EP0617477B1 - H-shaped waveguide structure defining a principal and two secondary waveguides for transporting waves having distinct frequencies. - Google Patents

H-shaped waveguide structure defining a principal and two secondary waveguides for transporting waves having distinct frequencies. Download PDF

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Publication number
EP0617477B1
EP0617477B1 EP94400524A EP94400524A EP0617477B1 EP 0617477 B1 EP0617477 B1 EP 0617477B1 EP 94400524 A EP94400524 A EP 94400524A EP 94400524 A EP94400524 A EP 94400524A EP 0617477 B1 EP0617477 B1 EP 0617477B1
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EP
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Prior art keywords
guide
line
primary
ribs
line according
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German (de)
French (fr)
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EP0617477A1 (en
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Bernard Debever
Thierry Jacqueminet
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Societe Anonyme de Telecommunications SAT
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Societe Anonyme de Telecommunications SAT
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    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q21/00Antenna arrays or systems
    • H01Q21/30Combinations of separate antenna units operating in different wavebands and connected to a common feeder system
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01PWAVEGUIDES; RESONATORS, LINES, OR OTHER DEVICES OF THE WAVEGUIDE TYPE
    • H01P3/00Waveguides; Transmission lines of the waveguide type
    • H01P3/12Hollow waveguides
    • H01P3/123Hollow waveguides with a complex or stepped cross-section, e.g. ridged or grooved waveguides
    • 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
    • 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
    • H01Q5/40Imbricated or interleaved structures; Combined or electromagnetically coupled arrangements, e.g. comprising two or more non-connected fed radiating elements

