EP2830156B1 - Émetteur de rayonnement à conducteur creux, émetteur de rayonnement de réseaux d'antennes et émetteur de rayonnement de radar à ouverture synthétique - Google Patents
Émetteur de rayonnement à conducteur creux, émetteur de rayonnement de réseaux d'antennes et émetteur de rayonnement de radar à ouverture synthétique Download PDFInfo
- Publication number
- EP2830156B1 EP2830156B1 EP14002534.7A EP14002534A EP2830156B1 EP 2830156 B1 EP2830156 B1 EP 2830156B1 EP 14002534 A EP14002534 A EP 14002534A EP 2830156 B1 EP2830156 B1 EP 2830156B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- waveguide
- slots
- radiator
- inner conductor
- slotted
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
- 239000004020 conductor Substances 0.000 claims description 73
- 239000003989 dielectric material Substances 0.000 claims description 8
- 230000005284 excitation Effects 0.000 claims description 7
- 230000009467 reduction Effects 0.000 claims description 4
- 230000003252 repetitive effect Effects 0.000 claims 2
- 238000010586 diagram Methods 0.000 description 9
- 230000009977 dual effect Effects 0.000 description 8
- 230000010287 polarization Effects 0.000 description 7
- 230000009466 transformation Effects 0.000 description 6
- 230000007704 transition Effects 0.000 description 5
- 238000004519 manufacturing process Methods 0.000 description 4
- 230000005855 radiation Effects 0.000 description 4
- 230000008878 coupling Effects 0.000 description 3
- 238000010168 coupling process Methods 0.000 description 3
- 238000005859 coupling reaction Methods 0.000 description 3
- 230000001419 dependent effect Effects 0.000 description 3
- 238000006073 displacement reaction Methods 0.000 description 3
- 230000008901 benefit Effects 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 238000004804 winding Methods 0.000 description 2
- 238000004026 adhesive bonding Methods 0.000 description 1
- 238000004458 analytical method Methods 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 239000006185 dispersion Substances 0.000 description 1
- 230000005684 electric field Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000004904 shortening Methods 0.000 description 1
- 238000004088 simulation Methods 0.000 description 1
- 238000005549 size reduction Methods 0.000 description 1
- 230000001629 suppression Effects 0.000 description 1
Images
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q13/00—Waveguide horns or mouths; Slot antennas; Leaky-waveguide antennas; Equivalent structures causing radiation along the transmission path of a guided wave
- H01Q13/20—Non-resonant leaky-waveguide or transmission-line antennas; Equivalent structures causing radiation along the transmission path of a guided wave
- H01Q13/203—Leaky coaxial lines
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q13/00—Waveguide horns or mouths; Slot antennas; Leaky-waveguide antennas; Equivalent structures causing radiation along the transmission path of a guided wave
- H01Q13/10—Resonant slot antennas
- H01Q13/18—Resonant slot antennas the slot being backed by, or formed in boundary wall of, a resonant cavity ; Open cavity antennas
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/50—Structural association of antennas with earthing switches, lead-in devices or lightning protectors
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q21/00—Antenna arrays or systems
- H01Q21/0006—Particular feeding systems
- H01Q21/0037—Particular feeding systems linear waveguide fed arrays
- H01Q21/0043—Slotted waveguides
- H01Q21/005—Slotted waveguides arrays
Definitions
- the invention relates to a waveguide radiator with a slotted waveguide with a plurality of slots mounted in the waveguide.
- the invention further relates to a group antenna radiator and a synthetic aperture radar system.
- Waveguide radiators or array antenna radiators are used, for example, in phased array antennas of synthetic aperture radar (SAR) systems with single and dual polarization. So far, so-called microstrip patch antennas or slotted waveguide antennas are used as emitters.
- SAR synthetic aperture radar
- Microstrip patch antennas have high electrical losses and their electrical feed network is not efficient in longer radiator lengths than about seven wavelengths feasible (in the X-band about 20 cm).
- T / R modules transmitting / receiving modules
- the problem arises of dissipating the heat of the active modules, which are mounted on the back of the radiators, to the front.
- the slotted waveguide antennas are limited by their electrically resonant behavior in the achievable relative bandwidth ( ⁇ 5%). In addition, they require a high manufacturing accuracy and are very expensive to produce as dual polarized group radiators.
- Concepts used in the prior art include waveguides with inner lands and longitudinal slots for vertical polarization, and rectangular waveguides with skewed wires and transverse slots for horizontal polarization. Here are Also, the necessary transitions of the connected coaxial cable in the waveguide problematic.
- a waveguide radiator which comprises a slotted waveguide in which an additional inner conductor, a so-called barline, is mounted.
- This inner conductor is polarization-dependent specially shaped to excite all slots of the waveguide in phase.
- the propagation modes are no longer dispersive but correspond to those in coaxial lines, ie TEM modes. This can increase the bandwidth.
- the cross-sections of the waveguide can be significantly reduced in size, since there is no lower limit frequency (so-called cutoff) in TEM modes.
- the coupling can be done by a direct coaxial transition, which is mechanically very easy to implement, for example, by commercially available SMA chassis sockets.
- the waveguide radiator should be broadband, efficient and inexpensive to produce, so that from this a planar array antenna can be built, the u.a. can be used in space or airborne synthetic aperture radar (SAR) systems.
