EP2469649B1 - Radiofrequency antenna with multiple radiating elements for transmission of a wave with variable propagation direction - Google Patents

Radiofrequency antenna with multiple radiating elements for transmission of a wave with variable propagation direction Download PDF

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Publication number
EP2469649B1
EP2469649B1 EP11306778.9A EP11306778A EP2469649B1 EP 2469649 B1 EP2469649 B1 EP 2469649B1 EP 11306778 A EP11306778 A EP 11306778A EP 2469649 B1 EP2469649 B1 EP 2469649B1
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European Patent Office
Prior art keywords
antenna elements
antenna
emission
emission surface
relative
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EP11306778.9A
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German (de)
French (fr)
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EP2469649A1 (en
Inventor
Jean-Pierre Brasile
Friedman Tchoffo Talom
Patrick Sirot
Dominique Fasse
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Thales SA
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Thales SA
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    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q3/00Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system
    • H01Q3/02Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical movement of antenna or antenna system as a whole
    • H01Q3/08Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical movement of antenna or antenna system as a whole for varying two co-ordinates of the orientation
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q11/00Electrically-long antennas having dimensions more than twice the shortest operating wavelength and consisting of conductive active radiating elements
    • H01Q11/02Non-resonant antennas, e.g. travelling-wave antenna
    • H01Q11/08Helical antennas
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q21/00Antenna arrays or systems
    • H01Q21/06Arrays of individually energised antenna units similarly polarised and spaced apart
    • H01Q21/061Two dimensional planar arrays
    • H01Q21/067Two dimensional planar arrays using endfire radiating aerial units transverse to the plane of the array
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q3/00Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system
    • H01Q3/26Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the relative phase or relative amplitude of energisation between two or more active radiating elements; varying the distribution of energy across a radiating aperture
    • H01Q3/30Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the relative phase or relative amplitude of energisation between two or more active radiating elements; varying the distribution of energy across a radiating aperture varying the relative phase between the radiating elements of an array

