EP3804034A1 - Module radiofréquence - Google Patents
Module radiofréquenceInfo
- Publication number
- EP3804034A1 EP3804034A1 EP18834018.6A EP18834018A EP3804034A1 EP 3804034 A1 EP3804034 A1 EP 3804034A1 EP 18834018 A EP18834018 A EP 18834018A EP 3804034 A1 EP3804034 A1 EP 3804034A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- layer
- waveguides
- module according
- radio frequency
- different
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
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Classifications
-
- 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
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q21/00—Antenna arrays or systems
- H01Q21/0006—Particular feeding systems
- H01Q21/0037—Particular feeding systems linear waveguide fed arrays
- H01Q21/0043—Slotted waveguides
- H01Q21/005—Slotted waveguides arrays
-
- 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
- H01Q13/02—Waveguide horns
- H01Q13/0275—Ridged horns
-
- 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
- H01Q15/00—Devices for reflection, refraction, diffraction or polarisation of waves radiated from an antenna, e.g. quasi-optical devices
- H01Q15/24—Polarising devices; Polarisation filters
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q21/00—Antenna arrays or systems
- H01Q21/0006—Particular feeding systems
Definitions
- the present invention relates to a radio frequency (RF) module intended to form the passive part of a direct radiation antenna (DRA, Direct Radiating Array).
- RF radio frequency
- Antennas are elements which serve to emit electromagnetic signals in the free space, or to receive such signals.
- Simple antennas, such as dipoles, have limited performance in terms of gain and directivity.
- Satellite dishes provide higher directivity, but are cumbersome and cumbersome, making them unsuitable for use in applications such as satellites, for example, when weight and volume need to be reduced.
- DRA antenna arrays are also known which combine several radiating elements (elementary antennas) out of phase in order to improve gain and directivity.
- the signals received on the different radiant elements, or emitted by these elements, are amplified with variable gains and out of phase with each other in order to control the shape of the receiving and transmitting lobes of the network.
- the different radiant elements are each connected to a waveguide which transmits the received signal towards the electronic modules.
- each radiant element may further be separated according to their polarization by means of a polarizer.
- the size of the polarizers and electronics most often determines the minimum pitch between the different radiant elements of a network.
- the important step that results generates side lobes emission respectively undesirable reception.
- radiofrequency modules require on the contrary to further space the radiant elements, for example to provide them with a transmission cone.
- An object of the present invention is therefore to propose a passive radio frequency module, intended to form the passive part of a direct radiation network DRA, which is free or minimizing the limitations of known devices.
- a first layer comprising an array of radiant elements, each radiant element having a section for supporting at least one wave propagation mode
- a second layer forming an array of waveguides; a fourth layer forming a network of ports; the second layer being interposed between the first layer and the fourth layer;
- each waveguide being adapted to transmit in one direction or the other a radiofrequency signal between a port of the fourth layer and a radiant element
- the surface of the first layer being different from the surface of the fourth layer
- the waveguides approaching each other between the fourth layer and the first layer or between the first layer and the fourth layer.
- radio frequency module comprising:
- a first layer comprising an array of radiant elements, each radiant element having a section for supporting at least one wave propagation mode, each section being provided with at least one stripe parallel to the direction of propagation of the signal;
- a second layer forming an array of waveguides; a fourth layer forming a network of ports; the second layer being interposed between the first layer and the fourth layer;
- each waveguide being adapted to transmit in one direction or the other a radiofrequency signal between a port of the fourth layer and a radiant element
- the surface of the first layer being smaller than the surface of the fourth layer; the waveguides approaching each other between the fourth layer and the first layer.
- the waveguides thus have a dual function; they make it possible, on the one hand, to transmit the signals between the ports of the fourth layer and the radiant elements of the first layer, and on the other hand to independently choose the pitch of the radiant elements and the pitch of the ports of the fourth layer.
- the waveguides approach each other between the fourth layer and the first layer, in a convergent manner.
- the surface of the first layer is then smaller than the surface of the fourth layer.
- the pitch (p 1) between two radiant elements of the first layer is preferably less than 1 2, 1 being the wavelength at the maximum operating frequency.
- Fourth layer towards the radiant elements also allows to space the ports of the fourth layer.
