EP4012834A1 - Antennenquelle für eine direkt strahlende gruppenantenne, strahlplatte und antenne mit mehreren antennenquellen - Google Patents

Antennenquelle für eine direkt strahlende gruppenantenne, strahlplatte und antenne mit mehreren antennenquellen Download PDF

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Publication number
EP4012834A1
EP4012834A1 EP21213068.6A EP21213068A EP4012834A1 EP 4012834 A1 EP4012834 A1 EP 4012834A1 EP 21213068 A EP21213068 A EP 21213068A EP 4012834 A1 EP4012834 A1 EP 4012834A1
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EP
European Patent Office
Prior art keywords
ribs
polarizer
antenna
filter
radiating element
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EP21213068.6A
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English (en)
French (fr)
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EP4012834B1 (de
EP4012834C0 (de
Inventor
Thierry Girard
Maïder ETCHARREN
Alexandre COT�
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Thales SA
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Thales SA
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Publication of EP4012834C0 publication Critical patent/EP4012834C0/de
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Classifications

    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01P—WAVEGUIDES; RESONATORS, LINES, OR OTHER DEVICES OF THE WAVEGUIDE TYPE
    • H01P3/00—Waveguides; Transmission lines of the waveguide type
    • H01P3/12—Hollow waveguides
    • H01P3/123—Hollow waveguides with a complex or stepped cross-section, e.g. ridged or grooved waveguides
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01P—WAVEGUIDES; RESONATORS, LINES, OR OTHER DEVICES OF THE WAVEGUIDE TYPE
    • H01P1/00—Auxiliary devices
    • H01P1/20—Frequency-selective devices, e.g. filters
    • H01P1/207—Hollow waveguide filters
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01P—WAVEGUIDES; RESONATORS, LINES, OR OTHER DEVICES OF THE WAVEGUIDE TYPE
    • H01P1/00—Auxiliary devices
    • H01P1/165—Auxiliary devices for rotating the plane of polarisation
    • H01P1/17—Auxiliary devices for rotating the plane of polarisation for producing a continuously rotating polarisation, e.g. circular polarisation
    • H01P1/171—Auxiliary devices for rotating the plane of polarisation for producing a continuously rotating polarisation, e.g. circular polarisation using a corrugated or ridged waveguide section
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01P—WAVEGUIDES; RESONATORS, LINES, OR OTHER DEVICES OF THE WAVEGUIDE TYPE
    • H01P1/00—Auxiliary devices
    • H01P1/165—Auxiliary devices for rotating the plane of polarisation
    • H01P1/17—Auxiliary devices for rotating the plane of polarisation for producing a continuously rotating polarisation, e.g. circular polarisation
    • H01P1/173—Auxiliary devices for rotating the plane of polarisation for producing a continuously rotating polarisation, e.g. circular polarisation using a conductive element
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01P—WAVEGUIDES; RESONATORS, LINES, OR OTHER DEVICES OF THE WAVEGUIDE TYPE
    • H01P5/00—Coupling devices of the waveguide type
    • H01P5/08—Coupling devices of the waveguide type for linking dissimilar lines or devices
    • H01P5/10—Coupling devices of the waveguide type for linking dissimilar lines or devices for coupling balanced with unbalanced lines or devices
    • H01P5/107—Hollow-waveguide/strip-line transitions
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q13/00—Waveguide horns or mouths; Slot antennas; Leaky-waveguide antennas; Equivalent structures causing radiation along the transmission path of a guided wave
    • H01Q13/06—Waveguide mouths
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q21/00—Antenna arrays or systems
    • H01Q21/06—Arrays of individually energised antenna units similarly polarised and spaced apart
    • H01Q21/061—Two dimensional planar arrays
    • H01Q21/064—Two dimensional planar arrays using horn or slot aerials

Definitions

  • the invention lies in the field of satellites and more particularly for satellites in low orbit which must transmit data everywhere on the Earth, in particular in the K and Ka bands (the K and Ka bands are grouped together in space telecommunications), in the Ku band, or even in the V band.
  • the invention can find an application for example for broadband Internet.
  • the Ka band corresponds to a frequency band between 27 and 40 GHz. It is used in particular for the Internet by satellite.
  • the Ka band is grouped with the K band and extends in reception from 27.5 to 30 GHz and in transmission from 17.7 to 20.2GHz.
  • the V band is divided into two frequency bands: the Q band (37.5-42.5 GHz) and the V band (47.2 - 50.2 GHz), with smaller dimensions.
  • the invention relates more specifically to the field of space antennas for satellites in low orbit where data must be transmitted in a large angular domain, and in particular direct radiation array antennas.
  • direct radiation array antenna or "DRA” in English means an antenna that can operate in transmission and/or reception and comprising an array of elementary radiation sources connected by a beamformer (known as "BFN” for " Beam Forming Network” in English).
  • BFN beamformer
  • Two types of orbiting satellites can be used to deliver broadband to Earth.
  • a first type concerns geostationary satellites (36,000 km) which will make it possible to provide broadband on Earth in a given region or zone. In this orbit the satellite moves exactly synchronously with the Earth and remains constantly above the same point on the surface.
  • a second type is based on the use of a constellation of satellites in low orbit (called “LEO” satellites for “Low Earth Orbit” in English) configured to make it possible to provide broadband throughout the Earth.
  • a constellation of satellites is a collection of artificial satellites that work together. The satellites orbit in chosen and synchronized orbits so that their respective ground coverages overlap and complement each other instead of interfering with each other.
  • One of the advantages of the constellation of satellites in low orbit is the latency time between transmission and reception of data because the satellites in low orbit used are closer to the earth (generally between 500 and 1200 km).