Definitions

  • the present invention relates to a radiofrequency antenna, of the type comprising a frame and an emission surface carrying a set of radiating antenna elements, each in a direction of emission own.
  • a radial antenna based on helical radiating antenna elements consists of a radial transmission line, which can be powered by its center or by its periphery, and a set of antenna elements. radiating regularly distributed.
  • Each antenna element comprises a helically radiating strand projecting from the emission face.
  • the strand is connected to a capture loop present inside the radial transmission line of the antenna, on the other side of the emission surface.
  • Each of the helically radiating strands is positioned with an initial angle so as to form, for example, a coherent electromagnetic field whose direction of propagation is perpendicular to the emission surface.
  • the starting angle of the helices of each antenna element is fixed once and for all so that the phase shift between the different antenna elements allows the coherent addition in the desired transmission direction.
  • the antenna In order to change the direction of transmission of the antenna, it is known to mount the antenna on an articulated and motorized support for moving the entire antenna, including its transmitting surface and all the elements. antennas that are present, as well as the support frame of the transmitting surface.
  • the source of electromagnetic radiation used to power the antenna with very high power is generally a relativistic source (high power magnetron, "Magnetically Insulated Line Oscillator” (MILO), carcinotron, relativistic klystron for example).
  • MILO Magnetically Insulated Line Oscillator
  • the source assembly, connection guide, antenna must then be kept under vacuum and is difficult to deform, because of the risk of breakdown limiting the technologies and architectures that allow pointing of the antenna in a particular direction, other than by moving the assembly.
  • the object of the invention is to propose a radiofrequency antenna that can be used in an arrangement where the direction of the field radiated by the antenna is angularly movable in one or two directions, without requiring complex deformable guide elements or displacement. large masses.
  • the subject of the invention is a radiofrequency antenna of the aforementioned type, according to claim 1.
  • Each antenna element is at least partially displaceable with respect to the emission surface in order to modify its own emission direction and it comprises means for moving the antenna elements in a coordinated manner along said surface to form, from the elementary waves produced by the antenna elements, a coherent wave propagating in a direction angularly offset relative to the normal to the emission surface.
  • the antenna elements each having a transmission strand rotatably mounted relative to the emission surface and the means for moving the antenna elements are adapted to drive the rotating antenna elements
  • the displacement means comprise racks slidably mounted relative to the emission surface and the transmission strands are integral with driving gears engaged with the racks and in that the displacement means comprise a mechanism for synchronized movement of the racks
  • the displacement mechanism synchronized comprises a rotary control ring relative to the frame and provided with control cams of the racks, the racks being each equipped with at least one cam follower cooperating with a cam, and a drive motor in rotation of the ring.
  • the antenna 20 according to the invention is shown in plan view and in section on the figure 1 and in cross section on the figure 2 . It has a general shape of disk axis X1-X1. According to the invention, each antenna 20 is able to emit in a direction TT angularly offset by an angle ⁇ with respect to the axis X1-X1 of the antenna.
  • Its planar emission surface consists of a circular plate 22 rotatable about the axis X1-X1 and on which is disposed a set of radiating antenna elements 24 regularly distributed on the surface of the plate 22.
  • the antenna elements are each able to produce an elementary wave, each following a own emission direction and with a proper phase shift so that the addition of the elementary waves produce a coherent wave in the direction TT.
  • These antenna elements each have an axis X2-X2 normally perpendicular to the plate 22.
  • the antenna is equipped according to the invention means 25 for moving the antenna elements relative to the emission surface to change their direction of emission and / or their phase.
  • the means 25 are able to produce a rotational movement on themselves of all or part of the antenna elements.
  • the plate 22 is carried by a frame 26 in the general shape of a bell flaring progressively from an inlet 27 for collecting the magnetic radiation from the source to a mouth 28 of the radiation output from the antenna elements 24.
  • the mouth is closed by an airtight protective wall 30 for creating the vacuum inside the frame 26.
  • the wall 30 is transparent to the electromagnetic radiation and radome form.
  • the inlet end 27 of the frame 26 is formed of a tube extended by a ring 34 forming the bottom of the frame.
  • This ring is of axis X1-X1.
  • the bottom is extended by a first peripheral wall 36 having at its end facing the mouth 28 a diverging shoulder 38 forming a support.
  • This shoulder is bordered by a second peripheral wall 40 carrying the protective wall 30.
  • the plate 22 is supported on an inner peripheral rim 44 of the side wall 34.
  • This flange 44 forms a bearing guide for rotation of the plate 22 about the axis X1-X1.
  • it is advantageously equipped with a ball bearing 46.
  • an intermediate partition wall 48 extending parallel to the plate 22 and separating the annular space defined by the side wall 36 into two adjacent spaces.
  • the wall 44 is carried, like the plate 22, by an abutment flange 50 advantageously equipped with a ball bearing 52.
  • Columns of connection and recovery of effort 54 are arranged between the plate 22 and the wall 48. They extend parallel to the axis X1-X1 and are equi-parts along one or more circles of axis X1-X1 on the plateau surface to ensure the mechanical strength of the assembly when the antenna is under vacuum. These columns rigidly connect the plate 22 and the wall 48.
  • Columns 56 extending the columns 44 extend between the wall 48 and the bottom 34 in the extension of the columns 56.
  • the columns 56 are connected to the wall 48 at one of their ends and have a sliding contact 58 at their other ends resting on the surface of the bottom 34.
  • columns 60 extend the columns 54 from the plate 22 to the protection wall 30. These columns are fixed to the plate 22 and bear in a sliding contact 62 on the wall 30.
  • the sliding support of the columns 52 and 60 on the bottom 34 and the wall 30 is provided for example by interposition of a free ball rotating at the end of each column.
  • the intermediate wall 48 carries, next to the duct 32, along the axis X1-X1, a metal cone 70 capable of modifying the propagation mode of the electromagnetic flux, while passing from a flow in TM01 mode along the axis X1-X1 at a centripetal flow according to the TEM mode extending from the axis X1-X1 outwards in the direction of the arrows 72.
  • the intermediate wall 48 is provided with through loops 74 regularly distributed in a circle centered along the axis X1-X1. These loops 74 are formed of a metal conductor closed on itself and have two lobes 74A, 74B protruding on either side of the intermediate wall 48.
  • the antenna elements 24 are represented on a larger scale on the figure 3 . According to the invention, these antenna elements are able to rotate on themselves about their axis X2-X2 parallel to the axis X1-X1.
  • Each antenna element comprises a transmission strand 80 disposed on the side of the antenna transmission port and a capture loop 82 disposed between the panel 22 and the intermediate wall 48.
  • the loop 82 is rigidly and fixedly connected to the wall 22 at one of its ends while remaining electrically isolated from the wall 22 in its passage towards the emission strand 84.
  • the loop has a shape known per se and is obtained by curvature on itself of a metal conductor.
  • the strand 80 has an emission portion 84 consisting of a solid wire describing a helix shape. This strand is extended by a core 86 engaged inside the hollow conductor constituting the loop 82 while providing an electrical connection.
  • a sliding contact 88 is provided between the conductor 83 and the core 86 according to an arrangement of any suitable type thus allowing rotation of the emission strand 80 with respect to the loop 82 while ensuring an electrical connection.
  • a drive gear 90 is disposed around the strand 80 at the connection between the helical emission portion 84 and the core 86.
  • This pinion extends perpendicular to the axis X2-X2 rotation of the emission strand and is arranged along the panel 22 on the side of the mouth 28 of emission. It is integral in rotation with the strand 80.
  • the mechanism 25 for rotating the antenna elements 24 themselves comprises a set of racks 102 arranged parallel to one another on the surface of the plate 22 facing the mouth 28. These racks thus extend according to cords of the disk forming the plate 22. They are perpendicular to the component of the direction TT according to the emission plane defined by the plate 22.
  • the racks 102 are mounted slidably movable along the surface of the plate 22. They are held laterally by the antenna elements arranged on either side.
  • the drive mechanism 25 further comprises a ring 104 for controlling the racks and a drive motor 106 of the control ring 104.
  • the ring 104 bears on the shoulder 38 and is guided laterally by the peripheral wall 40.
  • the ring is of axis X1-X1. It is angularly movable relative to the plate 22 about its axis following an angular deflection of the order of 60 °.
  • the motor 106 is attached to an extension of the plate 22 denoted 108.
  • the extension extends outside the enclosed space delimited by the frame 26 and the protective wall 30.
  • the output shaft of the engine is equipped with a pinion 110 received in a groove 112 of the crown 104.
  • This groove is in the shape of a circular arc centered on the axis X1-X1 and has on a cylindrical surface a toothing 114 engaged with the pinion 110 for the drive of the crown under the action of the engine 106.
  • Each rack 102 is extended in the space defined between the shoulder 38 and the crown 104. At its two ends, each rack has a drive pin 120 received in a groove 122 forming a cam of the control ring 104.
  • the grooves 122 forming a cam have a curved shape and have a width equal to the thickness of the drive finger 120. They generally extend in an angular opening around the crown 104 equal to the angular displacement of the crown 104 relative to the tray 22.
  • the grooves 122 are symmetrical to one another for the same rack with respect to a diameter of the disk forming the plate, this diameter extending perpendicularly to the racks 102.
  • the profile of the cam grooves 122 is such that for a given rack located at a distance Rh from the center of the plate 22, R being the radius of the plate, the movement of the rack is such as to produce an angular displacement of the element.
  • the inclination of the grooves forming the cam 22 increases from one side noted A to the other of the ring in the direction of the arrow F as is visible on the figure 1 .
  • the antenna elements are thus distributed in groups by being associated with the same rack. All the antenna elements of the same group are thus located in a band extending in the plane of the plate 22 perpendicular to the transmission direction T-T. These antenna elements are all able to be moved by the same angular offset during a movement of the associated rack.
  • the initial angular offset of the helices is calculated to allow coherent addition in the main axis of the antenna for positioning in the center of this rack to allow a deflection of the beam on either side of this axis.
  • a variant, favoring only a deflection of one side would correspond to an initial setting of the propellers to allow coherent addition along the main axis for a positioning of the racks in abutment.
  • the antenna finally comprises a mechanism 150 for global drive in rotation of the plate 22 and all the antenna elements around the axis X1-X1 relative to the frame 26.
  • This mechanism comprises a motor 152 carried by the chassis 26. It has on its output shaft a pinion 154 adapted to drive the plate 22.
  • the plate 22 has in the extension 108, a slot 156 of semi-circular shape centered on the axis X1-X1 including a wall 158 has a toothing 160 engaged with the pinion 154.
  • the electromagnetic flux arriving along the axis X1-X1 through the inlet 27 is distributed along the surface of the intermediate wall 28 by the mode converter 70.
  • centripetal flow is then captured by the lobes 74A of the loops and reemitted by the lobes 74B in the space between the plate 22 and the intermediate wall 48.
  • loops 82 of the antenna elements 24 capture again the electromagnetic wave inducing a current to the transmission strand 84, which re-emits the electromagnetic wave in a direction and with a phase which are specific to the angular positioning of the elements of antenna.
  • the amplitude of the displacement applied to each rack is defined by the shape of the cam groove 122 present at each end so that the more the rack is away from the point A, the greater the amplitude of its displacement is important.
  • the associated antenna elements are moved angularly, the rack driving the pinion 90 integral with the emission strand 80.
  • all the transmission strands associated with the same rack and belonging to the same group are moved angularly of the same amplitude, thus producing a phase shift between the elementary electromagnetic waves emitted by these antenna elements and those of the antenna elements associated with other racks which undergo a different displacement.
  • the phase shifts applied to the antenna elements are such that, depending on their position, the antenna elements produce an electromagnetic wave whose phase shift corresponds to the phase difference existing between the wave actually emitted and the wave that would have been emitted by antenna elements located in a plane angularly offset by an angle ⁇ with respect to the plane of the plate 22.
  • the electromagnetic wave resulting from the elementary waves produced by the elements is coherently, the elementary waves being in phase in a plane perpendicular to the propagation direction TT and that this coherent antenna wave propagating along the direction TT is angularly offset by an angle ⁇ relative to the normal of the plate 22.
  • the propagation direction TT describes a cone of revolution along the axis X1-X1 and with a half-angle at the apex ⁇ .
  • the angle ⁇ is adjustable independently of the movement overall and thus allows the realization of a two-dimensional pointing on a solid angle of half-angle at the apex ⁇ max ( ⁇ max being the angle at the maximum deflection of the racks)
  • the motor 152 acting on the plate 22 through the gear 154 meshing with the toothing 158 allows an overall displacement of all the antenna elements of the same angular offset around their axis X2-X2 by displacement of the plate 22, thus allowing phase shifting of all the antenna elements and therefore of the antenna.
  • This phase shifter is able to operate over a wide range of frequencies and at very high power.
  • the antenna thus formed thus allows, without articulated element in the wave supply guide duct, to emit an angularly offset wave.
  • This angular offset is obtained without the need to angularly move the frame of the antenna and its radome.
  • each antenna element 24 is formed of a radiating strand 184 fixedly fixed in rotation with respect to the panel 22. All the strands are identical and are oriented identically. Each strand is associated with a focusing lens 186 disposed in line with the corresponding strand. This lens is able to focus the electromagnetic wave produced the strand.
  • These lenses are associated with a mechanism 188 of angular displacement of each lens 186 about two axes 188A, 188B extending perpendicularly to each other and parallel to the plate 22.
  • the mechanism 188 is such that all the lenses have a same orientation, thus allowing a deflection of an angle ⁇ of the set of elementary electromagnetic waves normally initially transmitted to the plate 22 by each of the strands 184.
  • the coherent wave produced by the addition of the elementary electromagnetic waves produced by each antenna element propagates at a predefined angle ⁇ with respect to the normal to the plate 22.
  • the antenna strand noted 284, corresponding to the radiating strand 84, is helically wound around an elastically deformable mat 286. In the absence of stress, the mat 286 extends perpendicularly to the plate 22.
  • the mat 286 is connected to a mechanism 188 for moving its end, thus allowing the axis of the helix of the strand 284 to bend by deformation of the mat 286.
  • the mechanism 188 ensures a transmission of the wave elementary produced by each strand in a direction angularly offset from the normal to the wall 22.
  • a focusing lens 288 is added to the arrangement described with reference to FIG. figure 5 . This lens is placed at the free end of mat 286.
  • the wall 48 is removed and the antenna elements are then fed from the center.
  • the mode converter 70 is carried by the lower face of the wall 22.