- the important step between the ports makes it possible, for example, to have the amplification and phase shift electronic circuit feeding each port in the immediate vicinity of each port, reducing the constraints on the dimensions of this circuit.
- This important step also makes it possible to have, if necessary, polarizers of sufficient size near each port, to effect effective separation of the signals according to their polarization.
- the surface of the first layer is larger than the surface of the fourth layer. The waveguides then move away from each other between the fourth layer and the first layer. This embodiment makes it possible to use radiant elements of relatively large size, without requiring a layer of large ports.
- the arrangement of the radiant elements of the first layer may be different from the layout of the ports of the fourth layer.
- the radiant elements of the first layer may be arranged according to a rectangular matrix MxN while the ports of the fourth layer are arranged in a rectangular matrix KxL, M being different from K and N being different from L.
- This different arrangement may also involve different shapes, for example a rectangle layout on one of the layers and in a circle, oval, cross, hollow rectangle, polygon, etc. on the other layer.
- the radiofrequency module may comprise a third layer interposed between the second layer and the fourth layer.
- the elements of the third layer can perform a transformation of the signal.
- the third layer may also comprise an array of elements realizing a sectional adaptation between the section of the output of the ports of the fourth layer and the section of different shape of the waveguides.
- a third layer of this type may in particular be provided when only the ports or only the waveguides are striated.
- the third layer interposed between the second layer and the fourth layer may also include a network of polarizers as elements.
- the radiofrequency module may include external polarizers just after the radiant elements in the air.
- the third layer interposed between the second layer and the fourth layer may comprise a filter.
- Each radiant element of the first layer may be provided with at least one streak parallel to the direction of propagation of the signal.
- the radiant elements of the first layer may also be unstriated and constituted by open waveguides or square horns, circular, pyramidal, spline-shaped.
- the radiant elements may have an outer square, rectangular, or preferably hexagonal, circular or oval
- the pitch (p1) between two radiant elements can be variable within the module.
- the radiofrequency module may comprise waveguides having a square, rectangular, round, oval, or hexagonal cross section whose internal faces are provided with at least one stripe extending longitudinally along each inner face of the waveguides.
- Each waveguide of the second layer is preferably designed to transmit either only a fundamental mode or a fundamental mode and a single degenerate mode.
- the length of the different waveguides of the second layer is advantageously identical.
- the length of the different waveguides of the second layer may also be variable; in this case, it is preferable to use isophase waveguides at the wavelength considered, that is to say waveguides all producing an identical phase shift.
- the different waveguides have different lengths and different sections so as to compensate for the phase variation produced by the different lengths.
- the different waveguides are preferably isophases, that is to say that the phase shifts through the different waveguides are identical.
- the channel of different waveguides is preferably non-rectilinear.
- the waveguides of the second layer are preferably curved.
- the curvature of the different waveguides of the second layer may be variable.
- peripheral waveguides may be more curved than waveguides in the center.
- the ports of the fourth layer may constitute the inputs of a polarizer.
- a first end of all the waveguides may be in a first plane, while a second end of all the waveguides is in a second plane.
- the additive manufacturing makes it possible, in particular, to produce waveguides of complex shape, in particular curved waveguides. and converging into a funnel between the layer of radiant elements and the polarizer layer.
- additive manufacturing is meant any process of
- curing or coagulation of liquid or powder including, but not limited to, methods based on ink jetting (Binder jetting), DED (Direct Energy Deposition), EBFF (Electron beam freeform fabrication), FDM (fused deposition modeling), PFF (plastic freeforming), aerosol, BPM (ballistic particle manufacturing), powder bed, SLS (Selective Laser Sintering), ALM (additive Layer Manufacturing), polyjet, EBM (electron beam melting), photopolymerization, etc.
- ink jetting Binder jetting
- DED Direct Energy Deposition
- EBFF Electro Beam Form fabrication
- FDM fused deposition modeling
- PFF plastic freeforming
- aerosol aerosol
- BPM ballistic particle manufacturing
- SLS Selective Laser Sintering
- ALM additive Layer Manufacturing
- polyjet EBM (electron beam melting), photopolymerization, etc.
- EBM electron beam melting
- the module is preferably monolithic.
