EP3671957A1 - Antenne à ondes de fuite - Google Patents

Antenne à ondes de fuite Download PDF

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Publication number
EP3671957A1
EP3671957A1 EP18213890.9A EP18213890A EP3671957A1 EP 3671957 A1 EP3671957 A1 EP 3671957A1 EP 18213890 A EP18213890 A EP 18213890A EP 3671957 A1 EP3671957 A1 EP 3671957A1
Authority
EP
European Patent Office
Prior art keywords
line
layer
insulating layer
leaky wave
coupling
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.)
Granted
Application number
EP18213890.9A
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German (de)
English (en)
Other versions
EP3671957B1 (fr
Inventor
Lukas Walter Mayer
Andreas Hofmann
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Siemens AG
Original Assignee
Siemens AG
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Siemens AG filed Critical Siemens AG
Priority to EP18213890.9A priority Critical patent/EP3671957B1/fr
Priority to PCT/EP2019/081649 priority patent/WO2020126254A1/fr
Publication of EP3671957A1 publication Critical patent/EP3671957A1/fr
Application granted granted Critical
Publication of EP3671957B1 publication Critical patent/EP3671957B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q13/00Waveguide horns or mouths; Slot antennas; Leaky-waveguide antennas; Equivalent structures causing radiation along the transmission path of a guided wave
    • H01Q13/20Non-resonant leaky-waveguide or transmission-line antennas; Equivalent structures causing radiation along the transmission path of a guided wave
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q13/00Waveguide horns or mouths; Slot antennas; Leaky-waveguide antennas; Equivalent structures causing radiation along the transmission path of a guided wave
    • H01Q13/20Non-resonant leaky-waveguide or transmission-line antennas; Equivalent structures causing radiation along the transmission path of a guided wave
    • H01Q13/206Microstrip transmission line antennas
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/27Adaptation for use in or on movable bodies
    • H01Q1/32Adaptation for use in or on road or rail vehicles
    • H01Q1/325Adaptation for use in or on road or rail vehicles characterised by the location of the antenna on the vehicle
    • H01Q1/3291Adaptation for use in or on road or rail vehicles characterised by the location of the antenna on the vehicle mounted in or on other locations inside the vehicle or vehicle body
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q21/00Antenna arrays or systems
    • H01Q21/28Combinations of substantially independent non-interacting antenna units or systems
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q5/00Arrangements for simultaneous operation of antennas on two or more different wavebands, e.g. dual-band or multi-band arrangements
    • H01Q5/30Arrangements for providing operation on different wavebands
    • H01Q5/307Individual or coupled radiating elements, each element being fed in an unspecified way

Definitions

  • the invention relates to a leaky wave antenna and a method for producing a leaky wave antenna.
  • a leaky wave antenna is an antenna that delivers power in small quantities per unit of length either continuously or discretely from a leaky wave line or leaky wave structure to the free space.
  • leaky wave antennas in the form of coaxial lines are often used, which have a plurality of corresponding openings along the line in the outer jacket, each of which has the same shape due to the manufacture and which are used as slot antennas.
  • coaxial leaky wave antennas usually have the disadvantage that the respective output of electromagnetic power of the individual antennas along the line is not the same due to the manufacturing process, but rather decreases over the length.
  • a leaky wave antenna in which at least one line, each with a feed point, is embedded in an insulating layer, and the insulating layer is arranged between an electrically conductive lower layer and an electrically conductive upper layer, wherein a plurality of antenna elements in the form of openings along the at least one line are introduced in the upper layer, and a coupling means is provided between the at least one line and a respective antenna element from the plurality of antenna elements, which defines a respective coupling factor that describes the electromagnetic coupling between the at least one line and the respective antenna element, and, starting from the respective entry point, the coupling factor of the respective antenna element increases along the at least one line.
  • the invention consequently builds on an embedded strip line.
  • the conductor strip is covered by an equally thick dielectric at the top and bottom and runs parallel to two conductive layers (ground) which are applied to the dielectrics.
  • ground conductive layers
  • the distance to both ground surfaces can also be different (offset stripline).
  • layers and layers are parts of a composite material which is to form the leaky wave antenna in the finished state.
  • the term layer or layer should not be interpreted restrictively with regard to the type of material or the manufacturing process.
  • the layers and layers can for example be made of a flexible material such as plastic, foam with air pockets, metal foils or a woven fiber material. Depending on the application, materials based on glass fiber or Teflon can also be used.
  • a flexible material such as foam is preferably used for the layers, as is a material with a low relative permittivity, such as less than two or three, or a combination of a flexible material and with a low relative permittivity.
  • the layers and layers can, for example, be piece by piece from a solid material, such as FR4 or Teflon circuit board carriers with one-sided, two-sided or multilayer metallization for line layers, individual plates being fed piece by piece to the method according to the invention and then being connected in succession and to one another.