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  • Variable-Direction Aerials And Aerial Arrays (AREA)

Description

La présente invention concerne une antenne radiofréquence, du type comportant un châssis et une surface d'émission portant un ensemble d'éléments d'antenne rayonnant, chacun suivant une direction d'émission propre.The present invention relates to a radiofrequency antenna, of the type comprising a frame and an emission surface carrying a set of radiating antenna elements, each in a direction of emission own.

Les antennes réseau pour lesquelles les éléments émissifs de type hélicoïdaux sont connus, notamment par le brevet US 6 115 005 . De même ce type d'antenne compacte est susceptible de transmettre des puissances crête très élevées comme il est décrit par exemple dans le document Li, X.Q.; Liu, Q.X.; Zhang, J.Q.; Zhao, L.; Zhang, Z.Q.; , "The high-power radial line helical circular array antenna: Theory and development," Microwave and Millimeter Wave Technology (ICMMT), 2010, International Conference on , vol., no., pp.671-674, 8-11 May 2010 , doi: 10.1109/ICMMT.2010.5525020. Toutefois les possibilités de pointage d'une telle antenne à très forte puissance restent limitées en raison de la connexion directe, en général sous vide, entre la source de puissance et l'antenne. De manière générale une antenne radiale à base d'éléments d'antenne rayonnant de type hélicoïdaux est constituée d'une ligne de transmission radiale, pouvant être alimentée par son centre ou par sa périphérie, et d'un ensemble d'éléments d'antenne rayonnant régulièrement répartis. Chaque élément d'antenne comporte un brin rayonnant en hélice faisant saillie sur la face d'émission. Le brin est relié à une boucle de captation présente à l'intérieur de la ligne de transmission radiale de l'antenne, de l'autre côté de la surface d'émission. Chacun des brins rayonnant en hélice est positionné avec un angle initial de manière à former, par exemple, un champ électromagnétique cohérent dont la direction de propagation est perpendiculaire à la surface d'émission.Network antennas for which the helical type emissive elements are known, in particular by the patent US 6,115,005 . Similarly this type of compact antenna is capable of transmitting very high peak powers as described for example in the document Li, XQ; Liu, QX; Zhang, JQ; Zhao, L .; Zhang, ZQ; , "The High-Power Radial Line Helical Circular Array Antenna: Theory and Development," Microwave and Millimeter Wave Technology (ICMMT), 2010, International Conference on, vol., No., Pp. 671-674, 8-11 May 2010 , doi: 10.1109 / ICMMT.2010.5525020. However, the pointing possibilities of such a very high power antenna remain limited because of the direct connection, generally under vacuum, between the power source and the antenna. In general, a radial antenna based on helical radiating antenna elements consists of a radial transmission line, which can be powered by its center or by its periphery, and a set of antenna elements. radiating regularly distributed. Each antenna element comprises a helically radiating strand projecting from the emission face. The strand is connected to a capture loop present inside the radial transmission line of the antenna, on the other side of the emission surface. Each of the helically radiating strands is positioned with an initial angle so as to form, for example, a coherent electromagnetic field whose direction of propagation is perpendicular to the emission surface.

L'angle de départ des hélices de chaque élément d'antenne est fixé une fois pour toute de sorte que le déphasage entre les différents éléments d'antenne permette l'addition cohérente dans la direction d'émission souhaitée.The starting angle of the helices of each antenna element is fixed once and for all so that the phase shift between the different antenna elements allows the coherent addition in the desired transmission direction.

Afin de changer la direction d'émission de l'antenne, il est connu de monter l'antenne sur un support articulé et motorisé permettant de déplacer l'ensemble de l'antenne, notamment sa surface d'émission et l'ensemble des éléments d'antenne qui sont présents, ainsi que le châssis de support de la surface d'émission.In order to change the direction of transmission of the antenna, it is known to mount the antenna on an articulated and motorized support for moving the entire antenna, including its transmitting surface and all the elements. antennas that are present, as well as the support frame of the transmitting surface.

Il est alternativement connu des brevets US 6552695 , US 6407714 et US 4427984 de déplacer angulairement les éléments émissifs de type hélicoïdaux.It is alternately known patents US 6552695 , US 6407714 and US 4427984 to angularly move the emissive elements of helical type.

La source de rayonnement électromagnétique utilisée pour alimenter l'antenne à très forte puissance est constituée généralement d'une source relativiste (magnétron de forte puissance, « Magnetically Insulated Line Oscillator » (MILO), carcinotron, klystron relativiste par exemple). L'ensemble source, guide de liaison, antenne doit alors être maintenu sous vide et est difficilement déformable, en raison des risques de claquage limitant les technologies et les architectures permettant d'effectuer un pointage de l'antenne dans une direction particulière, autrement que par déplacement de l'ensemble.The source of electromagnetic radiation used to power the antenna with very high power is generally a relativistic source (high power magnetron, "Magnetically Insulated Line Oscillator" (MILO), carcinotron, relativistic klystron for example). The source assembly, connection guide, antenna must then be kept under vacuum and is difficult to deform, because of the risk of breakdown limiting the technologies and architectures that allow pointing of the antenna in a particular direction, other than by moving the assembly.

L'invention a pour but de proposer une antenne radiofréquence permettant d'être utilisée dans un agencement où la direction du champ rayonné par l'antenne est mobile angulairement dans une ou deux directions, sans nécessiter d'éléments de guidage déformables complexes ni de déplacement de masses importantes.The object of the invention is to propose a radiofrequency antenna that can be used in an arrangement where the direction of the field radiated by the antenna is angularly movable in one or two directions, without requiring complex deformable guide elements or displacement. large masses.

A cet effet, l'invention a pour objet une antenne radiofréquence du type précité, selon la revendication 1. Chaque élément d'antenne est au moins partiellement déplaçable par rapport à la surface d'émission pour modifier sa direction d'émission propre et en ce qu'il comporte des moyens de déplacement des éléments d'antenne de manière coordonnée suivant ladite surface pour former, à partir des ondes élémentaires produites par les éléments d'antenne, une onde cohérente se propageant suivant une direction décalée angulairement par rapport à la normale à la surface d'émission.For this purpose, the subject of the invention is a radiofrequency antenna of the aforementioned type, according to claim 1. Each antenna element is at least partially displaceable with respect to the emission surface in order to modify its own emission direction and it comprises means for moving the antenna elements in a coordinated manner along said surface to form, from the elementary waves produced by the antenna elements, a coherent wave propagating in a direction angularly offset relative to the normal to the emission surface.

Les éléments d'antenne comportant chacun un brin d'émission monté rotatif par rapport à la surface d'émission et les moyens de déplacement des éléments d'antenne sont propres à entraîner les éléments d'antenne en rotation, les moyens de déplacement comportent des crémaillères montées coulissantes par rapport à la surface d'émission et les brins d'émission sont solidaires de pignons d'entraînement en prise avec les crémaillères et en ce que les moyens de déplacement comportent un mécanisme de déplacement synchronisé des crémaillères, le mécanisme de déplacement synchronisé comporte une couronne de commande rotative par rapport au châssis et pourvue de cames de commande des crémaillères, les crémaillères étant chacune équipées d'au moins un suiveur de came coopérant avec une came, et un moteur d'entraînement en rotation de la couronne.The antenna elements each having a transmission strand rotatably mounted relative to the emission surface and the means for moving the antenna elements are adapted to drive the rotating antenna elements, the displacement means comprise racks slidably mounted relative to the emission surface and the transmission strands are integral with driving gears engaged with the racks and in that the displacement means comprise a mechanism for synchronized movement of the racks, the displacement mechanism synchronized comprises a rotary control ring relative to the frame and provided with control cams of the racks, the racks being each equipped with at least one cam follower cooperating with a cam, and a drive motor in rotation of the ring.