Definitions

  • the present invention relates to a waveguide line with two symmetrical internal ribs, arranged to provide a median constriction in the guide and reduce the cut-off frequency of the guide, and to an excitation probe plunging into the constriction.
  • a missile On board a missile, for example, it can be used, which is also radiated at the end to serve as an antenna, between a transmitter, for example again, for telemetry or trajectography, and an orifice made in the skin of the missile. Telemetry is carried out in a frequency band around 2 GHz, trajectography in a band around 5 GHz.
  • a waveguide Since a waveguide has a cross section adapted to a single frequency range, as many radiation guides and orifices are needed as there are applications. It is an expensive and cumbersome solution because the orifices must be protected by materials transparent to radiation and often withstand heating. In addition, the radiation holes are very troublesome, because they can create a surface discontinuity and alter the aerodynamics of the craft.
  • the present invention therefore aims to propose a waveguide line adapted to at least two distinct frequency ranges.
  • the invention relates to a line of the type defined above in which two secondary split guides of cross section smaller than that of the waveguide line with two ribs, called primary, being thus formed on both sides.
  • other of the median constriction, constituting a median slot for the secondary guides there is provided a another excitation probe plunging into one of the two secondary guides.
  • the primary guide is designed to transmit a first frequency band, thanks to the fact that the constriction creates a primary guide with double groove and two lateral secondary guides.
  • Each secondary guide can transmit, without being disturbed, despite the constriction acting as a median slot, a second frequency in a second frequency band which is specific to it.
  • a rib makes it possible to reduce the section of the primary waveguide line for the same band of transmitted frequencies, or else, with a maintained section, to reduce the cut-off frequency.
  • each secondary guide has a smaller section than that of the primary guide, the frequencies of the band of the secondary guides are higher than those of the primary band.
  • the secondary guides are internally ribbed, with the advantages mentioned above.
  • the ribs of the primary guide can be shaped to constitute a rib in each ribbed secondary guide.
  • the cross section of the primary guide is a rectangle.
  • the line is open at one end, to form a waveguide antenna with radiation at the end.
  • the line guide of Figures 1 and 2 is a guide with a rectangular cross section. It has two internal ribs 4 and 6, T-shaped which extend over the entire length of the guide. Transversally, they extend, by their feet, from the middle of the long sides of the rectangle of the guide section.
  • the two ribs 4 and 6 are symmetrical with respect to a longitudinal median plane 10 of the guide and form between them a median longitudinal throttle 8.
  • the constriction 8, of rectangular section in FIG. 1, constitutes the central part of a cavity 12, forming a primary guide, which therefore comprises two secondary cavities 14 and 16 physically connected by the constriction 8.
  • the secondary cavities 14 and 16 are arranged symmetrically on either side of a plane of symmetry 11 of the ribs 4 and 6, thus than the guide.
  • Each secondary cavity 14 and 16 forms a secondary guide of generally rectangular cross section, the length of which extends parallel to the width of the cross section of the primary guide 12.
  • the ends of the bars of the T of the ribs 4 and 6 form, in each secondary guide 14 and 16, a pair of ribs, respectively 41, 61 and 42, 62.
  • the distance separating the ribs 4 and 6 being relatively small compared to the length of the walls 7 and 9, the ribs of each secondary guide can be considered as adjacent, as if the constriction did not exist.
  • the probe 23 is arranged to excite the primary waveguide line in linear polarization at a first frequency, of a value chosen so that the corresponding electromagnetic wave propagates in the guide line using the entire volume of the primary guide 12.
  • the secondary guide 14 has a bore 24 formed in the wall 7 in the median plane 10.
  • the waveguide lines radiate at their ends opposite to that of the excitation probes 23 and 25.
  • the two electromagnetic waves generated by the probes 23 and 25 propagate perpendicular to the plane of FIG. 1, in the direction of the radiation end close to the cross section shown in FIG. 2.
  • the wave at the first frequency propagates occupying the entire volume of the primary guide 12.
  • the wave at the second frequency propagates with a polarization orthogonal to that of the first wave, so that there is absence of coupling and corresponding loss. Measurements have shown that decoupling exceeds 40 decibels. The direction of the polarization of the wave at the second frequency prevents a transfer of energy from this wave from the first secondary guide 14 to the other secondary guide 16 through the throttle 8.
  • the end of the constriction 8 opening into the secondary guide 14 constitutes a slot extending along the length of the secondary guide line, perpendicular to the plane of the figures.
  • the slot described above is located in the median plane 10.
  • a slot of this kind does not cause losses as long as its width is small relative to the length of the wall in which it is formed, which is the case here.
  • the radiating opening of the waveguide line forms an antenna, shown in cross section in Figure 2, the other end of the line being closed.
  • the upper bar of the T of each rib 4 and 6 has a central notch 65, 66, here rectangular, between its ends, respectively 41, 42 and 61, 62, which widens the constriction 8 in the central part of its cross section, while keeping the width of the constriction 8 constant at its outlet forming a slot in each secondary guide 14 and 16.
  • the depth of the notch indicated above is all the greater the closer the section considered is to the radiating opening.
  • the modification of the shape of the throttle 8 has the effect of adapting the characteristic line impedance to that presented by the load at the end of the line, that is to say the air.
  • the progressiveness of the transition avoids the creation of significant parasitic reflections, the report standing waveform being less than 1.5 in the vicinity of the central frequency of the primary guide 12.
  • the modification of the shape of the constriction 8 exposed above is only a particular example and other modifications of shape are possible. In particular, they can also bear on the shape of the ribs 41, 42, 61 and 62 of the secondary guides 14 and 16.
  • the secondary guides 14, 16 could comprise a second rib, like that (63, 64) s' extending along the wall 7, 9 opposite the slot 8, and shown in broken lines in Figure 1, for example in one piece with the associated wall.

Description

La présente invention concerne une ligne guide d'ondes à deux nervures internes symétriques, agencées pour ménager un étranglement médian dans le guide et diminuer la fréquence de coupure du guide, et à une sonde d'excitation plongeant dans l'étranglement.The present invention relates to a waveguide line with two symmetrical internal ribs, arranged to provide a median constriction in the guide and reduce the cut-off frequency of the guide, and to an excitation probe plunging into the constriction.

A bord d'un missile, par exemple, on peut en utiliser, qu'on fait d'ailleurs rayonner en bout pour servir d'antenne, entre un émetteur, par exemple encore, de télémesure ou de trajectographie, et un orifice ménagé dans la peau du missile. La télémesure est effectuée dans une bande de fréquences autour de 2 GHz, la trajectographie, dans une bande autour de 5 GHz.On board a missile, for example, it can be used, which is also radiated at the end to serve as an antenna, between a transmitter, for example again, for telemetry or trajectography, and an orifice made in the skin of the missile. Telemetry is carried out in a frequency band around 2 GHz, trajectography in a band around 5 GHz.

