CN102856664B - Cassegrain type metamaterial antenna - Google Patents
Cassegrain type metamaterial antenna Download PDFInfo
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Abstract
The invention discloses a cassssegrain type metamaterial antenna. The antenna comprises a main metamaterial reflector with a central through-hole, a feed source which is arranged in a central through-hole and an auxiliary reflector which is arranged in front of the feed source, wherein electromagnetic waves radiated by the feed source are sequentially subjected to the reflection of the auxiliary reflector and the main metamaterial reflector and are ejected in a plane wave mode, the main metamaterial reflector comprises a core layer and a reflection layer which is arranged on rear surface of the core layer, the core layer comprises at least one core layer sheet layer, the core layer sheet layer comprises a base material and a plurality of artificial microstructures which are arranged on the base material, the auxiliary reflector is one of curved surfaces of a rotary ellipse surface, and a phase center of the feed source overlaps a far focus of the rotary ellipse surface. According to the cassssegrain type metamaterial antenna, a conventional paraboloid is replaced with the main metamaterial reflector in a sheet shape, and the antenna is easy to produce and process and low in cost.
Description
Technical field
The present invention relates to the communications field, more particularly, relate to a kind of Cassegrain metamaterial antenna.
Background technology
Cassegrain antenna is made up of three parts, i.e. main reflector, subreflector and radiation source.Wherein main reflector is the paraboloid of revolution, and subreflector is one of them curved surface of the hyperboloid of revolution.Structurally, a bi-curved focus overlaps with paraboloidal focus, and hyperboloid focal axis overlaps with paraboloidal focal axis, and radiation source is positioned in another focus bi-curved.The primary event carried out the electromagnetic wave that radiation source sends by subreflector, by reflection of electromagnetic wave on main reflector, and then obtains the plane wave wave beam of respective direction, to realize directional transmissions after main reflector reflection.
Visible, the main reflector of traditional Cassegrain antenna needs to be processed into the very high parabola of precision, but process the parabola that such precision is high, difficulty is very large, and the height that cost is suitable.
Summary of the invention
Technical problem to be solved by this invention is, for the processing of existing Cassegrain antenna not easily, defect that cost is high, provide a kind of and process Cassegrain metamaterial antenna that is simple, low cost of manufacture.
The technical solution adopted for the present invention to solve the technical problems is: provide a kind of Cassegrain metamaterial antenna, comprise the Meta Materials main reflector with center through hole, be arranged on the feed in center through hole and be arranged on the subreflector in feed front, the electromagnetic wave of feed radiation is successively through subreflector, with the form outgoing of plane wave after the reflection of Meta Materials main reflector, described Meta Materials main reflector comprises core layer and is arranged on the reflector of core layer rear surface, described core layer comprises at least one core layer, described core layer comprises base material and is arranged on the multiple man-made microstructure on base material, described subreflector is one of them curved surface of revolution ellipsoid, the phase center of described feed overlaps with the over focus of revolution ellipsoid.
Further, the vertical Meta Materials main reflector of the real axis of described revolution ellipsoid.
Further, described feed is corrugated horn, and the real axis of described revolution ellipsoid passes through the center in the bore face of corrugated horn.
Further, the refraction index profile of arbitrary core layer meets following formula:
Wherein, n (r) represents that in this core layer, radius is the refractive index value at r place, and the refraction index profile center of circle of this core layer is the real axis of revolution ellipsoid and the intersection point of this core layer;
S is the distance of perifocus to the front surface of Meta Materials main reflector of described revolution ellipsoid;
D is the thickness of core layer;
N
maxrepresent the refractive index maximum in core layer;
N
minrepresent the refractive index minimum value in core layer;
λ represents the electromagnetic wavelength that center of antenna frequency is corresponding;
Floor represents downward round numbers.
Further, described base material comprises prebasal plate and the metacoxal plate of sheet, described multiple man-made microstructure is folded between prebasal plate and metacoxal plate, the thickness of described core layer is 0.21-2.5mm, wherein, the thickness of prebasal plate is 0.1-1mm, and the thickness of metacoxal plate is 0.1-1mm, and the thickness of multiple man-made microstructure is 0.01-0.5mm.