Suivant des modes particuliers de réalisation, l'antenne radiofréquence comporte l'une ou plusieurs des caractéristiques suivantes :

  • les éléments d'antenne sont répartis par groupes d'éléments d'antenne, les éléments d'un même groupe étant présents dans une bande de la surface d'émission s'étendant perpendiculairement à la projection de la direction d'émission sur la surface, les éléments d'antenne d'un même groupe étant positionnés pour produire des ondes élémentaires ayant un même déphasage par rapport aux ondes produites par des éléments d'antenne d'un autre groupe,
  • les moyens de déplacement des éléments d'antenne sont propres à positionner les éléments d'antenne pour qu'ils produisent chacun une onde élémentaire déphasée d'un déphasage δΦ par rapport aux autres éléments d'antenne défini par : δΦ = 2 πh tgθ / λ
    Figure imgb0001

    où θ est l'angle d'inclinaison de la direction d'émission par rapport à la normale à la surface d'émission, À est la longueur d'onde du rayonnement électromagnétique ; et h est la distance de l'élément d'antenne à un axe de référence mesurée suivant la direction d'émission sur la surface d'émission,
  • la surface d'émission portant les éléments d'antenne rayonnants est rotative par rapport au châssis et en ce qu'elle comporte des moyens d'entraînement en rotation de la surface d'émission.
  • le châssis délimite un espace clos sous vide dans lequel sont contenus les éléments d'antenne et en ce qu'elle comporte des colonnettes de reprise d'effort entre le châssis et la surface d'émission.
According to particular embodiments, the radiofrequency antenna comprises one or more of the following characteristics:
  • the antenna elements are distributed in groups of antenna elements, the elements of the same group being present in a band of the emission surface extending perpendicular to the projection of the emission direction on the surface the antenna elements of one and the same group being positioned to produce elementary waves having the same phase shift with respect to the waves produced by antenna elements of another group,
  • the means for moving the antenna elements are adapted to position the antenna elements so that they each produce an elementary wave phase-shifted by a phase shift δΦ with respect to the other antenna elements defined by: δΦ = 2 πh tgθ / λ
    Figure imgb0001

    where θ is the angle of inclination of the emission direction with respect to the normal to the emission surface, λ is the wavelength of the electromagnetic radiation; and h is the distance of the antenna element to a reference axis measured in the direction of emission on the emission surface,
  • the transmitting surface carrying the radiating antenna elements is rotatable relative to the frame and in that it comprises means for driving the emission surface in rotation.
  • the frame delimits a vacuum-enclosed space in which the antenna elements are contained and in that it comprises balancing columns of force between the frame and the emission surface.

Suivant des exemples, l'antenne radiofréquence comporte l'une ou plusieurs des charactéristiques suivantes:

  • les éléments d'antenne comportent un brin d'émission déformable et en ce que les moyens de déplacement comportent un mécanisme propre à assurer la déformation de chaque brin d'émission pour modifier la direction d'émission propre,
  • les éléments d'antenne comportent chacun une lentille de focalisation de l'onde électromagnétique élémentaire produite par l'élément d'antenne et en ce que les moyens de déplacement comportent un mécanisme de déplacement angulaire de chaque lentille de focalisation,
According to examples, the radiofrequency antenna comprises one or more of the following features:
  • the antenna elements comprise a deformable transmission strand and in that the displacement means comprise a mechanism capable of ensuring the deformation of each transmission strand to modify the own emission direction,
  • the antenna elements each comprise a focusing lens of the elementary electromagnetic wave produced by the antenna element and in that the displacement means comprise a mechanism for angular displacement of each focusing lens,

L'invention sera mieux comprise à la lecture de la description qui va suivre, donnée uniquement à titre d'exemple et faite en se référant aux dessins sur lesquels :

  • la figure 1 est une vue en coupe d'une antenne selon l'invention, vue de dessus, prise suivant la ligne I-I de la figure 2 ;
  • la figure 2 est une vue en coupe transversale de l'antenne selon l'invention prise suivant la ligne II-II de la figure 1 ;
  • la figure 3 est une vue en coupe de détail d'un élément d'antenne de l'antenne selon l'invention ; et
  • les figures 4, 5 et 6 sont des vues en élévation de variantes de réalisation d'éléments d'antenne selon l'invention.
The invention will be better understood on reading the description which follows, given solely by way of example and with reference to the drawings in which:
  • the figure 1 is a sectional view of an antenna according to the invention, seen from above, taken along line II of FIG. figure 2 ;
  • the figure 2 is a cross-sectional view of the antenna according to the invention taken along line II-II of FIG. figure 1 ;
  • the figure 3 is a detail sectional view of an antenna element of the antenna according to the invention; and
  • the figures 4 , 5 and 6 are elevational views of alternative embodiments of antenna elements according to the invention.

L'antenne 20 selon l'invention est représentée en vue de dessus et en coupe sur la figure 1 et en coupe transversale sur la figure 2. Elle présente une forme générale de disque d'axe X1-X1. Selon l'invention, chaque antenne 20 est propre à émettre suivant une direction T-T décalée angulairement d'un angle θ par rapport à l'axe X1-X1 de l'antenne.The antenna 20 according to the invention is shown in plan view and in section on the figure 1 and in cross section on the figure 2 . It has a general shape of disk axis X1-X1. According to the invention, each antenna 20 is able to emit in a direction TT angularly offset by an angle θ with respect to the axis X1-X1 of the antenna.

Sa surface plane d'émission est constituée d'un plateau circulaire 22 mobile en rotation autour de l'axe X1-X1 et sur lequel est disposé un ensemble d'éléments d'antenne rayonnant 24 répartis régulièrement sur la surface du plateau 22. Les éléments d'antenne sont propres à produire chacun une onde élémentaire, chacun suivant une direction d'émission propre et avec un déphasage propre de sorte que l'addition des ondes élémentaires produisent une onde cohérente suivant la direction T-T.Its planar emission surface consists of a circular plate 22 rotatable about the axis X1-X1 and on which is disposed a set of radiating antenna elements 24 regularly distributed on the surface of the plate 22. The antenna elements are each able to produce an elementary wave, each following a own emission direction and with a proper phase shift so that the addition of the elementary waves produce a coherent wave in the direction TT.

Ces éléments d'antenne ont chacun un axe X2-X2 normalement perpendiculaire au plateau 22.These antenna elements each have an axis X2-X2 normally perpendicular to the plate 22.

L'antenne est équipée selon l'invention de moyens 25 de déplacement des éléments d'antenne par rapport à la surface d'émission pour modifier leur direction d'émission et/ou leur phase. Dans le mode de réalisation décrit ici, les moyens 25 sont propres à produire un déplacement en rotation sur eux-mêmes de tout ou partie des éléments d'antenne.The antenna is equipped according to the invention means 25 for moving the antenna elements relative to the emission surface to change their direction of emission and / or their phase. In the embodiment described here, the means 25 are able to produce a rotational movement on themselves of all or part of the antenna elements.

Le plateau 22 est porté par un châssis 26 en forme générale de cloche s'évasant progressivement depuis une entrée 27 de collecte du rayonnement magnétique issu de la source jusqu'à une bouche 28 de sortie du rayonnement issu des éléments d'antenne 24. Cette bouche est obturée par une paroi de protection 30 étanche à l'air permettant de créer le vide à l'intérieur du châssis 26. La paroi 30 est transparente au rayonnement électromagnétique et forme radôme.The plate 22 is carried by a frame 26 in the general shape of a bell flaring progressively from an inlet 27 for collecting the magnetic radiation from the source to a mouth 28 of the radiation output from the antenna elements 24. The mouth is closed by an airtight protective wall 30 for creating the vacuum inside the frame 26. The wall 30 is transparent to the electromagnetic radiation and radome form.