- SAR synthetic aperture radar
- a waveguide radiator comprising a slotted waveguide having a plurality of transverse or longitudinal slots mounted in the waveguide. If the waveguide has transverse slots, the direction of the emitted polarization of the waveguide corresponds to the longitudinal direction of the waveguide. If the slotted waveguide has longitudinal slots, the direction of the emitted polarization of the waveguide corresponds to the transverse direction of the waveguide. Depending on the orientation of the slots, thus either horizontally or vertically polarized waves can be radiated.
- the additional inner conductor mounted in the waveguide is such that the distance between adjacent slots along the waveguide corresponds to exactly one wavelength of a traveling wave to provide in-phase excitation, thereby providing a traveling wave principle and all slots of the waveguide can be excited in phase.
- a layer of dielectric material is mounted in the waveguide, on the upper side of which the inner conductor is mounted, for example by gluing. According to the height varies July 14, 2015 the dielectric material along the waveguide at least in sections, whereby the amplitude assignment of the slots along the waveguide can be influenced.
- TEM mode transversely electrically magnetic propagation mode
- the inner conductor is polarization-dependent specially shaped to stimulate either longitudinal or transverse slots can.
- the proposed waveguide radiator is distinguished from that in the DE 10 2006 057 144 A1 described waveguide radiators through a significantly higher bandwidth.
- the height or thickness of the dielectric layer is not uniform along the waveguide, but has an individually shaped height profile. Due to the height profile and the shape of the inner conductor, the amplitude and phase of the electric field strength in the slots along the waveguide can be selectively influenced, so that any aperture can be realized, for example, to suppress secondary maxima in the antenna pattern below a predetermined value. In the same way, it is also possible to achieve a homogeneous amplitude and phase coverage along the waveguide, for example in order to maximize the antenna gain and to minimize the half-width.
- Each slot of the waveguide radiator can have individual geometric dimensions. It is understood, however, that the waveguide radiator has either only longitudinal or transverse slots.
- the special shape of the inner conductor is composed of repeating sections of similar geometry along the waveguide. The length of these sections is identical to the spacing of adjacent slots along the waveguide.
- the additional inner conductor may be formed from, in particular alternately arranged, straight and winding conductor sections.
- One feature of the standing wave resonant feed is an additional quarter wave transformer located in each of the repeating sections.
- This quarter-wave transformer is realized by a taper of the inner conductor, i. a reduction of the conductor width.
- the length of this taper or conductor width reduction is preferably chosen so that it corresponds to an electrical path length of exactly one quarter of a line wavelength.
- the reduction of the conductor width causes an increase of the characteristic impedance along the tapered portion.
- the thus realized quarter-wave transformers compensate for the reflection points that would otherwise result at these positions.
- the inner conductor may have in the region of the ends of the waveguide a straight section as an open stub.
- a coupling of a signal can take place in the middle of the waveguide radiator through a galvanically coupled coaxial transition, in which the inner conductor a connected coaxial cable (eg via SMA, SMP connection) is connected directly to the feed point of the inner conductor.
- the outer conductor of the connected coaxial cable is connected directly to the wall of the waveguide.
- the feed point may be slightly offset in the transverse direction, thus allowing the transition to a mounted on the back of the radiator board at a suitable location.
- the feed point of the waveguide with respect to the geometric center of the waveguide may be displaced in the longitudinal direction.
- the displacement may be about 6 to 7 mm in a specific implementation, depending on the wavelength or frequency of the signal to be generated.
- the feed point of the waveguide can be arranged in the waveguide such that the electrical phase position at the positions of all slits is identical at center frequency.
- the additional inner conductor has a feed point which is arranged in the longitudinal direction of the slotted waveguide in the geometric center. It may further be provided that the slotted waveguide is formed with the additional inner conductor mirror-symmetrical about the feed point.
- the invention has the advantage that, in contrast to the resonant power supply, significantly higher bandwidths can be realized.
- the in the DE 10 2006 057 144 A1 mentioned advantages to conventional slotted waveguides are all preserved without compromising, such as no dispersion, size reduction of the cross section, no lower limit frequency, robustness to manufacturing tolerances, greater possible radiator lengths, low production costs, short production times, unproblematic transition to coaxial cable, high power feedable, low ohmic Losses, high cross-polar suppression.
- the development of the waveguide radiator in particular the determination of the exact geometric dimensions of the inner conductor and the slots is carried out by means of electromagnetic simulation method.
- the behavior of the radiator described here can also be described by network models with suitable equivalent circuit diagrams. These models are usually used in a first step in order to optimize the sizes of the elements present in the equivalent circuit diagram. In the second step, these quantities are then translated into suitable geometric parameters.
- Commercially available software packages can be used for this, which use full-wave analysis to calculate the electromagnetic behavior of the actual geometry (3D models).
- An array antenna radiator comprises one or more slotted waveguides with transverse slots and one or more slotted waveguides with longitudinal slits of the type described above.
- the slotted waveguides may be juxtaposed transversely in one configuration, alternately a waveguide with transverse slits and a waveguide Waveguide with longitudinal slots next to each other.
- the waveguides, ie all waveguides, preferably have an identical length.
- the waveguides with transverse slots can be offset upwards relative to the waveguides with longitudinal slots, so that a step-like structure of the array antenna radiator is given.
- At the top is that side of a respective waveguide radiator, on which the waveguides have the slots.
- a synthetic aperture radar system particularly a high resolution synthetic aperture radar system, comprises at least one array antenna radiator of the type described above.
- a waveguide radiator according to the invention with a slotted waveguide (hereinafter referred to as waveguide 10, 30) and an inner conductor 14, 34 arranged in the waveguide 10, 30 will be described below. It is between slotted waveguides 10, 30 with transverse slots 12 (FIG. Fig. 1 ) and longitudinal slots 32 (FIG. Fig. 6 ), in which the shape of the inner conductor 14 and 34 used differs.