Further, the thickness of described core layer is 0.818mm, and wherein, the thickness of prebasal plate and metacoxal plate is 0.4mm, and the thickness of multiple man-made microstructure is 0.018mm.
Further, described man-made microstructure is metal micro structure, described metal micro structure is made up of one or more metal wire, described metal wire is copper cash, silver-colored line or aluminum steel, the multiple man-made microstructure on described base material by etching, plating, bore quarters, photoetching, electronics carve or ion quarter method obtain.
Further, multiple man-made microstructure on described base material obtain by the differentiation of the topological pattern in the alabastrine metal micro structure of plane, described have the first metal wire and the second metal wire mutually vertically divided equally in the alabastrine metal micro structure of plane, described first metal wire is identical with the length of the second metal wire, described first metal wire two ends are connected with two the first metal branch of equal length, described first metal wire two ends are connected on the mid point of two the first metal branch, described second metal wire two ends are connected with two the second metal branch of equal length, described second metal wire two ends are connected on the mid point of two the second metal branch, described first metal branch is equal with the length of the second metal branch.
Further, described is that each first metal branch of the alabastrine metal micro structure of plane and the two ends of each second metal branch are also connected with identical 3rd metal branch, and the mid point of corresponding 3rd metal branch is connected with the end points of the first metal branch and the second metal branch respectively.
Further, described the first metal wire in the alabastrine metal micro structure of plane is provided with two kinks with the second metal wire, and described is that the alabastrine metal micro structure of plane all overlaps with former figure to the figure of any direction 90-degree rotation with the intersection point of the second metal wire around the first metal wire in plane residing for metal micro structure.
According to Cassegrain metamaterial antenna of the present invention, be instead of the main reflector of traditional parabola form by the Meta Materials main reflector of tabular, manufacture processing and be more prone to, cost is cheaper.This Cassegrain metamaterial antenna, according to the difference of institute's selected frequency, can be applicable to the fields such as satellite antenna, microwave antenna and radar antenna.
Accompanying drawing explanation
Fig. 1 is the structural representation of Cassegrain metamaterial antenna of the present invention;
Fig. 2 is the perspective diagram of the metamaterial unit of a kind of form of the present invention;
Fig. 3 is the refraction index profile schematic diagram of the core layer of a kind of form of the present invention;
Fig. 4 is the structural representation of the core layer of a kind of form of the present invention;
Fig. 5 is the schematic diagram of the topological pattern of the alabastrine metal micro structure of plane of the present invention;
Fig. 6 is a kind of derived structure of the alabastrine metal micro structure of plane shown in Fig. 5;
Fig. 7 is a kind of distressed structure of the alabastrine metal micro structure of plane shown in Fig. 5;
Fig. 8 is the first stage of the differentiation of the topological pattern of the alabastrine metal micro structure of plane;
Fig. 9 is the second stage of the differentiation of the topological pattern of the alabastrine metal micro structure of plane.
Embodiment
As shown in Figures 1 to 4, according to Cassegrain metamaterial antenna of the present invention, comprise the Meta Materials main reflector ZF with center through hole TK, be arranged on the feed 1 in center through hole TK and be arranged on the subreflector FF in feed 1 front, the electromagnetic wave of feed 1 radiation is successively through subreflector FF, with the form outgoing of plane wave after the reflection of Meta Materials main reflector ZF, described Meta Materials main reflector ZF comprises core layer 100 and is arranged on the reflector 200 of core layer 100 rear surface, described core layer 100 comprises at least one core layer 10, described core layer 10 comprises base material JC and is arranged on the multiple man-made microstructure 2 on base material JC, described subreflector FF is one of them curved surface of revolution ellipsoid, the phase center of described feed 1 overlaps with the over focus F2 of revolution ellipsoid.The phase center of feed 1 is the equal point of electromagnetic wave phase place in feed, namely feed is equivalent to desirable point source, this position residing for desirable point source, the F2 point namely in figure.
In the present invention, the real axis Z1 vertical Meta Materials main reflector ZF of described revolution ellipsoid.The real axis Z1 of revolution ellipsoid is focal axis, is the perifocus F1 of revolution ellipsoid and the straight line at over focus F2 line place.Perifocus F1 is near subreflector FF, and over focus F2 overlaps with the phase center of feed 1.