L'extrémité d'entrée 27 du châssis 26 est formée d'un tube prolongé par une couronne 34 formant le fond du châssis. Cette couronne est d'axe X1-X1. Le fond est prolongé par une première paroi périphérique 36 présentant à son extrémité tournée vers la bouche 28 un épaulement divergeant 38 formant un support. Cet épaulement est bordé d'une seconde paroi périphérique 40 portant la paroi de protection 30.The inlet end 27 of the frame 26 is formed of a tube extended by a ring 34 forming the bottom of the frame. This ring is of axis X1-X1. The bottom is extended by a first peripheral wall 36 having at its end facing the mouth 28 a diverging shoulder 38 forming a support. This shoulder is bordered by a second peripheral wall 40 carrying the protective wall 30.

Le plateau 22 prend appui sur un rebord périphérique interne 44 de la paroi latérale 34. Ce rebord 44 forme un pallier de guidage en rotation du plateau 22 autour de l'axe X1-X1. A cet effet, il est avantageusement équipé d'un roulement à billes 46.The plate 22 is supported on an inner peripheral rim 44 of the side wall 34. This flange 44 forms a bearing guide for rotation of the plate 22 about the axis X1-X1. For this purpose, it is advantageously equipped with a ball bearing 46.

Entre le plateau 22 et le fond 34 est disposée une paroi intermédiaire de séparation 48 s'étendant parallèlement au plateau 22 et séparant l'espace annulaire délimité par la paroi latérale 36 en deux espaces adjacents. La paroi 44 est portée, comme le plateau 22, par un rebord formant pallier 50 avantageusement équipé de roulement à billes 52.Between the plate 22 and the bottom 34 is disposed an intermediate partition wall 48 extending parallel to the plate 22 and separating the annular space defined by the side wall 36 into two adjacent spaces. The wall 44 is carried, like the plate 22, by an abutment flange 50 advantageously equipped with a ball bearing 52.

Des colonnettes de liaison et de reprise d'effort 54 sont disposées entre le plateau 22 et la paroi 48. Elles s'étendent parallèlement à l'axe X1-X1 et sont équiréparties suivant un ou plusieurs cercles d'axe X1-X1 sur la surface du plateau afin d'assurer la tenue mécanique de l'ensemble lorsque l'antenne est sous vide. Ces colonnettes lient rigidement le plateau 22 et la paroi 48.Columns of connection and recovery of effort 54 are arranged between the plate 22 and the wall 48. They extend parallel to the axis X1-X1 and are equi-parts along one or more circles of axis X1-X1 on the plateau surface to ensure the mechanical strength of the assembly when the antenna is under vacuum. These columns rigidly connect the plate 22 and the wall 48.

Des colonnettes 56 de prolongement des colonnettes 44 s'étendent entre la paroi 48 et le fond 34 dans le prolongement des colonnettes 56. Les colonnettes 56 sont liées à la paroi 48 à une de leurs extrémités et présentent un contact glissant 58 à leurs autres extrémités en appui sur la surface du fond 34.Columns 56 extending the columns 44 extend between the wall 48 and the bottom 34 in the extension of the columns 56. The columns 56 are connected to the wall 48 at one of their ends and have a sliding contact 58 at their other ends resting on the surface of the bottom 34.

De même, des colonnettes 60 prolongent les colonnettes 54 depuis le plateau 22 jusqu'à la paroi de protection 30. Ces colonnettes sont fixées au plateau 22 et prennent appui suivant un contact glissant 62 sur la paroi 30.Likewise, columns 60 extend the columns 54 from the plate 22 to the protection wall 30. These columns are fixed to the plate 22 and bear in a sliding contact 62 on the wall 30.

L'appui glissant des colonnettes 52 et 60 sur le fond 34 et la paroi 30 est assuré par exemple par interposition d'une bille libre en rotation à l'extrémité de chaque colonnette.The sliding support of the columns 52 and 60 on the bottom 34 and the wall 30 is provided for example by interposition of a free ball rotating at the end of each column.

La paroi intermédiaire 48 porte en regard du conduit 32, suivant l'axe X1-X1, un cône métallique 70 propre à modifier le mode de propagation du flux électromagnétique, en passant d'un flux en mode TM01 suivant l'axe X1-X1 à un flux centripète suivant le mode TEM s'étendant depuis l'axe X1-X1 vers l'extérieur suivant le sens des flèches 72.The intermediate wall 48 carries, next to the duct 32, along the axis X1-X1, a metal cone 70 capable of modifying the propagation mode of the electromagnetic flux, while passing from a flow in TM01 mode along the axis X1-X1 at a centripetal flow according to the TEM mode extending from the axis X1-X1 outwards in the direction of the arrows 72.

La paroi intermédiaire 48 est munie de boucles traversantes 74 réparties régulièrement suivant un cercle centré suivant l'axe X1-X1. Ces boucles 74 sont formées d'un conducteur métallique refermé sur lui-même et présentent deux lobes 74A, 74B faisant saillie de part et d'autre de la paroi intermédiaire 48.Les éléments d'antenne 24 sont représentés à plus grande échelle sur la figure 3. Selon l'invention, ces éléments d'antenne sont propres à tourner sur eux-mêmes autour de leur axe X2-X2 parallèle à l'axe X1-X1.The intermediate wall 48 is provided with through loops 74 regularly distributed in a circle centered along the axis X1-X1. These loops 74 are formed of a metal conductor closed on itself and have two lobes 74A, 74B protruding on either side of the intermediate wall 48. The antenna elements 24 are represented on a larger scale on the figure 3 . According to the invention, these antenna elements are able to rotate on themselves about their axis X2-X2 parallel to the axis X1-X1.

Sur la figure 3, on retrouve le plateau 22 portant l'élément d'antenne 24. Chaque élément d'antenne comporte un brin d'émission 80 disposé du côté de la bouche d'émission de l'antenne et une boucle de captation 82 disposée entre le panneau 22 et la paroi intermédiaire 48.On the figure 3 , there is the plate 22 carrying the antenna element 24. Each antenna element comprises a transmission strand 80 disposed on the side of the antenna transmission port and a capture loop 82 disposed between the panel 22 and the intermediate wall 48.

La boucle 82 est liée rigidement et de manière fixe à la paroi 22 par l'une de ses extrémités tout en restant isolé électriquement de la paroi 22 dans sa traversée vers le brin d'émission 84 . La boucle présente une forme connue en soi et est obtenue par courbure sur lui-même d'un conducteur métallique.The loop 82 is rigidly and fixedly connected to the wall 22 at one of its ends while remaining electrically isolated from the wall 22 in its passage towards the emission strand 84. The loop has a shape known per se and is obtained by curvature on itself of a metal conductor.

Le brin 80 présente une partie d'émission 84 constituée d'un fil métallique plein décrivant une forme d'hélice. Ce brin se prolonge par une âme 86 engagée à l'intérieur du conducteur creux constituant la boucle 82 tout en assurant une liaison électrique.The strand 80 has an emission portion 84 consisting of a solid wire describing a helix shape. This strand is extended by a core 86 engaged inside the hollow conductor constituting the loop 82 while providing an electrical connection.

Un contact glissant 88 est assuré entre le conducteur 83 et l'âme 86 suivant un agencement de tout type adapté permettant ainsi une rotation du brin d'émission 80 par rapport à la boucle 82 tout en assurant une liaison électrique.A sliding contact 88 is provided between the conductor 83 and the core 86 according to an arrangement of any suitable type thus allowing rotation of the emission strand 80 with respect to the loop 82 while ensuring an electrical connection.

Un pignon d'entraînement 90 est disposé autour du brin 80 à la liaison entre la partie d'émission en hélice 84 et l'âme 86. Ce pignon s'étend perpendiculairement à l'axe X2-X2 de rotation du brin d'émission et est disposé le long du panneau 22 du côté de la bouche 28 d'émission. Il est solidaire en rotation du brin 80.A drive gear 90 is disposed around the strand 80 at the connection between the helical emission portion 84 and the core 86. This pinion extends perpendicular to the axis X2-X2 rotation of the emission strand and is arranged along the panel 22 on the side of the mouth 28 of emission. It is integral in rotation with the strand 80.

