EP1328042B1 - Sub-système d'antenne à commande de phase - Google Patents
Sub-système d'antenne à commande de phase Download PDFInfo
- Publication number
- EP1328042B1 EP1328042B1 EP02025792A EP02025792A EP1328042B1 EP 1328042 B1 EP1328042 B1 EP 1328042B1 EP 02025792 A EP02025792 A EP 02025792A EP 02025792 A EP02025792 A EP 02025792A EP 1328042 B1 EP1328042 B1 EP 1328042B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- radar system
- transmission
- data
- supply network
- transmitter
- 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.)
- Expired - Lifetime
Links
- 230000005540 biological transmission Effects 0.000 claims abstract description 27
- 239000000758 substrate Substances 0.000 claims description 49
- 238000001816 cooling Methods 0.000 claims description 33
- 238000012545 processing Methods 0.000 claims description 13
- 239000012809 cooling fluid Substances 0.000 claims description 3
- 229910000679 solder Inorganic materials 0.000 description 6
- 238000005476 soldering Methods 0.000 description 5
- PMHQVHHXPFUNSP-UHFFFAOYSA-M copper(1+);methylsulfanylmethane;bromide Chemical compound Br[Cu].CSC PMHQVHHXPFUNSP-UHFFFAOYSA-M 0.000 description 4
- 238000000034 method Methods 0.000 description 3
- 238000011161 development Methods 0.000 description 2
- 230000018109 developmental process Effects 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 238000003466 welding Methods 0.000 description 2
- 230000004308 accommodation Effects 0.000 description 1
- 239000000853 adhesive Substances 0.000 description 1
- 238000004026 adhesive bonding Methods 0.000 description 1
- 230000001070 adhesive effect Effects 0.000 description 1
- QLJCFNUYUJEXET-UHFFFAOYSA-K aluminum;trinitrite Chemical compound [Al+3].[O-]N=O.[O-]N=O.[O-]N=O QLJCFNUYUJEXET-UHFFFAOYSA-K 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 239000004020 conductor Substances 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000017525 heat dissipation Effects 0.000 description 1
- 230000010354 integration Effects 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
Images
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q21/00—Antenna arrays or systems
- H01Q21/0087—Apparatus or processes specially adapted for manufacturing antenna arrays
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q21/00—Antenna arrays or systems
- H01Q21/0006—Particular feeding systems
- H01Q21/0025—Modular arrays
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q23/00—Antennas with active circuits or circuit elements integrated within them or attached to them
Definitions
- the invention relates to a phased array antenna subsystem with a phased array antenna according to the preamble of claim 1.
- the invention is particularly applicable to a particular for a radar system, a SAR, for antennas for systems of electronic war or mission leadership and for navigation or communication systems.
- Possible platforms for the integration of the functions according to the invention are ground, naval systems, aircraft, satellites, drones and missiles as well as building or vehicle-bound systems.
- a radar system with a phased array antenna comprising a data and supply network and a number of interchangeable, each containing a transmitter and receiver circuit transceiver modules, a number of circulator circuits and comprises a number of antenna elements coupled via the circulator circuits to the transmitter and receiver shades.
- the transceiver modules are arranged on the rear side of the data and supply network, which is constructed in a plurality of layers containing a heat sink structure, a power supply structure and an RF supply structure.
- HF connectors are arranged at respective circulator circuits arranged at the front of the data and supply network and coupled to an antenna element.
- the transceiver modules are interchangeable from the back of the data and utility network, so the radar system must be accessible from the rear for maintenance.
- a transmission / reception module of the type described in the introduction in which the transmitter and receiver circuit, the circulator circuit and the antenna elements are combined and which is arranged interchangeably on the emission side of the radar system.
- the radar system is further characterized by the fact that a cooling system is provided for dissipating the heat generated by the transceiver module
- the object of the invention is to provide a radar system of the type mentioned with an improved cooling system.
- the object is achieved by the radar system specified in claim 1.
- the invention provides a radar system with a phased array antenna having a data and supply network and a number of interchangeable arranged on the data and supply network, each containing a transmitter and receiver circuit in multi-layer structure transceiver modules, a Number of circulator circuits and a number of antenna elements coupled via the circulator circuits to the transmitter and receiver circuits.
- each transmitter and receiver circuit, circulator circuit and antenna element are combined in each of the transmit / receive modules and the transmit / receive modules are arranged interchangeably on the emission side and at the front of the radar system.
