EP0888648B1 - Helical antenna with built-in duplexing means, and manufacturing methods therefore - Google Patents
Helical antenna with built-in duplexing means, and manufacturing methods therefore Download PDFInfo
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- EP0888648B1 EP0888648B1 EP97914395A EP97914395A EP0888648B1 EP 0888648 B1 EP0888648 B1 EP 0888648B1 EP 97914395 A EP97914395 A EP 97914395A EP 97914395 A EP97914395 A EP 97914395A EP 0888648 B1 EP0888648 B1 EP 0888648B1
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01P—WAVEGUIDES; RESONATORS, LINES, OR OTHER DEVICES OF THE WAVEGUIDE TYPE
- H01P5/00—Coupling devices of the waveguide type
- H01P5/12—Coupling devices having more than two ports
- H01P5/16—Conjugate devices, i.e. devices having at least one port decoupled from one other port
- H01P5/19—Conjugate devices, i.e. devices having at least one port decoupled from one other port of the junction type
- H01P5/22—Hybrid ring junctions
- H01P5/227—90° branch line couplers
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01P—WAVEGUIDES; RESONATORS, LINES, OR OTHER DEVICES OF THE WAVEGUIDE TYPE
- H01P5/00—Coupling devices of the waveguide type
- H01P5/12—Coupling devices having more than two ports
- H01P5/16—Conjugate devices, i.e. devices having at least one port decoupled from one other port
- H01P5/19—Conjugate devices, i.e. devices having at least one port decoupled from one other port of the junction type
- H01P5/22—Hybrid ring junctions
- H01P5/222—180° rat race hybrid rings
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q11/00—Electrically-long antennas having dimensions more than twice the shortest operating wavelength and consisting of conductive active radiating elements
- H01Q11/02—Non-resonant antennas, e.g. travelling-wave antenna
- H01Q11/08—Helical antennas
Definitions
- the field of the invention is that of wide bandwidth antennas and hemispherical or quasi-hemispherical radiation pattern. More precisely, the invention relates to resonant helical antennas operating in two bands of neighboring frequencies corresponding to transmission and reception, and in particular the decoupling of these two channels, and therefore the duplexer function.
- the antenna of the invention finds applications in particular in the context of mobile satellite communications between fixed users and all types of mobiles, for example aeronautical, maritime or terrestrial.
- mobile satellite communications between fixed users and all types of mobiles, for example aeronautical, maritime or terrestrial.
- systems in this area communication systems are implemented, or are currently being development (e.g. INMARSAT, INMARSAT-M systems, Globalstar ).
- These antennas are also of interest in the deployment personal communication systems (PCS) by geostationary satellites.
- PCS personal communication systems
- the invention can find applications in all systems requiring the use of a wide band, a cover diagram hemispherical, circular polarization and a good ellipticity ratio.
- the antennas must indeed have the above characteristics either in a very wide bandwidth, around 10%, ie in two neighboring sub-bands corresponding respectively to the reception and broadcast.
- This antenna called the resonant quadrifilar helix antenna (HQR)
- HQR resonant quadrifilar helix antenna
- a quadrifilar antenna is formed by four radiating strands.
- An example of realization is described in detail in the document "Analysis of quadrifilar resonant helical antenna for mobile communications "(analysis of the resonant quadrifilar helix antenna for communications with mobiles), by A. Sharaiha and C. Terret (IEEE - Proceedings H, vol. 140, no.4, August 1993).
- the radiating strands are printed on a substrate thin dielectric, then wound on a transparent cylindrical support of the radio point of view.
- the four strands of the propeller are open or short-circuited one end and electrically connected at the other end with segments conductors arranged on the base of the lower part of the support cylinder.
- the fourth strands of the helix are therefore excited through these conductive segments.
- This antenna conventionally requires a supply circuit, which ensures the excitation of the different antenna strands by signals of the same amplitude in phase quadrature.
- Several techniques are known for making such circuits Power.
- This technique has the advantage of being relatively simple to carry out and to put in action. On the other hand, it leads to a not insignificant bulk, compared to the size of the antenna (which can for example have a size of the order of ten centimeters). This drawback makes this solution incompatible with many applications, especially when maximum miniaturization is required.
- each two-wire propeller can be powered by a coaxial balun of the so-called "balun” type folded ".
- the two two-wire are then excited in phase quadrature using a hybrid coupler.
- balun / adapter assembly used for this type of antennas (made for example from a coaxial section, the core and sheath form dipole) is complex and bulky.
- this type of assembly has the disadvantage of forming a kind of band pass filter still too narrow.
- This technique eliminates hybrid couplers. It presents in however the disadvantage of requiring a delicate adjustment of the length of the strands. Moreover, the antenna is no longer symmetrical, and production will be more complex. Furthermore, this method remains specifically reserved for systems using a band of close operation.
- duplexer This is the role of the duplexer, usually placed at the power point of the antenna.
- duplexers Several types are known.
- the document “RF filters and Diplexers for Cellular Applications” by Gord Neilson and John Mchory (Antem'90) thus present various types of duplexers used in the field of radiocommunication.
- duplexers act as filters, and can therefore introduce loss of useful signal parts.
- the invention particularly aims to overcome these various disadvantages of the state of technique.
- an objective of the invention is to provide an antenna and its power system (thereafter, the term “antenna” includes the antenna itself and its power system) which has two sub-bands which are sufficiently decoupled so as not to require the presence of a conventional additional duplexer.
- the invention aims to provide an antenna bidirectional ensuring simple and efficient duplexing function, without call to known duplexers.
- Another objective of the invention is to provide such an antenna, which is of a cost cost of little importance, and easily achievable industrially.
- the invention aims to provide such an antenna, which can be manufactured in a very small number of successive operations.
- Another object of the invention is also to provide such an antenna, which does not requires specific and complex adjustments.
- Yet another objective of the invention is to provide such an antenna (and including its power system), which is compact, compared to to known devices.
- the invention also aims to provide such an antenna, which provides a excitation equiamplitude of the four strands and a law in exact phase quadrature, and therefore a good quality of circular polarization, in the two sub-bands.
- a helical antenna with integrated duplexing means comprising two decoupled coaxial propellers, each formed of radiating strands printed on a substrate, each of said helices being associated with a structure independent and miniaturized broadband feed of said radiating strands, said supply structures being printed on said corresponding substrate and comprising at least one hybrid coupler made from semi-localized elements, so as to reduce the dimensions.
- Realization of antenna strands and supply of printed elements allows the antenna, its power supply and the duplexer to be produced in a single operation, without specific connection means, and in a particularly reduced format.
- hybrid couplers made from semi-localized elements allows to obtain all the desired qualities, and in particular to reduce the overall size of the assembly, compared to the conventionally used lines.
- each of said coaxial helices being perfectly decoupled, this structure directly plays the role of duplexer, without any element additional.
- the feed points of each of the propellers correspond respectively and directly to the transmit signal and the receive signal.
- said propellers have, when they are laid flat, strands having directions symmetrical with respect to the axis of said antenna, and are wound in opposite winding directions, so that said strands are substantially parallel.
- This technique allows the printed side of the internal propeller to face inside, and that of the external propeller towards the outside.
- the excitation points of each of said quadrifilar propellers are offset with respect to each other, in a plane perpendicular to the axis of said propellers. According to an advantageous embodiment, they are offset by 135 °.
- said propeller is a quadrifilar propeller, formed of four radiating strands supplied by a supply structure comprising three couplers hybrids.
- said supply structure includes a first 180 ° hybrid coupler combining an input and / or output supplying said antenna with two phase-shifted outputs and / or intermediate inputs of 180 °, and two 90 ° hybrid couplers each associating one of said outputs and / or intermediate inputs of said first hybrid coupler at one end of two said radiating strands.
- said antenna is mounted on a support having first and second separate parts having different permittivities, said first part carrying said radiating strands and said second part carrying said supply structure.