Comme un guide d'ondes a une section adaptée à une seule plage de fréquences, il faut autant de guides et d'orifices de rayonnement que d'applications. C'est une solution coûteuse et encombrante car les orifices doivent être protégés par des matériaux transparents aux rayonnements et souvent résister à l'échauffement. En outre, les orifices de rayonnement sont très gênants, car ils peuvent créer une discontinuité de surface et altèrent l'aérodynamisme de l'engin. Since a waveguide has a cross section adapted to a single frequency range, as many radiation guides and orifices are needed as there are applications. It is an expensive and cumbersome solution because the orifices must be protected by materials transparent to radiation and often withstand heating. In addition, the radiation holes are very troublesome, because they can create a surface discontinuity and alter the aerodynamics of the craft.

L'article de J.E. STORER et al., paru dans IRE TRANSACTIONS ON MICROWAVE THEORY AND TECHNIQUES, vol. 3, no 2, Mars 1961, New-York (US), pages 116 à 123, intitulé "TEM impedance and cross-coupling for small circular center conductors in a double ridged waveguide" propose une structure guide d'ondes à étranglement médian, c'est-à-dire un guide en H, dans laquelle un conducteur central est disposé dans chacun des espaces situés de part et d'autre de l'étranglement de manière à transmettre des signaux en mode TEM.The article by J.E. STORER et al., Published in IRE TRANSACTIONS ON MICROWAVE THEORY AND TECHNIQUES, vol. 3, no 2, March 1961, New York (US), pages 116 to 123, entitled "TEM impedance and cross-coupling for small circular center conductors in a double ridged waveguide" proposes a waveguide structure with median throttling, that is to say, an H guide, in which a central conductor is arranged in each of the spaces situated on either side of the constriction so as to transmit signals in TEM mode.

En outre, le brevet américan US-A-4 119 967 décrit une structure de couplage par sonde introduite dans l'étranglement d'un guide d'ondes en H.In addition, American patent US-A-4 119 967 describes a probe coupling structure introduced into the throttle of an H wave guide.

La présente invention vise donc à proposer une ligne guide d'ondes adaptée à au moins deux plages de fréquences distinctes.The present invention therefore aims to propose a waveguide line adapted to at least two distinct frequency ranges.

A cet effet, l'invention concerne une ligne du type défini ci-dessus dans laquelle deux guides fendus secondaires de section transversale inférieure à celle de la ligne guide d'ondes à deux nervures, dite primaire, étant ainsi formés de part et d'autre de l'étranglement médian, constituant une fente médiane pour les guides secondaires, il est prévu une autre sonde d'excitation plongeant dans l'un des deux guides secondaires.To this end, the invention relates to a line of the type defined above in which two secondary split guides of cross section smaller than that of the waveguide line with two ribs, called primary, being thus formed on both sides. other of the median constriction, constituting a median slot for the secondary guides, there is provided a another excitation probe plunging into one of the two secondary guides.

On soulignera que, pour l'homme de métier, c'étaient la forme et la taille d'un guide d'ondes qui déterminaient, dans le mode fondamental, l'unique plage des fréquences pouvant être transmises et qu'il apparaissait donc a priori exclu de vouloir transmettre plusieurs plages de fréquences dans un même guide.It will be emphasized that, for the person skilled in the art, it was the shape and size of a waveguide which determined, in the fundamental mode, the only range of frequencies that can be transmitted and that it therefore appeared to be a priori excluded from wanting to transmit several frequency ranges in the same guide.

Ainsi, le guide primaire est prévu pour transmettre une première bande de fréquences, grâce au fait que l'étranglement crée un guide primaire à double rainure et deux guides secondaires latéraux.Thus, the primary guide is designed to transmit a first frequency band, thanks to the fact that the constriction creates a primary guide with double groove and two lateral secondary guides.

Chaque guide secondaire peut transmettre, sans être perturbé, malgré l'étranglement faisant office de fente médiane, une deuxième fréquence dans une deuxième bande de fréquences qui lui est propre.Each secondary guide can transmit, without being disturbed, despite the constriction acting as a median slot, a second frequency in a second frequency band which is specific to it.