- the data and supply network is designed as a mechanical support structure in multi-layer structure for the transmit / receive modules, which simultaneously in a first position on a the transmit / receive module side facing the data and supply network arranged, includes a cooling structure and arranged in at least one second layer below the cooling structure, comprising a circuit structure containing HF, data and power supply network.
- a significant advantage of the radar system according to the invention is that an exchange of transmit / receive modules can be carried out from the emission side or from the front of the radar system, which is a great advantage for many applications.
- a further advantage of the radar system according to the invention is that the antenna array can also be adapted to a curved surface if a structure-integrated antenna is desired.
- Yet another advantage of the radar system according to the invention Short RF cables to the antenna and thus a low noise figure, lower RF losses and lower signal coupling.
- it is an advantage of the radar system according to the invention that thereby a simple construction of the data and supply network is possible.
- the transmitter and receiver circuit and the circulator circuit and the antenna element are integrated in the form of a multi-layer structure in the transmission / reception module.
- the antenna element is arranged in the form of a planar antenna at the top of the transceiver module.
- the multilayer structure comprises a plurality of superimposed, the components of the transmitter and receiver circuit and the circulator circuit supporting substrates.
- a first substrate is arranged on the side facing the data and supply network side of the transmitting / receiving module and carries an RF power amplifier of the transmitter and receiver circuit.
- a second substrate is arranged on the side facing away from the data and supply network side of the transmission / reception module and carries the circulator circuit, the antenna element and parts of the transmitter and receiver circuit. This makes it possible to reduce the space requirement and to optimize the noise figure.
- At least between the first substrate and the second substrate at least a further substrate is arranged, which carries further circuits, in particular an HF processing part and / or a digital processing part.
- the substrates are integrally formed with a frame structure which simultaneously forms a housing of the transmission / reception module and a mechanical connection of the substrates to one another.
- the data and supply network is designed as a mechanical support structure for the transmit / receive modules, which simultaneously includes a cooling structure for the transmit / receive modules.
- the data and supply network is designed as a multi-layer structure, which comprises the cooling structure in the form of a first layer and at least one further, a HF, data and power supply network containing shading structure in the form of a second layer.
- the cooling structure is preferably arranged on the side of the data and supply network facing the transceiver modules.
- the cooling structure is preferably designed as an active cooling structure through which a cooling fluid flows.
- the first substrate carrying the RF power amplifier of the transmitter and receiver circuit is preferably in intensive cooling contact with the cooling structure of the data and supply network.
- the substrates and / or the frame structure are made of aluminum nitride (AIN).
- AIN aluminum nitride
- the substrates themselves are composed of several layers of aluminum nitride and contain vertical and horizontal electrical Contacts. These are multilayer systems that are made up of several layers. Between these layers are electrical conductors (horizontal electrical contacts). These tracks are connected by so-called vias vertically (vertical electrical contacts).
- the substrates are stacked on top of each other and soldered together.
- the solder joint is preferably made with hard solder balls encased in solder.
- the substrates are soldered to each other at the frame structures.
- the transmit / receive module is advantageously enclosed by a metal collar, which is attached by means of a soldering, welding or gluing technique.
- the collar is advantageously used to ensure electromagnetic chamfering of the module and the electrical contacts between the substrates and to hermetically seal the module.
- an electrical connection between the substrates forming electrical contacts are integrated in the frame structure.
- the transmit / receive modules are the same.
- the transmission / reception modules are placed on the data and supply network from the emission side or the front side.
- the transmit / receive modules are fastened to the data and supply network by means of screws engaging at their edge or corner regions.
- the reference numeral 30 denotes a phased array antenna, which is composed of a larger number of antenna elements 9.
- the antenna elements 9 are each part of a transmission / reception module 3.
- the transmission / reception modules 3 are provided for radiation and the reception of a radar transmission signal in the direction indicated by the arrow.
- a data and supply network 2 is provided for supplying the transmitting / receiving modules 3 with RF and data signals and for power supply and cooling thereof.
- a system circuit 40 is arranged, which includes further processing circuits of the radar system.
- the system circuit 40 may also be attached separately from the data and utility network.
- the transmission / reception module 3 includes a transmitter and receiver circuit 4 including an RF power amplifier 5, a digital processing section 6, and an RF processing section 7.
- the transmitter and receiver circuit 4 is coupled via a circulator circuit 8 to an antenna element 9, which is located at the top or front side of the transceiver module 3.
- the circulator circuit 8 and the antenna element 9 are thus combined.
- the antenna element 9 is in the form of a planar antenna arranged on the front side or upper side of the transceiver module 3.