  • the reduction in latency time is an advantage for areas requiring a very fast response (for example: for an autonomous car, for faster access to data, for video calls or videoconferences with better responsiveness, etc.).
  • the Earth is seen from the LEO satellite following a cone which can vary between +/- 45° and +/- 55° depending on the altitude of the satellite. This field is in strong development, with numerous missions and/or projects for satellite constellations in low orbit ( Starlink, Kuiper, Telesat, Leosat, Oneweb, etc.).
  • the data transmitted between these satellites and the Earth for high-speed Internet communications use the Ka bands (combining K and Ka for space), the Q and V bands but also the Ku band. It is therefore sought antennas which can operate in these bands and in particular in the Ka band.
  • the antenna generally used for LEO satellites is a direct radiating array antenna called “DRA” (“Direct Radiating Array” in English which is translated into French as “direct radiating array”).
  • DPA Direct Radiating Array
  • the DRA antennas in the field of the invention comprise a large number of sources (generally from 128 to 512 sources) and each source is composed of at least one radiating element, a polarizer and a filter which must be easily connected. amplifiers (or loads). All the sources form a radiating panel.
  • DRA antennas called “printed antennas” or “patch antennas”, allowing the transmission of data between LEO satellites and the Earth. They include elements (or “patches”) printed on a flat substrate, and are suitable for L-band or S-band type frequency bands, which are lower than the Ka band and for low bandwidths (less than 1 %).
  • the sources (radiating element, polarizer, filter) of these antennas are manufactured using printed circuit type technology, so they are easily manufactured, they are compact and of limited mass. Losses are not prohibitive in the L-band or S-band type frequency bands.
  • patch antennas are well suited for low passbands (less than 1%).
  • ridged waveguide is defined as a waveguide of any shape (square, circular, rectangular) capable of transmitting a microwave signal and comprising one or more ribs inside it.
  • the problem of the waveguide radiating element with a horn shape, whether ridged or not, is that it requires a system to circularly polarize the wave.
  • a deflector Since the size of the radiating element is in the range of 0.55 to 0.7 ⁇ , a deflector is generally used to connect the horn to the system which allows the wave to be circularly polarized. Indeed, systems of the OrthoMode transducer (OMT) type with coupler or polarizer with guide septum do not comply with this mesh or size constraint.
  • OMT OrthoMode transducer
  • the diverter allows, with a set of waveguides (as many as the number of radiating elements) which are curved, to change the size of a mesh between its entry and its exit.
  • the major constraint consists in having guides of identical lengths. This constraint implies that the feeder is difficult to design.
  • the use of a deflector involves a much larger size of the radiating panel, significant RF losses due to the deflector.
  • a deflector structure is difficult to make in one piece, even using an additive manufacturing technique.
  • the invention aims to overcome the aforementioned drawbacks of the prior art.
  • an antenna source for producing an array antenna DRA a source which is as compact as possible, which generates circular polarization without using a deflector, which is suitable for the Ka frequency band (or K, Q, V, Ku ...), whose elementary radiating element has a small aperture compared to the wavelength ⁇ , and which has low RF losses (typically less than 0.3 dB, or even 0.2 dB in Ka band).
  • the invention aims to have such an antenna source which can incorporate a filter and which can easily be connected to an amplifier.
  • the antenna source must be able to be manufactured easily, and at low cost.
  • end to end it is meant that the elements are joined by their ends.
  • the waveguide has a constant thickness over its entire length.
  • the impedance between the input and the output of the radiating element generally increases between a hundred ohms (in the waveguide) and 377 ohms (in air or vacuum).
  • cylinder or “cylindrical”, we mean the general definition, namely a solid generated by a straight line which moves parallel to an axis, resting on two isometric and parallel fixed planes.
  • a right cylinder designates a cylinder whose generatrices are perpendicular to the bases.
  • the base can be a circle or a polygon (square, hexagon, octagon, decagon). In the case where the base is a polygon, we can also speak of a prism. The base must have an axis of symmetry in its own plane. This is why we will speak of a polygon of even order (that is to say with an even number of sides).
  • polarizer is understood to mean an element intended to convert, on the one hand, the signals received in circular polarization into signals in linear polarization and, on the other hand, the signals to be transmitted from a linear polarization into a circular polarization.
  • input or “output” are defined according to the direction of circulation of the radio frequency (RF) waves in the source when the latter operates in transmission, that is to say from the filter or the polarizer towards the horn.
  • RF radio frequency
  • a radiating element can be designated by "horn” which is a term commonly used in the field of the invention and which designates an antenna element in the shape of a cylinder, and which can comprise a complementary part in the shape of a cone or a pyramid. truncated. In the case of a horn comprising a complementary part in the shape of a cone or a truncated pyramid, the widest part always corresponds to the output of the radiating element.
  • a waveguide comprising ribs inside said waveguide can be designated by the term “ridged waveguide”.
  • the term “length” is to be understood with reference to the longitudinal direction of the antenna source.
  • the term “radial” is to be understood with reference to a plane perpendicular to said longitudinal direction, called “transverse plane”, and the term “orthoradial” designates the direction perpendicular to the radial direction in said transverse plane.
  • the width of the blade designates the radial dimension of the blade, more generally the dimension of the blade which makes it possible to separate the polarizer input into two.
  • the thickness of the blade designates the other dimension in the transverse plane.
  • the height of a rib designates the radial dimension.
  • the thickness of a rib designates the dimension along the orthoradial direction.
  • the height of a stud designates the dimension substantially along the radial direction and the thickness of a stud designates the dimension substantially along the orthoradial direction.
  • the solution consists in forming a radiating element in waveguide with internal ribs, and a polarizer in waveguide with septum and internal ribs connected to the radiating element in the continuity of this one (in only one part) , the septum polarizer allowing to have two waveguide accesses. It is possible to arrange on one of the ports of the polarizer a filter with pads in waveguide with ribs.