  • a solid material such as FR4 or Teflon circuit board carriers with one-sided, two-sided or multilayer metallization for line layers, individual plates being fed piece by piece to the method according to the invention and then being connected in succession and to one another.
  • the layers and layers can be made of a material, for example, which is printed on, sprayed on, or sprayed on by foils or plates, or is applied by a chemical or physical process. Openings or structures, for example for coupling means, can also be provided in the layers and / or layers.
  • the plurality of antenna elements of the leaky wave antenna comprise at least ten, preferably at least thirty and particularly preferably at least fifty antenna elements, since the effect according to the invention can be perceived particularly advantageously with increasing line length compared to the prior art.
  • the necessary transmission power can be reduced accordingly, since Even the last located antenna element of the leaky wave antenna, starting from the entry point, can be adequately supplied with power. Furthermore, the reception of electromagnetic power from the last located antenna element of the leaky wave antenna can also be improved.
  • the leaky wave antenna according to the invention allows a uniform delivery and a uniform reception of electromagnetic power over the entire length of the leaky wave antenna. This makes the leaky wave antenna especially suitable for use when mounting on elongated objects with many antenna elements, in particular train wagons, fuselages or buildings.
  • the length of the at least one line of the leaky wave antenna is at least five meters, preferably at least ten meters and particularly preferably at least 20 meters and is therefore greater than a single typical use in the production of printed circuit boards.
  • a benefit usually includes several printed circuit boards during their manufacture and can be limited to the dimensions of the production systems used.
  • a maximum benefit size or PCB size can vary depending on the PCB manufacturer and technical equipment. Based on the standard panel cut 610 mm * 530 mm, which is often processed, many manufacturers have maximum dimensions of approx. 570 mm * 490 mm.
  • the base materials for printed circuit boards can undesirably shrink or stretch during a printed circuit board manufacturing process (dimensional stability), which increases the size can limit a circuit board. Furthermore, in the case of very large printed circuit boards or in the case of large benefits, the positioning of structures or components on the printed circuit boards cannot always be carried out with the required accuracy, or an undesirable offset from layer to layer of the printed circuit board can arise with increasing size. Bending a large panel during transport in transport devices can lead to unfavorable mechanical stresses, for example in the case of solder joints.
  • At least two lines are included, which are preferably provided for feeding in or coupling out electrical signals with different frequencies in each case.
  • the insulating layer has a first insulating layer and a second insulating layer, which are preferably each formed by a foam material. This results in a particularly inexpensive design, which is also mechanically flexible and therefore simplifies assembly.
  • the at least one line is arranged between the first insulating layer and the second insulating layer is. This results in a particularly inexpensive and compact design.
  • the respective coupling means is formed by the distance between the at least one line and the respective antenna element, the distance being determined in a plane transverse to the at least one line.
  • the respective coupling means is formed by a coupling structure in the form of a directional coupler.
  • the coupling between the line and the respective antenna element can be determined in a particularly simple manner, an even broader selection of antenna types being supported, for example circularly polarized antennas or antennas with specific radiation characteristics.
  • the respective coupling means is formed or arranged between the first insulating layer and the second insulating layer.
  • the coupling means can be integrated into the antenna in a cost-effective and simple manner and overall a compact design can be achieved.
  • the coupling means does not have to have a dedicated structural element, but can be formed by an arrangement of line and antenna element.
  • an adapter element is further inserted between the lower layer and the upper layer.
  • an electrical and / or mechanical connection can be created, by means of which the leaky wave antenna can be attached to other components, or a signal coupling or signal coupling for example with a corresponding high-frequency connector.
  • a leaky wave antenna according to the invention is provided as part of a communication device in an aircraft, a train or a building.
  • This provides a method for the simple and inexpensive production of a leaky wave antenna, which allows a uniform delivery and a uniform reception of electromagnetic power over the entire length of the leaky wave antenna, which is particularly suitable for long line lengths of the leaky wave antenna.
  • Additional layers can be provided between the first insulating layer and the second insulating layer, for example for further circuit components or also further mechanical carrier layers. It can be provided that a line or a coupling structure is arranged on an electrically non-conductive carrier layer and is thus fed to the method. It can also be provided that a line or a coupling structure form a composite, which is connected in advance by means of mechanical support layers and is thus fed to the method.
  • the respective values for the respective coupling factors are determined and fixed numerically, and for example stored in a lookup table for coupling factors in a memory.
  • the coupling factors stored in the memory can then be accessed for production and taken into account when introducing a respective opening.
  • the coupling factors are determined taking into account the material properties and the dimensions of the composite material and the antenna elements, as well as the desired electromagnetic properties of the leaky wave antenna.
  • the layers are aligned with one another so that they form the leaky-wave antenna when the material stack is formed, and the material stack is moved continuously in a production direction, the starting point being formed before the material stack is formed Opening is made at a fixed distance from the at least one line, which determines the coupling factor, in a plane transverse to the direction of production by means of a cutting device. This enables a leaky-wave antenna with a theoretically arbitrary length of line.