- said first part carrying the antenna strands has a permittivity greater than 1.
- An antenna as described above can be used alone, or in a network antennas.
- the invention also relates to the manufacture of such antennas, which turns out particularly simplified, compared to known techniques.
- the invention therefore relates to an antenna with a broadband feed system and integrated duplexer, produced using a simple manufacturing technique and presenting a low cost.
- the invention can be applied to any type of antenna in propellers.
- the preferred embodiment described above relates to an antenna with quadrifilar propellers.
- the antenna therefore has two coaxial propellers ensuring transmission and reception respectively.
- Each of these propellers is made up of four strands printed on a substrate, on which a structure is jointly printed Power.
- the antenna functions are implemented, feeder and duplexer. This makes it possible to obtain a very compact antenna, and at cost very low cost.
- Figure 1 illustrates the printed elements, when developed flat.
- it includes four radiating antenna strands 11 1 to 11 4 .
- They are for example made of copper, on a thin dielectric substrate, such as kapton ( ⁇ r ⁇ 3.8).
- the four strands 11 1 to 11 4 are preferably open at their upper end 15 1 to 15 4 . They can also be short-circuited. However, the system of the invention is particularly suitable for the excitation of antennas with more open strands which, for equal performance, have smaller dimensions than the antennas with short-circuited strands.
- the other end 16 1 to 16 4 of the strands is connected to the feed lines of the supply circuit.
- the supply system is produced on the same substrate, as an extension of the antenna. It is made up of three hybrid couplers 12, 13 and 14 designed in elements semi-localized.
- the first hybrid coupler 12 is connected on the one hand to the input (respectively output depending on use) 17 signal from the antenna, and the other at the two inputs (respectively outputs) 18 and 19 of the two other couplers 13 and 14. It is a 180 ° hybrid coupler.
- the hybrid couplers 13 and 14 are two identical 90 ° couplers. They are connected on the one hand to the input 18 (respectively 19) and on the other hand to the end of the strands 16 1 and 16 2 (respectively 16 3 and 16 4 ).
- the four strands are supplied in perfect phase quadrature, on a broadband.
- the cylindrical support is a transparent support from the radioelectric point of view, that is to say having a permittivity close to 1.
- FIG. 3 illustrates the elements forming the internal layer of the antenna, shown flat. These elements are quite similar to those described in connection with FIG. 1, except that the antenna strands 51 1 to 51 4 are inclined in the opposite direction, the winding direction 52 being opposite to the winding direction 17 of the first propeller.
- the dielectric substrate is identical to the first.
- the system power supply 53 is also in the extension of the antenna strands 511 and 514 and is made of semi-localized elements.
- the assembly is then wound inwards (arrow 52) on a support radio-transparent, to provide the internal helix of Figure 4.
- the 90 ° couplers 13 and 14 each consist of 4 wide elements 31 1 and 31 4 , connected 2 to 2 by 4 lines of small width 32 1 to 32 4 .
- the 190 ° coupler includes 6 wide elements 331 to 336 connected by 6 narrow lines 34 1 to 34 6 .
- Figures 7A and 7C illustrate the design of a -3 dB 90 ° coupler.
- FIG. 7A presents a conventional diagram of a -3 dB 90 ° coupler in elements distributed. It includes two sections of line 81, 82 of length ⁇ g / 4 and of impedance characteristic Zc, and two sections of line 83, 84 of length ⁇ g / 4, and of impedance Z c / ⁇ 2.
- Figures 10 and 11 relate to the radiation patterns measured in right circular polarization (a) and left circular polarization (6), with a dipole operating respectively at 1.98 GHz ( Figure 10) and 2.2 GHz ( Figure 11) frequencies.
- Figure 12 shows that the decoupling between the two propellers is greater than 20 dB.
- An antenna according to the invention can be produced in several ways.
- the propellers can be printed at flat, as illustrated in FIGS. 1 and 3. They are then rolled up on a support for form the antenna (figures 2 and 4).
- the substrate intended for receive the printed elements can be made directly in its cylindrical shape final.
- the printing of the strands and the feeding structure is carried out directly on the cylinder.
- the antenna the invention advantageously lends itself to the production of antenna arrays.
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Description
Le domaine de l'invention est celui des antennes à large bande passante et à diagramme de rayonnement hémisphérique ou quasi-hémisphérique. Plus précisément, l'invention concerne les antennes hélicoïdales résonnantes fonctionnant dans deux bandes de fréquence voisines correspondant à l'émission et à la réception, et en particulier le découplage de ces deux voies, et donc la fonction de duplexeur.The field of the invention is that of wide bandwidth antennas and hemispherical or quasi-hemispherical radiation pattern. More precisely, the invention relates to resonant helical antennas operating in two bands of neighboring frequencies corresponding to transmission and reception, and in particular the decoupling of these two channels, and therefore the duplexer function.
L'antenne de l'invention trouve notamment des applications dans le cadre des communications mobiles par satellite entre utilisateurs fixes et des mobiles de tout type, par exemple aéronautiques, maritimes ou terrestres. Dans ce domaine, plusieurs systèmes de communication par satellite sont mis en oeuvre, ou sont actuellement en cours de développement (par exemple les systèmes INMARSAT, INMARSAT-M, GLOBALSTAR,...). Ces antennes présentent également un intérêt dans le déploiement des systèmes de communications personnelles (PCS) par satellites géostationnaires.The antenna of the invention finds applications in particular in the context of mobile satellite communications between fixed users and all types of mobiles, for example aeronautical, maritime or terrestrial. Several systems in this area communication systems are implemented, or are currently being development (e.g. INMARSAT, INMARSAT-M systems, Globalstar ...). These antennas are also of interest in the deployment personal communication systems (PCS) by geostationary satellites.
Pour tous ces systèmes, qui prévoient des liaisons avec des satellites géostationnaires, les incidences très différentes des signaux reçus ou émis imposent aux antennes de posséder un diagramme de rayonnement à couverture hémisphérique. De plus la polarisation doit être circulaire avec un rapport d'ellipticité meilleur que 5 dB dans la bande utile.For all these systems, which provide for links with satellites geostationary, the very different incidences of the signals received or emitted impose on the antennas to possess a hemispherical coverage radiation pattern. Moreover the polarization must be circular with an ellipticity ratio better than 5 dB in the useful band.
Plus généralement, l'invention peut trouver des applications dans tous les systèmes nécessitant l'emploi d'une large bande, un diagramme à couverture hémisphérique, une polarisation circulaire et un bon rapport d'ellipticité.More generally, the invention can find applications in all systems requiring the use of a wide band, a cover diagram hemispherical, circular polarization and a good ellipticity ratio.
Dans les domaines d'application cités plus haut, les antennes doivent en effet présenter les caractéristiques précédentes soit dans une bande passante très large, de l'ordre de 10 %, soit dans deux sous-bandes voisines correspondant respectivement à la réception et à l'émission.In the fields of application mentioned above, the antennas must indeed have the above characteristics either in a very wide bandwidth, around 10%, ie in two neighboring sub-bands corresponding respectively to the reception and broadcast.
On connaít déjà, par le brevet FR-89 14952 au nom du même déposant, un type d'antenne particulièrement adapté à de telles applications.We already know, by patent FR-89 14952 in the name of the same applicant, a type antenna particularly suitable for such applications.
Cette antenne, appelée antenne hélice quadrifilaire résonnante (HQR), possède des caractéristiques très proches des critères énoncés dans une bande de fréquence limitée en général à 5 % par des problèmes d'adaptation d'impédance. Un fonctionnement sur deux bandes est possible en utilisant des antennes HQR bicouche. Ces antennes sont formées par l'''emboítement" concentriques de deux hélices quadrifilaires résonnantes coaxiales, couplées électromagnétiquement.This antenna, called the resonant quadrifilar helix antenna (HQR), has characteristics very close to the criteria set out in a frequency band limited by generally at 5% by impedance matching problems. Two out of two bands is possible using dual-layer HQR antennas. These antennas are formed by the concentric "nesting" of two coaxial resonant quadrifilar propellers, electromagnetically coupled.