- a monolithic manufacture of the module reduces costs, eliminating the need for assembly. It also makes it possible to guarantee precise relative positioning of the various components.
- the invention also relates to a module comprising the above elements and an electronic circuit with amplifiers and / or phase shifters linked to each port.
- FIG. 1 illustrates a schematic side view of the different layers of a module according to the invention.
- FIG. 2 illustrates two examples of embodiments of the third layer, in which each element of this layer comprises either one or two inputs on the fourth layer side.
- FIG. 3A illustrates a perspective view of the second and third layers of an exemplary module according to the invention.
- FIG. 3B illustrates a front view of the second and third layers of an exemplary module according to the invention, seen from the third layer.
- FIG. 3C illustrates a front view of the second and third layers of an exemplary module according to the invention, seen from the side corresponding to the first layer.
- FIG. 4 illustrates a perspective view of an example of a first layer of a module according to the invention.
- FIGS. 5A to 5C illustrate three examples of radiant elements that can be used in the first layer of a module according to the invention.
- FIG. 6 illustrates a front view of another example of a first layer of a module according to a second embodiment of the invention.
- FIG. 7 illustrates a perspective view of a module comprising a set of convergent waveguides in the direction of the radiant elements of the first layer according to a third embodiment of the invention.
- FIG. 8 illustrates a view from the fourth layer of the module according to the third embodiment of the invention.
- FIG. 9 illustrates a side view of the module according to the third embodiment of the invention.
- FIG. 10 illustrates another side view of the module according to the third embodiment of the invention.
- FIG. 11 illustrates a perspective view of a module comprising a set of diverging waveguides in the direction of the radiant elements of the first layer, according to a fourth embodiment of the invention.
- FIG. 12 illustrates a side view of the module according to the fourth embodiment of the invention.
- FIG. 1 illustrates a passive radio frequency module 1 according to a first embodiment of the invention, intended to form the passive part of a direct radiation network DRA.
- the radiofrequency module 1 comprises four layers 3, 4, 5, 6.
- the first layer 3 comprises a two-dimensional network of N radiant elements 30 (antennas) for emitting electromagnetic signals into the ether, respectively to receive the received signals.
- the second layer 4 comprises a network of waveguides 40.
- the third layer 5 is optional; it may also be integrated in the layer 4.
- the third layer 5 comprises an array of elements 50, for example polarizers or section adapters.
- the fourth layer 6 comprises a two-dimensional network, for example a rectangular matrix, with N waveguide ports 60.
- Each port 60 forms an interface with an active element of the DRA such as an amplifier and / or a phase-shifter, forming part of a beamforming network.
- a port thus makes it possible to connect a waveguide to an electronic circuit, in order to inject a signal into the waveguides or in the opposite direction to receive the electromagnetic signals in the waveguides.
- This module 1 is intended to be used in a multibeam environment.
- the radiant elements 30 are preferably brought closer to one another so that the pitch p1 between two adjacent radiating elements is smaller than the wavelength at the nominal frequency at which the module 1 is intended to be used. This reduces the amplitude of the secondary transmit and receive lobes.
- FIGS. 3A to 3C illustrate different views of an exemplary module according to a first embodiment of the invention, without the third and fourth layer.
- the waveguides 40 and the radiant elements 30 have a square section provided with four striations disposed symmetrically on the internal flanks.
- the waveguides are convergent towards the first layer 3.
- FIGS. 7 to 10 illustrate other views of an example of a module similar to that of FIGS. 3A to 3C, but in which the guides of FIG. Wave 40 and the radiant elements 30 have a rectangular section provided with two grooves disposed in the middle of the long sides of the internal flanks.
- the waveguides are also convergent towards the first layer 3. In these embodiments of FIGS.
- the distance between two adjacent ports 60 of the fourth layer 6 is preferably more large than the wavelength at the nominal frequency at which the module 1 is intended to be used. This arrangement makes it possible to bring the radiant elements 30 closer to each other, in order to reduce the unwanted side lobes in reception and in transmission, while spacing the ports 60 of the fourth layer 6, in order to facilitate the connection to the active electronic elements for transmitting or receive a signal in each waveguide.
- the first layer 3 comprising an array of radiant elements 30 thus has a surface, in a plane perpendicular to the direction of propagation of the signal, smaller than the fourth layer 6 with the network of ports 60.