- the data and supply network 2 which carries the transmitting / receiving module 3 on its front side or on its emission side, is in the form of a plurality of layers, which have a cooling structure 18 in the form of a first layer and further an HF, data and power supply network containing circuit structures 19 in the form of second layers.
- the cooling structure 18 is arranged on the side facing the transmitting / receiving module 3 side of the data and supply network 2, so that an intensive cooling contact between the cooling structure 18 and the transmitting / receiving module 3, in particular its RF power amplifier 5 exists.
- the transmitter and receiver circuit 4 the RF power amplifier 5, the digital processing part 6 and the RF processing part 7 includes, and the circulator circuit 8 integrated in the form of a multi-layer structure in the transmission / reception module 3.
- the antenna element 9 is arranged in the form of a planar antenna at the top or front side of the transceiver module 3.
- the multi-layer structure contains a plurality of superimposed, the components of the transmitter and receiver circuit 4 and the circulator circuit 8 supporting substrates 11, 12, 13.
- a first substrate 11 is disposed on the data and supply network 2 side facing the transceiver module 3 and carries the RF power amplifier 5 of the transmitter and receiver circuit 4.
- a second substrate 12 is arranged on the side facing away from the data and supply network side of the transceiver module 3 and carries the circulator circuit 8, the planar antenna and parts of the transmitter and receiver circuit, essentially for reasons of space and to improve the noise figure.
- a further substrate 13 is arranged, which carries further circuits, namely the digital processing part 6 and the RF processing part 7.
- the substrates 11, 12, 13 are integrally formed with a respective frame structure 14, 15 and 16, respectively. These frame structures 14, 15, 16 simultaneously form a housing 17 of the transmitting / receiving module 3 and a mechanical connection of the substrates 11, 12, 13 with each other.
- the transmit / receive module is advantageously at least partially enclosed by a metal collar, which is fastened by means of a soldering, welding or adhesive technique.
- the collar is advantageously used to ensure electromagnetic chamfering of the module and the electrical contacts between the substrates and to hermetically seal the module.
- the cuff is designated in the figures by the reference numeral 26.
- the data and supply network 2 is designed as a mechanical support structure for the transmit / receive modules 3 and at the same time contains a cooling structure 18 for the transmit / receive modules 3.
- the first substrate carrying the RF power amplifier 5 of the transmitter and receiver circuit 4 11 is in intensive cooling contact with the cooling structure 18 of the data and supply network. 2
- the data and supply network 2 in the form of a multi-layer structure is formed, which the cooling structure 18 in the form of a first layer and at least one further a circuit structure 19 containing an RF data and power supply network in the form of a second layer.
- the cooling structure 18 is arranged on the side of the data and supply network 2 facing the send / receive module 3.
- the first substrate 11 carrying the RF power amplifier 5 of the transmitter and receiver circuit 4 is kept in intensive cooling contact with the cooling structure 18 of the data and supply network 2.
- the cooling structure 18 is designed as an active cooling structure through which a cooling fluid flows.
- the substrates 11, 12, 13 and the respective integrally connected frame structures 14, 15 and 16 are made of Aln (aluminum nitrite) to ensure efficient heat dissipation.
- the substrates themselves are composed of several layers of aluminum nitride and contain vertical and horizontal electrical contacts.
- the substrates 11, 12, 13 are stacked and soldered together in the region of the frame structures 14, 15, 16.
- hard solder balls 26 are preferably used, which are surrounded by solder during the soldering process and thus connect the electrical contacts on the surface of the substrates. Blunt soldering without solder balls is also possible.
- the transmit / receive modules 3 are preferably all the same.
- FIGS. 4 a) and b which shows a small section of a practical embodiment of the radar system according to the invention, it can be seen that the transceiver modules 3 are connected to the data transmission from the emission side. and supply network 2 and secured by means engaging at the corners screws 25 on the data and supply network 2.
- the electrical connection between the individual transmitting / receiving modules 3 and the data and supply network 2 is accomplished by electrical contact strips 50, which are embedded in the top of the data and supply network 2, ie the cooling structure 18 thereof, and by corresponding contact strips 60th on the underside of the transceiver modules 3.
- the contact strips designated by the reference numeral 60 on the underside of the modules are not visible in FIG. 4b.
- the module should be connected to the data and supply network using CIN: APSE contacts. It is a flexible cylindrical wire mesh, which forms a pressure contact in a plastic socket, which produces the electrical connection between two surfaces which are pressed from both sides.
- the module is preferably connected to the data and supply network by means of such flexible pressure contacts.
