EP1328042A1 - Sub-système d'antenne à commande de phase - Google Patents
Sub-système d'antenne à commande de phase Download PDFInfo
- Publication number
- EP1328042A1 EP1328042A1 EP02025792A EP02025792A EP1328042A1 EP 1328042 A1 EP1328042 A1 EP 1328042A1 EP 02025792 A EP02025792 A EP 02025792A EP 02025792 A EP02025792 A EP 02025792A EP 1328042 A1 EP1328042 A1 EP 1328042A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- radar system
- data
- transmit
- 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.)
- Granted
Links
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 phase-controlled antenna subsystem with a phase-controlled Antenna array according to the preamble of claim 1.
- the invention is particularly applicable to a radar system in particular SAR, for antennas for electronic warfare or operational systems and for Navigation or communication systems.
- Possible platforms for the integration of the Functions according to the invention are ground, marine systems, aircraft, satellites, drones and missile as well as building or vehicle-bound systems.
- a radar system with a phase-controlled antenna array known that a data and supply network and a number of arranged thereon interchangeable, each containing a transmitter and receiver circuit Transmit / receive modules, a number of circulator circuits and a number of coupled to the transmitter and receiver circuits via the circulator circuits Includes antenna elements.
- the transmit / receive modules arranged at the back of the data and supply network which in several, a heat sink structure, an energy supply structure and an RF supply structure containing layers is built up.
- RF connecting elements to each located on the front of the data and supply network and each carried out with an antenna element coupled circulator circuits.
- the transmit / receive modules are from the back of the data and supply network interchangeable so that the radar system for the purpose of maintenance work must be accessible from the back.
- the object of the invention is to provide a radar system of the type mentioned in the introduction, which requires little space and in which the transmit / receive modules for Maintenance and repair purposes are easily interchangeable.
- the object is achieved by the radar system specified in claim 1.
- the invention provides a radar system with a phase-controlled antenna array created a data and supply network and a number of on the data and Supply network arranged interchangeable, each a transmitter and receiver circuit containing transmit / receive modules, a number of circulator circuits and a number of via the circulator circuits with the transmitter and receiver circuits coupled antenna elements. According to the invention, it is provided that in each of the transmit / receive modules transmitter and receiver circuit, Circulator circuit and antenna element are combined, and that the transmit / receive modules on the radiation side or on the front of the radar system are arranged interchangeably.
- a major advantage of the radar system according to the invention is that an exchange of transmit / receive modules from the radiation side or from the front of the Radar system can take place, which is a great advantage for many applications.
- the antenna array too can be adapted to a curved surface if a structure-integrated antenna is desired.
- Yet another advantage of the radar system according to the invention are short RF lines to the antenna and thus a low noise figure, lower RF losses and less signal coupling.
- it is an advantage of the invention Radar system that thereby a simple structure of the data and supply network is possible.
- the Transmitter and receiver circuit and the circulator circuit and the antenna element in Form of a multi-layer structure are integrated in the transmission / reception module.
- the antenna element is preferably in the form of a planar antenna on the top of the Transmit / receive module arranged.
- the multilayer structure contains several superimposed, the components of the transmitter and receiver circuit and substrates supporting the circulator circuit.
- a first substrate on the side of the transmission / reception module facing the data and supply network is arranged and an RF power amplifier of the transmitter and Receiver circuit carries.
- a second Substrate on the side of the transmitting / receiving network facing away from the data and supply network Module is arranged and the circulator circuit, the antenna element as well as parts of the transmitter and receiver circuit. This can result in a reduction of space requirements and an optimization of the noise figure possible.
- a further substrate is arranged, which further circuits, in particular an RF processing part and / or carries a digital processing part.
- the substrates are formed in one piece with a frame structure are, which are simultaneously a housing of the transmit / receive module and a mechanical Forms connection of the substrates to one another.
- the data and supply network is preferably in the form of a mechanical support structure trained for the transmit / receive modules, which at the same time a cooling structure for the Includes transmit / receive modules.
- the data and supply network is preferably designed as a multilayer structure, which the cooling structure in the form of a first layer and at least one further Circuit structure containing RF, data and power supply network in the form of a second layer includes.
- the cooling structure is preferably on the side facing the transmit / receive modules Side of the data and supply network arranged.
- the cooling structure is preferably in the form of an active cooling structure through which a cooling fluid flows educated.
- the substrates and / or the Frame structure made of aluminum nitride (AIN).