- the exact configuration of the inner conductor 14 for the waveguide 10 with transverse slots 12 is in the Fig. 3 to 5 shown.
- the exact configuration of the inner conductor 34 for the waveguide 30 with longitudinal slots 32 is in the Fig. 8 to 10 shown.
- the geometrical dimensions given below refer to an exemplary embodiment in the X-band at a center frequency of 9.6 GHz.
- the radiator described here can be readily designed for deviating center frequencies.
- the size dimensions in this case scale over the ratio of the respective wavelengths.
- the waveguides 10, 30 are formed from conventional rectangular waveguides, in the transverse slots 12 and longitudinal slots 32 are introduced.
- the interior of the waveguides 10, 30 is filled with a dielectric material.
- the dielectric layer 24, 44 is in the Fig. 2 and 7 shown. While prior art radiators have a constant layer thickness, the dielectric layers 24, 44 of the invention have a variable height in the longitudinal extent of the waveguide.
- the choice of the material used for the dielectric layer is determined by its electrical properties, namely the dielectric constant and the loss angle.
- the dielectric constant influences the propagation velocity of the traveling wave traveling on the inner conductor (shortening factor).
- the distance between adjacent slots along the waveguide corresponds to exactly one wavelength of the traveling wave in order to achieve an in-phase excitation.
- the slot spacing is smaller than a free space wavelength in order to avoid unwanted secondary maxima (so-called grating praise).
- the slot pitch is in the range of 0.5 to 0.9 times a free space wavelength. This results in the value of the dielectric constant, which is thus typically in the range from 1.2 to 3.0.
- the loss angle should be as small as possible in order to keep the dielectric losses as low as possible, for a suitable material the value should be smaller than 1 ⁇ 10 -3 .
- the thickness of the dielectric layer 24, 44 along the waveguide has a characteristic profile.
- the height at the positions of the slots 12, 32 determines the proportion of the decoupled power of the traveling wave. A larger height results in a stronger decoupling, a lower level correspondingly reversed.
- the thickness of the dielectric layer 24, 44 increases to the outer ends of the respective waveguide 10, 30, because of the decreasing power of the traveling wave an ever higher relative proportion must be disconnected.
- Fig. 1 shows a waveguide 10 with transverse slots 12.
- the shape of the inner conductor 14 in the waveguide 10 with the transverse slots 12 is in Fig. 3 shown.
- the positions of the slots are in Fig. 3 indicated by arrows
- the middle area, which includes a feed point 16, is in Fig. 4 shown enlarged.
- the feed point 16 is offset relative to the geometric center in the longitudinal direction by approximately 6 mm. This displacement causes a phase difference of 180 ° of the outgoing from the feed point 16 traveling wave in the right and left part of the waveguide 10. In this way, an in-phase excitation of the slots results both in the right and in the left part of the waveguide 10th
- the inner conductor 14 begins immediately at the feed point 16 with sections 18 (transformation lines) with reduced conductor width. These are used to transform the characteristic impedance of the connected and not shown here coaxial cable of typically 50 ohms.
- sections 18 transformation lines
- the further course of the inner conductor 14 to the ends of the waveguide 10 consists of straight sections 18 with reduced conductor width and tortuous sections 20. The straight sections thus act as transformation lines.
- the twisting of the remaining portions 20 causes a delay of the propagation velocity of the traveling wave in the longitudinal direction of the waveguide 10. A stronger expression of the distortion causes a greater delay and vice versa.
- the phase difference between adjacent slots 12 can be set to exactly 360 °.
- the slots 12 are cut transversely into the outer wall of the waveguide 10. They protrude into the side walls with a cutting depth of about 4mm.
- the width of the slots 12 is about 2-3mm.
- the slots 12 have resonant behavior, the resonance frequency coincides with the center frequency of the radiator.
- the outermost slot 12A at the ends of the waveguide 10 with the underlying portion 22 of the inner conductor 14 has a peculiarity.
- the ends of the traveling waveguide are often resistively terminated in traveling-wave-principle radiators. This leads to undesirable losses, since the power remaining at the end of the line is dissipated in a resistor.
- the power remaining at the end of the line is radiated completely over the outermost slot, whereby additional losses are avoided.
- the height profile of the dielectric layer is designed such that the power remaining at the outermost slot 12A corresponds to the power coupled out at the remaining slots, whereby a homogeneous coverage of all slots 12, 12A is achieved while maintaining this boundary condition.
- Fig. 5 this shows an enlarged view of the region of the ends of the inner conductor Fig. 3 , wherein the unclip, open line termination can be seen with the section 22, which supports the described properties.
- Fig. 6 shows a waveguide 30 with longitudinal slots.
- the shape of the inner conductor 34 in a waveguide with longitudinal slots 30 is shown in FIG Fig. 8 shown.
- the central area containing the feed point 36 is in Fig. 9 shown enlarged.
- the feed point 36 is seen in the longitudinal direction in the geometric center. Displacement in the longitudinal direction, as in a waveguide with transverse slots 10, is not necessary in this case symmetrical construction of the right and left half of the waveguide 30, an in phase excitation of the slots 32 can be achieved.
- the inner conductor 34 begins immediately at the feed point 36 with transformation lines with reduced conductor width. These are used to transform to the characteristic impedance of the connected coaxial cable of typically 50 ohms.