Une antenne quadrifilaire est formée de quatre brins rayonnants. Un exemple de réalisation est décrit en détail dans le document "Analysis of quadrifilar resonant helical antenna for mobile communications" (analyse de l'antenne hélice quadrifilaire résonnante pour les communications avec les mobiles), par A. Sharaiha et C. Terret (IEEE - Proceedings H, vol. 140, n° 4, août 1993).A quadrifilar antenna is formed by four radiating strands. An example of realization is described in detail in the document "Analysis of quadrifilar resonant helical antenna for mobile communications "(analysis of the resonant quadrifilar helix antenna for communications with mobiles), by A. Sharaiha and C. Terret (IEEE - Proceedings H, vol. 140, no.4, August 1993).
Selon ce mode de réalisation, les brins rayonnants sont imprimés sur un substrat diélectrique de faible épaisseur, puis enroulé sur un support cylindrique transparent du point de vue radioélectrique. Les quatre brins de l'hélice sont ouverts ou court-circuités à une extrémité et connectés électriquement à l'autre extrémité avec des segments conducteurs disposés sur la base de la partie inférieure du cylindre support. Les quatre brins de l'hélice sont donc excités à travers ces segments conducteurs.According to this embodiment, the radiating strands are printed on a substrate thin dielectric, then wound on a transparent cylindrical support of the radio point of view. The four strands of the propeller are open or short-circuited one end and electrically connected at the other end with segments conductors arranged on the base of the lower part of the support cylinder. The fourth strands of the helix are therefore excited through these conductive segments.
Cette antenne nécessite, classiquement, un circuit d'alimentation, qui assure l'excitation des différents brins d'antenne par des signaux de même amplitude en quadrature de phase. Plusieurs techniques sont connues pour réaliser de tels circuits d'alimentation.This antenna conventionally requires a supply circuit, which ensures the excitation of the different antenna strands by signals of the same amplitude in phase quadrature. Several techniques are known for making such circuits Power.
Dans le document "Analysis of quadrifilar resonant helical antenna for mobile communications" cité ci-dessus, cette fonction est réalisée à partir de structure de coupleurs (3 dB, -90 °) et d'un anneau hybride. Cet ensemble est implanté sur un circuit imprimé qui est placé à la base de l'antenne.In the document "Analysis of quadrifilar resonant helical antenna for mobile communications "cited above, this function is performed from the structure of couplers (3 dB, -90 °) and a hybrid ring. This set is located on a circuit printed which is placed at the base of the antenna.
Cette technique présente l'avantage d'être relativement simple à réaliser et à mettre en oeuvre. En revanche, elle conduit à un encombrement non négligeable, par rapport à la taille de l'antenne (qui peut par exemple présenter une taille de l'ordre d'une dizaine de centimètres). Cet inconvénient rend cette solution incompatible avec de nombreuses applications, notamment lorsqu'une miniaturisation maximum est requise.This technique has the advantage of being relatively simple to carry out and to put in action. On the other hand, it leads to a not insignificant bulk, compared to the size of the antenna (which can for example have a size of the order of ten centimeters). This drawback makes this solution incompatible with many applications, especially when maximum miniaturization is required.
Selon une deuxième technique, décrite dans le document "UHF satellite array nulls adjacent signais" par J. L. Wong et H. E. King (Microwaves & RF, mars 1984), chaque hélice bifilaire peut être alimentée par un symétriseur coaxial du type dit "balun replié". Les deux bifilaires sont ensuite excitées en quadrature de phase à l'aide d'un coupleur hybride.According to a second technique, described in the document "UHF satellite array nulls adjacent signais "by J. L. Wong and H. E. King (Microwaves & RF, March 1984), each two-wire propeller can be powered by a coaxial balun of the so-called "balun" type folded ". The two two-wire are then excited in phase quadrature using a hybrid coupler.
L'avantage de cette méthode est qu'elle ne nécessite l'utilisation que d'un seul élément hybride externe. En revanche, le montage symétriseur/adaptateur utilisé pour ce type d'antennes (réalisé par exemple à partir d'un tronçon de coaxial, dont l'âme et la gaine forment dipôle) est complexe et encombrant.The advantage of this method is that it only requires the use of one external hybrid element. However, the balun / adapter assembly used for this type of antennas (made for example from a coaxial section, the core and sheath form dipole) is complex and bulky.
Par ailleurs, ce type de montage présente l'inconvénient de former une sorte de filtre passe-bande à bande encore trop étroite.Furthermore, this type of assembly has the disadvantage of forming a kind of band pass filter still too narrow.
Une troisième technique, plus complexe, est décrite dans le document "resonant quadrifilar helix" (hélice résonnante quadrifilaire) par C.C. Kilgus (Microwave Journal, décembre 1970) La ligne coaxiale d'alimentation est fendue à son extrémité pour constituer un symétriseur. La quadrature de phase est assurée en ajustant la longueur des brins.A third, more complex technique is described in the document "resonant quadrifilar helix "(resonant quadrifilar propeller) by C.C. Kilgus (Microwave Journal, December 1970) The coaxial supply line is split at its end to constitute a balun. Phase quadrature is ensured by adjusting the length of the strands.
Cette technique permet de supprimer les coupleurs hybrides. Elle présente en revanche l'inconvénient de nécessiter un réglage délicat de la longueur des brins. De plus, l'antenne n'est plus symétrique, et la réalisation sera plus complexe. Par ailleurs, cette méthode reste spécifiquement réservée aux systèmes utilisant une bande de fonctionnement étroite.This technique eliminates hybrid couplers. It presents in however the disadvantage of requiring a delicate adjustment of the length of the strands. Moreover, the antenna is no longer symmetrical, and production will be more complex. Furthermore, this method remains specifically reserved for systems using a band of close operation.
Dans le cas des antennes bidirectionnelles, devant assurer l'émission et la réception de signaux, il est bien sûr nécessaire de découpler au tant que faire se peut la bande de fréquence d'émission et la bande de fréquence de réception, qui sont généralement voisines.In the case of bidirectional antennas, which must ensure the transmission and reception of signals, it is of course necessary to decouple as far as possible the transmit frequency band and receive frequency band, which are generally neighboring.
C'est le rôle du duplexeur, généralement placé au niveau du point d'alimentation de l'antenne. Plusieurs types de duplexeurs sont connus. Le document "RF filters and Diplexers for Cellular Applications", par Gord Neilson et John Mchory (Antem'90) présentent ainsi divers types de duplexeurs utilisés dans le domaine de la radiocommunication.This is the role of the duplexer, usually placed at the power point of the antenna. Several types of duplexers are known. The document "RF filters and Diplexers for Cellular Applications ", by Gord Neilson and John Mchory (Antem'90) thus present various types of duplexers used in the field of radiocommunication.
D'une façon générale, ces dispositifs connus ont l'inconvénient de se présenter sous la forme d'un élément indépendant et complémentaire à l'antenne. Ils entraínent donc un encombrement non négligeable, notamment dans les cas où les antennes sont de taille très réduite.In general, these known devices have the disadvantage of being in the form of an independent and complementary element to the antenna. So they train significant footprint, especially in cases where the antennas are large very small.
Par ailleurs, il s'agit d'éléments complexes à réaliser et à mettre en oeuvre. En conséquence, leur coût de revient est important, par rapport au coût de l'antenne proprement dite.Furthermore, these are complex elements to be produced and implemented. In consequently, their cost price is high, compared to the cost of the antenna proper.
Enfin, ces duplexeurs agissent comme des filtres, et peuvent donc introduire des pertes de parties utiles de signal.Finally, these duplexers act as filters, and can therefore introduce loss of useful signal parts.