In the present invention, preferably, described feed 1 is corrugated horn, and the real axis of described revolution ellipsoid passes through the center in the bore face of corrugated horn.
In the present invention, reflector can for having the metallic reflection plate on smooth surface, and can be such as the copper coin of polishing, aluminium sheet or iron plate etc., may also be PEC (perfect electric conductor) reflecting surface, can certainly be metal coating, such as copper coating.In the present invention, the described arbitrary longitudinal section of core layer 10 is of similar shape and area, and longitudinal section herein refers to section vertical with the real axis of described revolution ellipsoid in core layer 10.The longitudinal section of described core layer can be for square, may also be circular or oval, the square of such as 300 × 300mm or 450 × 450mm, or diameter is the circle of 250,300 or 450mm.
In the present invention, the refraction index profile of arbitrary core layer 10 meets following formula:
Wherein, n (r) represents that in this core layer 10, radius is the refractive index value at r place, and the refraction index profile center of circle of this core layer is the real axis of revolution ellipsoid and the intersection point of this core layer;
S is the distance of perifocus to the front surface of Meta Materials main reflector of described revolution ellipsoid;
D is the thickness of core layer;
N
maxrepresent the refractive index maximum in core layer;
N
minrepresent the refractive index minimum value in core layer;
λ represents the electromagnetic wavelength that center of antenna frequency is corresponding;
Floor represents downward round numbers;
Such as, when
(r is in a certain number range) is more than or equal to 0 when being less than 1, and k gets 0, when
(r is in a certain number range) is more than or equal to 1 when being less than 2, and k gets 1, and the rest may be inferred.
In the present invention, for the ease of understanding, as shown in Figure 4, described core layer 10 can be divided into multiple metamaterial unit D as shown in Figure 2 of rectangular array arrangement, each metamaterial unit D comprises prebasal plate unit U, metacoxal plate unit V and is arranged on the man-made microstructure 2 between prebasal plate unit U, metacoxal plate unit V, the length and width of usual metamaterial unit D and thickness are all not more than 1/5th of electromagnetic wavelength corresponding to center of antenna frequency, be preferably 1/10th, therefore, the size of metamaterial unit D can be determined according to the centre frequency of antenna.Fig. 2 is the technique of painting of perspective, and to represent the position of man-made microstructure in metamaterial unit D, as shown in Figure 2, described man-made microstructure 2 is sandwiched between base board unit U, metacoxal plate unit V, and its surface, place represents with SR.
By formula (1) to formula (3) determined core layer, remain unchanged along its normal direction refractive index, perpendicular to its refraction index profile in the plane of normal as shown in Figure 3, it comprises multiple homocentric annular region, its center of circle is the O point in figure, preferably, the center of circle is the center of this plane, annular region H1 is schematically depicted to annular region H6 in Fig. 3, in each annular region, the refractive index at same radius r place is equal, and along with radius r increase refraction reduce gradually, and have adjacent two annular regions to be hopping pattern in the position refractive index that it connects, namely in adjacent two annular regions, its the outermost refractive index of annular region being positioned at inner side is n
min, the refractive index being positioned at its inner side of annular region in outside is n
max, such as, in Fig. 3, the outermost refractive index of annular region H1 is n
min, the refractive index of annular region H2 inner side is n
max.It should be noted that annular region is not necessarily complete, also can be incomplete, such as, annular region H5 in Fig. 3 and H6, and only have when the longitudinal section of core layer 10 is for time circular, its multiple annular regions obtained then are complete annular region.
In the present invention, above-mentioned radius r refers to the distance of the center of circle O in Fig. 3 to the centre of surface of each metamaterial unit, it above-mentioned radius stricti jurise is not a continuous print excursion, but because each metamaterial unit is far smaller than electromagnetic wavelength corresponding to center of antenna frequency, thus can be similar to think that above-mentioned radius is continually varying.
By formula (1) to formula (3) determined core layer, there is refraction index profile rule as shown in Figure 3, according to center of antenna frequency, the number of plies (i.e. the thickness of core layer) of appropriate design core layer, namely can make the electromagnetic wave sent by the perifocus F1 of described revolution ellipsoid can with the form outgoing of the plane wave perpendicular to core layer after Meta Materials main reflector, namely the focus of Meta Materials main reflector overlaps with the perifocus F1 of described revolution ellipsoid.