Une nervure permet de réduire la section de la ligne guide d'onde primaire pour une même bande de fréquences transmises, ou bien, à section maintenue, de diminuer la fréquence de coupure.A rib makes it possible to reduce the section of the primary waveguide line for the same band of transmitted frequencies, or else, with a maintained section, to reduce the cut-off frequency.

Comme chaque guide secondaire a une section inférieure à celle du guide primaire, les fréquences de la bande des guides secondaires sont plus élevées que celles de la bande primaire.As each secondary guide has a smaller section than that of the primary guide, the frequencies of the band of the secondary guides are higher than those of the primary band.

Avantageusement, les guides secondaires sont intérieurement nervurés, avec les avantages ci-dessus mentionnés.Advantageously, the secondary guides are internally ribbed, with the advantages mentioned above.

En particulier, les nervures du guide primaire peuvent être conformées pour constituer une nervure dans chaque guide secondaire nervuré.In particular, the ribs of the primary guide can be shaped to constitute a rib in each ribbed secondary guide.

Avantageusement, la section transversale du guide primaire est un rectangle.Advantageously, the cross section of the primary guide is a rectangle.

Dans la forme de réalisation préférée de l'invention, la ligne est ouverte à un bout, pour constituer une antenne guide d'ondes à rayonnement en bout.In the preferred embodiment of the invention, the line is open at one end, to form a waveguide antenna with radiation at the end.

L'invention sera mieux comprise à l'aide de la description suivante de la forme de réalisation préférée de la ligne-antenne de l'invention, en référence au dessin annexé sur lequel :

  • la figure 1 est une vue en coupe transversale de la ligne guide d'ondes de l'invention, selon un plan proche de son extrémité d'excitation et
  • la figure 2 est une vue en coupe analogue à celle de la figure 1, mais dans un plan proche de son extrémité de rayonnement.
The invention will be better understood using the following description of the preferred embodiment of the antenna line of the invention, with reference to the attached drawing in which:
  • FIG. 1 is a cross-sectional view of the waveguide line of the invention, along a plane close to its excitation end, and
  • Figure 2 is a sectional view similar to that of Figure 1, but in a plane close to its radiation end.

Le guide de la ligne des figures 1 et 2 est un guide à section transversale rectangulaire. Il comporte deux nervures internes 4 et 6, en forme de T qui s'étendent sur toute la longueur du guide. Transversalement, elles s'étendent, par leur pied, depuis le milieu des grands côtés du rectangle de la section du guide. Les deux nervures 4 et 6 sont symétriques par rapport à un plan médian longitudinal 10 du guide et ménagent entre elles un étranglement longitudinal médian 8.The line guide of Figures 1 and 2 is a guide with a rectangular cross section. It has two internal ribs 4 and 6, T-shaped which extend over the entire length of the guide. Transversally, they extend, by their feet, from the middle of the long sides of the rectangle of the guide section. The two ribs 4 and 6 are symmetrical with respect to a longitudinal median plane 10 of the guide and form between them a median longitudinal throttle 8.

L'étranglement 8, de section rectangulaire sur la figure 1, constitue la partie centrale d'une cavité 12, formant un guide primaire, qui comporte donc deux cavités secondaires 14 et 16 reliées physiquement par l'étranglement 8. Les cavités secondaires 14 et 16 sont disposées symétriquement de part et d'autre d'un plan de symétrie 11 des nervures 4 et 6, ainsi que du guide. Chaque cavité secondaire 14 et 16 forme un guide secondaire de section transversale globalement rectangulaire, dont la longueur s'étend parallèlement à la largeur de la section transversale du guide primaire 12. Les parois 7 et 9, disposées chacune selon une largeur de la section transversale du guide primaire 12, forment respectivement deux parois des deux guides secondaires 14 et 16 et constituent des longueurs des sections transversales des guides secondaires.The constriction 8, of rectangular section in FIG. 1, constitutes the central part of a cavity 12, forming a primary guide, which therefore comprises two secondary cavities 14 and 16 physically connected by the constriction 8. The secondary cavities 14 and 16 are arranged symmetrically on either side of a plane of symmetry 11 of the ribs 4 and 6, thus than the guide. Each secondary cavity 14 and 16 forms a secondary guide of generally rectangular cross section, the length of which extends parallel to the width of the cross section of the primary guide 12. The walls 7 and 9, each arranged along a width of the cross section of the primary guide 12, respectively form two walls of the two secondary guides 14 and 16 and constitute lengths of the cross sections of the secondary guides.