L'invention a notamment pour objectif de pallier ces divers inconvénients de l'état de la technique.The invention particularly aims to overcome these various disadvantages of the state of technique.
Plus précisément, un objectif de l'invention est de fournir une antenne et son système d'alimentation (par la suite, le terme "antenne" englobe l'antenne proprement dite et son système d'alimentation) qui présente deux sous-bandes qui sont suffisamment découplées pour ne pas nécessiter la présence d'un duplexeur supplémentaire classique.More specifically, an objective of the invention is to provide an antenna and its power system (thereafter, the term "antenna" includes the antenna itself and its power system) which has two sub-bands which are sufficiently decoupled so as not to require the presence of a conventional additional duplexer.
En d'autres termes, l'invention a pour objectif de fournir une antenne bidirectionnelle assurant de façon simple et efficace la fonction de duplexage, sans faire appel aux duplexeurs connus.In other words, the invention aims to provide an antenna bidirectional ensuring simple and efficient duplexing function, without call to known duplexers.
Un autre objectif de l'invention est de fournir une telle antenne, qui soit d'un coût de revient peu important, et aisément réalisable industriellement. En particulier, l'invention à pour objectif de fournir une telle antenne, qui puisse être fabriquée en un nombre très réduit d'opérations successives.Another objective of the invention is to provide such an antenna, which is of a cost cost of little importance, and easily achievable industrially. In particular, the invention aims to provide such an antenna, which can be manufactured in a very small number of successive operations.
Un autre objectif de l'invention est également de fournir une telle antenne, qui ne nécessite par de réglages spécifiques et complexes.Another object of the invention is also to provide such an antenna, which does not requires specific and complex adjustments.
Encore un autre objectif de l'invention est de fournir une telle antenne (et notamment son système d'alimentation), qui soit d'un encombrement réduit, par rapport aux dispositifs connus.Yet another objective of the invention is to provide such an antenna (and including its power system), which is compact, compared to to known devices.
L'invention a également pour objectif de fournir une telle antenne, qui assure une excitation équiamplitude des quatre brins et une loi en exacte quadrature de phase, et donc une bonne qualité de polarisation circulaire, dans les deux sous-bandes.The invention also aims to provide such an antenna, which provides a excitation equiamplitude of the four strands and a law in exact phase quadrature, and therefore a good quality of circular polarization, in the two sub-bands.
Ces objectifs, ainsi que d'autres qui apparaítront par la suite, sont atteints selon l'invention à l'aide d'une antenne hélicoïdale à moyens de duplexage intégrés, comprenant deux hélices coaxiales découplées, formées chacune de brins rayonnants imprimés sur un substrat, chacune desdites hélices étant associée à une structure indépendante et miniaturisée d'alimentation large bande desdits brins rayonnants, lesdites structures d'alimentation étant imprimées sur ledit substrat correspondant et comprenant au moins un coupleur hybride réalisé à partir d'éléments semi-localisés, de façon à en réduire les dimensions.These objectives, as well as others that will appear later, are achieved according to the invention using a helical antenna with integrated duplexing means, comprising two decoupled coaxial propellers, each formed of radiating strands printed on a substrate, each of said helices being associated with a structure independent and miniaturized broadband feed of said radiating strands, said supply structures being printed on said corresponding substrate and comprising at least one hybrid coupler made from semi-localized elements, so as to reduce the dimensions.
La réalisation des brins d'antenne et de l'alimentation en éléments imprimés permet de produire l'antenne, son alimentation et le duplexeur en une seule opération, sans moyens de connexion spécifiques, et sous un format particulièrement réduit.Realization of antenna strands and supply of printed elements allows the antenna, its power supply and the duplexer to be produced in a single operation, without specific connection means, and in a particularly reduced format.
L'utilisation de coupleurs hybrides réalisés à partir d'éléments semi-localisés permet d'obtenir l'ensemble des qualités désirées, et notamment de réduire l'encombrement de l'ensemble, par rapport aux lignes classiquement utilisées.The use of hybrid couplers made from semi-localized elements allows to obtain all the desired qualities, and in particular to reduce the overall size of the assembly, compared to the conventionally used lines.
Les deux couches formant chacune desdites hélices coaxiales étant parfaitement découplées, cette structure joue directement le rôle de duplexeur, sans aucun élément supplémentaire. Les points d'alimentation de chacune des hélices correspondent respectivement, et directement, au signal d'émission et au signal de réception.The two layers forming each of said coaxial helices being perfectly decoupled, this structure directly plays the role of duplexer, without any element additional. The feed points of each of the propellers correspond respectively and directly to the transmit signal and the receive signal.
On obtient ainsi une antenne bidirectionnelle très simple, et à faible coût de revient.This gives a very simple, low-cost bidirectional antenna. come back.
De façon avantageuse, lesdites hélices présentent, lorsqu'elles sont mises à plat, des brins présentant des directions symétriques par rapport à l'axe de ladite antenne, et sont enroulées selon des sens d'enroulement opposés, de façon que lesdits brins soient sensiblement parallèles.Advantageously, said propellers have, when they are laid flat, strands having directions symmetrical with respect to the axis of said antenna, and are wound in opposite winding directions, so that said strands are substantially parallel.
Cette technique permet que la face imprimée de l'hélice interne soit dirigée vers l'intérieur, et celle de l'hélice externe vers l'extérieur.This technique allows the printed side of the internal propeller to face inside, and that of the external propeller towards the outside.
Préférentiellement, dans le but d'augmenter le découplage, les points d'excitation de chacune desdites hélices quadrifilaires sont décalés l'un par rapport à l'autre, dans un plan perpendiculaire à l'axe desdites hélices. Selon un mode de réalisation avantageux, ils sont décalés de 135°.Preferably, in order to increase the decoupling, the excitation points of each of said quadrifilar propellers are offset with respect to each other, in a plane perpendicular to the axis of said propellers. According to an advantageous embodiment, they are offset by 135 °.
L'invention peut s'appliquer à tous les types d'antennes en hélices. Selon un mode de réalisation préférentiel, ladite hélice est une hélice quadrifilaire, formée de quatre brins rayonnants alimentés par une structure d'alimentation comprenant trois coupleurs hybrides.The invention can be applied to all types of helical antennas. According to a preferred embodiment, said propeller is a quadrifilar propeller, formed of four radiating strands supplied by a supply structure comprising three couplers hybrids.
De façon avantageuse, dans ce dernier cas, ladite structure d'alimentation comprend un premier coupleur hybride à 180° associant une entrée et/ou sortie d'alimentation de ladite antenne à deux sorties et/ou entrées intermédiaires déphasées de 180°, et deux coupleurs hybrides à 90° associant chacun l'une desdites sorties et/ou entrées intermédiaires dudit premier coupleur hybride à une des extrémités de deux desdits brins rayonnants.Advantageously, in the latter case, said supply structure includes a first 180 ° hybrid coupler combining an input and / or output supplying said antenna with two phase-shifted outputs and / or intermediate inputs of 180 °, and two 90 ° hybrid couplers each associating one of said outputs and / or intermediate inputs of said first hybrid coupler at one end of two said radiating strands.
Selon un mode de réalisation avantageux de l'invention, ladite antenne est montée sur un support présentant une première et une seconde parties distinctes ayant des permittivités différentes, ladite première partie portant lesdits brins rayonnants et ladite seconde partie portant ladite structure d'alimentation.According to an advantageous embodiment of the invention, said antenna is mounted on a support having first and second separate parts having different permittivities, said first part carrying said radiating strands and said second part carrying said supply structure.
Préférentiellement, ladite première partie portant les brins d'antenne présente une permittivité supérieure à 1.Preferably, said first part carrying the antenna strands has a permittivity greater than 1.