- the pitch p1 between two corresponding points of two adjacent radiant elements 30 is therefore smaller than the pitch p2 between two corresponding points of two adjacent ports 60.
- the pitch p1 between adjacent elements may be identical in the two orthogonal directions, or different.
- the pitch p2 between adjacent elements can be identical in both directions
- Figures 11 to 12 illustrate another embodiment of a module according to the invention, wherein the waveguides 40 are divergent towards the radiant elements 30.
- the surface of the first layer 3 is thus more large than the surface of the fourth layer 6, and the pitch p1 between the radiant elements 30 of the first layer 3 is greater than the pitch p2 between the ports of the fourth layer 6.
- This arrangement makes it possible to produce a module with radiant elements 30 of large size, for example horn, without increasing the size of the ports 60 and the network of active elements (not shown) connected to these ports.
- Figures 3A to 3C and 7 to 12 illustrate waveguides 40 which are separated from each other.
- these waveguides are linked to one another so as to maintain their relative positioning and to form a preferably monolithic set.
- the link between the waveguides can be established for example by the first layer 3, by the third layer 5 and / or by the fourth layer 6. It is also possible to produce bridging elements between different guides. wave.
- FIG. 4 An example of an array of radiant elements 30 in the layer 3 is illustrated in FIG. 4.
- the N radiant elements 30 are arranged in a rectangular matrix, here a square matrix.
- the section of each radiating element 30 is square and provided with a ridge 300 on each inner edge, the arrangement of the striations being symmetrical.
- the adjacent radiant elements share a common lateral edge, allowing them to be brought closer together.
- the phase and the amplitude of each radiant element of the first layer 3 make it possible to obtain high insulation between the different beams. Radiant elements smaller than the wavelength reduce the impact of sidelobes in the area covered.
- FIG. 6 illustrates another example of a first layer 3 of radiant elements consisting of lines of radiant elements 30 with a number of radiant elements varies according to the lines, the general shape of the layer forming an octagon.
- the value of the phase shift may be less than the pitch p1 between two adjacent elements 30 on the same line.
- a first layer 3 of any polygonal shape, or substantially circular can also be performed.
- the radiant elements 30 may also be arranged in a triangle, in a rectangle, or in a diamond, with aligned or out of phase lines.
- the elements 30 are preferably constituted by waveguides whose internal cavity is provided with streaks 300, for example two or four streaks 300 distributed. at equal angular distances.
- FIG. 5A illustrates an exemplary radiating element with a square cross section with four ridges, called "quad-ridge square”.
- FIG. 5B illustrates an example of a cross sectional radiant element
- FIG. 5C illustrates an exemplary radiating element with a circular cross-section with four ridges, called “quad-ridge circular". The design of the radiant elements illustrated with such streaks makes it possible to produce radiant elements with dimensions smaller than the wavelength of the signal to be transmitted or received.
- radiant elements supporting at least one propagation mode may be implemented, including rectangular shapes, circular or rounded, striated or not. Streaks can be 2, 3 or 4.
- the radiant elements 30 may be single-polarization or double-polarization.
- the polarization can be linear, inclined or circular.
- the pitch p1 between two radiant elements 30 of the first layer 3 is preferably less than or equal to 1/2, 1 being the wavelength at the maximum frequency for which the module is provided.
- the radiant elements may include polarizers not shown, for example at the junction with the second layer 4.
- polarizers are provided just after the free air portion in which the emitted signal is canceled.
- polarizers can also be provided in the
- the second layer 4 comprises N waveguides 40.
- Each waveguide 40 transmits a signal from a port 60 and / or an element of the third layer 5 to a corresponding radiating element 30 in transmission, and vice versa. versa in reception.
- the waveguides 40 furthermore convert between the arrangement of the elements 60 on the layers 5 and 6 and the arrangement different from the first layer of radiant elements 3.
- the waveguides 40 preferably have a cross section of substantially constant shape and size.
- the waveguides 40 are preferably curved so as to make the transition between the surface of the third or fourth layer 5 and the different surface of the first layer 3 of radiant elements.
- the waveguides thus form a funnel volume.
- the waveguides converge towards the first layer 3.