  • the antenna source integrates a radiating element with internal ribs compatible with a very small DRA array antenna mesh (0.5 to 0.7 ⁇ ), but also a low-loss septum polarizer compatible with the same mesh. DRA array antenna, and which generates circular polarization without using a deflector.
  • the antenna source according to the invention may further comprise one or more of the following characteristics taken individually or in any possible technical combination.
  • the number of first ribs and/or second ribs is preferably an even number, both at the input and at the output of the radiating element and/or of the polarizer.
  • An even number favors symmetry of the antenna source.
  • the even number also favors the introduction of the plate of the septum polarizer which in this case is attached to two opposite ribs and makes it possible to simplify the dimensioning of the septum polarizer.
  • the second ribs can be continuous with the first ribs at the input of the radiating element (corresponding to the last step), which facilitates the design and manufacture of the source.
  • the second ribs may not be continuous with the first ribs at the input of the radiating element.
  • the base of the right cylinder is a regular polygon of even order, preferably a hexagon.
  • the internal blade and all or part of the first ribs and/or of the second ribs can be arranged at the level of the edges of the right polygonal cylinder.
  • the internal blade and all or part of the first ribs and/or of the second ribs can be arranged on the inner side surfaces of the polygonal right cylinder.
  • the first and second variants can be combined such that the inner blade can be arranged at two opposite edges of the polygonal right cylinder or on two opposite inner side surfaces of the polygonal right cylinder, and the first ribs and/or the second ribs can be arranged both at the edges of the polygonal right cylinder and on the inner side surfaces of the polygonal right cylinder.
  • the base of the right cylinder is a circle.
  • the number of third ribs is an even number, both at the input and at the output of the filter.
  • An even number favors symmetry of the antenna source.
  • the third ribs can be continuous with the second ribs of the polarizer, which facilitates the design and manufacture of the source.
  • the third ribs may not be continuous with the second ribs.
  • the waveguide is entirely in the form of a hollow right cylinder over its entire length.
  • the main part represents the whole length of the waveguide.
  • the waveguide comprises a main part in the shape of a hollow straight cylinder and a complementary part at the output of the radiating element, said complementary part possibly being in the shape of a cone or of a truncated pyramid, the most flared part being arranged at the output of the radiating element.
  • the complementary part is free of grooves. Furthermore, the length of the complementary part is very short compared to the length of the main part of the waveguide.
  • a second object of the invention is a radiating panel for a direct radiation array antenna, said panel comprising a plurality of sources according to the invention comprising a plurality of antenna sources according to the first object of the invention; said radiating panel being in one piece, preferably produced using an additive manufacturing technique.
  • the sources of the same radiating panel are all substantially identical.
  • the radiating panel comprises sources each having radiating elements of small dimensions (0.5 to 0.7 ⁇ ) with very low RF losses (typically less than 0.3 dB, or even 0.2 dB in Ka band) and can be easily manufactured.
  • the radiating panel is connected to the at least one amplifier and/or the at least one load via at least one Vivaldi antipodal transition, and preferably by at least one suitable transition/adaptation to change the position, the dimensions and/or the shape of the ribs of the waveguide at the input of the source so as to be able to position the Vivaldi transition within said waveguide.
  • the antenna source, the radiating panel and the direct radiation array antenna according to the invention may comprise any one of the characteristics listed above, taken in isolation or according to any technically possible combination with other characteristics.
  • the radiating element may be designated by the term “horn”.
  • the longitudinal direction is identified by the reference X and the arrow is oriented in the direction of entry towards exit of each of the elements (horn, polarizer, filter).
  • the longitudinal direction X also corresponds to the axis of the cylinder.
  • the polarizer is disposed end to end with the horn in the longitudinal direction, and the filter, if any, is disposed end to end with the polarizer in the longitudinal direction.
  • the antenna source can be made of metallic, metallized, or metallizable material.
  • it can be aluminum, titanium, or any other material which can be metallized on the surface.
  • the material of the antenna source is adapted to manufacture the antenna source, and to manufacture the radiating panel of the array antenna (comprising a plurality of sources in one piece) by an additive manufacturing technique.
  • a source comprises a waveguide having at least one main part in the form of a hollow right cylinder extending along a longitudinal direction X, the base of said cylinder having at least one axis of symmetry in its plane.
  • the external transverse dimensions of this main part are constant along the longitudinal direction X.
  • the sources represented in the figures and described in the rest of the description are in the shape of a hollow right cylinder, and this, over their entire length (in other words, the main part extends over the entire length of the guide of wave).
  • the source may comprise, at the output of the radiating element, a complementary part in the shape of a cone or truncated pyramid, the widest part being arranged at the output of the radiating element.
  • the source may comprise, at the output of the radiating element, a complementary part of cylindrical shape with external transverse dimensions and/or of different base shape from the main part.
  • the complementary part is free of grooves.
  • the length of the complementary part is very short compared to the main part of the waveguide. For example, it represents about 1/10 or even 1/20 of the length of the horn and can represent 1/100 of the total length of the source.
  • the Figures 1A and 1B represent an antenna source according to a first embodiment of the invention, the Figure 1A being a 3D view and the figure 1 B being a side view (view from the horn exit).
  • the antenna source 1 shown is in the form of a waveguide which comprises a first portion forming a horn 2 and a second portion forming a polarizer 3, the two forming a single piece (waveguide) whose outer shape is a cylinder straight with a hexagonal base 10, the cylinder being hollow.
  • the horn 2 represented comprises an input E c (marked in Figure 3A ) and an output S c . It has an external shape in the form of a hexagonal cylinder 10, and comprises six ribs 21 (first ribs), which project towards the inside of said horn from of each edge 10A of the hexagonal cylinder 10 and extend in the longitudinal direction X.