  • the cutting device makes the opening by punching, laser cutting or a combination thereof.
  • the opening for a respective antenna element can be introduced in a simple and cost-effective manner, the respective position of the opening being flexibly adjustable, in particular in a plane transverse to the direction of production, and the setting of the respective coupling factor thus being carried out simply.
  • connection is carried out by laminating, gluing, pressing or a combination thereof. This allows a simple and reliable mechanical connection of the material stack during the continuous movement in the production direction in the manufacturing process.
  • the respective coupling means for the respective antenna element is formed by the distance between the respective antenna element and the at least one line, in a plane transverse to the at least one line, whereby the coupling factor is determined. It is thereby achieved that the coupling factor can be set in a simple manner without further structural measures being necessary.
  • the lower layer has a first transverse projection and / or the upper layer has a second transverse projection in a plane transverse to the at least one line, which transverse projections compared to the line position and / or the first insulating layer and / or the second insulating layer protrude, and the first and / or second transverse protrusion are connected to the other of the lower layer and / or the upper layer in a method step following step i becomes.
  • an electromagnetic shield can be created at the edge of the material composite of the leaky wave line, which reduces an undesired radiation of signals which are coupled into the at least one line.
  • the lower layer has a first longitudinal protrusion and / or the upper layer has a second longitudinal protrusion in a plane along at least one line, which longitudinal protrusions compared to the line position and / or the first insulating layer and / or the second insulating layer protrude, and an adapter element is introduced between the respective projections in a method step following step i.
  • the adapter element can be used to create an electrical or mechanical coupling of the material composite of the leaky wave antenna at a fastening point or an electrical contact element.
  • At least one plated-through hole which connects the lower layer with the upper layer () is introduced in a method step following step i. This enables the electromagnetic coupling of signals on two or more lines in the material composite Leaky wave antenna are reduced, or an unwanted radiation of signals from an open edge of the composite material of the leaky wave line, which are coupled into the at least one line, are reduced.
  • the respective coupling means for the respective antenna element is formed by a coupling structure which determines the coupling factor between the at least one line and the respective antenna element, an electrically conductive material is provided as a coupling layer of the material composite and is structured accordingly for the respective antenna element, and is arranged in alignment with one another between the first insulation layer and the second insulation layer, and all layers which are aligned with one another form the material stack before step i is carried out.
  • a coupling for a circularly polarized antenna can be implemented.
  • the coupling position corresponds to the line position, as a result of which the coupling structure and the line can be produced in the same position and by which the method is simplified.
  • first and second insulating layers, the line layer and the lower and upper layers are each a material in strip form, which layers are fed to the process in rolled up form, rolled up there and made available in the corresponding process steps.
  • Fig. 1 illustrates a first exemplary embodiment of a leaky wave antenna 100 according to the invention schematically in a cross-sectional view.
  • the leaky wave antenna 100 has two lines 110, 111, which are embedded in an insulating layer 120 and form a symmetrical strip line.
  • the lines 110, 111 lie in one plane and form a common line layer 115.
  • the insulating layer 120 has a first insulating layer 121 and a second insulating layer 122, which are preferably each formed by a foam material.
  • the insulating layer 120 is arranged between an electrically conductive lower layer 130 and an electrically conductive upper layer 140.
  • the lines 110, 111 are arranged between the first insulating layer 121 and the second insulating layer 122.
  • a plurality of antenna elements in the form of openings 150, 155 along the lines 110, 111 are introduced in the upper layer 140.
  • the lower layer 130 and the upper layer 140, the first insulating layer 121 and the second insulating layer 122 together with the line layer 115 form a material stack or a material composite 303.
  • the material stack means a loose stack of layers and layers that are only mechanically connected, for example by gluing.
  • the material composite 303 means the already mechanically connected material stack.
  • a transverse core region 400 can be seen in the figure, which contains a section of the material stack (or of the material composite 303) with the lines 110, 111.
  • the leaky wave antenna 100 also has longitudinal edge regions 401, 402, which form the edge or termination of the material stack or the material composite 303 and run along or parallel to the lines 110, 111.
  • the longitudinal edge regions 401, 402 can, for example, as shown in the figure, form a common termination of the layers and layers of the material stack along the lines 110, 111.
  • Fig. 2 the leaky wave antenna 100 is shown schematically in top view.
  • the two lines 110, 111 are for feeding in electrical signals with different frequencies in each case, and can be generated, for example, by a communication device for use in an aircraft, a train or a building.
  • the lines 110, 111 each have an entry point 101, 102 and run in parallel.
  • a parallel course of two or more lines is advantageous for a very long leaky wave antenna, since theoretically any length of line for the leaky wave antenna can be generated.
  • the openings 150-153, 155-159 each have a slot length 103, 105 and a slot width 104, 106, the geometry of the openings being determined by the center frequency of the respective antenna elements 150-153, 155-158.