- the second layer 4 can not only allow to adapt the pitch between adjacent elements; in one embodiment, it may also be made to make a transition between the arrangement of the radiant elements 30 of the first layer 3 and a different arrangement of the ports 60 of the fourth layer 6.
- the second layer 4 may transition between a network of elements or ports arranged in a rectangular matrix and an array of elements or ports arranged in a different matrix, or polygon, or circle.
- At least some waveguides 40 are curved, as can be seen for example in FIGS. 3A, 7 and 11.
- at least some waveguides are curved in two planes perpendicular to each other and parallel to each other.
- the longitudinal axis d of the module as seen in particular in Figures 9 and 10 (first embodiment) and 12 (second embodiment). These waveguides 40 are thus bent at S in two orthogonal planes and parallel to the main direction of transmission of the signal.
- connection plane between the waveguides 40 and the radiant elements 30 on one side, and the connection plane between the waveguides 40 and the elements 50 on the other side, are preferably parallel between them and perpendicular to the main direction of transmission of the signal.
- the waveguides 40 at the periphery of the second layer 4 are curved more than those near the center, and longer.
- the waveguides 40 near the center may be rectilinear.
- the dimensions of the internal channel through the waveguides 40 and those of the layer 41, as well as their shapes, are determined as a function of the operational frequency of the module, that is to say the frequency of the signal electromagnetic system for which the module 1 is manufactured and for which a stable transmission mode and optionally with a minimum of attenuation is obtained.
- the different waveguides 40 in the second layer 4 have different lengths and curvatures, which influence their frequency response curve. These differences can be compensated by the electronics supplying each port 60 or processing the received signals. Preferably, these differences are however at least partially compensated by adapting the section of the different waveguides 40, which then have shapes and / or different dimensions between them.
- the length of the different waveguides 40 of the second layer is advantageously identical, which makes it possible to ensure an identical phase shift of the signals crossing the different waveguides, and thus to maintain their relative offset.
- the length of the different waveguides 40 may be different; in this case, it is preferable to use isophase waveguides at the wavelength considered, that is to say waveguides all producing an identical phase shift.
- the different waveguides have different lengths and different sections so as to compensate for the phase variation produced by the different lengths. It is also possible to use waveguides of different length, and / or producing different phase shifts, and to exploit or compensate for these phase shifts with the active phase shifting electronic circuits network, in order to control the relative phase shift between radiant elements, and for example to control the beamforming.
- the second layer 4 may also, according to the embodiments, include other waveguide elements such as filters,
- Each waveguide 40 may be intended to transmit a single-polarization or dual-polarization signal.
- the third layer 5 is optional and comprises elements 50.
- the elements 50 make it possible to make a transition between the cross section of the ports 60 of the fourth layer 6 and the cross section which may be different from the waveguides 40 of the second layer 4, generally corresponding to the section
- the waveguides of the third layer 5 ensure for example a transition between the square or rectangular section of the output of the ports 60 and the section of the waveguides 40 and radiant elements 30 which is provided with ridges 400 and 300, respectively.
- the elements 50 of the third layer 5 may also, according to the embodiments, perform a transformation of the signal, for example using other waveguide elements such as filters,
- the transverse surface of the third layer 5 is preferably equal to the transverse surface of the fourth layer 6.
- FIG. 2 illustrates an exemplary element 50 of the third layer 5.
- this element 50 comprises an inlet 51 connected to a port 60 and an inlet 53 connected to the input 41 of a waveguide 40.
- this element 50 has two inputs 52A, 52B, each being connected to a port 60A respectively 60B of the fourth layer, and an input 53 connected to the input 41 of
- the element 60 preferably comprises a polarizer for combining respectively separating two polarities on the ports 60A, 60B, from / to a combined signal on the waveguide 40.
- the entire module 1 is preferably made monolithically, by additive manufacturing. It is also possible to make the entire module 1 in several blocks assembled together, each block comprising the four layers 3,4, 5,6, or at least the layers 3,4 and 6. A manufacturing by subtractive machining or by assembly is also possible.
- the module is made entirely of metal, for example aluminum, by additive manufacturing.
- the module 1 comprises a core made of polymer, PEEK, metal or ceramic, and a conductive casing deposited on the faces of this core.