Can obtain according to common practise, electromagnetic wave after the upper reflection of its curved surface (subreflector) at revolution ellipsoid of the electromagnetic wave sent by the phase center (i.e. over focus F2) of feed 1 necessarily passes perifocus F1, like this, if the focus that design perifocus F1 is Meta Materials main reflector just can make the electromagnetic wave after the reflection of Meta Materials main reflector with the form outgoing of plane wave; Vice versa, i.e. the plane electromagnetic wave of vertical Meta Materials main reflector incidence can focus on the phase center place of feed (being also over focus F2 place).
In the present invention, preferably, described subreflector curve form and area adapt to shape and the area of main reflector, namely as shown in Figure 1, make the edge just being arrived main reflector by the electromagnetic wave of subreflector edge outgoing.
In the present invention, as shown in Figure 4, described base material JC comprises prebasal plate 13 and the metacoxal plate 15 of sheet, described multiple man-made microstructure is folded between prebasal plate 13 and metacoxal plate 15, the thickness of described core layer is 0.21-2.5mm, and wherein, the thickness of prebasal plate is 0.1-1mm, the thickness of metacoxal plate is 0.1-1mm, and the thickness of multiple man-made microstructure 2 is 0.01-0.5mm.
As an example, the thickness of described core layer is 0.818mm, and wherein, the thickness of prebasal plate and metacoxal plate is 0.4mm, and the thickness of multiple man-made microstructure is 0.018mm.
The thickness of each core layer determines, then can set the different numbers of plies as required, thus forms the core layer with thickness d.
In the present invention, described base material is obtained by ceramic material, polystyrene, polypropylene, polyimides, polyethylene, polyether-ether-ketone or polytetrafluoroethylene.Such as, polyfluortetraethylene plate (PS plate), it has good electrical insulating property, can not produce interference, and have excellent chemical stability, corrosion resistance, long service life to electromagnetic electric field.
In the present invention, preferably, described man-made microstructure 2 is metal micro structure, described metal micro structure is made up of one or more metal wire, described metal wire is copper cash, silver-colored line or aluminum steel, the multiple man-made microstructure on described base material JC by etching, plating, bore quarters, photoetching, electronics carve or ion quarter method obtain.Core layer such as shown in Fig. 4, can first by one of them in prebasal plate 13 or metacoxal plate 15 covers copper, unwanted copper is removed again by techniques such as etchings, namely obtain the planar arrangement of multiple man-made microstructure, namely finally prebasal plate and metacoxal plate to be bonded together with PUR defines a core synusia.Multiple core layer can be formed, by bonding for each core layer PUR core layer that can obtain multilayer by said method.The material of PUR material that is best and core layer is consistent.
In the present invention, preferably, the differentiation of the topological pattern in the alabastrine metal micro structure of plane as shown in Figure 5 of the multiple man-made microstructure on described base material obtains.The topological pattern of the metal micro structure namely shown in Fig. 5 is the basic flat topology pattern in the alabastrine metal micro structure of plane, and the topological pattern of all metal micro structures on same base material develops by the pattern shown in Fig. 5 and obtains.
As shown in Figure 5, described have the first metal wire J1 and the second metal wire J2 that mutually vertically divide equally in the alabastrine metal micro structure of plane, described first metal wire J1 is identical with the length of the second metal wire J2, described first metal wire J1 two ends are connected with two the first metal branch F1 of equal length, described first metal wire J1 two ends are connected on the mid point of two the first metal branch F1, described second metal wire J2 two ends are connected with two the second metal branch F2 of equal length, described second metal wire J2 two ends are connected on the mid point of two the second metal branch F2, described first metal branch F1 is equal with the length of the second metal branch F2.
Fig. 6 is a kind of derived structure of the alabastrine metal micro structure of plane shown in Fig. 5.It is all connected with identical 3rd metal branch F3 at the two ends of each first metal branch F1 and each second metal branch F2, and the mid point of corresponding 3rd metal branch F3 is connected with the end points of the first metal branch F1 and the second metal branch F2 respectively.The rest may be inferred, and the present invention can also derive the metal micro structure of other form.Equally, the just basic flat topology pattern shown in Fig. 6.