- the further course of the inner conductor 34 to the ends of the waveguide consists of straight sections 38 and winding sections 40.
- the tortuous shape of the sections 40 is designed so that the inner conductor extends at the middle positions of the slots 32 in the transverse direction. This is necessary for a coupling of the longitudinal slots 32, since for this purpose a flow of the induced current in the transverse direction must be present on the wall of the waveguide 30.
- the position of the slots is in Fig. 8 indicated by arrows.
- the tortuous shape of the sections 40 additionally causes a delay of the propagation velocity of the traveling wave in the longitudinal direction of the waveguide. A stronger expression of the tortuous shape causes a greater delay and vice versa. This allows the phase difference between adjacent slots to be set to exactly 360 °.
- the slits 32 are cut longitudinally (longitudinally) into the outer wall of the waveguide 30.
- the slots 32 have a length of approximately half the free space wavelength. The exact length can vary slightly from slot to slot.
- the width of the slots is about 2 mm.
- the slots have resonant behavior, the resonance frequency coincides with the center frequency of the radiator.
- the outermost slot 32A at the ends of the waveguide 30 with the underlying portion 42 of the inner conductor 42 has a peculiarity. According to the prior art in emitter with traveling wave principle often the ends the traveling wave line resistive completed. This leads to undesirable losses, since the power remaining at the end of the line is dissipated in a resistor. In the concept of a traveling wave radiator with homogeneous excitation of all slots 32 presented here, the power remaining at the end of the line is radiated completely over the outermost slot 32A, whereby additional losses are avoided.
- the height profile of the dielectric layer 44 is designed in such a way that the power remaining at the outermost slot 32A corresponds to the power coupled to the remaining slots 32, so that a homogeneous coverage of all the slots 32, 32A can be achieved in compliance with this boundary condition.
- Fig. 10 shows an enlarged view of the region of the ends of the inner conductor Fig. 8 , Evident is the unsound, open line termination with the section 42 of the inner conductor 34, which supports the described properties.
- dual polarized radiator groups 60 can be realized in a simple manner. Since the widths of the waveguides can be greatly reduced with the emitter concept described here (up to a quarter of the wavelength), dual-polarized, electronically controllable array antennas with a very large swivel range can be realized (> ⁇ 60 °).
- Fig. 11 shows the construction of a dual polarized radiator group 60 (group antenna radiator). It consists of a combination of alternately a slotted waveguide 10 with transverse slots 12 and a waveguide 30 with longitudinal slots 32.
- the waveguides 10 with transverse slots 12 are about 7 mm to 8 mm in relation to the waveguides 30 with longitudinal slots 12 offset upwards, so that a step-like structure is formed.
- the proposed waveguide radiator is distinguished from the well-known from the prior art waveguide radiators by a significantly higher bandwidth. This is in the FIGS. 12 to 15 exemplified for a radiator of length 250mm for the X-band.
- Fig. 12 shows a representation of the total occurring in the radiator electrical losses in dB compared to an ideal aperture of the same size.
- the solid line curve represents traveling wave power source losses
- the dashed line curve represents resonant standing wave power losses.
- Fig. 13 shows a representation of the adjustment in dB, wherein the solid line curve to a radiator with traveling wave feed and the dashed line curve is assigned to a radiator with resonant feed (standing wave).
- Fig. 14 shows a plot of the radiation characteristics in dB (antenna diagram) of a radiator with traveling wave feed, where the dashed line curve shows the antenna pattern at 8.7 GHz, the solid line curve the antenna diagram at 9.6 GHz (center frequency) and the dotted line curve the antenna diagram at 10.5GHz show.
- Fig. 15 shows a plot of the radiation characteristics in dB (antenna diagram) of a resonant power source with a standing wave, where the dashed line curve shows the antenna pattern at 8.7GHz, the solid line curve the antenna pattern at 9.6GHz (center frequency) and the curve with dotted line show the antenna diagram at 10.5GHz.
Landscapes
- Waveguide Aerials (AREA)
- Variable-Direction Aerials And Aerial Arrays (AREA)
- Radar Systems Or Details Thereof (AREA)
Claims (13)
- Emetteur de rayonnement à conducteur creux, comprenant- un conducteur creux (10; 30) fendu et pourvu d'une pluralité de fentes (12; 32) transversales ou longitudinales ménagées dans le conducteur creux (10; 30); et- un conducteur interne (14; 34) supplémentaire placé à l'intérieur du conducteur creux (10; 30) et comportant des segments de conducteur (18, 20; 38, 40) qui présentent une largeur de conducteur réduite par rapport au conducteur restant, la longueur sur laquelle la largeur de conducteur est réduite étant choisie de manière à correspondre à une longueur de parcours électrique exactement égale au quart d'une longueur d'onde de conducteur de sorte que l'alimentation des fentes s'effectue selon le principe des ondes progressives dans le cadre duquel la distance entre les fentes (12; 32) contiguës le long du conducteur d'onde correspond exactement à une longueur d'onde d'une onde progressive pour obtenir une excitation en phase;- le conducteur creux (10; 30) fendu étant partiellement rempli d'un matériau (24; 44) diélectrique sur lequel est disposé le conducteur interne (14; 34) supplémentaire;caractérisé en ce que la hauteur du matériau (24; 44) diélectrique varie au moins localement le long du conducteur creux (10; 30) faisant ainsi que le réglage d'amplitude des fentes (12; 32) est influençable le long du conducteur creux (10; 30).