  • the openings 150-153, 155-159 are of the same size, but the openings 150-153, 155-159 are spaced differently apart from the respective line 110, 111.
  • a coupling means is provided between the lines 110, 111 and a respective antenna element 150-153, 155-158 from the large number of antenna elements, which defines a respective coupling factor.
  • the respective coupling factor describes the electromagnetic coupling between the line 110, 111 and the respective antenna element 150-153, 155-158.
  • the respective coupling means is formed by a transverse distance 160-163, 165-168 between the lines 110, 111 and the respective antenna element 150-153, 155-158.
  • the transverse distance 160-163, 165-168 is determined in a plane across the lines 110, 111 and can be measured, for example, in the plane from the center of the line 110, 111 to an edge of the antenna element 150-153, 155-158.
  • Other definitions are also allowed provided that they are applied to all transverse distances 160-163, 165-168.
  • the coupling factor of the respective antenna element 150-153, 155-158 increases along the respective line 110, 111, that is to say with increasing longitudinal distance 170-173, 175-178.
  • the leaky wave antenna 100 has a static radiation characteristic. Basically, however, is also a beam swivel possible by considering appropriate mechanisms, such as in the WO2001043228A1 executed.
  • the plurality of antenna elements of the leaky wave antenna 100 comprise at least ten, preferably at least 30 and particularly preferably at least fifty antenna elements 150-153, 155-158.
  • the leaky wave antenna 100 is particularly suitable for use when mounting on elongated objects, in particular train wagons, aircraft fuselages or corresponding buildings.
  • the length of the lines 101, 102 of the leaky wave antenna 100 is at least five meters, preferably at least ten meters and particularly preferably at least 20 meters.
  • a longitudinal core region 500 can be seen, which contains a section of the material stack or the material composite 303 with the lines 110, 111.
  • the leaky wave antenna 100 also has transverse edge regions 501, 502, which form the edge or termination of the material stack or the material composite 303 and run transversely to the lines 110, 111.
  • the transverse edge regions 501, 502 can, for example, as shown in the figure, form a common termination of the layers and layers of the material stack transverse to the lines 110, 111. In this specific arrangement there is no subdivision into regions, but the longitudinal core region 500 and the transverse edge regions 501, 502 form a common region.
  • the feed points 101, 102 of the lines 110, 111 are located in the transverse edge regions 501.
  • the feed points 101, 102 of the lines 110, 111 are located in the longitudinal core area 500.
  • FIG. 3 A second exemplary embodiment of a leaky wave antenna 200 is shown schematically in plan view.
  • the respective coupling means is formed by a coupling structure in the form of a directional coupler.
  • the lines 210, 211 each have an entry point 201, 202 and run in parallel.
  • the openings 250-253, 255-258 each comprise two partial openings in the form of slot antennas, which are rotated at an angle of 90 ° to one another and, by means of an appropriately designed coupling, generate a circularly polarized electromagnetic field of the leaky wave antenna 200 .
  • the coupling is set up to feed the respective two partial openings from the respective line 210, 211 at a phase angle that differs by 90 °, the amplitude coupling along the respective line 210, 211 also decreasing according to the invention.
  • the openings 250-253, 255-258 are of the same size and shape and are spaced differently from the respective line 210, 211.
  • a coupling means is provided between the lines 110, 111 and a respective antenna element 150-153, 155-158 from the large number of antenna elements, which defines a respective coupling factor.
  • the respective coupling factor describes the electromagnetic coupling between the line 110, 111 and the respective antenna element 150-153, 155-158.
  • the respective coupling means is formed by a transverse distance 160-163, 165-168 between the lines 110, 111 and the respective antenna element 150-153, 155-158.
  • the transverse distance 160-163, 165-168 is determined in a plane across the lines 110, 111 and can be measured, for example, in the plane from the center of the line 110, 111 to an edge of the antenna element 150-153, 155-158. Other definitions for determining the transverse distance are also possible.
  • the coupling factor of the respective antenna element 150-153, 155-158 increases along the respective line 110, 111, that is to say with increasing longitudinal distance 170-173, 175-178.
  • the respective coupling means is formed by the transverse distance 160-163, 165-168 and thus is not a dedicated structural means and is consequently formed between the first insulating layer 221 and the second insulating layer 222.
  • Fig. 4 shows a first example of a production plant 1 for carrying out a method 300 for producing the leaky wave antenna 100 Fig. 1 and 2nd .
  • the leaky wave antenna 100 has a multiplicity of antenna elements, two lines 110, 111, each with a feed point 101, 102, and the material composite 303.
  • the first and second insulating layers 121, 122 can also each be formed from a different material which, for example, only functions as a spacer, that is to say has a relative dielectric constant of almost one.
  • the lower and upper layers 130, 130 can also be formed from another electrically conductive material, for example aluminum, silver-plated copper, a conductive plastic composite, embossed or corrugated foils, grids or fabrics.