Ainsi, il est possible de réduire encore l'encombrement de l'antenne.Thus, it is possible to further reduce the size of the antenna.
Une antenne telle que décrite ci-dessus peu être utilisée seule, ou en réseau d'antennes.An antenna as described above can be used alone, or in a network antennas.
L'invention concerne également la fabrication de telles antennes, qui s'avère particulièrement simplifiée, par rapport aux techniques connues.The invention also relates to the manufacture of such antennas, which turns out particularly simplified, compared to known techniques.
Selon un premier procédé de fabrication d'une antenne hélicoïdale résonnante, on prévoit les étapes suivantes :
- impression sur un substrat plan d'au moins deux brins rayonnants, destinés à former une hélice, et d'une structure indépendante d'alimentation miniaturisée large bande desdits brins rayonnants comprenant au moins un coupleur hybride réalisé à partir d'éléments semi-localisés, de façon à en réduire les dimensions ;
- enroulement dudit substrat autour d'un support cylindrique.
- printing on a flat substrate of at least two radiating strands, intended to form a helix, and of an independent broadband miniaturized power supply of said radiating strands comprising at least one hybrid coupler produced from semi-localized elements, so as to reduce its dimensions;
- winding said substrate around a cylindrical support.
Selon un second procédé de fabrication d'une antenne hélicoïdale résonnante, encore plus simple à mettre en oeuvre, on réalise les étapes suivantes :
- obtention d'un support cylindrique portant un substrat ;
- impression sur ledit substrat d'au moins deux brins rayonnants, destinés à former une hélice, et d'une structure indépendante d'alimentation miniaturisée large bande desdits brins rayonnants comprenant au moins un coupleur hybride réalisé à partir d'éléments serai-localisés, de façon à en réduire les dimensions.
- obtaining a cylindrical support carrying a substrate;
- printing on said substrate of at least two radiating strands, intended to form a helix, and of an independent miniaturized broadband power supply structure of said radiating strands comprising at least one hybrid coupler produced from serai-localized elements, so as to reduce the dimensions.
D'autres caractéristiques et avantages de l'invention apparaítront à la lecture de la description suivante d'un mode de réalisation préférentiel de l'invention, donné à titre de simple exemple illustratif et non limitatif, et des dessins annexés parmi lesquels :
- la figure 1 illustre un exemple d'hélice quadrifilaire à alimentation intégrée selon l'invention, formant la couche externe de l'antenne, développée à plat;
- la figure 2 présente l'hélice de la figure 1, enroulée cylindriquement, de façon à former une première hélice opérationnelle ;
- la figure 3 illustre une seconde hélice quadrifilaire à alimentation intégrée selon l'invention formant la couche interne de l'antenne, développée à plat;
- la figure 4 présente l'hélice de la figure 3, enroulée cylindriquement, de façon à former une seconde hélice opérationnelle ;
- la figure 5 présente une vue en coupe de l'antenne montée, comprenant les
hélices des figures 2
et 4, montées en décalage ; - la figure 6 présente de façon plus détaillée la structure d'alimentation des figures 1 et 3 ;
- les figures 7A à 7C illustrent la conception d'un coupleur -
3 dB 90° selon l'invention :- figure 7A : coupleur classique en éléments distribués ;
- figure 7B : représentation correspondante à l'aide de cellules en π ;
- figure 7C : coupleur en lignes microrubans correspondant ;
- les figures 8A et 8B illustrent la conception d'un coupleur -3 dB 180°;
- figure 8A : représentation d'un anneau hybride 180° ;
- figure 8B : coupleur en lignes microrubans correspondant.
- la figure 9 illustre le rapport d'onde stationnaire (ROS) d'un mode de réalisation particulier de l'antenne des figures 1 et 2 ;
- les figures 10 et 11 présentent des diagrammes de rayonnement mesurés en polarisation circulaire droite et gauche du même mode de réalisation, respectivement aux fréquences 1,98 GHz et 2,2 GHz ;
- la figure 12 montre le découplage (S21) entre les deux hélices.
- FIG. 1 illustrates an example of a quadrifilar propeller with integrated feed according to the invention, forming the outer layer of the antenna, developed flat;
- Figure 2 shows the propeller of Figure 1, wound cylindrically, so as to form a first operational propeller;
- FIG. 3 illustrates a second quadrifilar helix with integrated feed according to the invention forming the internal layer of the antenna, developed flat;
- FIG. 4 shows the propeller of FIG. 3, wound cylindrically, so as to form a second operational propeller;
- Figure 5 shows a sectional view of the mounted antenna, comprising the propellers of Figures 2 and 4, mounted offset;
- Figure 6 shows in more detail the supply structure of Figures 1 and 3;
- FIGS. 7A to 7C illustrate the design of a -
3 dB 90 ° coupler according to the invention:- FIG. 7A: conventional coupler in distributed elements;
- FIG. 7B: corresponding representation using cells in π;
- FIG. 7C: corresponding microstrip line coupler;
- Figures 8A and 8B illustrate the design of a -3 dB 180 ° coupler;
- FIG. 8A: representation of a 180 ° hybrid ring;
- FIG. 8B: corresponding microstrip line coupler.
- FIG. 9 illustrates the standing wave ratio (ROS) of a particular embodiment of the antenna of FIGS. 1 and 2;
- FIGS. 10 and 11 present radiation diagrams measured in right and left circular polarization of the same embodiment, respectively at the frequencies 1.98 GHz and 2.2 GHz;
- Figure 12 shows the decoupling (S 21 ) between the two propellers.
L'invention concerne donc une antenne à système d'alimentation à large bande et duplexeur intégrés, réalisée selon une technique de fabrication simple et présentant un faible coût de revient.The invention therefore relates to an antenna with a broadband feed system and integrated duplexer, produced using a simple manufacturing technique and presenting a low cost.
Comme indiqué précédemment, l'invention peut s'appliquer à tout type d'antenne en hélices. Le mode de réalisation préférentiel décrit ci-dessus concerne une antenne à hélices quadrifilaires.As indicated above, the invention can be applied to any type of antenna in propellers. The preferred embodiment described above relates to an antenna with quadrifilar propellers.
Selon l'invention, l'antenne présente donc deux hélices coaxiales assurant respectivement l'émission et la réception. Chacune de ces hélices est formée de quatre brins imprimés sur un substrat, sur lequel est conjointement imprimé une structure d'alimentation.According to the invention, the antenna therefore has two coaxial propellers ensuring transmission and reception respectively. Each of these propellers is made up of four strands printed on a substrate, on which a structure is jointly printed Power.
Ainsi, en une seule opération sont implantée les fonctions d'antenne, d'alimentation et de duplexeur. Cela permet d'obtenir une antenne très compacte, et à coût de revient très faible.Thus, in a single operation, the antenna functions are implemented, feeder and duplexer. This makes it possible to obtain a very compact antenna, and at cost very low cost.
On décrit maintenant en détail la première hélice formant la couche.The first helix forming the layer will now be described in detail.
La figure 1 illustre les éléments imprimés, lorsqu'elle est développée à plat.Figure 1 illustrates the printed elements, when developed flat.
Elle comprend tout d'abord quatre brins d'antenne rayonnants 111 à 114.First of all, it includes four radiating antenna strands 11 1 to 11 4 .
Un mode de détermination des caractéristiques de ces brins est par exemple donné dans le brevet FR-89 14952 déjà cité.A method of determining the characteristics of these strands is for example given in patent FR-89 14952 already cited.
Les dimensions de l'antenne varient en fonction de la bande de fréquence et des couvertures exigées. A titre d'exemple, les dimensions de ces brins peuvent être les suivantes :
- longueur : 90 mm ;
- largeur : 2 mm ;
- épaisseur : 35 µm ;
- angle d'inclinaison : 54,5°.
- length: 90 mm;
- width: 2 mm;
- thickness: 35 µm;
- tilt angle: 54.5 °.