- the substrates themselves are made up of several Layers of aluminum nitride built up and contain vertical and horizontal electrical Contacts. These are multilayer systems that consist of several layers are built up. Electrical conductor tracks (horizontal electrical contacts). These interconnects are vertically interconnected by so-called vias connected (vertical electrical contacts).
- the substrates are stacked on top of each other and soldered together.
- the solder joint is preferably with hard solder balls, which are surrounded by solder.
- the substrates are preferably soldered to one another on the frame structures.
- the transmit / receive module is advantageously enclosed by a metal sleeve, which is attached using a soldering, welding or adhesive technique.
- the cuff will advantageously used to electromagnetic shrinkage of the module and to ensure the electrical contacts between the substrates and to make the module hermetic seal.
- the transmit / receive modules are preferably the same.
- the transmit / receive modules are advantageously from the radiation side or the Front placed on the data and supply network.
- a phase-controlled antenna array consisting of a larger number of antenna elements 9 is composed.
- the antenna elements 9 are part of each of a transmit / receive module 3.
- the transmit / receive modules 3 are for radiation and the reception of a radar transmission signal in the direction indicated by the arrow intended.
- a data and supply network 2 is used to supply the transmit / receive Module 3 with RF and data signals and for power supply and cooling the same provided.
- a system circuit 40 is arranged, which further processing circuits of the radar system includes. System circuit 40 may also be from the data and utility network be attached separately.
- the transceiver module 3 comprises a transmitter and receiver circuit 4 an RF power amplifier 5, a digital processing section 6 and an RF processing section 7 contains.
- the transmitter and receiver circuit 4 is via a circulator circuit 8 coupled to an antenna element 9, which is on the top or front of the transmit / receive module 3.
- each transmit / receive module 3 are thus each transmitter and receiver circuit 4, circulator circuit 8 and antenna element 9 summarized.
- the antenna element 9 is in the form of a front or top of the transmit / receive module 3 arranged planar antenna.
- the data and supply network 2, which the send / receive module 3 on its Front or on its radiation side is in the form of several layers, which a cooling structure 18 in the form of a first layer and another one RF, data and Circuit structures 19 comprising power supply networks in the form of second ones Layers.
- the cooling structure 18 is on that of the transmit / receive module 3 facing side of the data and supply network 2 arranged so that an intensive cooling contact between the cooling structure 18 and the transmit / receive module 3, in particular its HF power amplifier 5.
- Fig. 3 which shows an embodiment, such as a transmit / receive module 3 could be constructed in practice, are the transmitter and receiver circuit 4, the the RF power amplifier 5, the digital processing section 6 and the RF processing section 7, and the circulator circuit 8 in the form of a multi-layer structure in the transmit / receive module 3 integrated.
- the antenna element 9 is in the form of a planar antenna arranged on the top or front of the transmission / reception module 3.
- the multilayer structure contains several components arranged one above the other Transmitter and receiver circuit 4 and the circulator circuit 8 carrying substrates 11, 12, 13.
- a first substrate 11 is on the data and supply network 2 facing Arranged side of the transmit / receive module 3 and carries the RF power amplifier 5 of the transmitter and receiver circuit 4.
- a second substrate 12 is on the Data and supply network remote side of the transmit / receive module 3 arranged 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.
- the substrates 11, 12, 13 are in one piece formed with a respective frame structure 14, 15 or 16. These framework structures 14, 15, 16 simultaneously form a housing 17 of the transmit / receive module 3 and a mechanical one Connection of the substrates 11, 12, 13 to one another.
- the transmit / receive module is advantageously at least partially enclosed by a metal sleeve, which is fastened by means of a soldering, welding or adhesive technique.
- the sleeve is advantageously used to ensure electromagnetic shredding of the module and the electrical contacts between the substrates and to hermetically seal the module.
- the cuff is designated by the reference numeral 26 in the figures.
- 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 is designed in the form of a multi-layer structure, which the cooling structure 18 in the form of a first layer and at least one further a circuit structure 19 in the form of an RF data and power supply network a second layer.
- the cooling structure 18 is on the Transmit / receive module 3 facing side of the data and supply network 2 arranged.
- the one carrying the RF power amplifier 5 of the transmitter and receiver circuit 4 first substrate 11 is in intensive cooling contact with the cooling structure 18 of the Data and supply network 2 held.
- the cooling structure 18 is one of one Active cooling structure through which cooling fluid flows.
- the substrates 11, 12, 13 and the respective frame structures connected to it in one piece 14, 15 and 16 are made of Aln (aluminum nitrite) for efficient heat dissipation to ensure.
- the substrates themselves are made up of several layers of aluminum nitride constructed and contain vertical and horizontal electrical contacts.