Landscapes
- Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- Variable-Direction Aerials And Aerial Arrays (AREA)
- Radar Systems Or Details Thereof (AREA)
- Transceivers (AREA)
Claims (18)
- Système radar avec un arrangement d'antenne à commande de phase, qui comprend un réseau de données et d'alimentation (2) et un nombre de modules d'émission/réception (3) interchangeables, disposés sur le réseau de données et d'alimentation (2), contenant chacun un circuit d'émetteur et de récepteur (4) et un élément d'antenne (9) couplé au circuit d'émetteur et de récepteur (4), et réalisés en une structure à plusieurs couches, dans lequel un circuit d'émetteur et de récepteur (4), un circuit de circulateur (8) et un élément d'antenne (9) sont chaque fois rassemblés dans chacun des modules d'émission/réception (3) et les modules d'émission/réception (3) sont disposés de façon interchangeable sur la face rayonnante du système radar (1), caractérisé en ce que le réseau de données et d'alimentation (2) est réalisé comme une structure de support mécanique en une structure à plusieurs couches pour les modules d'émission/réception (3), qui comporte en même temps dans une première couche une structure de refroidissement (18) disposée sur une face du réseau de données et d'alimentation (2) tournée vers le module d'émission/réception (3) et qui comprend une structure de circuit (19) contenant un réseau HF, de données et d'alimentation électrique disposé dans au moins une deuxième couche en dessous de la structure de refroidissement (18).
- Système radar selon la revendication 1, caractérisé en ce que le circuit d'émetteur et de récepteur (4) et le circuit de circulateur (8) sont intégrés dans le module d'émission/réception (3) sous la forme d'une structure à plusieurs couches.
- Système radar selon la revendication 1 ou 2, caractérisé en ce que l'élément d'antenne (9) est disposé sur la face supérieure du module d'émission/réception (3) sous la forme d'une antenne planaire.
- Système radar selon la revendication 2 ou 3, caractérisé en ce que la structure à plusieurs couches contient plusieurs substrats disposés l'un au-dessus de l'autre, portant les composants du circuit d'émetteur et de récepteur (4) et le circuit de circulateur (8).
- Système radar selon la revendication 4, caractérisé en ce qu'un premier substrat (11) est disposé sur la face du module d'émission/réception (3) tournée vers le réseau de données et d'alimentation (2) et porte un amplificateur de puissance HF (5) du circuit d'émission/réception (4).
- Système radar selon la revendication 4 ou 5, caractérisé en ce qu'un deuxième substrat (12) est disposé sur la face du module d'émission/rëception (3) située à l'opposé du réseau de données et d'alimentation (2) et porte le circuit de circulateur (8).
- Système radar selon la revendication 4, 5 ou 6, caractérisé en ce qu'encore au moins un autre substrat (13) est disposé entre le premier substrat (11) et le deuxième substrat (12), qui porte d'autres circuits (6, 7), en particulier une partie de traitement HF (7) et/ou une parte de traitement numérique (6).
- Système radar selon l'une quelconque des revendications 4 à 7, caractérisé en ce que les substrats (11, 12, 13) sont réalisés d'un seul tenant avec une structure de cadre (14, 15, 16), qui forme en même temps un boîtier (17) du module d'émission/réception (3) et une liaison mécanique des substrats (11, 12, 13) l'un à l'autre.
- Système radar selon l'une quelconque des revendications 1 à 8, caractérisé en ce que la structure de refroidissement (18) est réalisée comme une structure de refroidissement active parcourue par un fluide de refroidissement.
- Système radar selon la revendication 9 en liaison avec une des revendications 5 à 8, caractérisé en ce que le premier substrat portant l'amplificateur de puissance HF (5) du circuit d'émission/réception (4) se trouve en contact de refroidissement intense avec la structure de refroidissement (18) du réseau de données et d'alimentation (2).
- Système radar selon l'une quelconque des revendications 4 à 10, caractérisé en ce que les substrats (11, 12, 13) et/ou la structure de cadre (14, 15, 16) sont fabriqués en AlN.
- Système radar selon l'une quelconque des revendications 4 à 11, caractérisé en ce que les substrats (11, 12, 13) sont empilés les uns sur les autres et brasés les uns aux autres.
- Système radar selon la revendication 12 en liaison avec la revendication 8, caractérisé en ce que les substrats (11, 12, 13) sont brasés les uns aux autres sur les structures de cadre (14, 15, 16).
- Système radar selon l'une quelconque des revendications 8 à 13, caractérisé en ce que des contacts électriques (20, 21, 22, 23, 24) formant une liaison électrique entre les substrats (11, 12, 13) sont intégrés dans la structure de cadre (14, 15, 16).