- the core of the module 1 may be formed of a polymer material, ceramic, a metal or an alloy, for example aluminum, titanium or steel.
- the core of the module 1 can be made by stereolithography or by selective laser melting.
- the core may comprise different assembled parts, for example glued or welded together.
- the metal layer forming the envelope can optionally include a metal selected from Cu, Au, Ag, Ni, Al, stainless steel, brass or a combination of these metals.
- the inner surface and the outer surface of the core are covered with a conductive metal layer, for example copper, silver, gold, nickel, etc. plated by chemical deposition without electrical current.
- this layer is for example between 1 and 20 microns, for example between 4 and 10 microns.
- the thickness of this conductive coating must be sufficient for the surface to be electrically conductive to the radio frequency chosen. This is typically achieved using a conductive layer whose thickness is greater than the skin depth d.
- This thickness is preferably substantially constant on all internal surfaces to obtain a finished part with precise dimensional tolerances.
- the deposition of conductive metal on the inner and possibly outer faces is done by immersing the core in a series of successive baths, typically 1 to 15 baths. Each bath involves a fluid with one or more reagents. The deposition does not require applying a current on the core to be covered. Stirring and regular deposition are obtained by stirring the fluid, for example by pumping the fluid in the transmission channel and / or around the module 1 or by vibrating the core and / or the fluid container, for example with a device vibrating ultrasound to create ultrasonic waves.
- the metallic conductive envelope can cover all the faces of the core uninterruptedly.
- the module 1 comprises lateral walls with external and internal surfaces, the internal surfaces delimiting a channel, said conductive envelope covering said internal surface but not all of the external surface.
- the module 1 may comprise a smoothing layer intended to smooth at least partially the irregularities of the surface of the core.
- the conductive envelope is deposited over the smoothing layer.
- the module 1 may comprise a fastening layer (or boot) deposited on the core so as to cover it uninterruptedly.
- the attachment layer may be of conductive or non-conductive material.
- the bonding layer makes it possible to improve the adhesion of the conductive layer to the core. Its thickness is preferably less than the roughness Ra of the core, and less than the resolution of the additive manufacturing process of the core.
- the module 1 comprises
- the bonding layer and the smoothing layer make it possible to reduce the roughness of the surface of the waveguide channel.
- the bonding layer makes it possible to improve the adhesion of the conductive or non-conductive core with the smoothing layer and the conductive layer.
- the shape of the module 1 can be determined by a computer file stored in a computer data carrier and for controlling an additive manufacturing device.
- the module may be linked to an electronic circuit, for example in the form of a printed circuit mounted behind the layer 5 of ports, with amplifiers and / or phase shifters linked to each port.
- an electronic circuit for example in the form of a printed circuit mounted behind the layer 5 of ports, with amplifiers and / or phase shifters linked to each port.
Landscapes
- Variable-Direction Aerials And Aerial Arrays (AREA)
Abstract
Description
Claims
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH6992018 | 2018-06-01 | ||
PCT/IB2018/059734 WO2019229515A1 (fr) | 2018-06-01 | 2018-12-06 | Module radiofréquence |
Publications (1)
Publication Number | Publication Date |
---|---|
EP3804034A1 true EP3804034A1 (fr) | 2021-04-14 |
Family
ID=65023945
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP18834018.6A Pending EP3804034A1 (fr) | 2018-06-01 | 2018-12-06 | Module radiofréquence |