  • the production plant 1 has a base 302, over which the lower layer 130 is guided over deflection rollers 350, 351.
  • the deflection rollers 350, 351 also serve to tension the lower layer 130 and thus ensure or support the subsequent alignment of the individual layers or layers with one another.
  • the lower layer 130 is continuously moved in a production direction 301 over the base 302 and the method steps according to the invention are carried out.
  • the first insulating layer 121 is fed via a deflection roller 352 to a laminating device 360 with a pretensioning roller guide 371, a transfer roller 372 producing a laminating connection between the lower layer 130 and the first insulating layer 121 by pressing and heating.
  • lamination is, on the one hand, a cohesive, thermal joining process without auxiliary materials, which means the connection of a thin, often film-like layer to a carrier material by means of an adhesive.
  • lamination also refers to the connection of at least two film layers of thermoplastics by reaching the glass transition temperature and corresponding pressure.
  • the roller guide 371 is used to adjust or produce an aligned arrangement of layers from the lower layer 130 and the first insulating layer 121, as a result of which a material stack is formed.
  • the layers of the material stack are connected by means of the lamination by the transfer roller 372, as a result of which a first part of the material composite 303 is produced.
  • the transfer roller 372 supplies heat and pressure to the joining process.
  • an adhesive material is already applied to the first insulating layer 121, which is provided for the connection between the lower layer 130 and the first insulating layer 121 and the joining process achieves permanent bonding of the lower layer 130 and the first insulating layer 121.
  • the line layer 115 is fed via a deflection roller 353 to a laminating device 361 with a pretensioning roller guide 373, a transfer roller 374 producing a laminating connection between the first insulating layer 121 and the line layer 115 by pressing and heating.
  • the alignment or the production of an arrangement of layers aligned with one another is carried out by means of the roller guide 373, as a result of which the material stack previously produced is expanded by the line layer 115.
  • the lamination is carried out analogously to the laminating device 360, as a result of which the previously produced material composite 303 is expanded by the line layer 115.
  • the line layer 115 has the lines 110, 111.
  • the lines are applied to a plastic film as a carrier layer, on which an adhesive material for lamination with the first insulating layer 121 is additionally applied.
  • the lines 110, 111 could also be fed to the method directly, that is to say without a carrier layer, for example in the form of copper strips.
  • the lines 110, 111 each have a predefined line width. Together with the layer thicknesses of the first and second insulating layers 121, 122, and their dielectric material properties the respective characteristic impedance of the lines 110, 111 is defined.
  • the second insulating layer 122 is fed via a deflection roller 354 to a laminating device 362 with a pretensioning roller guide 375, a transfer roller 376 establishing a laminating connection between the line layer 115 and the second insulating layer 122 by pressing and heating.
  • An adhesive material for subsequent lamination with the line layer 115 has already been applied to the second insulating layer 122.
  • the lamination is carried out analogously to the laminating device 360, whereby the previously produced material composite 303 is expanded by the second insulating layer 122.
  • the upper layer 140 is fed via a deflection roller 355 to a cutting device 380 in the form of a punching device with roller guide.
  • the cutting device 380 has tensioning roller guides 381, 382 which tension the material of the upper layer 140 on a punching base 383.
  • the cutting device 380 comprises a punch 384 which, through a punch stroke 385, normally introduces an opening 150-153, 155-158 into the upper layer 140 on the surface of the tensioned upper layer 140.
  • the shape of the stamp 384 corresponds to the desired shape of the respective antenna element 150-153, 155-158.
  • the punch pad 383 is matched to the stamp 384.
  • the stamp 384 is also movably controllable transversely to the production direction 301.
  • the positioning of the plunger 384 transversely to the respective line 110, 111 as a function of the distance from the respective entry point 101, 102 can be set at a distance 160-163, 165-168, as a result of which the coupling of the respective antenna element 150-153, 155 -158 to the respective line 110, 111 is adjustable.
  • the respective coupling is formed by the respective distance 160-163, 165-168 between the respective antenna element 150-153, 155-158 and the respective line 110, 111 in a plane transverse to the respective line 110, 111.
  • the material to be punched can be briefly stopped in its movement, since the deflection rollers 355 and 356 are designed in such a way that they compensate for the brief stopping of the material without slowing down or stopping the continuous lamination process.
  • the punch 384 and the punch pad 383 of the cutting device 380 can be moved with the tensioned upper layer 140 during the punching process. After the stamping process, the stamp 384 and the stamping base 383 are then moved back into the original position.
  • the now punched upper layer 140 is fed via a deflection roller 356 to a laminating device 363 with a pretensioning roller guide 377, a transfer roller 378, by pressing and heating, a laminating connection between the second insulating layer 122 and the produces upper layer 140.
  • An adhesive material for subsequent lamination with the second insulating layer 122 has already been applied to the upper layer 140.