Fig. 7 is a kind of distressed structure of the alabastrine metal micro structure of plane shown in Fig. 5, the metal micro structure of this kind of structure, first metal wire J1 and the second metal wire J2 is not straight line, but folding line, first metal wire J1 and the second metal wire J2 is provided with two kink WZ, but the first metal wire J1 remains vertical with the second metal wire J2 to be divided equally, by arrange kink towards with the relative position of kink on the first metal wire and the second metal wire, metal micro structure shown in Fig. 7 is all overlapped with former figure to the figure of any direction 90-degree rotation around the axis perpendicular to the first metal wire and the second metal wire intersection point.In addition, other can also be had to be out of shape, such as, the first metal wire J1 and the second metal wire J2 all arranges multiple kink WZ.Equally, the just basic flat topology pattern shown in Fig. 7.
Known refractive index
wherein μ is relative permeability, and e is relative dielectric constant, and μ and e is collectively referred to as electromagnetic parameter.Experiment proves, when electromagnetic wave is by refractive index dielectric material heterogeneous, and can to the large direction deviation of refractive index.When relative permeability is certain (usually close to 1), refractive index is only relevant with dielectric constant, when base material is selected, utilize the arbitrary value (within the specific limits) that only can realize metamaterial unit refractive index to the man-made microstructure of electric field response, under this center of antenna frequency, utilize simulation software, as CST, MATLAB, COMSOL etc., the situation that the dielectric constant being obtained the man-made microstructure (the alabastrine metal micro structure of plane as shown in Figure 5) of a certain given shape by emulation is changed along with the refractive index variable of topological pattern, data one to one can be listed, the core layer 10 of the specific refractive index distribution that we need can be designed.
In the present embodiment, the planar arrangement of the man-made microstructure in core layer obtains by Computer Simulation (such as CST emulation), specific as follows:
(1) the attachment base material of man-made microstructure is determined.Such as dielectric constant is the medium substrate of 2.7, and the material of this medium substrate can be FR-4, F4b or PS.
(2) size of metamaterial unit is determined.The size of metamaterial unit is obtained by the centre frequency of antenna, frequency is utilized to obtain its wavelength, get again be less than wavelength 1/5th a numerical value as the length CD of metamaterial unit D and width KD, then get be less than wavelength 1/10th a numerical value as metamaterial unit D thickness.Such as correspond to the center of antenna frequency of 11.95G, described metamaterial unit D is long CD as shown in Figure 2 and wide KD is 2.8mm, thickness HD is 0.543mm square platelet.
(3) material of man-made microstructure and basic flat topology pattern thereof is determined.In the present invention, man-made microstructure is metal micro structure, and the material of described metal micro structure is copper, and the basic flat topology pattern of metal micro structure is the alabastrine metal micro structure of the plane shown in Fig. 5, and its live width W is consistent everywhere; Basic flat topology pattern herein, refers to the differentiation basis of the topological pattern of all man-made microstructure on same base material.
(4) the topological pattern parameter of man-made microstructure is determined.As shown in Figure 5, in the present invention, the topological pattern parameter of the alabastrine metal micro structure of plane comprises the live width W of metal micro structure, the length a of the first metal wire J1, the length b of the first metal branch F1, and the thickness HD of metal micro structure, in the present invention, thickness is constant, is taken as 0.018mm.
(5) the differentiation restrictive condition of the topological pattern of metal micro structure is determined.In the present invention, the differentiation restrictive condition of the topological pattern of metal micro structure has, the minimum spacing WL (namely as shown in Figure 5, the long limit of metal micro structure and metamaterial unit or the distance of broadside are WL/2) between metal micro structure, the live width W of metal micro structure, the size of metamaterial unit; Due to processing technology restriction, WL is more than or equal to 0.1mm, and equally, live width W is greater than to equal 0.1mm.First time is when emulating, WL can get 0.1mm, W can get 0.3mm, it is 2.8mm that metamaterial unit is of a size of long and wide, thickness is that (thickness of metal micro structure is 0.018mm to 0.818mm, the thickness of base material is 0.8mm), now the topological pattern parameter of metal micro structure only has a and b Two Variables.The topological pattern of metal micro structure, by the differentiation mode as shown in Fig. 8 to Fig. 9, corresponding to a certain characteristic frequency (such as 11.95GHZ), can obtain a continuous print variations in refractive index scope.