Les extrémités des barres des T des nervures 4 et 6 forment, dans chaque guide secondaire 14 et 16, une paire de nervures, respectivement 41, 61 et 42, 62. La distance séparant les nervures 4 et 6 étant relativement faible par rapport à la longueur des parois 7 et 9, les nervures de chaque guide secondaire peuvent être considérées comme voisines, comme si l'étranglement n'existait pas.The ends of the bars of the T of the ribs 4 and 6 form, in each secondary guide 14 and 16, a pair of ribs, respectively 41, 61 and 42, 62. The distance separating the ribs 4 and 6 being relatively small compared to the length of the walls 7 and 9, the ribs of each secondary guide can be considered as adjacent, as if the constriction did not exist.

Un alésage 22, traversant le pied de la nervure 4, sensiblement dans le plan 11, reçoit une sonde d'excitation 23 disposée perpendiculairement au plan médian 10 et dont l'extrémité plonge dans l'étranglement 8. La sonde 23 est agencée pour exciter la ligne guide d'ondes primaire en polarisation linéaire à une première fréquence, de valeur choisie pour que l'onde électromagnétique correspondante se propage dans la ligne guide en utilisant la totalité du volume du guide primaire 12.A bore 22, passing through the base of the rib 4, substantially in the plane 11, receives an excitation probe 23 disposed perpendicular to the median plane 10 and the end of which plunges into the constriction 8. The probe 23 is arranged to excite the primary waveguide line in linear polarization at a first frequency, of a value chosen so that the corresponding electromagnetic wave propagates in the guide line using the entire volume of the primary guide 12.

Le guide secondaire 14 comporte un alésage 24 ménagé dans la paroi 7 dans le plan médian 10. Une sonde d'excitation 25, traversant l'alésage 24 perpendiculairement à la paroi 7 et plongeant dans le guide secondaire 14, transmet à celui-ci une excitation électromagnétique en polarisation linéaire à une deuxième fréquence dont la valeur permet la propagation de l'onde électromagnétique correspondante le long de la seule ligne guide secondaire 14.The secondary guide 14 has a bore 24 formed in the wall 7 in the median plane 10. An excitation probe 25, passing through the bore 24 perpendicular to the wall 7 and plunging into the secondary guide 14, transmits to the latter a electromagnetic excitation in linear polarization at a second frequency whose value allows the propagation of the corresponding electromagnetic wave along the single secondary guide line 14.

Dans le présent exemple, les lignes guides d'ondes rayonnent par leur extrémité opposée à celle des sondes d'excitation 23 et 25.In the present example, the waveguide lines radiate at their ends opposite to that of the excitation probes 23 and 25.

Le fonctionnement des lignes guides d'ondes est le suivant.The operation of the waveguide lines is as follows.

Les deux ondes électromagnétiques engendrées par les sondes 23 et 25 se propagent perpendiculairement au plan de la figure 1, en direction de l'extrémité de rayonnement voisine de la section transversale représentée sur la figure 2.The two electromagnetic waves generated by the probes 23 and 25 propagate perpendicular to the plane of FIG. 1, in the direction of the radiation end close to the cross section shown in FIG. 2.

L'onde à la première fréquence se propage en occupant la totalité du volume du guide primaire 12.The wave at the first frequency propagates occupying the entire volume of the primary guide 12.

Dans le guide secondaire 14, l'onde à la deuxième fréquence se propage avec une polarisation orthogonale à celle de la première onde, si bien qu'il y a absence de couplage et de perte correspondante. Des mesures ont prouvé que le découplage dépasse 40 décibels. La direction de la polarisation de l'onde à la deuxième fréquence empêche un transfert d'énergie de cette onde du premier guide secondaire 14 vers l'autre guide secondaire 16 à travers l'étranglement 8.In the secondary guide 14, the wave at the second frequency propagates with a polarization orthogonal to that of the first wave, so that there is absence of coupling and corresponding loss. Measurements have shown that decoupling exceeds 40 decibels. The direction of the polarization of the wave at the second frequency prevents a transfer of energy from this wave from the first secondary guide 14 to the other secondary guide 16 through the throttle 8.