Ils sont par exemple réalisés en cuivre, sur un substrat diélectrique de faible épaisseur, tel que du kapton (εr ≈ 3,8).They are for example made of copper, on a thin dielectric substrate, such as kapton (ε r ≈ 3.8).
Les quatre brins 111 à 114 sont préférentiellement ouverts à leur extrémité
supérieure 151 à 154. Ils peuvent également être court-circuités. Toutefois, le système de
l'invention convient particulièrement à l'excitation d'antennes à brins plus ouverts qui, à
performances égales, possèdent des dimensions plus réduites que les antennes à brins
court-circuités.The four strands 11 1 to 11 4 are preferably open at their
L'autre extrémité 161 à 164 des brins est connectée aux lignes d'attaque du circuit
d'alimentation.The
Le système d'alimentation est réalisé sur le même substrat, dans le prolongement
de l'antenne. Il est formé de trois coupleurs hybrides 12, 13 et 14 conçus en éléments
semi-localisés.The supply system is produced on the same substrate, as an extension
of the antenna. It is made up of three
Le premier coupleur hybride 12 est relié d'une part à l'entrée (respectivement
sortie selon l'utilisation) 17 de signal de l'antenne, et d'autre aux deux entrées
(respectivement sorties) 18 et 19 des deux autres coupleurs 13 et 14. Il s'agit d'un
coupleur hybride 180°.The first
Les coupleurs hybrides 13 et 14 sont deux coupleurs identiques 90 °. Ils sont
reliés d'une part à l'entrée 18 (respectivement 19) et d'autre part à l'extrémité des brins
161 et 162 (respectivement 163 et 164).The
Ainsi, les quatre brins sont alimentés en parfaite quadrature de phase, sur une large bande.Thus, the four strands are supplied in perfect phase quadrature, on a broadband.
L'ensemble ainsi obtenu est ensuite enroulé sur un support cylindrique dans le sens trigonométrique, vers l'extérieur (les éléments imprimés étant à l'extérieur du cylindre), pour obtenir l'hélice externe, représentée en vue de face en figure 2.The assembly thus obtained is then wound on a cylindrical support in the counterclockwise, outward (the printed elements being outside the cylinder), to obtain the external propeller, shown in front view in Figure 2.
Le support cylindrique est un support transparent du point de vue radioélectrique, c'est-à-dire présentant une permittivité voisine de 1.The cylindrical support is a transparent support from the radioelectric point of view, that is to say having a permittivity close to 1.
Il est à noter qu'il est aisé de réduire encore la hauteur de l'ensemble, en utilisant un support de permittivité supérieure à 1, pour la partie correspondant aux brins d'antenne.It should be noted that it is easy to further reduce the height of the assembly, by using a support of permittivity greater than 1, for the part corresponding to the strands antenna.
La figure 3 illustre les éléments formant la couche interne de l'antenne,
représentés à plat. Ces éléments sont tout à fait similaires à ceux décrits en relation avec la
figure 1, si ce n'est que les brins d'antennes 511 à 514, sont inclinés dans le sens opposé,
le sens d'enroulement 52 étant opposé au sens d'enroulement 17 de la première hélice.FIG. 3 illustrates the elements forming the internal layer of the antenna, shown flat. These elements are quite similar to those described in connection with FIG. 1, except that the antenna strands 51 1 to 51 4 are inclined in the opposite direction, the winding
Le substrat diélectrique est dans cet exemple identique au premier. Le système
d'alimentation 53 se trouve également dans le prolongement des brins d'antennes 511 et
514 et est réalisé en éléments semi-localisés.In this example, the dielectric substrate is identical to the first. The system
power supply 53 is also in the extension of the
L'ensemble est ensuite, enroulé vers l'intérieur (flèche 52) sur un support transparent du point de vue radioélectrique, pour fournir l'hélice interne de la figure 4.The assembly is then wound inwards (arrow 52) on a support radio-transparent, to provide the internal helix of Figure 4.
Les deux couches ainsi obtenues sont finalement montées concentriquement l'une dans l'autre, ainsi que cela est illustré par la vue en coupe de la figure 5.The two layers thus obtained are finally mounted concentrically one in the other, as illustrated by the sectional view in FIG. 5.
La couche externe (formée des conducteurs externes 61) et la couche externe (formée des conducteurs internes 62) sont décalés d'un angle α = 135° par rapport à leurs points d'excitation.The outer layer (formed of the outer conductors 61) and the outer layer (formed of internal conductors 62) are offset by an angle α = 135 ° relative to their excitement points.
La figure 6 illustre de façon plus précise la structure d'alimentation en éléments serai-localisés selon l'invention, grossie sensiblement d'un facteur 3 par rapport à la réalité. Elle comprend deux types de lignes imprimées :
- des lignes de faible largeur, présentant une caractéristique inductive ;
- des lignes plus larges, présentant une caractéristique capacitive.
- lines of small width, having an inductive characteristic;
- wider lines, having a capacitive characteristic.
Ainsi, les coupleurs 90 ° 13 et 14 sont constitués chacun de 4 éléments larges 311
et 314, reliés 2 à 2 par 4 lignes de faible largeur 321 à 324. Le coupleur 190 ° comprend 6
éléments larges 331 à 336 reliés par 6 lignes de faible largeur 341 à 346.Thus, the 90 °
Les figures 7A et 7C illustrent la conception d'un coupleur -3 dB 90°.Figures 7A and 7C illustrate the design of a -
De plus amples informations pourront être trouvées, si nécessaire, dans la thèse de M. Coupez, Université de Bretagne Occidentale, "Etude de structures de déphaseurs potentiellement intégrables à 900 MHz", mai 1988.Further information can be found, if necessary, in the thesis from M. Coupez, University of Western Brittany, "Study of phase shifter structures potentially integrable at 900 MHz ", May 1988.
La figure 7A présente un schéma classique d'un coupleur -3 dB 90° en éléments
distribués. Il comprend deux tronçons de ligne 81, 82 de longueur λg/4 et d'impédance
caractéristique Zc, et deux tronçons de ligne 83, 84 de longueur λg/4, et d'impédance
Zc/√2.FIG. 7A presents a conventional diagram of a -
On peut remplacer chacun de ces tronçons de ligne par des cellules en π d'éléments localisés, formées de capacités C et d'inductances L et L', tel que cela est illustré en figure 7B.We can replace each of these line sections by cells in π of localized elements, formed of capacitances C and of inductances L and L ', such as illustrated in Figure 7B.
En utilisant les propriétés inductive (lignes de faible largeur 85) et capacitive (lignes plus large 86) des lignes microrubans, on peut alors transformer à nouveau le coupleur en éléments distribués, ainsi qu'illustré en figure 7C.Using the inductive (lines of small width 85) and capacitive properties (wider lines 86) microstrip lines, we can then transform the coupler in distributed elements, as illustrated in FIG. 7C.
On procède de même pour transformer la structure classique d'un anneau hybride -3 dB, 180 illustrée en figure 8A, en un coupleur en éléments semi-localisés, illustré en figure 8B.We do the same to transform the classic structure of a hybrid ring -3 dB, 180 illustrated in FIG. 8A, in a coupler in semi-localized elements, illustrated in Figure 8B.
Une telle hélice présente notamment les avantages suivants :
- elle est à brins ouverts, donc l'impédance de chaque brin est aisément adaptable à 50 Ω pour une antenne ayant les propriétés souhaitées (couverture hémisphérique et polarisation inverse faible) ;
- la structure d'alimentation utilisant des hybrides est large bande, et
parfaitement équilibrée :
- en amplitude (identique pour chaque brin) ; et
- en phase (0° ; ± 90° ; ± 180° ; ± 270°) ;
- les dimensions du dispositif d'alimentation sont plus faibles que celles des systèmes connus (un gain de l'ordre de 50 % peut être obtenu). En effet, on constate aisément que chaque élément semi-localisé est de taille très inférieure à la ligne qu'il remplace (qui est généralement d'une taille multiple de λ/4) ;
- l'antenne présente une forte isolation brin à brin.