Particularly, the differentiation of the topological pattern of described metal micro structure comprises two stages (basic pattern that topological pattern develops is the metal micro structure shown in Fig. 5):
First stage: according to differentiation restrictive condition, when b value remains unchanged, a value is changed to maximum from minimum value, the metal micro structure in this evolution process is " ten " font when minimum value (a get except).In the present embodiment, the minimum value of a is 0.3mm (live width W), and the maximum of a is (CD-WL).Therefore, in the first phase, the differentiation of the topological pattern of metal micro structure as shown in Figure 8, is namely the square JX1 of W from the length of side, develops into maximum " ten " font topology pattern JD1 gradually.In the first phase, along with the differentiation of the topological pattern of metal micro structure, the refractive index of the metamaterial unit corresponding with it increases (respective antenna one characteristic frequency) continuously.
Second stage: according to differentiation restrictive condition, when a is increased to maximum, a remains unchanged; Now, b is increased continuously maximum from minimum value, the metal micro structure in this evolution process is plane flakes.In the present embodiment, the minimum value of b is 0.3mm, and the maximum of b is (CD-WL-2W).Therefore, in second stage, the differentiation of the topological pattern of metal micro structure as shown in Figure 9, namely from maximum " ten " font topology pattern JD1, develop into the alabastrine topological pattern JD2 of maximum plane gradually, the alabastrine topological pattern JD2 of maximum plane herein refers to, the length b of the first metal branch J1 and the second metal branch J2 can not extend again, otherwise the first metal branch is crossing by generation with the second metal branch.In second stage, along with the differentiation of the topological pattern of metal micro structure, the refractive index of the metamaterial unit corresponding with it increases (respective antenna one characteristic frequency) continuously.
If the variations in refractive index scope being obtained metamaterial unit by above-mentioned differentiation contains n
minto n
maxconsecutive variations scope, then meet design needs.If the variations in refractive index scope that above-mentioned differentiation obtains metamaterial unit does not meet design needs, such as maximum is too little or minimum value is excessive, then change WL and W, again emulate, until obtain the variations in refractive index scope of our needs.
According to formula (1) to (3), a series of metamaterial unit emulation obtained, according to after the refractive index arrangement of its correspondence (being in fact exactly the arrangement of multiple man-made microstructure on base material of different topology pattern), can obtain core layer of the present invention.
By reference to the accompanying drawings embodiments of the invention are described above; but the present invention is not limited to above-mentioned embodiment; above-mentioned embodiment is only schematic; instead of it is restrictive; those of ordinary skill in the art is under enlightenment of the present invention; do not departing under the ambit that present inventive concept and claim protect, also can make a lot of form, these all belong within protection of the present invention.
Claims (8)
1. a Cassegrain metamaterial antenna, it is characterized in that, comprise the Meta Materials main reflector with center through hole, be arranged on the feed in center through hole and be arranged on the subreflector in feed front, the electromagnetic wave of feed radiation is successively through subreflector, with the form outgoing of plane wave after the reflection of Meta Materials main reflector, described Meta Materials main reflector comprises core layer and is arranged on the reflector of core layer rear surface, described core layer comprises at least one core layer, described core layer comprises base material and is arranged on the multiple man-made microstructure on base material, described subreflector is one of them curved surface of revolution ellipsoid, the phase center of described feed overlaps with the over focus of revolution ellipsoid, the vertical Meta Materials main reflector of real axis of described revolution ellipsoid,
Wherein, the refraction index profile of arbitrary core layer meets following formula:
Wherein, n (r) represents that in this core layer, radius is the refractive index value at r place, and the refraction index profile center of circle of this core layer is the real axis of revolution ellipsoid and the intersection point of this core layer;
S is the distance of perifocus to the front surface of Meta Materials main reflector of described revolution ellipsoid;
D is the thickness of core layer;
N
maxrepresent the refractive index maximum in core layer;
N
minrepresent the refractive index minimum value in core layer;
λ represents the electromagnetic wavelength that center of antenna frequency is corresponding;
Floor represents downward round numbers.