- Emetteur de rayonnement à conducteur creux selon la revendication 1, caractérisé en ce que le conducteur interne (14; 34) supplémentaire est formé par des segments de conducteur (18, 20; 38, 40) droits et des segments de conducteur sinueux disposés plus particulièrement en alternance.
- Emetteur de rayonnement à conducteur creux selon l'une des revendications précédentes, caractérisé en ce que le conducteur interne (14; 34) supplémentaire se compose de segments de conducteur (18, 20; 38, 40) répétitifs le long du conducteur creux (10; 30), la longueur des segments de conducteur étant identique à la distance entre les fentes (12; 32) contiguës le long du conducteur creux (10; 30).
- Emetteur de rayonnement à conducteur creux selon l'une des revendications précédentes, caractérisé en ce que le conducteur interne (14; 34) présente dans la zone des extrémités du conducteur creux (10; 30) un tronçon droit en tant qu'extrémité de ligne (22; 42) en circuit ouvert.
- Emetteur de rayonnement à conducteur creux selon l'une des revendications 1 à 4, caractérisé en ce que dans le cas d'un conducteur creux (10) fendu et pourvu de fentes (12) transversales, un point d'alimentation (16) du conducteur creux (10) est décalé dans le sens longitudinal par rapport au centre géométrique du conducteur creux.
- Emetteur de rayonnement à conducteur creux selon la revendication 5, caractérisé en ce que le point d'alimentation (16) du conducteur creux (10) est décalé par rapport au centre géométrique du conducteur creux (10) dans le sens longitudinal de sorte telle que la position de phase électrique est identique aux positions de toutes les fentes (12) à fréquence centrale.
- Emetteur de rayonnement à conducteur creux selon l'une des revendications 1 à 4, caractérisé en ce que dans le cas d'un conducteur creux (30) fendu et pourvu de fentes (32) longitudinales, le conducteur interne (34) présente un point d'alimentation (36) qui est disposé au centre géométrique dans le sens longitudinal du conducteur creux (30) fendu.
- Emetteur de rayonnement à conducteur creux selon la revendication 7, caractérisé en ce que le conducteur creux (30) fendu est réalisé avec le conducteur interne (34) supplémentaire de manière symétrique en image miroir autour du point d'alimentation (36).
- Emetteur de rayonnement de groupes d'antennes, comprenant un ou plusieurs conducteurs creux (10) fendus et pourvus de fentes (12) transversales selon l'une des revendications 1 à 6 et un ou plusieurs conducteurs creux (10) fendus et pourvus de fentes (32) longitudinales selon l'une des revendications 1 à 4 et 7 ou 8.
- Emetteur de rayonnement de groupes d'antennes selon la revendication 9, caractérisé en ce que les conducteurs creux (10; 30) fendus sont disposés les uns à côté des autres dans le sens transversal, un conducteur creux (10) pourvu de fentes (12) transversales et un conducteur creux (30) pourvu de fentes (32) longitudinales étant disposés en alternance l'un à côté de l'autre.
- Emetteur de rayonnement de groupes d'antennes selon la revendication 9, caractérisé en ce que les conducteurs creux (10; 30) présentent une longueur identique.
- Emetteur de rayonnement de groupes d'antennes selon l'une des revendications
9 à 11, caractérisé en ce que les conducteurs creux (10) pourvus de fentes (12) transversales sont décalés vers le haut par rapport aux conducteurs creux (30) pourvus de fentes (32) longitudinales si bien que l'émetteur de rayonnement de groupes d'antennes présente une structure en gradins. - Système radar à synthèse d'ouverture, plus particulièrement un système radar à synthèse d'ouverture à haute résolution, comprenant un émetteur de rayonnement de groupes d'antennes (60) selon l'une des revendications 9 à 12.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102013012315.1A DE102013012315B4 (de) | 2013-07-25 | 2013-07-25 | Hohlleiter-Strahler. Gruppenantennen-Strahler und Synthetik-Apertur-Radar-System |
Publications (2)
Publication Number | Publication Date |
---|---|
EP2830156A1 EP2830156A1 (fr) | 2015-01-28 |
EP2830156B1 true EP2830156B1 (fr) | 2016-12-07 |
Family
ID=51229797
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP14002534.7A Active EP2830156B1 (fr) | 2013-07-25 | 2014-07-22 | Émetteur de rayonnement à conducteur creux, émetteur de rayonnement de réseaux d'antennes et émetteur de rayonnement de radar à ouverture synthétique |
Country Status (6)
Country | Link |
---|---|
US (1) | US10651560B2 (fr) |
EP (1) | EP2830156B1 (fr) |
JP (1) | JP6370143B2 (fr) |
KR (1) | KR101926895B1 (fr) |
CA (1) | CA2857658C (fr) |
DE (1) | DE102013012315B4 (fr) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP3817147A1 (fr) | 2019-10-31 | 2021-05-05 | Airbus Defence and Space GmbH | Dispositif de conduit interne pour un émetteur de rayonnement à conducteur creux |
Families Citing this family (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US11605903B2 (en) * | 2016-08-10 | 2023-03-14 | Mitsubishi Electric Corporation | Array antenna apparatus and method for manufacturing array antenna apparatus |
US11830831B2 (en) | 2016-09-23 | 2023-11-28 | Intel Corporation | Semiconductor package including a modular side radiating waveguide launcher |
US11309619B2 (en) | 2016-09-23 | 2022-04-19 | Intel Corporation | Waveguide coupling systems and methods |
US10566672B2 (en) | 2016-09-27 | 2020-02-18 | Intel Corporation | Waveguide connector with tapered slot launcher |
US10256521B2 (en) | 2016-09-29 | 2019-04-09 | Intel Corporation | Waveguide connector with slot launcher |