L'extrémité de l'étranglement 8 débouchant dans le guide secondaire 14 constitue une fente s'étendant selon la longueur de la ligne guide secondaire, perpendiculairement au plan des figures. Dans le plan de celles-ci, la fente décrite ci-dessus est située dans le plan médian 10. Comme cela est connu, une fente de ce genre n'est pas cause de pertes tant que sa largeur est faible par rapport à la longueur de la paroi dans laquelle elle est ménagée, ce qui est le cas ici.The end of the constriction 8 opening into the secondary guide 14 constitutes a slot extending along the length of the secondary guide line, perpendicular to the plane of the figures. In the plane of these, the slot described above is located in the median plane 10. As is known, a slot of this kind does not cause losses as long as its width is small relative to the length of the wall in which it is formed, which is the case here.

Pour la clarté de l'exposé, il n'a pas été prévu de transmettre une troisième fréquence dans le guide secondaire 16.For the sake of clarity, it has not been planned to transmit a third frequency in the secondary guide 16.

L'ouverture rayonnante de la ligne guide d'ondes, primaire ou secondaire, forme une antenne, représentée en coupe transversale sur la figure 2, l'autre bout de la ligne étant fermé. A la différence de ce qui est représenté sur la figure 1, la barre supérieure du T de chaque nervure 4 et 6 comporte une échancrure centrale 65, 66, ici rectangulaire, entre ses extrémités, respectivement 41, 42 et 61, 62, ce qui élargit l'étranglement 8 dans la partie centrale de sa section transversale, tout en maintenant constante la largeur de l'étranglement 8 à son débouché formant fente dans chaque guide secondaire 14 et 16. Pour d'autres sections de ligne guide parallèles à celle de la figure 2 et voisines de celle-ci, la profondeur de l'échancrure indiquée ci-dessus est d'autant plus grande que la section considérée est proche de l'ouverture rayonnante.The radiating opening of the waveguide line, primary or secondary, forms an antenna, shown in cross section in Figure 2, the other end of the line being closed. Unlike what is shown in FIG. 1, the upper bar of the T of each rib 4 and 6 has a central notch 65, 66, here rectangular, between its ends, respectively 41, 42 and 61, 62, which widens the constriction 8 in the central part of its cross section, while keeping the width of the constriction 8 constant at its outlet forming a slot in each secondary guide 14 and 16. For other guide line sections parallel to that of Figure 2 and adjacent to it, the depth of the notch indicated above is all the greater the closer the section considered is to the radiating opening.

La modification de la forme de l'étranglement 8 a pour effet d'adapter l'impédance caractéristique de ligne à celle présentée par la charge en bout de ligne, c'est-à-dire l'air. La progressivité de la transition évite la création de réflexions parasites importantes, le rapport relevé d'onde stationnaire étant inférieur à 1,5 au voisinage de la fréquence centrale du guide primaire 12.The modification of the shape of the throttle 8 has the effect of adapting the characteristic line impedance to that presented by the load at the end of the line, that is to say the air. The progressiveness of the transition avoids the creation of significant parasitic reflections, the report standing waveform being less than 1.5 in the vicinity of the central frequency of the primary guide 12.

La modification de la forme de l'étranglement 8 exposée ci-dessus n'est qu'un exemple particulier et d'autres modifications de forme sont envisageables. En particulier, elles peuvent aussi porter sur la forme des nervures 41, 42, 61 et 62 des guides secondaires 14 et 16. De même, les guides secondaires 14, 16 pourraient comporter une deuxième nervure, comme celle (63, 64) s'étendant le long de la paroi 7, 9 opposée à la fente 8, et représentée en tirets sur la figure 1, par exemple d'une seule pièce avec la paroi associée.The modification of the shape of the constriction 8 exposed above is only a particular example and other modifications of shape are possible. In particular, they can also bear on the shape of the ribs 41, 42, 61 and 62 of the secondary guides 14 and 16. Similarly, the secondary guides 14, 16 could comprise a second rib, like that (63, 64) s' extending along the wall 7, 9 opposite the slot 8, and shown in broken lines in Figure 1, for example in one piece with the associated wall.