- Système radar selon l'une quelconque des revendications 1 à 14, caractérisé en ce que les modules d'émission/réception (3) sont identiques.
- Système radar selon l'une quelconque des revendications 1 à 15, caractérisé en ce que les modules d'émission/réception (3) sont empilés sur le réseau de données et d'alimentation (2) à partir de la face rayonnante.
- Système radar selon la revendication 16, caractérisé en ce que les modules d'émission/réception (3) sont fixés sur le réseau de données et d'alimentation (2) au moyen de vis (25) de fixation sur les arêtes et les coins de ceux-ci.
- Système radar selon l'une quelconque des revendications précédentes, caractérisé en ce que le module d'émission/réception (3) est au moins en partie entouré d'une manchette (26).
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE10200561 | 2002-01-09 | ||
DE10200561A DE10200561B4 (de) | 2002-01-09 | 2002-01-09 | Radarsystem mit einem phasengesteuerten Antennen-Array |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1328042A1 EP1328042A1 (fr) | 2003-07-16 |
EP1328042B1 true EP1328042B1 (fr) | 2006-03-29 |
Family
ID=7711752
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP02025792A Expired - Lifetime EP1328042B1 (fr) | 2002-01-09 | 2002-11-16 | Sub-système d'antenne à commande de phase |
Country Status (6)
Country | Link |
---|---|
US (1) | US6876323B2 (fr) |
EP (1) | EP1328042B1 (fr) |
JP (1) | JP4156382B2 (fr) |
AT (1) | ATE322090T1 (fr) |
DE (2) | DE10200561B4 (fr) |
ES (1) | ES2258588T3 (fr) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102009048838B3 (de) * | 2009-10-09 | 2011-01-20 | Eads Deutschland Gmbh | Hermetisches dichtes Hochfrequenz-Frontend |
Families Citing this family (28)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6825817B2 (en) * | 2002-08-01 | 2004-11-30 | Raytheon Company | Dielectric interconnect frame incorporating EMI shield and hydrogen absorber for tile T/R modules |
WO2004015764A2 (fr) * | 2002-08-08 | 2004-02-19 | Leedy Glenn J | Integration de systeme verticale |
US7545323B2 (en) * | 2005-10-31 | 2009-06-09 | The Boeing Company | Phased array antenna systems and methods |
US7439901B2 (en) * | 2006-08-08 | 2008-10-21 | Garmin International, Inc. | Active phased array antenna for aircraft surveillance systems |
US7825858B2 (en) * | 2007-02-28 | 2010-11-02 | Garmin International, Inc. | Methods and systems for frequency independent bearing detection |
US7831225B2 (en) * | 2007-07-26 | 2010-11-09 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Radio frequency power load and associated method |
JP4823263B2 (ja) * | 2008-03-31 | 2011-11-24 | 株式会社東芝 | 空中線装置 |
NL1035878C (en) * | 2008-08-28 | 2010-03-11 | Thales Nederland Bv | An array antenna comprising means to establish galvanic contacts between its radiator elements while allowing for their thermal expansion. |
NL1035877C (en) * | 2008-08-28 | 2010-03-11 | Thales Nederland Bv | An array antenna comprising means to suppress the coupling effect in the dielectric gaps between its radiator elements without establishing galvanic contacts. |
JP5208817B2 (ja) * | 2009-03-10 | 2013-06-12 | 株式会社東芝 | 飛行体の冷却システム |
US8270169B2 (en) | 2009-03-24 | 2012-09-18 | Raytheon Company | Translating hinge |
IL197906A (en) * | 2009-04-05 | 2014-09-30 | Elta Systems Ltd | Antenna arrays and method for creating them |
WO2011026034A2 (fr) | 2009-08-31 | 2011-03-03 | Andrew Llc | Ensemble antenne cellulaire de type modulaire |
JP5685816B2 (ja) * | 2010-01-28 | 2015-03-18 | 株式会社村田製作所 | 高周波受信モジュール |
JP5591760B2 (ja) * | 2011-06-06 | 2014-09-17 | 株式会社東芝 | アンテナユニット及びパネルアレイアンテナ装置 |
EP2549589A1 (fr) * | 2011-07-20 | 2013-01-23 | Alcatel Lucent | Dispositifs de communication sans fil et procédé pour la dissipation de chaleur dans de tels dispositifs |
US8902015B1 (en) | 2011-11-18 | 2014-12-02 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Radio frequency power load and associated method |
EP2642587B1 (fr) * | 2012-03-21 | 2020-04-29 | LEONARDO S.p.A. | Dispositif rayonnant actif modulaire pour antennes réseau balayées électroniquement |
US8982931B2 (en) * | 2013-03-15 | 2015-03-17 | Raytheon Company | RF puck |
EP2992569A4 (fr) * | 2013-05-02 | 2016-12-28 | Commonwealth Scient & Ind Res Organisation ( C S I R O ) | Structure d'antenne à balayage électronique à grande échelle, et procédé de fabrication |