Comme illustré sur la figure 1, le mécanisme 25 d'entraînement en rotation sur eux-mêmes des éléments d'antenne 24 comporte un ensemble de crémaillères 102 disposées parallèlement les unes aux autres sur la surface du plateau 22 tournée vers la bouche 28. Ces crémaillères s'étendent ainsi suivant des cordes du disque formant le plateau 22. Elles sont perpendiculaires à la composante de la direction T-T suivant le plan d'émission défini par le plateau 22.As illustrated on the figure 1 , the mechanism 25 for rotating the antenna elements 24 themselves comprises a set of racks 102 arranged parallel to one another on the surface of the plate 22 facing the mouth 28. These racks thus extend according to cords of the disk forming the plate 22. They are perpendicular to the component of the direction TT according to the emission plane defined by the plate 22.

Ces crémaillères présentent de part et d'autre des dentures rectilignes engagées avec les pignons 90 des éléments d'antenne adjacents. Ainsi, les éléments d'antenne associés à une même crémaillère sont répartis alternativement de part et d'autres de la crémaillère.These racks have on each side rectilinear teeth engaged with the gables 90 of the adjacent antenna elements. Thus, the antenna elements associated with the same rack are distributed alternately on both sides of the rack.

Les crémaillères 102 sont montées déplaçables à coulissement suivant la surface du plateau 22. Elles sont maintenues latéralement par les éléments d'antenne disposés de part et d'autre.The racks 102 are mounted slidably movable along the surface of the plate 22. They are held laterally by the antenna elements arranged on either side.

Le mécanisme d'entraînement 25 comporte en outre une couronne 104 de commande des crémaillères et un moteur d'entraînement 106 de la couronne de commande 104.The drive mechanism 25 further comprises a ring 104 for controlling the racks and a drive motor 106 of the control ring 104.

La couronne 104 prend appui sur l'épaulement 38 et est guidée latéralement par la paroi périphérique 40. La couronne est d'axe X1-X1. Elle est déplaçable angulairement par rapport au plateau 22 autour de son axe suivant un débattement angulaire de l'ordre de 60 °.The ring 104 bears on the shoulder 38 and is guided laterally by the peripheral wall 40. The ring is of axis X1-X1. It is angularly movable relative to the plate 22 about its axis following an angular deflection of the order of 60 °.

Le moteur 106 est fixé à un prolongement du plateau 22 noté 108. Le prolongement s'étend à l'extérieur de l'espace clos délimité par le châssis 26 et la paroi de protection 30. L'arbre de sortie du moteur est équipé d'un pignon 110 reçu dans une gorge 112 de la couronne 104. Cette gorge est en forme d'arc de cercle centré sur l'axe X1-X1 et présente sur une surface cylindrique une denture 114 engagée avec le pignon 110 pour l'entraînement de la couronne sous l'action du moteur 106.The motor 106 is attached to an extension of the plate 22 denoted 108. The extension extends outside the enclosed space delimited by the frame 26 and the protective wall 30. The output shaft of the engine is equipped with a pinion 110 received in a groove 112 of the crown 104. This groove is in the shape of a circular arc centered on the axis X1-X1 and has on a cylindrical surface a toothing 114 engaged with the pinion 110 for the drive of the crown under the action of the engine 106.

Chaque crémaillère 102 se prolonge dans l'espace délimité entre l'épaulement 38 et la couronne 104. A ses deux extrémités, chaque crémaillère présente un doigt d'entraînement 120 reçu dans une gorge 122 formant came de la couronne de commande 104.Each rack 102 is extended in the space defined between the shoulder 38 and the crown 104. At its two ends, each rack has a drive pin 120 received in a groove 122 forming a cam of the control ring 104.

Les gorges 122 formant came présentent une forme courbe et ont une largeur égale à l'épaisseur du doigt d'entraînement 120. Elles s'étendent généralement suivant une ouverture angulaire autour de la couronne 104 égal au débattement angulaire de la couronne 104 par rapport au plateau 22.The grooves 122 forming a cam have a curved shape and have a width equal to the thickness of the drive finger 120. They generally extend in an angular opening around the crown 104 equal to the angular displacement of the crown 104 relative to the tray 22.

Les gorges 122 sont symétriques l'une de l'autre pour une même crémaillère par rapport à un diamètre du disque formant le plateau, ce diamètre s'étendant perpendiculairement aux crémaillères 102.The grooves 122 are symmetrical to one another for the same rack with respect to a diameter of the disk forming the plate, this diameter extending perpendicularly to the racks 102.

Le profil des gorges formant came 122 est tel que pour une crémaillère donnée située à une distance R-h du centre du plateau 22, R étant le rayon du plateau, le déplacement de la crémaillère soit tel qu'elle produise un déplacement angulaire de l'élément d'antenne 24 qui lui est engrené égal à δΦ suivant la formule : δΦ = 2 πh tgθ / λ

Figure imgb0002

où θ est l'angle d'inclinaison par rapport à la normale de la direction d'émission T-T de l'antenne et À est la longueur d'ondes du rayonnement électromagnétique à émettre. De manière générale, l'inclinaison des gorges formant la came 22 augmentent d'un côté noté A à l'autre de la couronne suivant le sens de la flèche F comme cela est visible sur la figure 1.The profile of the cam grooves 122 is such that for a given rack located at a distance Rh from the center of the plate 22, R being the radius of the plate, the movement of the rack is such as to produce an angular displacement of the element. of antenna 24 which is geared to it equal to δΦ according to the formula: δΦ = 2 πh tgθ / λ
Figure imgb0002

where θ is the angle of inclination with respect to the normal of the transmission direction TT of the antenna and λ is the wavelength of the electromagnetic radiation to be emitted. In general, the inclination of the grooves forming the cam 22 increases from one side noted A to the other of the ring in the direction of the arrow F as is visible on the figure 1 .

Les éléments d'antenne sont ainsi répartis par groupe en étant associés à une même crémaillère. Tous les éléments d'antenne d'un même groupe sont ainsi situés dans une bande s'étendant dans le plan du plateau 22 perpendiculairement à la direction d'émission T-T. Ces éléments d'antenne sont propres à tous être déplacés d'un même décalage angulaire lors d'un déplacement de la crémaillère associée. Le décalage angulaire initial des hélices est calculé pour permettre l'addition cohérente dans l'axe principal de l'antenne pour un positionnement au centre de cette crémaillère pour permettre un débattement du faisceau de part et d'autre de cet axe. Une variante, ne privilégiant qu'un débattement d'un seul côté, correspondrait à un réglage initial des hélices pour permettre l'addition cohérente suivant l'axe principal pour un positionnement des crémaillères en buté.The antenna elements are thus distributed in groups by being associated with the same rack. All the antenna elements of the same group are thus located in a band extending in the plane of the plate 22 perpendicular to the transmission direction T-T. These antenna elements are all able to be moved by the same angular offset during a movement of the associated rack. The initial angular offset of the helices is calculated to allow coherent addition in the main axis of the antenna for positioning in the center of this rack to allow a deflection of the beam on either side of this axis. A variant, favoring only a deflection of one side, would correspond to an initial setting of the propellers to allow coherent addition along the main axis for a positioning of the racks in abutment.

L'antenne comporte enfin un mécanisme 150 d'entraînement global en rotation du plateau 22 et de l'ensemble des éléments d'antenne autour de l'axe X1-X1 par rapport au châssis 26. Ce mécanisme comporte un moteur 152 porté par le châssis 26. Il présente sur son arbre de sortie un pignon 154 propre à entraîner le plateau 22. A cet effet, le plateau 22 présente dans le prolongement 108, une fente 156 de forme semi-circulaire centrée sur l'axe X1-X1 dont une paroi 158 présente une denture 160 engagée avec le pignon 154.The antenna finally comprises a mechanism 150 for global drive in rotation of the plate 22 and all the antenna elements around the axis X1-X1 relative to the frame 26. This mechanism comprises a motor 152 carried by the chassis 26. It has on its output shaft a pinion 154 adapted to drive the plate 22. For this purpose, the plate 22 has in the extension 108, a slot 156 of semi-circular shape centered on the axis X1-X1 including a wall 158 has a toothing 160 engaged with the pinion 154.