Claims (9)

  1. A wave guide line with two symmetrical internal ribs (4, 6) arranged to provide a median restriction (8) in the guide and to decrease the cut-off frequency of the guide, and with an excitation probe (23) plugged in the restriction (8), characterised in that two secondary slit guides (14, 16) with a transverse section smaller than that of the wave guide line with two ribs, called primary (12), being thus formed on both sides of the median restriction (8) constituting a middle slit for the secondary guides, another excitation probe (25) is provided which is plugged one of the two secondary guides (14).
  2. A line according to claim 1, wherein both secondary guides (14, 16) are also internally ribbed (41, 61, 63; 42, 62, 64).
  3. A line according to one of claims 1 and 2, wherein the ribs (4, 6) of the primary guide (12) are formed so as to constitute a rib (41, 61; 42, 62) in each ribbed secondary guide (14, 16).
  4. A line according to one of claims 1 to 3, wherein the two probes (23, 25) are disposed to produce two orthogonal fields respectively.
  5. A line according to one of claims 1 to 4, wherein the restriction (8) of the primary guide (12) is relatively thin in relation to the dimensions of its transverse section (7).
  6. A line according to one of claims 1 to 5, wherein the transverse section of the primary guide is a rectangle.
  7. A line according to claim 6, wherein the restriction (8) of the primary guide (12) extends in parallel with the length of the said rectangle.
  8. An end radiating wave guide antenna characterised in that it is made of the wave guide line according to one of claims 1 to 7, which, further, is also open at one end.
  9. An antenna according to claim 8, wherein the ribs of the ribbed primary guide (12) and ribbed secondary guide (14, 16) of the line which is open at one end are formed to match the impedances at the opening of the line.
EP94400524A 1993-03-23 1994-03-10 H-shaped waveguide structure defining a principal and two secondary waveguides for transporting waves having distinct frequencies. Expired - Lifetime EP0617477B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR9303301A FR2703189B1 (en) 1993-03-23 1993-03-23 Waveguide line.
FR9303301 1993-03-23

Publications (2)

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EP0617477A1 EP0617477A1 (en) 1994-09-28
EP0617477B1 true EP0617477B1 (en) 1997-06-04

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EP94400524A Expired - Lifetime EP0617477B1 (en) 1993-03-23 1994-03-10 H-shaped waveguide structure defining a principal and two secondary waveguides for transporting waves having distinct frequencies.

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DE (1) DE69403530T2 (en)
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Publication number Priority date Publication date Assignee Title
US20170237176A1 (en) * 2015-02-17 2017-08-17 City University Of Hong Kong Differential planar aperture antenna

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Publication number Priority date Publication date Assignee Title
JP7117409B1 (en) * 2021-03-01 2022-08-12 アンリツ株式会社 Transmission line coupling structure

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US4119967A (en) * 1976-05-21 1978-10-10 Teledyne, Inc. Microwave dual mode non-interfering CW and pulsed signal system method and apparatus

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US2441574A (en) * 1944-02-29 1948-05-18 Sperry Corp Electromagnetic wave guide
IT1149770B (en) * 1982-02-25 1986-12-10 Italtel Spa CIRCUIT TO SEPARATE TWO BANDS OF FREQUENCIES FOR HIGH-FREQUENCY DOUBLE POLARIZATION SIGNALS

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US4119967A (en) * 1976-05-21 1978-10-10 Teledyne, Inc. Microwave dual mode non-interfering CW and pulsed signal system method and apparatus

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20170237176A1 (en) * 2015-02-17 2017-08-17 City University Of Hong Kong Differential planar aperture antenna
US10050350B2 (en) * 2015-02-17 2018-08-14 City University Of Hong Kong Differential planar aperture antenna

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Publication number Publication date
EP0617477A1 (en) 1994-09-28
DE69403530T2 (en) 1998-01-29
FR2703189B1 (en) 1995-05-24
DE69403530D1 (en) 1997-07-10
FR2703189A1 (en) 1994-09-30

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