2. Cassegrain metamaterial antenna according to claim 1, is characterized in that, described feed is corrugated horn, and the real axis of described revolution ellipsoid passes through the center in the bore face of corrugated horn.
3. Cassegrain metamaterial antenna according to claim 1, it is characterized in that, described base material comprises prebasal plate and the metacoxal plate of sheet, described multiple man-made microstructure is folded between prebasal plate and metacoxal plate, the thickness of described core layer is 0.21-2.5mm, and wherein, the thickness of prebasal plate is 0.1-1mm, the thickness of metacoxal plate is 0.1-1mm, and the thickness of multiple man-made microstructure is 0.01-0.5mm.
4. Cassegrain metamaterial antenna according to claim 3, is characterized in that, the thickness of described core layer is 0.818mm, and wherein, the thickness of prebasal plate and metacoxal plate is 0.4mm, and the thickness of multiple man-made microstructure is 0.018mm.
5. Cassegrain metamaterial antenna according to claim 1, it is characterized in that, described man-made microstructure is metal micro structure, described metal micro structure is made up of one or more metal wire, described metal wire is copper cash, silver-colored line or aluminum steel, the multiple man-made microstructure on described base material by etching, plating, bore quarters, photoetching, electronics carve or ion quarter method obtain.
6. Cassegrain metamaterial antenna according to claim 5, it is characterized in that, multiple man-made microstructure on described base material are obtained by the differentiation of the topological pattern in the alabastrine metal micro structure of plane, described have the first metal wire and the second metal wire mutually vertically divided equally in the alabastrine metal micro structure of plane, described first metal wire is identical with the length of the second metal wire, described first metal wire two ends are connected with two the first metal branch of equal length, described first metal wire two ends are connected on the mid point of two the first metal branch, described second metal wire two ends are connected with two the second metal branch of equal length, described second metal wire two ends are connected on the mid point of two the second metal branch, described first metal branch is equal with the length of the second metal branch.
7. Cassegrain metamaterial antenna according to claim 6, it is characterized in that, described is that each first metal branch of the alabastrine metal micro structure of plane and the two ends of each second metal branch are also connected with identical 3rd metal branch, and the mid point of corresponding 3rd metal branch is connected with the end points of the first metal branch and the second metal branch respectively.
8. Cassegrain metamaterial antenna according to claim 6, it is characterized in that, described the first metal wire in the alabastrine metal micro structure of plane is provided with two kinks with the second metal wire, and described is that the alabastrine metal micro structure of plane all overlaps with former figure to the figure of any direction 90-degree rotation with the intersection point of the second metal wire around the first metal wire in plane residing for metal micro structure.
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| Application Number | Priority Date | Filing Date | Title |
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| CN201210269062.3A CN102856664B (en) | 2012-07-31 | 2012-07-31 | Cassegrain type metamaterial antenna |
| PCT/CN2013/080576 WO2014019524A1 (en) | 2012-07-31 | 2013-07-31 | Cassegrain-type metamaterial antenna |
| EP13826029.4A EP2882038B1 (en) | 2012-07-31 | 2013-07-31 | Cassegrain-type metamaterial antenna |
| US14/607,463 US9742074B2 (en) | 2012-07-31 | 2015-01-28 | Cassegrain-type metamaterial antenna |
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| CN201210269062.3A CN102856664B (en) | 2012-07-31 | 2012-07-31 | Cassegrain type metamaterial antenna |
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| EP2882038B1 (en) | 2012-07-31 | 2019-10-16 | Kuang-Chi Innovative Technology Ltd. | Cassegrain-type metamaterial antenna |
| CN107039780B (en) * | 2015-07-24 | 2023-12-15 | 深圳光启高等理工研究院 | Reflection antenna and design method thereof |
| CN108767489B (en) * | 2018-05-24 | 2020-04-07 | 西安电子科技大学 | Transmission type Cassegrain antenna based on super surface |
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| CN102856664A (en) | 2013-01-02 |
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