EP2840647A1 (fr) * | 2013-08-22 | 2015-02-25 | Alcatel Lucent | Module d'antenne |
IL228426B (en) * | 2013-09-15 | 2018-10-31 | Elta Systems Ltd | Temperature control for show array antenna |
EP3392969B1 (fr) * | 2015-12-17 | 2021-10-20 | Mitsubishi Electric Corporation | Antenne réseau à commande de phase |
WO2018135003A1 (fr) * | 2017-01-23 | 2018-07-26 | 三菱電機株式会社 | Antenne réseau à commande de phase |
US11209306B2 (en) | 2017-11-02 | 2021-12-28 | Fluke Corporation | Portable acoustic imaging tool with scanning and analysis capability |
WO2020023622A1 (fr) | 2018-07-24 | 2020-01-30 | Fluke Corporation | Systèmes et procédés de projection et d'affichage de données acoustiques |
KR102616879B1 (ko) * | 2019-08-19 | 2023-12-26 | 삼성전자주식회사 | 복합 방열 부재를 포함하는 전자 장치 및 그 제조 방법 |
CN111541001B (zh) * | 2020-07-08 | 2020-09-29 | 成都雷电微力科技股份有限公司 | 一体化瓦片有源相控阵天线 |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US594031A (en) * | 1897-11-23 | Combined match-safe and cigar-cutter | ||
US3818386A (en) * | 1967-04-03 | 1974-06-18 | Texas Instruments Inc | Solid-state modular microwave system |
US5412414A (en) * | 1988-04-08 | 1995-05-02 | Martin Marietta Corporation | Self monitoring/calibrating phased array radar and an interchangeable, adjustable transmit/receive sub-assembly |
DE4203932A1 (de) * | 1992-02-11 | 1993-08-12 | Deutsche Aerospace | Sende-/empfangsmodul |
US5493305A (en) * | 1993-04-15 | 1996-02-20 | Hughes Aircraft Company | Small manufacturable array lattice layers |
DE4446189A1 (de) * | 1994-12-23 | 1996-06-27 | Daimler Benz Aerospace Ag | Phasengesteuerte Antenne und Verfahren zu deren Herstellung |
GB2297651B (en) * | 1995-02-03 | 1999-05-26 | Gec Marconi Avionics Holdings | Electrical apparatus |
US5644277A (en) * | 1995-02-27 | 1997-07-01 | Hughes Aircraft Company | Three-wire-line vertical interconnect structure for multilevel substrates |
JP3618858B2 (ja) * | 1995-10-30 | 2005-02-09 | 日本放送協会 | 移動体sng装置 |
US5745076A (en) * | 1996-09-05 | 1998-04-28 | Northrop Grumman Corporation | Transmit/receive module for planar active apertures |
US6166705A (en) * | 1999-07-20 | 2000-12-26 | Harris Corporation | Multi title-configured phased array antenna architecture |
-
2002
- 2002-01-09 DE DE10200561A patent/DE10200561B4/de not_active Expired - Fee Related
- 2002-11-16 AT AT02025792T patent/ATE322090T1/de not_active IP Right Cessation
- 2002-11-16 ES ES02025792T patent/ES2258588T3/es not_active Expired - Lifetime
- 2002-11-16 DE DE50206215T patent/DE50206215D1/de not_active Expired - Lifetime
- 2002-11-16 EP EP02025792A patent/EP1328042B1/fr not_active Expired - Lifetime
-
2003
- 2003-01-08 JP JP2003001934A patent/JP4156382B2/ja not_active Expired - Fee Related
- 2003-01-09 US US10/338,886 patent/US6876323B2/en not_active Expired - Lifetime
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102009048838B3 (de) * | 2009-10-09 | 2011-01-20 | Eads Deutschland Gmbh | Hermetisches dichtes Hochfrequenz-Frontend |
WO2011042000A1 (fr) | 2009-10-09 | 2011-04-14 | Eads Deutschland Gmbh | Frontal haute fréquence hermétique étanche |
Also Published As
Publication number | Publication date |
---|---|
JP4156382B2 (ja) | 2008-09-24 |
ES2258588T3 (es) | 2006-09-01 |
US6876323B2 (en) | 2005-04-05 |
DE10200561B4 (de) | 2006-11-23 |
DE50206215D1 (de) | 2006-05-18 |
US20030218566A1 (en) | 2003-11-27 |
JP2004028980A (ja) | 2004-01-29 |
EP1328042A1 (fr) | 2003-07-16 |
ATE322090T1 (de) | 2006-04-15 |
DE10200561A1 (de) | 2003-07-24 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP1328042B1 (fr) | Sub-système d'antenne à commande de phase | |
DE102006023123B4 (de) | Abstandserfassungsradar für Fahrzeuge mit einem Halbleitermodul mit Komponenten für Höchstfrequenztechnik in Kunststoffgehäuse und Verfahren zur Herstellung eines Halbleitermoduls mit Komponenten für ein Abstandserfassungsradar für Fahrzeuge in einem Kunststoffgehäuse | |
DE602004008653T2 (de) | Flexible konforme antenne | |
DE60313447T2 (de) | Eingebetteter planarer zirkulator und verfahren zu seiner herstellung | |
DE69715715T2 (de) | Streifenleiter mit Luft als Dielektrikum | |
DE602004003191T2 (de) | Mehrschichtige Hochfrequenzvorrichtung mit Planarantenne und Herstellungsverfahren | |
DE69821327T2 (de) | Kurzgeschlossene Streifenleiterantenne und Gerät damit | |
DE60111753T2 (de) | Dickschicht-millimeterwellen-sende-empfängermodul | |