- it is open stranded, so the impedance of each strand is easily adaptable to 50 Ω for an antenna having the desired properties (hemispherical coverage and weak reverse polarization);
- the feed structure using hybrids is broadband, and perfectly balanced:
- in amplitude (identical for each strand); and
- in phase (0 °; ± 90 °; ± 180 °; ± 270 °);
- the dimensions of the supply device are smaller than those of known systems (a gain of the order of 50% can be obtained). Indeed, we can easily see that each semi-localized element is very much smaller than the line it replaces (which is generally of a size multiple of λ / 4);
- the antenna has strong strand-by-strand insulation.
A titre indicatif, on présente maintenant les résultats de mesure obtenus à partir d'un mode de réalisation particulier, destiné aux communications avec les matériels et aux communications de proximité.As an indication, we now present the measurement results obtained from of a particular embodiment, intended for communications with the materials and for proximity communications.
Les dimensions de l'ensemble formé par l'antenne et l'alimentation intégrée sont les suivantes :
- diamètre : 26 mm ;
- hauteur : 130 mm;
- poids total : 70 g.
- diameter: 26 mm;
- height: 130 mm;
- total weight: 70 g.
Les caractéristiques radio-électriques relevées sont :
- émission : 2.17 - 2.2 GHz
- réception : 1.98 - 2.01 GHz
- polarisation : circulaire droite
- couverture : 180°
- ellipticité : < 5 dB pour < 90°
< 2 dB pour < 75° - défaut d'omnidirectionnalité : ± 0,6 dB à l'horizon.
- transmission: 2.17 - 2.2 GHz
- reception: 1.98 - 2.01 GHz
- polarization: right circular
- coverage: 180 °
- ellipticity: <5 dB for <90 °
<2 dB for <75 ° - omnidirectionality fault: ± 0.6 dB on the horizon.
Sur la figure 9 on présente le rapport d'onde stationnaire (ROS) à l'entrée de chaque antenne, en fonction de la fréquence de chacune des hélices. On constate que l'on obtient un ROS inférieur à 2 pour chaque antenne, dans une bande de 400 MHz.In Figure 9 we present the standing wave ratio (ROS) at the input of each antenna, as a function of the frequency of each of the propellers. We see that we obtains a ROS lower than 2 for each antenna, in a band of 400 MHz.
Les figures 10 et 11 sont relatives aux diagrammes de rayonnement mesurés en polarisation circulaire droite (a) et en polarisation circulaire gauche (6), avec un dipôle tournant respectivement aux fréquences 1,98 GHz (figure 10) et 2,2 GHz (figure 11).Figures 10 and 11 relate to the radiation patterns measured in right circular polarization (a) and left circular polarization (6), with a dipole operating respectively at 1.98 GHz (Figure 10) and 2.2 GHz (Figure 11) frequencies.
On peut observer que l'on obtient :
- une ouverture moyenne à -3 dB quasi-hémisphérique supérieure à 180° ;
- une réjection de la polarisation inverse supérieure à -15 dB dans toute la couverture.
- an average aperture at -3 dB quasi-hemispherical greater than 180 °;
- rejection of reverse polarization greater than -15 dB throughout the coverage.
La figure 12 montre que le découplage entre les deux hélices est supérieur à 20 dB.Figure 12 shows that the decoupling between the two propellers is greater than 20 dB.
Une antenne selon l'invention peut être réalisée de plusieurs façons.An antenna according to the invention can be produced in several ways.
Ainsi, selon un premier mode de réalisation, les hélices peuvent être imprimées à plat, tel qu'illustré en figure 1 et 3. Elles sont ensuite enroulées sur un support pour former l'antenne (figure 2 et 4).Thus, according to a first embodiment, the propellers can be printed at flat, as illustrated in FIGS. 1 and 3. They are then rolled up on a support for form the antenna (figures 2 and 4).
Selon un autre mode de réalisation, encore plus rapide, le substrat destiné à recevoir les éléments imprimés peut être réalisé directement dans sa forme cylindrique définitive. Dans ce cas, l'impression des brins et de la structure d'alimentation est effectué directement sur le cylindre. According to another, even faster embodiment, the substrate intended for receive the printed elements can be made directly in its cylindrical shape final. In this case, the printing of the strands and the feeding structure is carried out directly on the cylinder.
Par ailleurs, il est à noter que, bien qu'elle soit utilisable à l'unité, l'antenne de l'invention se prête avantageusement à la réalisation de réseaux d'antennes.In addition, it should be noted that, although it can be used individually, the antenna the invention advantageously lends itself to the production of antenna arrays.
Claims (10)
- Helical antenna operating in two neighbouring frequency bands corresponding respectively to transmission and reception, of the type having two coaxial helices each formed by radiating strands (111 to 114; 511 to 514) printed on a substrate,
characterised in that each of the said helices is associated with an independent feed and duplex structure, also printed on the said substrate and comprising at least one hybrid coupler (12, 13, 14) made from semi-localised elements which are obtained in the following way:designing a coupler comprising distributed elements, each section having a length at least equal to _g/4, _g being the maximum operating wavelength of the said antenna;determining a corresponding structure comprising localised elements, each of the said sections being replaced with a n cell formed by a capacitor C and two inductors L and L';determining a structure comprising semi-localised elements, in which structure each of the said capacitors C is replaced with a broad line (86) and each of the said inductors L and L' is replaced with a narrower line (85), - Antenna according to Claim 1, characterised in that the said helixes have, when they are placed flat, strands (111 to 114; 511 to 514) having symmetrical directions with respect to the axis of the said antenna, and are wound according to opposite winding directions so that the said strands are substantially parallel.
- Antenna according to either one of Claims 1 and 2, characterised in that the excitation points (61, 62) of each of the said quadrifilar helices are offset with respect to one another in a plane perpendicular to the axis of the said helices.
- Antenna according to Claim 3, characterised in that the said excitation points (61, 62) are offset by 135°.
- Antenna according to any one of Claims 1 to 4, characterised in that the said helices are quadrifilar helices, each formed by four radiating strands (111 to 114; 511 to 514) fed by a feed structure comprising three hybrid couplers.
- Antenna according to Claim 5, characterised in that each of the said feed structures comprises a first 180° hybrid coupler (12) associating a feed input and/or output of the said antenna with two intermediate outputs and/or inputs which are 180° out of phase, and two 90° hybrid couplers (13, 14) each associating one of the said intermediate outputs and/or inputs of the first hybrid coupler with one of the ends of two of the said radiating strands.
- Antenna according to one of Claims 1 to 6, characterised in that at least one of the said helices is mounted on a support having a first and a second separate part with different permittivities, the said first part carrying the said radiating strands (111 to 114; 511 to 514) and the said second part carrying the said feed structure.
- Antenna according to Claim 7, characterised in that the said first part carrying the said radiating strands (111 to 114; 511 to 514) has a permittivity which is greater than the permittivity of the said second part.
- Method of manufacturing a resonant helical antenna with integrated miniaturised duplex and feed means comprising two decoupled coaxial helices, characterised in that it comprises the following steps:printing, on a plane substrate, at least two radiating strands (111 to 114; 511 to 514) which are intended to form a helix, and an independent miniaturised broadband feed structure for the said radiating strands, comprising at least one hybrid coupler (12, 13, 14) made from semi-localised elements which are obtained in the following way:designing a coupler comprising distributed elements, each section having a length at least equal to _g/4, _g being the maximum operating wavelength of the said antenna;determining a corresponding structure comprising localised elements, each of the said sections being replaced with a n cell formed by a capacitor C and two inductors L and L';determining a structure comprising semi-localised elements, in which structure each of the said capacitors C is replaced with a broad line (86) and each of the said inductors L and L' is replaced with a narrower line (85),winding the said substrate around a cylindrical support.