En fonctionnement, dans une telle antenne, le flux électromagnétique arrivant suivant l'axe X1-X1 par l'entrée 27 est répartie suivant la surface de la paroi intermédiaire 28 par le convertisseur de mode 70.In operation, in such an antenna, the electromagnetic flux arriving along the axis X1-X1 through the inlet 27 is distributed along the surface of the intermediate wall 28 by the mode converter 70.

Le flux alors centripète se trouve capté par les lobes 74A des boucles et réémis par les lobes 74B dans l'espace entre le plateau 22 et la paroi intermédiaire 48. Les boucles 82 des éléments d'antenne 24 captent à nouveau l'onde électromagnétique induisant un courant jusqu'au brin d'émission 84, lequel réémet l'onde électromagnétique suivant une direction et avec une phase qui sont propres au positionnement angulaire des éléments d'antenne.The centripetal flow is then captured by the lobes 74A of the loops and reemitted by the lobes 74B in the space between the plate 22 and the intermediate wall 48. loops 82 of the antenna elements 24 capture again the electromagnetic wave inducing a current to the transmission strand 84, which re-emits the electromagnetic wave in a direction and with a phase which are specific to the angular positioning of the elements of antenna.

Lorsque la couronne 104 est dans une position extrême, tous les éléments d'antenne sont orientés dans la même direction, de sorte qu'ils produisent des ondes électromagnétiques élémentaires avec des déphasages relatifs nuls.When the ring gear 104 is in an extreme position, all the antenna elements are oriented in the same direction, so that they produce elementary electromagnetic waves with zero relative phase shifts.

Lorsque sous l'action du moteur 106, la couronne de commande 104 est déplacée angulairement, les crémaillères 102 se trouvent déplacées parallèlement les unes aux autres en étant entraînées par leurs deux extrémités par les doigts d'entraînement sollicités par une paroi des gorges 122 formant came.When under the action of the motor 106, the control ring 104 is angularly displaced, the racks 102 are moved parallel to each other by being driven by their two ends by the driving fingers urged by a wall of the grooves 122 forming cam.

L'amplitude du déplacement appliqué à chaque crémaillère est défini par la forme de la gorge formant came 122 présente à chaque extrémité de sorte que plus la crémaillère est à l'écart du point A, plus l'amplitude de son déplacement est importante.The amplitude of the displacement applied to each rack is defined by the shape of the cam groove 122 present at each end so that the more the rack is away from the point A, the greater the amplitude of its displacement is important.

Lors du déplacement des crémaillères, les éléments d'antenne associés se trouvent déplacés angulairement, la crémaillère entraînant le pignon 90 solidaire du brin d'émission 80. Dans ces conditions, on comprend que tous les brins d'émission associés à une même crémaillère et appartenant au même groupe sont déplacés angulairement de la même amplitude, produisant ainsi un déphasage entre les ondes électromagnétiques élémentaires émises par ces éléments d'antenne et ceux des éléments d'antenne associés à d'autres crémaillères qui subissent un déplacement différent.During the movement of the racks, the associated antenna elements are moved angularly, the rack driving the pinion 90 integral with the emission strand 80. Under these conditions, it is understood that all the transmission strands associated with the same rack and belonging to the same group are moved angularly of the same amplitude, thus producing a phase shift between the elementary electromagnetic waves emitted by these antenna elements and those of the antenna elements associated with other racks which undergo a different displacement.

On comprend, du fait de la formule (1) que les déphasages appliqués aux éléments d'antenne sont tels qu'en fonction de leur position, les éléments d'antenne produisent une onde électromagnétique dont le déphasage correspond au déphasage existant entre l'onde réellement émise et l'onde qui aurait été émise par des éléments d'antenne situés dans un plan décalé angulairement d'un angle θ par rapport au plan du plateau 22. Ainsi, l'onde électromagnétique résultant des ondes élémentaires produites par les éléments est cohérente, les ondes élémentaires étant en phase dans un plan perpendiculaire à la direction de propagation T-T et que cette onde cohérente d'antenne se propageant suivant la direction T-T est décalée angulairement d'un angle θ par rapport à la normale du plateau 22.It can be understood from formula (1) that the phase shifts applied to the antenna elements are such that, depending on their position, the antenna elements produce an electromagnetic wave whose phase shift corresponds to the phase difference existing between the wave actually emitted and the wave that would have been emitted by antenna elements located in a plane angularly offset by an angle θ with respect to the plane of the plate 22. Thus, the electromagnetic wave resulting from the elementary waves produced by the elements is coherently, the elementary waves being in phase in a plane perpendicular to the propagation direction TT and that this coherent antenna wave propagating along the direction TT is angularly offset by an angle θ relative to the normal of the plate 22.

On comprend qu'un tel agencement permet de modifier la direction de propagation de l'onde suivant un angle θ qui dépend de la position de la couronne de commande 104, laquelle est commandée par le moteur 106. Lors d'une rotation de 360° de la couronne 104 la direction de propagation T-T décrit un cône de révolution suivant l'axe X1-X1 et de demi-angle au sommet θ. L'angle θ est réglable de façon indépendante du mouvement d'ensemble et permet ainsi la réalisation d'un pointage en deux dimensions sur un angle solide de demi-angle au sommet θmax (θmax étant l'angle lors du débattement maximal des crémaillères)It is understood that such an arrangement makes it possible to modify the direction of propagation of the wave along an angle θ which depends on the position of the control ring 104, which is controlled by the motor 106. During a rotation of 360 ° of the ring gear 104, the propagation direction TT describes a cone of revolution along the axis X1-X1 and with a half-angle at the apex θ. The angle θ is adjustable independently of the movement overall and thus allows the realization of a two-dimensional pointing on a solid angle of half-angle at the apex θmax (θmax being the angle at the maximum deflection of the racks)

De même, le moteur 152 par action sur le plateau 22 au travers du pignon 154 engrené avec la denture 158 permet un déplacement global de tous les éléments d'antenne d'un même décalage angulaire autour de leur l'axe X2-X2 par déplacement du plateau 22, permettant ainsi de déphaser l'ensemble des éléments d'antenne et donc de l'antenne.. Ce déphaseur est apte à fonctionner sur une large gamme de fréquence et à très forte puissance.Similarly, the motor 152 acting on the plate 22 through the gear 154 meshing with the toothing 158 allows an overall displacement of all the antenna elements of the same angular offset around their axis X2-X2 by displacement of the plate 22, thus allowing phase shifting of all the antenna elements and therefore of the antenna. This phase shifter is able to operate over a wide range of frequencies and at very high power.

L'antenne ainsi formée permet donc, sans élément articulé dans le conduit de guidage d'amenée de l'onde, d'émettre une onde décalée angulairement.The antenna thus formed thus allows, without articulated element in the wave supply guide duct, to emit an angularly offset wave.

Ce décalage angulaire est obtenu sans qu'il soit besoin de bouger angulairement le châssis de l'antenne et son radome.This angular offset is obtained without the need to angularly move the frame of the antenna and its radome.

Suivant un exemple, illustrée en regard de la figure 4, chaque élément d'antenne 24 est formé d'un brin rayonnant 184 monté fixe en rotation par rapport au panneau 22. Tous les brins sont identiques et sont orientés de manière identique. Chaque brin est associé à une lentille de focalisation 186 disposée au droit du brin correspondant. Cette lentille est propre à focaliser l'onde électromagnétique produite le brin.Following an example, illustrated next to the figure 4 each antenna element 24 is formed of a radiating strand 184 fixedly fixed in rotation with respect to the panel 22. All the strands are identical and are oriented identically. Each strand is associated with a focusing lens 186 disposed in line with the corresponding strand. This lens is able to focus the electromagnetic wave produced the strand.