DE602004001041T2 (de) | Aktive elektronisch gescannte antenne (aesa) mit niedrigem profil für ka-band-radarsysteme | |
DE60218101T2 (de) | Hochfrequenzschaltungsmodul | |
DE602005000137T2 (de) | Antennenanordnung für Flugzeugfensteröffnung | |
DE60122160T2 (de) | Antennenstruktur und zugehöriges verfahren | |
DE3887649T2 (de) | Schaltbarer Übergang zwischen einer Mikrostreifen- und einer Streifenleitung. | |
DE10129664C2 (de) | Antennenscheibe mit einem Hochfrequenzbauteil | |
DE60123141T2 (de) | Phasenarrayantenne mit patch-antennenelementen mit verbesserter leistung der parasitären antennenelementen bei millimeterwellenlängen-hochfrequenzsignalen | |
DE102017124974B3 (de) | Verbindungseinheit für Hochfrequenzgeräte | |
DE69904750T2 (de) | Elektrisches bauteil und elektrischer schaltungsmodul mit verbundenen erdungsflächen | |
DE102014011514A1 (de) | Kapazitiv geschmiertes Gehäuse, insbesondere kapazitiv geschmiertes Komponenten-Gehäuse für eine Antenneneinrichtung | |
DE69835664T2 (de) | Mikrostreifenleiterverteilungsarray für gruppenantenne und eine solche gruppenantenne | |
DE60119586T2 (de) | Phasenarrayantenne mit gestapeltem Patchantennenelement mit Einzelmillimeterwellenlängenspeisung und Mikrostreifen-Quadratur-zur-Zirkularpolarisationsschaltung | |
DE3876862T2 (de) | Mikrowellenprimaersende- und empfangsduplexer fuer orthogonalpolarisierte wellen. | |
WO2002063334A2 (fr) | Radar | |
DE69600976T2 (de) | Integrierte Flachantenne mit Umwandlungsfunktion | |
DE102009027530A1 (de) | Leiterplatte | |
DE69720837T2 (de) | Planares Antennenmodul |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
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 |
|
AK | Designated contracting states |
Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR IE IT LI LU MC NL PT SE SK TR |
|
AX | Request for extension of the european patent |
Extension state: AL LT LV MK RO SI |
|
17P | Request for examination filed |
Effective date: 20030807 |
|
AKX | Designation fees paid |
Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR IE IT LI LU MC NL PT SE SK TR |
|
17Q | First examination report despatched |
Effective date: 20040316 |
|
GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
GRAS | Grant fee paid |
Free format text: ORIGINAL CODE: EPIDOSNIGR3 |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR IE IT LI LU MC NL PT SE SK TR |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT;WARNING: LAPSES OF ITALIAN PATENTS WITH EFFECTIVE DATE BEFORE 2007 MAY HAVE OCCURRED AT ANY TIME BEFORE 2007. THE CORRECT EFFECTIVE DATE MAY BE DIFFERENT FROM THE ONE RECORDED. Effective date: 20060329 Ref country code: IE 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: 20060329 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: 20060329 |
|
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 |
|
REG | Reference to a national code |
Ref country code: IE Ref legal event code: FG4D Free format text: LANGUAGE OF EP DOCUMENT: GERMAN |
|
REF | Corresponds to: |
Ref document number: 50206215 Country of ref document: DE Date of ref document: 20060518 Kind code of ref document: P |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
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: 20060629 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: 20060629 |
|
REG | Reference to a national code |
Ref country code: SE Ref legal event code: TRGR |
|
GBT | Gb: translation of ep patent filed (gb section 77(6)(a)/1977) |
Effective date: 20060717 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
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: 20060829 |
|
REG | Reference to a national code |
Ref country code: ES Ref legal event code: FG2A Ref document number: 2258588 Country of ref document: ES Kind code of ref document: T3 |
|
ET | Fr: translation filed | ||
REG | Reference to a national code |
Ref country code: IE Ref legal event code: FD4D |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LI Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20061130 Ref country code: BE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20061130 Ref country code: MC Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20061130 Ref country code: CH Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20061130 |
|
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: 20070102 |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: PL |
|
BERE | Be: lapsed |