  • the first six ribs all have the same shapes and they are shaped like steps along the longitudinal direction X.
  • the first ribs are staggered along three steps 211, 212, 213 whose dimensions (heights, thicknesses and/or lengths) vary along the longitudinal direction X.
  • the number and dimensions of the steps are configured to allow a given impedance variation between the input and output of the radiating element.
  • transverse external dimensions of the cylindrical main part of the waveguide do not vary along the longitudinal direction X and in particular do not decrease. It is the ribs inside the horn, with their steps, which make it possible to vary the impedance in said horn.
  • this makes it possible to have the largest possible opening at the horn input in order to then be able to produce the septum polarizer which is connected to the horn input.
  • This makes it possible to introduce the blade of the polarizer and push the first upper mode as far as possible from the operating band of the array antenna. This particularity is even truer for cylindrical (or prismic) horns with a square base for which the cut-off frequency of the first higher mode appears for a lower frequency.
  • the horn is described in more detail in the remainder of this description, according to different (non-limiting) variants, each of the variants being able to be implemented in the first embodiment, or in the second embodiment described below.
  • the polarizer 3 has two inputs E P1 , E P2 separated by an internal blade 30, or septum, extending along the longitudinal direction X, and an output Sp (marked in figure 4A ) which corresponds to the input E c of the horn 2.
  • the internal plate comprises several bearings 301, 302, 303, 304 in the longitudinal direction X. The bearings are configured to transform an electromagnetic field of circular polarization at the polarizer input into a linear polarization electromagnetic field at the polarizer output, and vice versa.
  • ribs 31 (second ribs) protrude inwardly from said polarizer from each edge 10A of the hexagonal cylinder 10 and extend in the longitudinal direction X.
  • two other second ribs 32 (marked in figure 4A and 4B ) are formed, which correspond to the two radial ends of the blade 30 which disappears at the polarizer output.
  • the second ribs 31, 32 have the same thicknesses and heights as the first steps 211 of the first ribs 21.
  • the second ribs 31, 32 are in continuity with the corresponding first ribs 21 at the input. of the horn 2.
  • the dimensions of the second ribs are shown constant in the longitudinal direction, and are substantially equal to each other.
  • the ribs in the polarizer make it possible to reduce the minimum operating frequency of the latter and allow the propagation of the wave in the latter.
  • the dimensions of the ribs are such that the main mode propagates in the polarizer.
  • the cut-off frequency of the first upper mode must be greater than the maximum operating frequency so that it cannot propagate in the structure.
  • this makes it possible to reduce the transverse dimensions of the polarizer compared to a conventional septum polarizer, in order to make it compatible with the opening of the horn.
  • the polarizer is described in more detail in the remainder of this description, according to different (non-limiting) variants, each of the variants being able to be implemented in the first embodiment, or in the second embodiment described below.
  • the Figures 2A, 2B , 2C and 2D represent an antenna source according to a second embodiment of the invention which differs from the first mode in that it further comprises a third portion 4 which comprises a filter 40.
  • the figure 2A is a 3D view
  • the figure 2B is a sectional view along a plane passing through the X axis and the Y axis (corresponding to the plane of the blade)
  • the Fig. 2C is a sectional view along a plane passing through the X axis and the Z axis and the 2D figure being a side view (view from the exit of the horn).
  • the antenna source 1' shown thus comprises a first portion forming a horn 2, a second portion forming a polarizer 3 and a third portion 4 comprising a filter 40, the three portions forming a single piece whose outer shape is a right cylinder with a base hexagonal 10.
  • the filter 40 corresponds to half of the right hexagonal cylinder in the third portion 4 (the output of the filter corresponds to one of the two inputs of the polarizer).
  • the filter comprises, in the continuity of one of the two inputs of the polarizer, a series 42 of frequency filter pads, the pads being positioned one after the other in the longitudinal direction X and arranged on the central blade. Filter pads are chosen to allow certain frequencies to pass while other frequencies are retained.
  • the pads have a 45° inclination so that the antenna source is produced by additive manufacturing in one and the same part, therefore in the same material as the horn and the polarizer.
  • the various studs have dimensions (lengths, thicknesses and/or heights) which may differ from one stud to another. Furthermore, the distances between two adjacent plots may differ.
  • a conventional “combline” type filter is generally produced by introducing metal rods into a rectangular guide, the size of the rods as well as the distance relative to the upper wall of the guide making it possible to transmit or reject certain frequencies.
  • This type of filter is well known to those skilled in the art.
  • the filter is sized to produce a low-pass filter.
  • the third portion 4 further comprises third ribs 41 extending towards the inside thereof and over all or part of the length of said third portion.
  • said third ribs are continuous with the second ribs. These third ribs are dimensioned in such a way that the wave can propagate in the waveguide.
  • the filter is described in more detail in the remainder of this description, according to various possible variants (non-limiting). Any variant can be implemented in the second embodiment.
  • the figure 3A (3D view) and 3B (side view) represent in detail a hexagonal horn 2 according to a first variant of the invention, which corresponds to the hexagonal horn of figures 1A, 1B , 2A and 2B .
  • the hexagonal horn 2 comprises six first ribs 21 which project towards the inside of said horn from each edge of the hexagonal cylinder.
  • the first six ribs all have the same shapes, and they are formed into steps along the longitudinal direction X.
  • three steps 211, 212, 213 are shown whose dimensions (heights, thicknesses and/or lengths ) vary along the longitudinal direction, the thicknesses of the steps decreasing in the direction going from the entry E C towards the exit S C of the horn (direction of circulation).