Ces lentilles sont associées à un mécanisme 188 de déplacement angulaire de chaque lentille 186 autour de deux axes 188A, 188B s'étendant perpendiculairement l'un à l'autre et parallèlement au plateau 22. Le mécanisme 188 est tel que toutes les lentilles présentent une même orientation, permettant ainsi une déviation d'un angle θ de l'ensemble des ondes électromagnétiques élémentaires émises initialement normalement au plateau 22 par chacun des brins 184.These lenses are associated with a mechanism 188 of angular displacement of each lens 186 about two axes 188A, 188B extending perpendicularly to each other and parallel to the plate 22. The mechanism 188 is such that all the lenses have a same orientation, thus allowing a deflection of an angle θ of the set of elementary electromagnetic waves normally initially transmitted to the plate 22 by each of the strands 184.

On conçoit qu'avec un tel agencement, l'onde cohérente produite par l'addition des ondes électromagnétiques élémentaires produites par chaque élément d'antenne se propage suivant un angle prédéfini θ par rapport à la normale au plateau 22.It is conceivable that with such an arrangement, the coherent wave produced by the addition of the elementary electromagnetic waves produced by each antenna element propagates at a predefined angle θ with respect to the normal to the plate 22.

Sur la figure 5 est représentée encore un exemple. Le brin d'antenne noté 284, correspondant au brin rayonnant 84, est enroulé en hélice autour d'un mat déformable élastiquement 286. En l'absence de sollicitation, le mat 286 s'étend perpendiculairement au plateau 22.On the figure 5 is shown again an example. The antenna strand noted 284, corresponding to the radiating strand 84, is helically wound around an elastically deformable mat 286. In the absence of stress, the mat 286 extends perpendicularly to the plate 22.

Comme précédemment, le mat 286 est lié à un mécanisme 188 de déplacement de son extrémité, permettant ainsi un fléchissement de l'axe de l'hélice du brin 284 par déformation du mat 286. Ainsi, le mécanisme 188 assure une émission de l'onde élémentaire produite par chaque brin suivant une direction décalée angulairement par rapport à la normale à la paroi 22.As previously, the mat 286 is connected to a mechanism 188 for moving its end, thus allowing the axis of the helix of the strand 284 to bend by deformation of the mat 286. Thus, the mechanism 188 ensures a transmission of the wave elementary produced by each strand in a direction angularly offset from the normal to the wall 22.

Dans l'exemple illustré sur la figure 6, une lentille de focalisation 288 est ajoutée à l'agencement décrit en regard de la figure 5. Cette lentille est placée à l'extrémité libre du mat 286.In the example shown on the figure 6 , a focusing lens 288 is added to the arrangement described with reference to FIG. figure 5 . This lens is placed at the free end of mat 286.

Suivant une variante du mode de réalisation de la figure 1, la paroi 48 est supprimée et les éléments d'antenne sont alors alimentés depuis le centre. Le convertisseur de mode 70 est porté par la face inférieure de la paroi 22.According to a variant of the embodiment of the figure 1 , the wall 48 is removed and the antenna elements are then fed from the center. The mode converter 70 is carried by the lower face of the wall 22.

Claims (5)

  1. A radiofrequency antenna comprising a chassis (26) and an emission surface (22) supporting a set of radiating antenna elements (24), each radiating in a unique emission direction, each antenna element (24) being at least partially movable relative to the emission surface (22) to modify its phase shift and including an emission wire (30) rotatably mounted relative to the emission surface (22), the antenna comprising means (25) for moving the antenna elements (24) in a coordinated manner along said surface (22) to form, from the elementary waves produced by the antenna elements (24), a coherent wave propagating in a direction (T-T) that is angularly offset relative to the normal to the emission surface, characterized in that the movement means (25) comprising racks (102) slidingly mounted relative to the emission surface (22) and the emission wires (80) being integral with drive pinions engaged with the racks (102), the movement means (25) comprising a mechanism (104, 106) for synchronized movement of the racks (102) and being capable of rotating the antenna elements (24),
    the synchronized movement mechanism (104, 106) includes a rotary control crown (104) relative to the chassis (26) and provided with control cams (122) of the racks (102), the racks each being equipped with at least one cam follower (120) cooperating with a cam (122), and a motor (106) for rotating the crown (104).
  2. The radiofrequency antenna according to claim 1, characterized in that the antenna elements (24) are distributed by groups of antenna elements, the elements of a same group being present in a strip of the emission surface extending perpendicular to the projection of the emission direction (T-T) on the surface, the antenna elements of a same group being positioned to produce elementary waves having a same phase shift relative to the waves produced by the antenna elements of another group.
  3. The radiofrequency antenna according to claim 1 or 2, characterized in that the means (25) for moving the antenna elements are adapted to position the antenna elements (24) so that they each produce an elementary wave phase shifted by a phase shift δΦ relative to the other antenna elements (24) defined by: δΦ = 2 πhtgθ / λ
    Figure imgb0005

    where θ is the incline angle of the emission direction (T-T) relative to the normal to the emission surface (22), λ is the wavelength of the electromagnetic radiation, and h is the distance of the antenna element (24) from a reference axis measured along the emission direction (T-T) on the emission surface (22).
  4. The radiofrequency antenna according to any one of the preceding claims, characterized in that the emission surface (22) supporting the radiating antenna elements (24) is rotary relative to the chassis (26), and in that it comprises means (152) for rotating the emission surface (22).
  5. The radiofrequency antenna according to any one of the preceding claims, characterized in that the chassis (26) delimits a closed vacuum space (26) in which the antenna elements are contained, and in that it comprises force-reacting guide pins between the chassis (26) and the emission surface (22).
EP11306778.9A 2010-12-27 2011-12-26 Radiofrequency antenna with multiple radiating elements for transmission of a wave with variable propagation direction Active EP2469649B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1005125A FR2969833A1 (en) 2010-12-27 2010-12-27 RADIO FREQUENCY ANTENNA HAVING MULTIPLE RADIATION ELEMENTS FOR TRANSMITTING A VARIABLE PROPAGATION-DIRECTING WAVE

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EP2469649A1 EP2469649A1 (en) 2012-06-27
EP2469649B1 true EP2469649B1 (en) 2013-06-12

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Publication number Priority date Publication date Assignee Title
US10742088B2 (en) 2016-12-30 2020-08-11 Panosense Inc. Support assembly for rotating body
US10109183B1 (en) * 2016-12-30 2018-10-23 Panosense Inc. Interface for transferring data between a non-rotating body and a rotating body

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Publication number Priority date Publication date Assignee Title
US3005983A (en) * 1947-10-30 1961-10-24 Charles H Chandler Focussing and deflection of centimeter waves
US2663869A (en) * 1950-07-07 1953-12-22 Adcock Mack Donald Helical antenna scanning system
US4427984A (en) * 1981-07-29 1984-01-24 General Electric Company Phase-variable spiral antenna and steerable arrays thereof
AU687349B2 (en) * 1992-04-24 1998-02-26 Industrial Research Limited Steerable beam helix antenna
JPH0677722A (en) * 1992-08-19 1994-03-18 Mitsubishi Electric Corp Antenna device
US6115005A (en) 1998-06-29 2000-09-05 Harris Corporation Gain-optimized lightweight helical antenna arrangement
DE10065024A1 (en) * 2000-12-23 2002-07-04 Bosch Gmbh Robert Device for adjusting the main beam direction of a radar sensor
US6407714B1 (en) * 2001-06-22 2002-06-18 Ems Technologies Canada, Ltd. Mechanism for differential dual-directional antenna array
CN1602564A (en) * 2001-11-09 2005-03-30 Ems技术公司 Antenna array for moving vehicles
US6552695B1 (en) * 2002-02-22 2003-04-22 Ems Technologies Canada, Ltd. Spin-scan array

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EP2469649A1 (en) 2012-06-27
US20120188136A1 (en) 2012-07-26

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