- Method of manufacturing a resonant helical antenna with integrated miniaturised duplex and feed means comprising two decoupled coaxial helices, characterised in that it comprises the following steps:obtaining a cylindrical support carrying a substrate;printing, on the said substrate, at least two radiating strands (111 to 114; 511 to 514) which are intended to form a helix, and an independent miniaturised broadband feed structure for the said radiating strands, comprising at least one hybrid coupler (12, 13, 14) made from semi-localised elements which are obtained in the following way:designing a coupler comprising distributed elements, each section having a length at least equal to _g/4, _g being the maximum operating wavelength of the said antenna ;determining a corresponding structure comprising localised elements, each of the said sections being replaced with a n cell formed by a capacitor C and two inductors L and L';determining a structure comprising semi-localised elements, in which structure each of the said capacitors C is replaced with a broad line (86) and each of the said inductors L and L' is replaced with a narrower line (85),
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9603699 | 1996-03-19 | ||
FR9603699A FR2746548B1 (en) | 1996-03-19 | 1996-03-19 | HELICAL ANTENNA WITH INTEGRATED DUPLEXING MEANS, AND MANUFACTURING METHODS THEREOF |
PCT/FR1997/000456 WO1997035357A1 (en) | 1996-03-19 | 1997-03-13 | Helical antenna with built-in duplexing means, and manufacturing methods therefor |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0888648A1 EP0888648A1 (en) | 1999-01-07 |
EP0888648B1 true EP0888648B1 (en) | 2003-11-05 |
Family
ID=9490519
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP97914395A Expired - Lifetime EP0888648B1 (en) | 1996-03-19 | 1997-03-13 | Helical antenna with built-in duplexing means, and manufacturing methods therefore |
Country Status (9)
Country | Link |
---|---|
US (1) | US6608604B1 (en) |
EP (1) | EP0888648B1 (en) |
CN (1) | CN1218434C (en) |
AU (1) | AU2165197A (en) |
CA (1) | CA2248884A1 (en) |
DE (1) | DE69725972T2 (en) |
ES (1) | ES2212088T3 (en) |
FR (1) | FR2746548B1 (en) |
WO (1) | WO1997035357A1 (en) |
Families Citing this family (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6072441A (en) * | 1997-11-06 | 2000-06-06 | Nec Corporation | Method of producing a helical antenna and the helical antenna apparatus |
SE514568C2 (en) | 1998-05-18 | 2001-03-12 | Allgon Ab | An antenna device comprising feed means and a hand-held radio communication device for such an antenna device |
SE514530C2 (en) | 1998-05-18 | 2001-03-12 | Allgon Ab | An antenna device comprising capacitively coupled radio tower elements and a hand-held radio communication device for such an antenna device |
FR2814285A1 (en) * | 2000-09-15 | 2002-03-22 | France Telecom | VARIABLE STEP HELICOID ANTENNA, AND CORRESPONDING METHOD |
US7245268B2 (en) * | 2004-07-28 | 2007-07-17 | Skycross, Inc. | Quadrifilar helical antenna |
US7173576B2 (en) * | 2004-07-28 | 2007-02-06 | Skycross, Inc. | Handset quadrifilar helical antenna mechanical structures |
CN1314287C (en) * | 2005-06-24 | 2007-05-02 | 京信通信技术(广州)有限公司 | High-integrated universal duplexer module used for mobile communication duplex tower top amplifier |
DE102006021839A1 (en) * | 2006-05-10 | 2007-11-15 | Siemens Ag | Antenna and transmitting / receiving unit |
GB0700276D0 (en) * | 2007-01-08 | 2007-02-14 | Sarantel Ltd | A dielectrically-loaded antenna |
US8089421B2 (en) * | 2008-01-08 | 2012-01-03 | Sarantel Limited | Dielectrically loaded antenna |
WO2010103264A1 (en) * | 2009-03-12 | 2010-09-16 | Sarantel Limited | A dielectrically loaded antenna |
US8456375B2 (en) * | 2009-05-05 | 2013-06-04 | Sarantel Limited | Multifilar antenna |
CN101600269B (en) * | 2009-06-30 | 2011-06-08 | 华为技术有限公司 | Device, system and method for sharing antenna feeder |
CN102412859B (en) * | 2010-09-21 | 2013-12-04 | 中国科学院上海微系统与信息技术研究所 | Mixed radio-frequency duplexer based on discrete device |
US9923266B1 (en) | 2013-12-16 | 2018-03-20 | First Rf Corporation | Antenna array with tilted conical helical antennas |
US9343796B2 (en) * | 2014-07-15 | 2016-05-17 | Novatel Inc. | Wideband and low-loss quadrature phase quad-feeding network for high-performance GNSS antenna |
US10374299B1 (en) | 2015-02-06 | 2019-08-06 | First Rf Corporation | Method for making a radiator structure for a helical antenna |
EP4106106A1 (en) * | 2021-06-17 | 2022-12-21 | Rosenberger Hochfrequenztechnik GmbH & Co. KG | Antenna arrangement, transceiver arrangement and communication system |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4008479A (en) * | 1975-11-03 | 1977-02-15 | Chu Associates, Inc. | Dual-frequency circularly polarized spiral antenna for satellite navigation |
FR2654554B1 (en) * | 1989-11-10 | 1992-07-31 | France Etat | ANTENNA IN PROPELLER, QUADRIFILAIRE, RESONANT BICOUCHE. |
US5198831A (en) * | 1990-09-26 | 1993-03-30 | 501 Pronav International, Inc. | Personal positioning satellite navigator with printed quadrifilar helical antenna |
US5235296A (en) * | 1990-11-28 | 1993-08-10 | Matsushita Electric Industrial Co., Ltd. | Directional coupler using a microstrip line |
US5581268A (en) * | 1995-08-03 | 1996-12-03 | Globalstar L.P. | Method and apparatus for increasing antenna efficiency for hand-held mobile satellite communications terminal |
US5828348A (en) * | 1995-09-22 | 1998-10-27 | Qualcomm Incorporated | Dual-band octafilar helix antenna |
-
1996
- 1996-03-19 FR FR9603699A patent/FR2746548B1/en not_active Expired - Fee Related
-
1997
- 1997-03-13 US US09/142,967 patent/US6608604B1/en not_active Expired - Fee Related
- 1997-03-13 EP EP97914395A patent/EP0888648B1/en not_active Expired - Lifetime
- 1997-03-13 CA CA002248884A patent/CA2248884A1/en not_active Abandoned
- 1997-03-13 AU AU21651/97A patent/AU2165197A/en not_active Abandoned
- 1997-03-13 DE DE69725972T patent/DE69725972T2/en not_active Expired - Fee Related
- 1997-03-13 ES ES97914395T patent/ES2212088T3/en not_active Expired - Lifetime
- 1997-03-13 CN CN971945128A patent/CN1218434C/en not_active Expired - Fee Related
- 1997-03-13 WO PCT/FR1997/000456 patent/WO1997035357A1/en active IP Right Grant
Also Published As
Publication number | Publication date |
---|---|
WO1997035357A1 (en) | 1997-09-25 |
DE69725972D1 (en) | 2003-12-11 |
CN1218581A (en) | 1999-06-02 |
CN1218434C (en) | 2005-09-07 |
EP0888648A1 (en) | 1999-01-07 |
FR2746548B1 (en) | 1998-06-19 |
US6608604B1 (en) | 2003-08-19 |
ES2212088T3 (en) | 2004-07-16 |
CA2248884A1 (en) | 1997-09-25 |
DE69725972T2 (en) | 2004-09-02 |
FR2746548A1 (en) | 1997-09-26 |
AU2165197A (en) | 1997-10-10 |
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