  • the thickness e 211 of the first step 211 is greater than the thickness e 212 of the second step 212, itself greater than the thickness e 213 of the third step. Furthermore, the height h 211 of the first step 211 is slightly greater than the height h 212 of the second step 212, itself greater than the height h 213 of the third step 213.
  • the thicknesses and the heights of the steps are not necessary for the thicknesses and the heights of the steps to vary in an increasing or decreasing manner in the direction of circulation, these can take any values as long as this makes it possible to achieve the impedance variation. desired.
  • the number of steps as well as the dimensions of the steps of the first ribs are parameters that can be configured by those skilled in the art, so as to allow a given impedance variation. between the inlet and the outlet of the horn.
  • the number of steps can be equal to three as illustrated or four.
  • first ribs and their locations are not limited to the illustrated modes and variants.
  • the first ribs can have all the same shapes, as illustrated, or have different shapes.
  • the number of first ribs is an even number, both at the entry and at the exit of the horn, and they are arranged in a regular manner around the perimeter of the cylinder.
  • An even number favors symmetry of the antenna source.
  • the even number then favors the introduction of the plate of the septum polarizer which in this case is attached to two opposite ribs and makes it possible to simplify the dimensioning of the septum polarizer.
  • a last section without rib can be added at the level of the exit of the horn in order to improve the efficiency and the directivity of the latter (these two notions are well known of a person skilled in the art).
  • the horn has a complementary part, for example in the shape of a cone or a truncated pyramid, at the outlet of said horn, this complementary part does not have a rib.
  • the figure 4A (3D view in the input-output direction of the polarizer), 4B (3D view in the output-input direction of the polarizer) and 4C (side view) represent a hexagonal polarizer according to the first variant of the invention, which corresponds to the polarizer hexagonal figures 1A, 1B , 2A and 2B .
  • the hexagonal polarizer 3 has two inputs E P1 , E P2 separated by an internal blade 30, or septum, extending along the longitudinal direction X. Transversely, the internal blade 30 extends between two radially opposite edges of the cylinder, either on a width l 30 .
  • the internal plate 30 comprises four bearings 301, 302, 303, 304 configured to transform an electromagnetic field of circular polarization at the input into an electromagnetic field of linear polarization at the output, and vice versa. But this number of stages is not limiting and may be less than four (two or three) or five or more.
  • the thicknesses e 31 and the heights h 31 of the four second ribs 31 are constant in the longitudinal direction and are substantially equal to one another.
  • the thicknesses e 32 and the heights h 32 of the two second complementary ribs 32 are constant in the longitudinal direction and are substantially equal to each other and to those of the four second ribs 31.
  • the number of bearings of the internal blade, as well as the thickness of the blade, and the dimensions of the bearings can be configured by a person skilled in the art.
  • the blade of the polarizer may also have different shapes from that shown.
  • a large number of shapes other than the stepped shape are found in the literature, shapes which can also be used within the scope of the invention. Mention may be made, for example, of a blade whose shape has been approximated by a mathematical equation of the Legendre polynomial type. Any other form adapted to the function of transforming an electromagnetic field of linear polarization into an electromagnetic field of circular polarization, and vice versa can be envisaged.
  • there is a very large number of possible configurations which cannot all be described in the present description.
  • the thickness e 30 of the internal blade 30 is substantially equal to the thickness e 31 , e 32 of the second ribs 31, 32. This makes it possible to facilitate the design and the manufacture of the antenna source, and to the array antenna, and to promote the symmetry of the whole.
  • the thickness e 31 , e 32 (and/or the height h 31 , h 32 ) of the second ribs 31, 32 is substantially equal to the thickness e 211 (and/or the height h 211 ) of the first ribs 21 (first step 211) at the entrance of the horn.
  • the second ribs 31 can thus be positioned in the continuity of the first ribs 21 at the entrance E C of the horn 2.
  • the figure 5A (3D view), 5B (side view) and 5C (another 3D view) represent a filter in detail, which corresponds to filter 40 of the figures 2A and 2B .
  • the filter is only formed on one of the inputs of the polarizer because the antenna operates in mono-polarization.
  • the filter 40 corresponds to half of the right hexagonal cylinder in the third portion 4 (the output of the filter corresponds to one of the two inputs of the polarizer).
  • the filter comprises, in continuity with one of the two inputs of the polarizer, a series 42 of four pads 421, 422, 423, 424 for frequency filtering, the pads being positioned one after the other in the longitudinal direction X and arranged on the internal plate 30 (extended between the polarizer and the third portion). Filter pads are chosen to allow certain frequencies to pass while other frequencies are retained.
  • the various studs have dimensions (lengths, thicknesses and/or heights) which may differ from one stud to another. Furthermore, the distances between two adjacent plots may differ.
  • the second and third studs 422, 423 have equivalent dimensions (thickness e 422 , height h 422 , length L 422 ), and the first and fourth studs 421, 424 also have equivalent dimensions (thickness e 421 , height h 421 , length L 421 ) but different from the second and third studs.
  • the four studs are spaced apart by distances which are not necessarily equal.
  • the number of studs illustrated is not limiting, the same applies to the dimensions of the studs as well as the distances between the adjacent studs.
  • the dimensions of the pads as well as the distance between two adjacent pads are defined to make it possible to produce a filter of the “combline filter” type of the low-pass filter type, the shape of which can be adapted in order to integrate it into the ridged waveguide.
  • the dimensions and the number of pads depend on the value desired for the rejection of the filter. If we want to increase the level of rejection, we increase the number of studs.
  • the third portion 4 further comprises third ribs 41 extending inwards and over all or part of the length of said third portion, said third ribs being in the continuity of the second ribs 31, 32. These third ribs are dimensioned in such a way that the wave can propagate in the waveguide.