Country Status (4)
Country | Link |
---|---|
US (2) | US11742589B2 (fr) |
EP (1) | EP3804034A1 (fr) |
IL (1) | IL278692B1 (fr) |
WO (1) | WO2019229515A1 (fr) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US11890676B2 (en) | 2021-02-15 | 2024-02-06 | Raytheon Missiles & Defense (RMD) | Waveguide fence support |
FR3128590B1 (fr) | 2021-10-27 | 2024-03-22 | Swissto12 Sa | Module radiofréquence comprenant un réseau de guides d’ondes isophases |
Family Cites Families (21)
Publication number | Priority date | Publication date | Assignee | Title |
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FR2550892B1 (fr) | 1983-08-19 | 1986-01-24 | Labo Electronique Physique | Sortie d'antenne en guide d'onde pour une antenne plane hyperfrequence a reseau d'elements rayonnants ou recepteurs et systeme d'emission ou de reception de signaux hyperfrequences comprenant une antenne plane equipee d'une telle sortie d'antenne |
US6703976B2 (en) * | 2001-11-21 | 2004-03-09 | Lockheed Martin Corporation | Scaleable antenna array architecture using standard radiating subarrays and amplifying/beamforming assemblies |
US8188932B2 (en) * | 2007-12-12 | 2012-05-29 | The Boeing Company | Phased array antenna with lattice transformation |
EP2260537B1 (fr) | 2008-03-18 | 2012-08-15 | Astrium Limited | Ensemble alimentation d'antenne |
JP4988002B2 (ja) | 2010-03-25 | 2012-08-01 | シャープ株式会社 | 無線通信装置 |
US9112279B2 (en) * | 2011-02-25 | 2015-08-18 | Honeywell International Inc. | Aperture mode filter |
US9472853B1 (en) | 2014-03-28 | 2016-10-18 | Google Inc. | Dual open-ended waveguide antenna for automotive radar |
US9711870B2 (en) | 2014-08-06 | 2017-07-18 | Waymo Llc | Folded radiation slots for short wall waveguide radiation |
US9698492B2 (en) * | 2015-01-28 | 2017-07-04 | Northrop Grumman Systems Corporation | Low-cost diplexed multiple beam integrated antenna system for LEO satellite constellation |
US9859597B2 (en) * | 2015-05-27 | 2018-01-02 | Viasat, Inc. | Partial dielectric loaded septum polarizer |
US9991607B1 (en) * | 2015-06-04 | 2018-06-05 | Rockwell Collins, Inc. | Circular array of ridged waveguide horns |
EP3311450B1 (fr) | 2015-06-18 | 2022-08-24 | VEGA Grieshaber KG | Injection par guide d'ondes pour un dispositif de balayage linéaire |
FR3048556B1 (fr) * | 2016-03-04 | 2018-03-02 | Swissto 12 Sa | Procede de fabrication additive d'un guide d'onde ainsi que dispositifs a guide d'onde fabriques selon ce procede |
US10381177B2 (en) | 2016-03-14 | 2019-08-13 | Citizen Electronics Co., Ltd. | Push switch, method of manufacturing push switch, and electronic device including push switch |
CN108475852A (zh) | 2016-03-15 | 2018-08-31 | 康普技术有限责任公司 | 具有集成极化旋转器的平板阵列天线 |
EP3460908B1 (fr) * | 2017-09-25 | 2021-07-07 | Gapwaves AB | Antenne de réseau en phase |
WO2019204782A1 (fr) | 2018-04-19 | 2019-10-24 | Metawave Corporation | Procédé et appareil pour faire rayonner des éléments d'un réseau d'antennes |
CN112236903B (zh) * | 2018-06-01 | 2024-05-10 | 瑞士十二公司 | 射频模块 |
SE1930047A1 (en) * | 2019-02-08 | 2020-06-30 | Gapwaves Ab | Antenna array based on one or more metamaterial structures |
US10897090B2 (en) | 2019-02-15 | 2021-01-19 | The Boeing Company | Electronics and filter-integrated, dual-polarized transition and radiator for phased array sensors |
CN111585050B (zh) * | 2020-05-18 | 2021-03-02 | 宁波大学 | 一种宽频带平板阵列天线 |
-
2018
- 2018-12-06 EP EP18834018.6A patent/EP3804034A1/fr active Pending
- 2018-12-06 IL IL278692A patent/IL278692B1/en unknown
- 2018-12-06 WO PCT/IB2018/059734 patent/WO2019229515A1/fr unknown
-
2022
- 2022-04-04 US US17/657,802 patent/US11742589B2/en active Active
-
2023
- 2023-07-25 US US18/358,344 patent/US20230378659A1/en active Pending
Also Published As
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US11742589B2 (en) | 2023-08-29 |
IL278692B1 (en) | 2024-05-01 |
WO2019229515A1 (fr) | 2019-12-05 |
IL278692A (en) | 2020-12-31 |
US20230378659A1 (en) | 2023-11-23 |
US20220231424A1 (en) | 2022-07-21 |
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