-95 of ILJIN NANOTECH Co. Ltd. (Korea) was used as carbon nanotubes (MWNT).
The glass fiber fabric may be a plain weave fabric which is slightly different in fiber count between fill and warp directions, and may be, for example, an insulation mat for #110 PCB, manufactured by HANKUK Fiber, which has small cells and is thin.
In addition, the epoxy resin is based on a bisphenol-A type resin with an aromatic amine type curing agent plus a diluent for easy application to a fabric, and a small amount of a reaction accelerator. The weight percentages of the carbon nanomaterials used in the resin ware 5.30 wt % for carbon black, 2.08 wt % for carbon nanofibers, and 4.78 wt % for carbon nanotubes. The weight percentages of the carbon nanomaterials were based on the total weight of the epoxy resin exclusive of the weight of the diluent. The resin content in the electromagnetic wave-absorbing screen was about 50%.
With reference to
Further, the electromagnetic wave-absorbing screens were measured for complex permittivity and complex permeability.
Because the carbon materials are electrically conductive, the electromagnetic wave-absorbing screen exhibits a complex permeability of 1. The complex permittivity of the composite was measured using the vector network analyzer Agilent N5230A, and a 7 mm coaxial tube. The results are the same as given in
The resin-permeable, highly conductive backing layer 140′ may be inserted into the composite 100′ of the sandwich structure, functioning to reflect electromagnetic waves. The resin-permeable, highly conductive backing layer 140′ can be formed of at least one carbon fiber fabric laminate.
By way of examples, the resin-permeable, highly conductive backing layer 140′ may be inserted into the external face layer 120′, between the external face layer 120′ and the core 130′, or into the core 130′. When the resin-permeable, highly conductive backing layer is inserted into the core, it may be located at a certain position in the thickness direction of the core, allowing the matching of the electromagnetic wave absorber.
A carbon fabric is a material which is widely used, together with glass fiber, for high-performance composite structures such as composite airfoil blades. In the present invention, the backing layer is made of WSN3K (FAW=195 g/m2, thickness=0.223 mm) of SK Chemicals, Korea, which is weaved on the basis of TR30 (Mitsubishi, Japan).
In this regard, an epoxy resin-permeable, 1-, 2- or 3-ply WSN3k laminate was evaluated for utility as the highly conductive backing layer by measuring its electromagnetic wave reflectance and transmittance in X-band (8.2 GHz-12.4 GHz) with an HVS Free Space Measurement System.
Given a maximal reflection loss of −0.1 dB, a carbon fiber fabric exhibits a reflectance of at least 98%. As shown in
In practice, a substance with reflectance of about 95% or higher can serve as a backing layer. Preferably, the resin-permeable backing layer has electromagnetic wave reflectance of at least 95% or higher.
Meanwhile, when a liquid resin flows through a certain medium, the flow rate of the liquid resin can be represented by the following Math Formula 4.
(U: flow rate [m/s], K: permeability coefficient of medium [m2], δp/δx: pressure gradient in thickness direction [N/m2], μ: viscosity [N·s/m2])
In this regard, the resin-permeable, highly conductive backing layer may have a permeability coefficient of 10−6˜10−14 m2 against the flow of liquid resin in the thickness direction.
a to 18c are reflection loss graphs showing the absorption performance of wind turbine blades fabricated with the dielectric lossy, electromagnetic wave absorbing screen.
The electromagnetic wave absorption performances of wind turbine blades fabricated in accordance with one embodiment of the present invention are shown in
In detail,
Below, a detailed description will be given of a method for fabricating a wind turbine blade having an electromagnetic wave absorbing function in accordance with the present invention.
With reference to
As shown in
In the forming step (S10), an epoxy resin in which a carbon nanomaterial is homogeneously dispersed is applied to a glass fiber fabric to form an electromagnetic wave absorbing screen.
The selecting step (S20) is to select a position at which a carbon fiber fabric, used as a resin-permeable, highly conductive backing layer, is located in a composite in a sandwich structure.
In the selecting step (S20), the resin-permeable, highly conductive backing layer 140 may be determined to be inserted into the external face layer, between the external face layer and the core, or into the core of the composite such that matching is achieved in the electromagnetic wave absorber.
When the resin-permeable, highly conductive backing layer is inserted into the core, any position in the thickness direction may be preferably suitable for generating the matching of the electromagnetic wave absorber.
In the constructing step (S30), an internal face layer, a core, and an external face layer are laminated, together with the resin-permeable, highly conductive backing layer, in that order to form a sandwich-type composite with the resin-permeable, highly conductive backing layer embedded therein.
Constitutional elements and structures of the rein-permeable, highly conductive backing layer, the electromagnetic wave absorbing screen, and the sandwich-type composite in the method are the same as are described in the wind turbine blade having an electromagnetic wave absorbing function, and thus a description is omitted herein.
In the layering step (S50), as shown in
The method for fabricating a wind turbine blade having an electromagnetic wave absorbing function in accordance with another embodiment of the present invention, as shown in
The placing step (S40), as shown in
As described hitherto, the present invention provides a wind turbine blade having an electromagnetic wave function, and a method for the fabrication thereof, in which a dielectric material used in a wind turbine blade is employed as a support layer for an electromagnetic wave absorber to allow the avoidance of radar interference without requiring an additional absorber, thus reducing a burden on production cost, fabrication time, and maintenance.
While the present invention has been particularly shown and described with reference to the foregoing preferred and alternative embodiments, it should be understood by those skilled in the art that various alternatives to the embodiments of the invention described herein may be employed in practicing the invention without departing from the spirit and scope of the invention as defined in the following claims. It is intended that the following claims define the scope of the invention and that the method and absorber within the scope of these claims and their equivalents be covered thereby. This description of the invention should be understood to include all novel and non-obvious combinations of elements described herein, and claims may be presented in this or a later application to any novel and non-obvious combination of these elements. The foregoing embodiments are illustrative, and no single feature or element is essential to all possible combinations that may be claimed in this or a later application.
| Number | Date | Country | Kind |
|---|---|---|---|
| 10-2010-0111425 | Nov 2010 | KR | national |
| 10-2010-0112699 | Nov 2010 | KR | national |
| 10-2011-0116597 | Nov 2011 | KR | national |
| Filing Document | Filing Date | Country | Kind | 371c Date |
|---|---|---|---|---|
| PCT/KR2011/008562 | 11/10/2011 | WO | 00 | 5/9/2013 |