  • the shape of the polarizer being very variable, and depending on the shape of the horn (cylinder with a circular or polygonal base, etc.), it is possible to have a wide variety of shapes for the ribbed waveguide forming the filter. Possible, non-limiting forms are illustrated in the figure 11 (shown with the ribs but without the studs).
  • the transition can be made by removing ribs ( Figure 12A ), adding ribs ( figure 12B ), or by bending existing ribs ( figure 12C ), or even by combining several of these solutions.
  • the figures 6A (3D view) and 6B (side view) show a hexagonal horn 2' according to a second variant of the invention, which differs from the first variant in that the first ribs 21' are not arranged at the edges of the cylinder hexagonal 10 but in the middle of the side surfaces 10B of said cylinder.
  • first ribs and steps are not limiting. Preferably there is an even number of first ribs, both at the entrance and at the exit of the horn.
  • the figure 7A (3D view in the input-output direction of the polarizer), 7B (3D view in the output-input direction of the polarizer) and 7C (side view) represent a 3' hexagonal polarizer according to the second variant of the invention, which differs of the first variant in that the second ribs 31', 32' as well as the inner blade 30 are not arranged at the edges of the hexagonal cylinder but in the middle of the side surfaces of said cylinder.
  • the first and second variants can be combined with each other, so that the first ribs (and the second ribs) can be arranged both at the edges of the hexagonal cylinder and in the middle of the side surfaces of said cylinder. It is thus possible to obtain, for example, 12 first ribs in the horn and 12 second ribs at the output in the polarizer.
  • the second ribs are generally arranged at the same locations over the entire length occupied by said second ribs.
  • the first ribs may be disposed at the same locations over the entire length occupied by the first ribs, as illustrated.
  • the first ribs can be positioned according to a first configuration over a first length (or first section), then according to a second configuration over a second length (or second section), then possibly again according to a third configuration over a third length (or third section) etc. It is however important to respect the impedance steps and to respect the best possible symmetry of the horn (and of the antenna source) with respect to the longitudinal axis X.
  • figure 8 represents a horn 3'" in which first ribs 21 (configured in a single step) are positioned on the edges of a right hexagonal cylinder at the entry E C of the horn on a first section L1 then first ribs 21' (configured in three steps) are positioned in the middle of the side surfaces of the hexagonal cylinder on a second section L2 which can go as far as the exit S C of the horn
  • first ribs 21 (configured in a single step) are positioned on the edges of a right hexagonal cylinder at the entry E C of the horn on a first section L1 then first ribs 21' (configured in three steps) are positioned in the middle of the side surfaces of the hexagonal cylinder on a second section L2 which can go as far as the exit S C of the horn
  • This configuration is obviously not limiting.
  • the second ribs at the output of the polarizer are positioned in continuity with the first ribs at the input of the horn.
  • it is possible to envisage a change in the location of the ribs between the exit of the polarizer and the entry of the horn for example at the level of the edges in polarizer then on the middle of the surfaces in horn or vice versa, always in the limit of compliance with the desired impedances.
  • the figure 9A (3D view) and 9B (side view) represent a 2" horn according to a fourth variant of the invention, which differs from the first, the second variant and the third variant in that the straight cylinder 10' is circular and no hexagonal.
  • the first ribs 21" are positioned evenly around the circle. In the example shown, there are six first ribs 21" with three steps each. But the number of ribs and steps is not limiting. Preferably there is an even number of first ribs, both at the entrance and at the exit of the horn.
  • the figure 10A (3D view in the input-output direction of the polarizer), 10B (3D view in the output-input direction of the polarizer) and 10C (side view) represent a 3" polarizer according to the fourth variant of the invention, which differs of the first, the second variant and the third variant in that the right cylinder 10' is circular and not hexagonal.
  • the second ribs 31", 32" and the internal blade 30" are positioned evenly around the perimeter of the circle.
  • the number of ribs is not limiting, preferably there is a number pair of second ribs, both at the input and at the output of the polarizer.
  • the shape of the right cylinder is not limited to the hexagonal or circular shape.
  • the shape of the right cylinder can be square, octagonal, decagonal, and more generally in the shape of a regular polygon of even order (even number of sides), in order to present the most symmetrical shape possible.
  • the ribs must be positioned symmetrically around the perimeter of the cylinder.
  • first ribs indicated above is given for the entry and the exit of the horn.
  • the number of second ribs indicated above corresponds to the number of ribs at the output of the latter (at the input of polarizer there are two less corresponding to the blade).
  • the ribs (and the inner blade) can be positioned at the interior edges and/or on the interior side surfaces of the polygon, preferably in the middle of the interior side surfaces of the polygon.
  • the ribs (and the internal blade) are also regularly distributed around the perimeter of the circle, inside said circular cylinder.
  • the number of first ribs, second ribs, or even third ribs when there is a filter, can be 4, 6, 8, 10...
  • first ribs at the input and output of the horn there are preferably 6 first ribs at the input and output of the horn, 6 second ribs at the output of the polarizer (corresponding to the input of the horn), 4 second ribs at the input of the polarizer, and 4 third ribs at the input and output of the filter, if applicable.
  • the number of first ribs, as well as second ribs, or even third ribs when there is a filter is preferably an even number, preferably at the input and at the output of the horn, of the polarizer, and of the filter if applicable.
  • the shape of the horn conditions the shape of the polarizer.
  • the polarizer is too.
  • the outer shape of the third portion which includes the filter respects the outer shape of the horn and of the polarizer.
  • the figure 13 shows in 3D view (seen from the exit of the horns) a radiating panel 110 for an array antenna, comprising a plurality of sources according to the invention.
  • the sources 1 all have the shape of a straight hexagonal cylinder 10, the first ribs 21' being on the middle of the side surfaces of said cylinder.