Owner name: EADS DEUTSCHLAND G.M.B.H. Effective date: 20061130 |
|
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: 20061116 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
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: 20060329 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: 20060630 |
|
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: 20060329 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: 20060329 |
|
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: 20060329 Ref country code: LU Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20061116 |
|
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: 20060329 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: NL Payment date: 20131121 Year of fee payment: 12 Ref country code: ES Payment date: 20131128 Year of fee payment: 12 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R081 Ref document number: 50206215 Country of ref document: DE Owner name: AIRBUS DEFENCE AND SPACE GMBH, DE Free format text: FORMER OWNER: EADS DEUTSCHLAND GMBH, 85521 OTTOBRUNN, DE Effective date: 20140916 Ref country code: DE Ref legal event code: R081 Ref document number: 50206215 Country of ref document: DE Owner name: AIRBUS DS ELECTRONICS AND BORDER SECURITY GMBH, DE Free format text: FORMER OWNER: EADS DEUTSCHLAND GMBH, 85521 OTTOBRUNN, DE Effective date: 20140916 Ref country code: DE Ref legal event code: R081 Ref document number: 50206215 Country of ref document: DE Owner name: HENSOLDT SENSORS GMBH, DE Free format text: FORMER OWNER: EADS DEUTSCHLAND GMBH, 85521 OTTOBRUNN, DE Effective date: 20140916 |
|
REG | Reference to a national code |
Ref country code: NL Ref legal event code: V1 Effective date: 20150601 |
|
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 NON-PAYMENT OF DUE FEES Effective date: 20150601 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 14 |
|
REG | Reference to a national code |
Ref country code: ES Ref legal event code: FD2A Effective date: 20151229 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: ES Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20141117 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R081 Ref document number: 50206215 Country of ref document: DE Owner name: AIRBUS DS ELECTRONICS AND BORDER SECURITY GMBH, DE Free format text: FORMER OWNER: AIRBUS DEFENCE AND SPACE GMBH, 85521 OTTOBRUNN, DE Ref country code: DE Ref legal event code: R081 Ref document number: 50206215 Country of ref document: DE Owner name: HENSOLDT SENSORS GMBH, DE Free format text: FORMER OWNER: AIRBUS DEFENCE AND SPACE GMBH, 85521 OTTOBRUNN, DE |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 15 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: FR Payment date: 20161118 Year of fee payment: 15 Ref country code: DE Payment date: 20161121 Year of fee payment: 15 Ref country code: GB Payment date: 20161122 Year of fee payment: 15 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: IT Payment date: 20161123 Year of fee payment: 15 Ref country code: SE Payment date: 20161118 Year of fee payment: 15 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R082 Ref document number: 50206215 Country of ref document: DE Representative=s name: LIFETECH IP SPIES & BEHRNDT PATENTANWAELTE PAR, DE Ref country code: DE Ref legal event code: R081 Ref document number: 50206215 Country of ref document: DE Owner name: HENSOLDT SENSORS GMBH, DE Free format text: FORMER OWNER: AIRBUS DS ELECTRONICS AND BORDER SECURITY GMBH, 82024 TAUFKIRCHEN, DE |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R119 Ref document number: 50206215 Country of ref document: DE |
|
REG | Reference to a national code |
Ref country code: SE Ref legal event code: EUG |
|
GBPC | Gb: european patent ceased through non-payment of renewal fee |
Effective date: 20171116 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20171117 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: ST Effective date: 20180731 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: FR Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20171130 Ref country code: DE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20180602 Ref country code: IT Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20171116 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: GB Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20171116 |