US11394094B2 (en) | 2016-09-30 | 2022-07-19 | Intel Corporation | Waveguide connector having a curved array of waveguides configured to connect a package to excitation elements |
US10461388B2 (en) | 2016-12-30 | 2019-10-29 | Intel Corporation | Millimeter wave fabric network over dielectric waveguides |
RU174536U1 (ru) * | 2017-03-30 | 2017-10-19 | Федеральное государственное бюджетное образовательное учреждение высшего образования "Сибирский государственный университет геосистем и технологий" (СГУГиТ) | Волноводный излучатель |
JP6752394B2 (ja) * | 2018-05-02 | 2020-09-09 | 三菱電機株式会社 | 導波管スロットアレーアンテナ |
US11201414B2 (en) * | 2018-12-18 | 2021-12-14 | Veoneer Us, Inc. | Waveguide sensor assemblies and related methods |
US11196171B2 (en) * | 2019-07-23 | 2021-12-07 | Veoneer Us, Inc. | Combined waveguide and antenna structures and related sensor assemblies |
WO2021050173A1 (fr) * | 2019-09-10 | 2021-03-18 | Commscope Technologies Llc | Antennes à guide d'ondes à fuite ayant des nœuds rayonnants espacés ayant des rapports de couplage respectifs qui supportent un rayonnement efficace |
EP4197064A4 (fr) * | 2020-10-13 | 2024-02-28 | The Board of Regents of the University of Oklahoma | Cellule unitaire de réseau d'antennes guide d'ondes à fentes (swga) à double polarisation à bande x pour grands systèmes de radar à balayage électronique |
EP4148901A1 (fr) | 2021-09-09 | 2023-03-15 | Aptiv Technologies Limited | Antenne |
KR102710215B1 (ko) * | 2022-11-04 | 2024-09-26 | 엘아이지넥스원 주식회사 | 복사 소자 어레이 구조 및 이를 포함하는 aesa 레이더 시스템 |
WO2024151832A1 (fr) * | 2023-01-12 | 2024-07-18 | The Penn State Research Foundation | Guides d'ondes électromagnétiques déployables |
Family Cites Families (41)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2914766A (en) * | 1955-06-06 | 1959-11-24 | Sanders Associates Inc | Three conductor planar antenna |
NL277059A (fr) * | 1961-04-11 | |||
US3106713A (en) * | 1962-01-26 | 1963-10-08 | Furukawa Electric Co Ltd | Slot antenna having short radiating slots and long nonradiating distributed capacitance tuning slot |
US3193830A (en) * | 1963-07-25 | 1965-07-06 | Joseph H Provencher | Multifrequency dual ridge waveguide slot antenna |
US3701162A (en) * | 1964-03-24 | 1972-10-24 | Hughes Aircraft Co | Planar antenna array |
US3688225A (en) * | 1969-05-21 | 1972-08-29 | Us Army | Slot-line |
US3599216A (en) * | 1969-08-11 | 1971-08-10 | Nasa | Virtual-wall slot circularly polarized planar array antenna |
US3697993A (en) * | 1969-09-15 | 1972-10-10 | Westinghouse Electric Corp | Airborne pulse doppler radar system |
US3696433A (en) * | 1970-07-17 | 1972-10-03 | Teledyne Ryan Aeronautical Co | Resonant slot antenna structure |
US4197549A (en) * | 1977-08-17 | 1980-04-08 | Harris Corporation | Slot antenna |
US4160145A (en) * | 1978-02-16 | 1979-07-03 | Armstrong Cork Company | Microwave applicator device |
JPS553584U (fr) * | 1978-06-22 | 1980-01-10 | ||
US4243990A (en) * | 1979-04-30 | 1981-01-06 | International Telephone And Telegraph Corporation | Integrated multiband array antenna |
JPS56132805U (fr) * | 1980-03-07 | 1981-10-08 | ||
US4409595A (en) * | 1980-05-06 | 1983-10-11 | Ford Aerospace & Communications Corporation | Stripline slot array |
US4435715A (en) * | 1980-09-29 | 1984-03-06 | Hughes Aircraft Company | Rod-excited waveguide slot antenna |
FR2654555B1 (fr) * | 1989-11-14 | 1992-06-19 | Thomson Csf | Guide a fentes rayonnantes non inclinees a excitation par motif rayonnant. |
US5010351A (en) * | 1990-02-08 | 1991-04-23 | Hughes Aircraft Company | Slot radiator assembly with vane tuning |
SE469540B (sv) * | 1991-11-29 | 1993-07-19 | Ericsson Telefon Ab L M | Vaagledarantenn med slitsade haalrumsvaagledare |
US5483248A (en) * | 1993-08-10 | 1996-01-09 | Hughes Aircraft Company | Continuous transverse stub element devices for flat plate antenna arrays |
SE501714C2 (sv) * | 1993-09-06 | 1995-05-02 | Ericsson Telefon Ab L M | Gruppantenn |
SE510082C2 (sv) * | 1993-11-30 | 1999-04-19 | Saab Ericsson Space Ab | Vågledarantenn med tvärgående och längsgående slitsar |
US5650793A (en) * | 1995-06-06 | 1997-07-22 | Hughes Missile Systems Company | Centered longitudinal series/series coupling slot for coupling energy between a boxed stripline and a crossed rectangular waveguide and antenna array employing same |
US5914694A (en) * | 1996-09-19 | 1999-06-22 | Cal Corporation | Dual-band, dual polarization radiating structure |
FR2764739B1 (fr) * | 1997-06-13 | 1999-09-17 | Thomson Csf | Antenne reseau a fentes rayonnantes |
US6201507B1 (en) * | 1998-04-09 | 2001-03-13 | Raytheon Company | Centered longitudinal shunt slot fed by a resonant offset ridge iris |
US6166701A (en) * | 1999-08-05 | 2000-12-26 | Raytheon Company | Dual polarization antenna array with radiating slots and notch dipole elements sharing a common aperture |
US6304228B1 (en) * | 2000-10-06 | 2001-10-16 | Space Systems/Loral, Inc. | Stepped waveguide slot array with phase control and satellite communication system employing same |
JP4021150B2 (ja) * | 2001-01-29 | 2007-12-12 | 沖電気工業株式会社 | スロットアレーアンテナ |
US6731241B2 (en) * | 2001-06-13 | 2004-05-04 | Raytheon Company | Dual-polarization common aperture antenna with rectangular wave-guide fed centered longitudinal slot array and micro-stripline fed air cavity back transverse series slot array |
US6977621B2 (en) * | 2004-01-07 | 2005-12-20 | Motia, Inc. | Vehicle mounted satellite antenna system with inverted L-shaped waveguide |
US7202832B2 (en) * | 2004-01-07 | 2007-04-10 | Motia | Vehicle mounted satellite antenna system with ridged waveguide |