  • the radiant panel shown is in one piece.
  • the number of sources represented here is 37 but it is not nothing limiting, and it is usually much higher.
  • the sources can be chosen according to any one of the modes, variants, alternatives described above.
  • the sources of the same radiating panel are all substantially identical.
  • the structure of the radiant panel being complex, and the sources having small dimensions (of the order of 10 cm in height, 15 cm in width and 20 cm in length), a preferred solution for manufacturing the radiant panel is additive manufacturing.
  • SLM selective laser melting technique
  • LBM selective Laser Melting
  • the SLM technique consists of depositing a layer of metallic powder of controlled thickness (and generally under controlled atmosphere) on a manufacturing plate, using a laser source to achieve a selective melting of the powder in the manufacturing plane, then depositing another layer of powder on the previous layer, the manufacturing iteration continuing so as to form the desired part. Titanium or aluminum metal powder can be used, although this is not limiting.
  • the SLM technique allows the manufacture of complex parts, while reducing manufacturing time and costs.
  • Such a radiant panel with a plurality of sources is not feasible with certain conventional manufacturing methods (of the milling type, etc.) or involves a complex, long and high manufacturing cost manufacturing process with other manufacturing methods.
  • conventional electro-erosion type, etc.
  • an additive manufacturing technique based on the use of polymers for example the additive manufacturing technique by material extrusion (“Material Extrusion” also called “Fused Deposition Modeling” or “FDM” in English) in which at least one heated printhead extrudes a polymer matrix filament so as to manufacture a part; the movement of the print head along the three axes makes it possible to deposit small volumes of molten polymer locally and to build a part layer by layer. Mention may also be made of additive manufacturing by material jetting, which is a process in which at least one printing head movable along the three axes projects a photosensitive polymer, which plays the role of an ink , which is then polymerized by UV radiation. Other techniques exist which are not cited here but which are well known to those skilled in the art. Whatever the additive manufacturing technique based on the use of polymers, the part produced must be metallized (deposition of a layer of metallization).
  • a metallization layer is preferably produced on the part.
  • the metallization layer can be produced using electrolytic deposition or chemical deposition, for example depending on the shape of the part and/or the intended field of use.
  • the studs 421, 422, 423 of the filters 4 can have an inclination (maximum inclination of 45°), as illustrated in the figure 14A (filter 4' comprising pads 421', 422', 423' without inclination) and 14B (filter 4 with inclination).
  • a solution for manufacturing a radiant panel is the die casting technique.
  • Die Casting is a metal casting process characterized by forcing molten metal under high pressure into a mold cavity.
  • the mold cavity is created using two hardened steel dies that have been machined into shape and function similar to an injection mold during the process.
  • Most of the castings under pressure are made from non-ferrous metals, particularly zinc, copper, aluminum, magnesium, lead, tin and tin-based alloys.
  • a hot or cold chamber machine is used.
  • the figure 16 diagrams a functional architecture of an array antenna 100 with direct radiation which comprises a radiating panel 110 comprising several sources 1' (each source 1' is represented with a horn 2, a polarizer 3 and a filter 4), such as the radiating panel illustrated in the figure 13 .
  • the radiating panel 110 is connected to amplifiers 120 and/or loads 121.
  • the assembly is connected to a network trainer 140 or "BFN" for "Beam Forming Network" which makes it possible to distribute the energy (in amplitude and in phase) between the different sources to direct the antenna beam in a given direction.
  • a load absorbs the RF energy it receives and dissipates it as heat.
  • the figure 17 and 18 illustrate a radiant panel 110, such as the radiant panel shown in figure 13 (with more sources), seen from the filter input.
  • the radiant panel shown has 256 radiant elements. It therefore has 512 ports at the input of the septum polarizers.
  • access E P1 see identification for example in figure 4A
  • access E P2 see location for example in figure 4A
  • PCD right circular polarization
  • antenna is generally designed to operate in mono-polarization and for the case presented in this example in right-hand polarization.
  • the right polarization is called “main polarization” and the left polarization “crossed polarization”.
  • the 256 accesses E P2 are monitored by filters then they must be connected to the amplifiers to generate the signal.
  • the 256 E P1 accesses are not monitored by filters and must be connected to loads to limit the cross component which corresponds to noise.
  • connection 131 the figure 17 illustrates a first solution (connection 131), the second solution being illustrated in figure 18 (connection 132).
  • the first connection mode 131 illustrated in figure 17 uses a few cross-polarization accesses (E P1 access of the polarizers in the case considered) which are filled with material to be able to have a tapping in order to connect the amplifiers to the radiating panels with screws.
  • the second connection mode 132 illustrated in figure 18 uses the 2 accesses of the same source (access E P1 and E P2 of the polarizers in the case considered) which are filled with material to be able to have a tapping in order to connect the amplifiers to the radiating panels with screws.
  • the 256 accesses E P1 are monitored by filters then connected to the amplifiers and the 256 accesses E P2 are not monitored by filters and are connected to loads.
  • the amplifiers are preferably grouped together in block(s) of several amplifiers, a block which can be referred to as an “amplification module”.
  • the connection of the amplification modules to the radiating panel is therefore done via the intermediary of fixings which are fixed at the level of the connections made, for example screws which are screwed into the tappings of the connections. Connections can be made at the time of manufacture of the radiant panel (for example during additive manufacturing) or after manufacture (for example by tapping once the radiant panel has been manufactured).
  • the first connection mode makes it possible not to degrade the RF performance too much compared to the second connection mode but requires having more compact amplification modules.
  • the second connection mode is easier to achieve.
  • the number of amplifiers in an amplification module depends on several parameters and objectives: it may be to facilitate the production and assembly of the antenna in order to reduce the cost of the antenna, or to target RF performance for the antenna (the greater the number of short circuits, the more the RF performance is degraded), or to integrate thermal control (the aim of the thermal control being to evacuate the power dissipated by the amplifiers out of the antenna).