  • the lamination is carried out analogously to the laminating device 360, as a result of which the previously produced material composite 303 is expanded and completed by the upper layer 140.
  • the material composite that has gradually developed is also continuously moved in the production direction 301. It is thereby achieved that the individual steps of the manufacturing process are repeated for each antenna element for all antenna elements 150-153, 155-158 from the large number of antenna elements.
  • the material composite 303 of the leaky wave antenna 100 is defined in section AA, which is shown in FIG Fig. 1 is recognizable.
  • Fig. 5 shows a second example of a production plant 2 for carrying out a method 400 for producing the leaky wave antenna 200.
  • the production plant 2 largely corresponds to the production plant 1. Therefore, the above statements apply to the production plant 1 of the Fig. 4 alike.
  • Fig. 4 is the respective coupling means by an additional coupling structure Fig. 3 educated. In this respect, the above statements also apply to the leaky wave antenna 200 of FIG Fig. 3 .
  • the openings 250-253, 255-258 each have two partial openings, and a different shape or orientation with respect to the openings 150-153, 155-158.
  • the punch 386 is accordingly designed for punching two partial openings.
  • the punch pad 387 is matched to the stamp 386.
  • the respective coupling structure is formed in the form of a two-part directional coupler, which in this example is printed on the line layer 115 as an electrically conductive printing ink by means of a printing method. After the ink has dried, the layer can be further processed in the further lamination process.
  • the printing process is carried out by a printing device 390, which has, for example, a printing matrix, a screen printing arrangement or a digitally controllable print head of an inkjet printer.
  • the printing device 390, or those parts which generate the printed image can be moved movably transversely to the production direction 302 in order to adjust the position of the coupling structure with respect to the lines 201, 202.
  • the coupling position which comprises the coupling structures, corresponds to the line position 215.
  • the respective coupling structure can also be applied, for example, by means of local adhesive elements by simple gluing.
  • the respective coupling structure can be generated and provided in advance, for example, on a carrier layer of the line layer 215.
  • the material composite 304 of the leaky wave antenna 200 is defined in section BB.
  • Steps h and i can be distributed over several of steps a to g, as in FIGS Fig. 4 and 5 shown. In other words, it is not necessary to first of all form a complete material stack which has all the layers and only then is a connection made between the individual layers. It can also be provided, for example, that individual layers are successively erected and connected to one another.
  • Steps a and b are applied sequentially.
  • Step c is independent of the other steps.
  • Steps d to g take place independently of the other steps, but chronologically in the sequence defg, where f denotes the repetition of step e.
  • the layers created are aligned with one another in step h as a material stack and structurally connected to one another in step i.
  • steps a, b, c and g can be carried out independently of one another.
  • sequence of steps d to f. The layers generated are in turn aligned in step h as a material stack and structurally connected to one another in step i.
  • steps d and e or step f in which step e is repeated
  • steps h and i are sequential.
  • Fig. 9 shows in a sectional view the leaky wave antenna 100 with alternative designs for longitudinal edge regions, which the longitudinal edge regions 401, 402 of FIG Fig. 1 should replace.
  • the lower layer 130 and the upper layer 140 each extend beyond the first insulating layer 121 and the second insulating layer 122, and in each case form optional transverse projections 413, 414, 415, 416 of the respective layer 130, 140, whereby at other applications, only a transverse projection can be provided.
  • the cross projections 413, 414, 415, 416 can be used to achieve a lateral electromagnetic seal of the leaky wave antenna 100. If necessary, this can reduce undesired electromagnetic radiation from open longitudinal edge regions 401, 402 during operation of the leaky wave antenna 100.
  • the cross projections 413, 414, 415, 416 are used to electrically connect the lower layer 130 and the upper layer 140 to one another.
  • the lower layer 130 thus has a first transverse projection 414, 416, 424, 444
  • the upper layer 140 has a second transverse projection 413, 415, 423, 433, 443, in each case in a plane transverse to the lines 110, 111.
  • transverse projections 413, 414, 415, 416, 423, 424, 433, 443, 444 protrude from the line layer 115 and the first insulating layer 121 and the second insulating layer 121.
  • the first and the second cross overhang 413, 414, 415, 416, 423, 424, 433, 443, 444 are connected to the other of the lower layer 130 and / or the upper layer 140 in a method step following step i.
  • connection between the lower layer 130 and the upper layer 140 can take place in different ways, as in FIGS 10 to 12 shown.
  • Advantageous exemplary embodiments for the transverse projections 413, 414, 415, 416 are provided in the longitudinal edge regions 411, 412, which the longitudinal edge regions 401, 402 of the Fig. 1 should replace accordingly.