US6999039B2 (en) * | 2004-07-04 | 2006-02-14 | Victory Microwave Corporation | Extruded slot antenna array and method of manufacture |
WO2006019339A1 (fr) * | 2004-08-18 | 2006-02-23 | Telefonaktiebolaget Lm Ericsson (Publ) | Antenne a fentes de guide d'onde |
US7109928B1 (en) * | 2005-03-30 | 2006-09-19 | The United States Of America As Represented By The Secretary Of The Air Force | Conformal microstrip leaky wave antenna |
JP4822262B2 (ja) * | 2006-01-23 | 2011-11-24 | 沖電気工業株式会社 | 円形導波管アンテナ及び円形導波管アレーアンテナ |
WO2008068825A1 (fr) * | 2006-12-01 | 2008-06-12 | Mitsubishi Electric Corporation | Antenne de réseau à fente de ligne coaxiale et son procédé de fabrication |
DE102006057144B4 (de) | 2006-12-01 | 2013-10-17 | Astrium Gmbh | Hohlleiter-Strahler |
US8149177B1 (en) * | 2008-05-09 | 2012-04-03 | The United States Of America As Represented By The Secretary Of The Air Force | Slotted waveguide antenna stiffened structure |
JP5091044B2 (ja) * | 2008-07-31 | 2012-12-05 | 株式会社デンソー | マイクロストリップアレーアンテナ |
EP2587586B1 (fr) * | 2011-10-26 | 2017-01-04 | Alcatel Lucent | Système d'antennes distribuées et procédé pour fabriquer un système d'antennes distribuées |
-
2013
- 2013-07-25 DE DE102013012315.1A patent/DE102013012315B4/de not_active Expired - Fee Related
-
2014
- 2014-07-22 EP EP14002534.7A patent/EP2830156B1/fr active Active
- 2014-07-23 KR KR1020140093307A patent/KR101926895B1/ko active IP Right Grant
- 2014-07-23 CA CA2857658A patent/CA2857658C/fr active Active
- 2014-07-24 US US14/340,077 patent/US10651560B2/en active Active
- 2014-07-24 JP JP2014150583A patent/JP6370143B2/ja active Active
Non-Patent Citations (1)
Title |
---|
None * |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP3817147A1 (fr) | 2019-10-31 | 2021-05-05 | Airbus Defence and Space GmbH | Dispositif de conduit interne pour un émetteur de rayonnement à conducteur creux |
WO2021083661A1 (fr) * | 2019-10-31 | 2021-05-06 | Airbus Defence and Space GmbH | Dispositif conducteur interne pour élément rayonnant à guide d'ondes |
Also Published As
Publication number | Publication date |
---|---|
JP2015027086A (ja) | 2015-02-05 |
DE102013012315A1 (de) | 2015-01-29 |
KR20150013051A (ko) | 2015-02-04 |
EP2830156A1 (fr) | 2015-01-28 |
JP6370143B2 (ja) | 2018-08-08 |
CA2857658C (fr) | 2019-10-29 |
DE102013012315B4 (de) | 2018-05-24 |
KR101926895B1 (ko) | 2018-12-07 |
US10651560B2 (en) | 2020-05-12 |
CA2857658A1 (fr) | 2015-01-25 |
US20150029069A1 (en) | 2015-01-29 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP2830156B1 (fr) | Émetteur de rayonnement à conducteur creux, émetteur de rayonnement de réseaux d'antennes et émetteur de rayonnement de radar à ouverture synthétique | |
EP2256864B1 (fr) | Antenne destinée à la polarisation circulaire et dotée d'une surface de base conductrice | |
EP3411921B1 (fr) | Antenne à double polarisation | |
DE69008116T2 (de) | Ebene Antenne. | |
DE69907322T2 (de) | Antenne | |
DE60315654T2 (de) | Kompakte Mehrbandantenne | |
DE102009035359B4 (de) | Mikrostreifenleiterarrayantenne | |
DE60009874T2 (de) | V-Schlitz-Antenne für zirkulare Polarisation | |
DE69608132T2 (de) | Schlitzspiralantenne mit integrierter symmetriereinrichtung und integrierter zuleitung | |
DE60035003T2 (de) | Dualpolarisierte gedruckte Antenne und entsprechende Gruppenantenne | |
DE60034042T2 (de) | Rahmenantenne mit vier resonanzfrequenzen | |
DE102014112467B4 (de) | Speisenetzwerk für antennensysteme | |
DE3931752A1 (de) | Koaxialschlitzantenne des wanderwellenleitungstyps | |
DE102011076209B4 (de) | Antenne | |
EP3533110B1 (fr) | Cornet d'émission à double polarisation | |
DE69013199T2 (de) | Übergang von einem Hohlleiter mit reduzierter Höhe auf eine Mikrostreifenleitung. | |
EP2100348B1 (fr) | Émetteur de rayonnement à conducteur creux pour systèmes de radar à ouverture synthétique | |
DE102010014916B4 (de) | Phasengesteuerte Gruppenantenne | |
EP0933833B1 (fr) | Radiateur à guide d'ondes | |
DE102010014864B4 (de) | Hohlleiterverbindung für ein Antennensystem und Antennensystem | |
DE102020121358A1 (de) | Mäanderförmige Antennenanordnung | |
EP0285879B1 (fr) | Filtre de polarisation à large bande | |
WO2022038003A1 (fr) | Antenne | |
DE102013004707A1 (de) | Richtantenne für elektromagnetische Wellen | |
DE3009734A1 (de) | Antenne in form eines trichterhorns zur abstrahlung orthogonal polarisierter wellen |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
17P | Request for examination filed |
Effective date: 20140722 |
|
AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
AX | Request for extension of the european patent |
Extension state: BA ME |
|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
R17P | Request for examination filed (corrected) |
Effective date: 20150727 |
|
17Q | First examination report despatched |
Effective date: 20151211 |
|
GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
INTG | Intention to grant announced |
Effective date: 20160621 |
|
GRAS | Grant fee paid |
Free format text: ORIGINAL CODE: EPIDOSNIGR3 |
|
RAP1 | Party data changed (applicant data changed or rights of an application transferred) |
Owner name: AIRBUS DS GMBH |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE PATENT HAS BEEN GRANTED |
|
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
REG | Reference to a national code |
Ref country code: GB Ref legal event code: FG4D Free format text: NOT ENGLISH |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: EP Ref country code: AT Ref legal event code: REF Ref document number: 852451 Country of ref document: AT Kind code of ref document: T Effective date: 20161215 |