  • microwaves in the amplifiers and in the radiating panel are different. Indeed, the waves at the output of the radiating panel are transmitted via a waveguide (ridged) while the waves in the amplifier are generally propagated using a line called "microstrip line”. or “microstrip line” which is a microwave transmission line known to those skilled in the art and will not be developed here.
  • the transition from the HF wave propagation mode to a ridged waveguide from the radiating panel to the microstrip line of the amplifiers must be carried out via an appropriate transition.
  • the so-called “Vivaldi” antipodal transition makes it possible to make a transition between a waveguide and a microstrip line, but it is generally implemented for a conventional, non-ridged waveguide. Its principle illustrated in figures 19A and 19B .
  • a so-called “Vivaldi” antipodal transition 50 consists of the insertion of a substrate 51 inside the waveguide 55 (generally in the middle of the waveguide).
  • a first etching 51 on its upper face (its end furthest from the waveguide inlet is refined in the form of a conductive strip 51 A) and a second etching 52 on its underside (its end furthest from the waveguide entrance is widened to become ground plane 52A).
  • the electric field E arrives at the level of the etched substrate which captures the electric field, then comprised between the two metal etchings.
  • the shape of the metal engravings makes it possible to rotate the electric field, and to transmit it to the conductive strip.
  • the inventors have developed a new transition based on the Vivaldi antipodal transition.
  • the principle is to produce a preliminary transition piece making it possible to change the position, the dimensions and/or the shapes of the ribs of the waveguide at the input of the source (at the input of the polarizer or filter) to free up space for the center of it.
  • An exemplary embodiment of such a prior transition 60 is illustrated in Figures 20A, 20B and 20C .
  • the figure 20A represents a side view of the output 60A of the transition (for example at the input of the filter) where the ribs 41 of the filter 4 appear.
  • figure 20B shows in side view the input 60B of the transition/adaptation (amplifier side).
  • the Fig. 20C represents in 3D view the transition/adaptation 60 in the continuity of the filter.
  • the loads can be connected to the radiant panels in the same way.
  • the loads are in fact generally integrated in the amplification module and can be connected in the same way as the amplifiers to the radiant panel, with the same guide transition/adaptation and the same Vivaldi transition.
  • the load can be connected at the end of the microstrip line as a surface mount device (SMD).
  • SMD surface mount device
  • the antenna source, the radiating panel and the array antenna can thus include one or more of the characteristics listed above taken in isolation or in any possible technical combination.
  • the invention finds applications in the field of spatial network antennas for satellites in low orbit where data must be transmitted in a large angular domain, in particular in the K, Ka, Ku, Q, V bands, etc. example for broadband internet.

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  • Waveguide Aerials (AREA)
  • Variable-Direction Aerials And Aerial Arrays (AREA)
EP21213068.6A 2020-12-10 2021-12-08 Antennenquelle für eine direkt strahlende gruppenantenne, strahlplatte und antenne mit mehreren antennenquellen Active EP4012834B1 (de)

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FR2012951A FR3117685B1 (fr) 2020-12-10 2020-12-10 Source d'antenne pour une antenne réseau à rayonnement direct, panneau rayonnant comprenant plusieurs sources d'antenne.

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EP3561947A1 (de) * 2018-04-25 2019-10-30 Rosenberger Hochfrequenztechnik GmbH & Co. KG Polarisator für einen wellenleiter und system zur übertragung von hochfrequenten elektromagnetischen signalen
US11881607B1 (en) * 2021-10-05 2024-01-23 Lockheed Martin Corporation Longitudinally ridged septum orthomode transducer polarizer
KR102510434B1 (ko) * 2022-08-17 2023-03-16 국방과학연구소 안테나 장치

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Publication number Priority date Publication date Assignee Title
DE3445399A1 (de) * 1984-12-13 1986-06-19 Wilhelm Sihn jun. KG, 7532 Niefern-Öschelbronn Septum-polarisationsweiche
EP2497146A1 (de) * 2009-11-04 2012-09-12 Raytheon Company Verlustarme planare breitband-übertragungsleitung zu wellenleiterübergang
WO2020194270A1 (fr) * 2019-03-28 2020-10-01 Swissto12 Sa Composant radiofréquence comportant plusieurs dispositifs à guide d'onde muni de stries

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Publication number Priority date Publication date Assignee Title
CH668507A5 (de) * 1984-10-10 1988-12-30 Huber+Suhner Ag Hohlleiter mit einem strahler.
JP3692273B2 (ja) * 2000-02-03 2005-09-07 アルプス電気株式会社 一次放射器

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Publication number Priority date Publication date Assignee Title
DE3445399A1 (de) * 1984-12-13 1986-06-19 Wilhelm Sihn jun. KG, 7532 Niefern-Öschelbronn Septum-polarisationsweiche
EP2497146A1 (de) * 2009-11-04 2012-09-12 Raytheon Company Verlustarme planare breitband-übertragungsleitung zu wellenleiterübergang
WO2020194270A1 (fr) * 2019-03-28 2020-10-01 Swissto12 Sa Composant radiofréquence comportant plusieurs dispositifs à guide d'onde muni de stries

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WEN-JUAN YE, A COMPACTED DUAL LINEARLY POLARIZATION WIDEBAND FEED FOR PARABOLIC REFLECTOR ANTENNA

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CA3141535A1 (en) 2022-06-10
FR3117685A1 (fr) 2022-06-17
US20220190477A1 (en) 2022-06-16
FR3117685B1 (fr) 2024-03-15
EP4012834C0 (de) 2024-02-21

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