  • FIG. 10 A longitudinal edge region 421 of the leaky wave antenna 100 can be seen in a sectional view, the transverse projections 423, 424 each having a length which is shorter than the height of the material stack from the first insulating layer 121, the second insulating layer 122 and the embedded conductor layer 115
  • the transverse projections 423, 424 can thus be hammered in and attached to the lateral ends of the first and second insulating layers 121, 122 and connected to one another, for example by gluing with the aid of an electrically conductive adhesive.
  • transverse protrusions 423, 424 can be driven in by appropriate guiding of the lower and upper layers 130, 140, if necessary by support with pressure rollers.
  • FIG. 11 A longitudinal edge region 431 of the leaky wave antenna 100 can be seen in a sectional view, wherein the transverse projection 433 has a length which is longer than the height of the material stack from the first insulating layer 121, the second insulating layer 122 and the line layer 115.
  • a second transverse projection has a length of zero, that is to say the second transverse projection does not protrude. Therefore, in this example, the second cross-overhang with the length zero is replaced by the cross-overhang 433.
  • the second transverse protrusion protrudes slightly or is set back in order to allow higher tolerances in production.
  • the transverse projection 433 can thus be knocked in and attached to the side terminations of the first and second insulating layers 121, 122 and to the lower layer 130 and connected to one another, for example by gluing with the aid of an electrically conductive adhesive.
  • FIG. 12 A longitudinal edge region 441 of the leaky wave antenna 100 can be seen in a sectional view, the transverse projections 443, 444 each having a length, so that the lower layer 130 and the upper layer 140 can be connected directly to one another, for example by gluing with the aid of an electrical connection conductive adhesive.
  • Fig. 13 the transverse core region 500 can be seen in a sectional view of the leaky wave antenna 100.
  • the explanations of Fig. 2 Alternative designs for the transverse edge regions 511, 512 are shown, which the transverse edge regions 501, 502 of Fig. 2 should replace.
  • the space formed between optional longitudinal projections 513, 514 can be used to accommodate an adapter element 550, 560, 570 for the leaky wave antenna 100.
  • an adapter element 550, 560, 570 between the lower layer 130 and upper layer 140 may be inserted.
  • an adapter element is accommodated in the transverse edge region 512.
  • the adapter element 550, 560, 570 can be provided, for example, for mechanical or electrical tasks.
  • a mechanical adapter element 550, 560, 570 can, for example, be provided to provide a mechanically stable layer, by means of which the leaky wave antenna 100 can be fastened at an operating location, for example when using the leaky wave antenna 100 in a communication system in a train, building or aircraft .
  • the attachment can be done using mechanical connectors such as screws and mounting holes.
  • An electrical adapter element 550, 560, 570 can, for example, be provided for establishing a mechanical and electrical connection from the leaky wave antenna 100 to an electrical connection element, such as a coaxial connector, which is fastened on the adapter element 550, 560, 570.
  • the adapter element 550, 560, 570 can be made, for example, of a printed circuit board material such as FR4 and corresponding conductor tracks on one or more layers for a respective planar coaxial stripline transition for the lines 110, 111, as well as optional electronic modules or high-frequency electronic modules such as transmitters , Receivers, terminating resistors or power measuring devices exhibit.
  • another type of line preferred for the respective application can also be provided for connecting the leaky wave antenna.
  • a combination of electrical and mechanical connecting elements can also be provided by means of the adapter element 550, 560, 570.
  • additional reinforcement elements can be applied to the surfaces of the lower and upper layers 130, 140, for example by adhesive, which connect the transverse edge region 501, 502, 511, 512 to the transverse core region 500.
  • the adapter element 550, 560 can be easily inserted, for example, into the material composite 303 in a respective insertion direction 561, 562 and glued in the material stack.
  • the adapter element 550, 560 should have the same thickness as specified by the volume between the longitudinal projections 513, 514.
  • An adhesive layer can be provided between the longitudinal projections 513, 514 and the adapter element 550, for example by means of adhesive, in order to produce a mechanical connection.
  • the lower layer 130 has a first longitudinal protrusion 514 and the upper layer 140 a second longitudinal protrusion 513 each in one plane along the at least one line 110, 111.
  • the longitudinal projections 513, 514 protrude from the line layer 115 and / or the first insulation layer 121 and / or the second insulation layer 121.
  • the adapter element 550, 560 is introduced between the respective protrusions in a method step following step i, as in FIG Fig. 14 in a longitudinal section of the leaky wave antenna 100 along the production direction 301 or shown parallel to lines 110, 111. Furthermore, in the Fig. 13 a via 600 can be seen, which can be used to reduce unwanted radiation of electromagnetic signals, which are fed into the lines 110, 111, from longitudinal edge regions 401, 402.
  • the plated-through hole 600 which connects the lower layer 130, 230 to the upper layer 140, 240, can be introduced in a method step following step i. Usually, several vias along the line are required to create an electromagnetic shield.
  • FIG. 15 A further example of a transverse edge region 521 of the leaky wave antenna 100 is shown with a further example of an adapter element 570 in a section along the production direction 301.