|
REG | Reference to a national code |
Ref country code: IE Ref legal event code: FG4D Free format text: LANGUAGE OF EP DOCUMENT: GERMAN |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R096 Ref document number: 502014002112 Country of ref document: DE |
|
REG | Reference to a national code |
Ref country code: SE Ref legal event code: TRGR |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LV Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20161207 |
|
REG | Reference to a national code |
Ref country code: LT Ref legal event code: MG4D |
|
REG | Reference to a national code |
Ref country code: NL Ref legal event code: MP Effective date: 20161207 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20161207 Ref country code: GR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170308 Ref country code: NO Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170307 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: FI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20161207 Ref country code: ES Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20161207 Ref country code: HR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20161207 Ref country code: RS Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20161207 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: NL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20161207 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 4 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20161207 Ref country code: CZ Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20161207 Ref country code: EE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20161207 Ref country code: IS Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170407 Ref country code: RO Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20161207 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: PL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20161207 Ref country code: SM Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20161207 Ref country code: BG Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170307 Ref country code: PT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170407 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R097 Ref document number: 502014002112 Country of ref document: DE |
|
PLBE | No opposition filed within time limit |
Free format text: ORIGINAL CODE: 0009261 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT |
|
26N | No opposition filed |
Effective date: 20170908 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20161207 Ref country code: DK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20161207 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R082 Ref document number: 502014002112 Country of ref document: DE Representative=s name: WUESTHOFF & WUESTHOFF, PATENTANWAELTE PARTG MB, DE Ref country code: DE Ref legal event code: R081 Ref document number: 502014002112 Country of ref document: DE Owner name: AIRBUS DEFENCE AND SPACE GMBH, DE Free format text: FORMER OWNER: AIRBUS DS GMBH, 82024 TAUFKIRCHEN, DE |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: PL |
|
REG | Reference to a national code |
Ref country code: IE Ref legal event code: MM4A |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20170722 Ref country code: CH Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20170731 Ref country code: LI Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20170731 |
|
REG | Reference to a national code |
Ref country code: GB Ref legal event code: 732E Free format text: REGISTERED BETWEEN 20180405 AND 20180411 |
|
REG | Reference to a national code |
Ref country code: BE Ref legal event code: MM Effective date: 20170731 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LU Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20170722 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 5 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: BE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20170731 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20161207 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MC Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20161207 Ref country code: HU Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT; INVALID AB INITIO Effective date: 20140722 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: CY Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20161207 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20161207 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: TR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20161207 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: AL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20161207 |
|
REG | Reference to a national code |
Ref country code: AT Ref legal event code: MM01 Ref document number: 852451 Country of ref document: AT Kind code of ref document: T Effective date: 20190722 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: AT Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20190722 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: IT Payment date: 20230724 Year of fee payment: 10 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: SE Payment date: 20230719 Year of fee payment: 10 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: DE Payment date: 20240719 Year of fee payment: 11 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: GB Payment date: 20240725 Year of fee payment: 11 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: FR Payment date: 20240730 Year of fee payment: 11 |