  • the adapter element 570 has the same thickness as the lower insulating layer 121 and is arranged adjacent to it.
  • a longitudinal protrusion 524 of the lower layer 130 and / or a longitudinal protrusion 523 of the upper layer 140 can each be connected to the adapter element 570. If the adapter element 570 is designed as a printed circuit board, the longitudinal projections 523, 524 can be electrically connected to corresponding electrically conductive surfaces on the adapter element 570, for example by gluing with an electrically conductive adhesive.
  • Parts of the line layer 115, in particular the ends of the lines 110, 111 with the feed points 101, 102 have a corresponding longitudinal projection 525, which projects beyond the lower insulation layer 121, and a corresponding one Longitudinal shelter 527 with respect to the upper insulating layer 122, behind which the line layer 115 remains.
  • the upper insulating layer 122 consequently has a longitudinal projection 526 with respect to the lower insulating layer 121, which additionally projects beyond the longitudinal projection 525 of the line layer 115. This ensures electrical insulation between the longitudinal projection 525 of the line layer 115 and the upper electrically conductive layer 140.
  • the adapter element 570 can be introduced between the longitudinal protrusion 525 of the line layer 115 and the longitudinal protrusion 524 of the lower layer 130 and, subsequently, the material stack can be electrically conductively connected to the adapter element 570.
  • the upper layer 140 is provided with a longitudinal overhang 523 which projects beyond the overhang of the upper insulating layer 526 and has a length which corresponds at least to the height of the upper insulating layer 122.
  • the protrusion 523 can be connected to the adapter element 570 in order to establish a mechanical and / or electrical connection, for example by gluing with an electrically conductive adhesive.
  • the adapter element 570 in the form of a single-sided, double-sided or multilayer printed circuit board can be used to lead electrical signals from the core 400 of the leaky wave antenna 100 to a connection, for example in the form of a plug and / or to electronic assemblies.
  • FIG. 16 A dual-band mobile radio communication system 107 with a leaky wave antenna 100 is shown schematically. This ensures even radio coverage within of a wagon, which leads to improved transmission and reception performance for mobile devices in the wagon.

Landscapes

  • Variable-Direction Aerials And Aerial Arrays (AREA)
  • Waveguide Aerials (AREA)
EP18213890.9A 2018-12-19 2018-12-19 Antenne à ondes de fuite Active EP3671957B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
EP18213890.9A EP3671957B1 (fr) 2018-12-19 2018-12-19 Antenne à ondes de fuite
PCT/EP2019/081649 WO2020126254A1 (fr) 2018-12-19 2019-11-18 Antenne à ondes de fuite

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP18213890.9A EP3671957B1 (fr) 2018-12-19 2018-12-19 Antenne à ondes de fuite

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EP3671957A1 true EP3671957A1 (fr) 2020-06-24
EP3671957B1 EP3671957B1 (fr) 2023-08-23

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Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1247546A (en) * 1968-12-19 1971-09-22 Decca Ltd Microwave antennas
US4728962A (en) * 1984-10-12 1988-03-01 Matsushita Electric Works, Ltd. Microwave plane antenna
JPS63260302A (ja) * 1987-04-17 1988-10-27 Hitachi Cable Ltd 放射形電波漏洩ケ−ブル
WO2001043228A1 (fr) 1999-12-07 2001-06-14 Robert Bosch Gmbh Antenne a ondes de fuite
US20100194500A1 (en) * 2009-02-05 2010-08-05 Fujikura Ltd. Leaky cable
US20120229364A1 (en) * 2010-03-17 2012-09-13 Denso Corporation Antenna
US20180053981A1 (en) * 2016-08-16 2018-02-22 Samsung Electronics Co., Ltd. Flexible flat cable and method for manufacturing the same

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2914766A (en) * 1955-06-06 1959-11-24 Sanders Associates Inc Three conductor planar antenna
US3524189A (en) * 1966-11-09 1970-08-11 Us Army Slotted waveguide antenna array providing dual frequency operation

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1247546A (en) * 1968-12-19 1971-09-22 Decca Ltd Microwave antennas
US4728962A (en) * 1984-10-12 1988-03-01 Matsushita Electric Works, Ltd. Microwave plane antenna
JPS63260302A (ja) * 1987-04-17 1988-10-27 Hitachi Cable Ltd 放射形電波漏洩ケ−ブル
WO2001043228A1 (fr) 1999-12-07 2001-06-14 Robert Bosch Gmbh Antenne a ondes de fuite
US20100194500A1 (en) * 2009-02-05 2010-08-05 Fujikura Ltd. Leaky cable
US20120229364A1 (en) * 2010-03-17 2012-09-13 Denso Corporation Antenna
US20180053981A1 (en) * 2016-08-16 2018-02-22 Samsung Electronics Co., Ltd. Flexible flat cable and method for manufacturing the same

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WO2020126254A1 (fr) 2020-06-25

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