- the substrates 11, 12, 13 are stacked one on top of the other and in the area of the frame structures 14, 15, 16 soldered together.
- Hard solder balls 26 are preferably used for the soldering, which are surrounded by solder during the soldering process and thus the electrical Connect contacts on the surface of the substrates. A blunt soldering without solder balls is also possible.
- the transmit / receive modules 3 are preferably all the same.
- a small section shows from a practical embodiment of the radar system according to the invention, it can be seen that the transmit / receive modules 3 from the radiation side to the data and supply network 2 put on and by attacking at the corner areas Screws 25 are attached to the data and supply network 2.
- the electrical Connection between the individual transmit / receive modules 3 and the data and supply network 2 is accomplished by electrical contact strips 50 which are in the top of the data and supply network 2, i.e. the cooling structure 18 embedded therein are, and by corresponding contact strips 60 on the underside of the transmission / reception modules 3.
- the contact strips designated by reference number 60 on the The underside of the modules is not visible in FIG. 4b.
- the module is to be connected to the data and supply network using CIN: APSE contacts be connected. It is a flexible cylindrical one Wire mesh, which forms a pressure contact in a plastic socket, which the electrical Connection between two surfaces that are pressed on from both sides, manufactures.
- the module is preferably with the help of such flexible pressure contacts Data and supply network connected.
Landscapes
- Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- Radar Systems Or Details Thereof (AREA)
- Variable-Direction Aerials And Aerial Arrays (AREA)
- Transceivers (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE10200561A DE10200561B4 (de) | 2002-01-09 | 2002-01-09 | Radarsystem mit einem phasengesteuerten Antennen-Array |
DE10200561 | 2002-01-09 |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1328042A1 true EP1328042A1 (fr) | 2003-07-16 |
EP1328042B1 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 (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2004013934A1 (fr) * | 2002-08-01 | 2004-02-12 | Raytheon Company | Cadre d'interconnexion dielectrique comprenant un protecteur d'interferences electromagnetiques et absorbeur d'hydrogene pour modules emetteurs/recepteurs en mosaique |
EP2159875A1 (fr) * | 2008-08-28 | 2010-03-03 | Thales Nederland B.V. | Antenne de réseau comprenant un moyen de suppression de l'effet de couple dans les espaces diélectriques entre les éléments de son radiateur sans établir de contacts galvaniques |
EP2159876A1 (fr) * | 2008-08-28 | 2010-03-03 | Thales Nederland B.V. | Antenne de réseau comprenant un moyen pour établir des contacts galvaniques entre les éléments de son radiateur tout en permettant leur expansion thermique |
WO2010116357A1 (fr) * | 2009-04-05 | 2010-10-14 | Elta Systems Ltd | Antenne à balayage électronique et son procédé de production |
WO2010111012A3 (fr) * | 2009-03-24 | 2010-11-18 | Raytheon Company | Articulation de translation |
WO2011042000A1 (fr) * | 2009-10-09 | 2011-04-14 | Eads Deutschland Gmbh | Frontal haute fréquence hermétique étanche |
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 |
EP2840647A1 (fr) * | 2013-08-22 | 2015-02-25 | Alcatel Lucent | Module d'antenne |
WO2011026034A3 (fr) * | 2009-08-31 | 2015-11-19 | Andrew Llc | Ensemble antenne cellulaire de type modulaire |
CN111541001A (zh) * | 2020-07-08 | 2020-08-14 | 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 |
Families Citing this family (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
AU2003255254A1 (en) * | 2002-08-08 | 2004-02-25 | Glenn J. Leedy | Vertical system integration |
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 |
JP5208817B2 (ja) * | 2009-03-10 | 2013-06-12 | 株式会社東芝 | 飛行体の冷却システム |
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 |
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 |
US20160072193A1 (en) * | 2013-05-02 | 2016-03-10 | Commonwealth Scientific And Industrial Research Organisation | Large Scale Phased Array Structure and Method of Fabrication |
IL228426B (en) | 2013-09-15 | 2018-10-31 | Elta Systems Ltd | Temperature control for show array antenna |
JP6391852B2 (ja) * | 2015-12-17 | 2018-09-19 | 三菱電機株式会社 | フェーズドアレイアンテナ |
JP6723382B2 (ja) * | 2017-01-23 | 2020-07-15 | 三菱電機株式会社 | フェーズドアレイアンテナ |
US11209306B2 (en) | 2017-11-02 | 2021-12-28 | Fluke Corporation | Portable acoustic imaging tool with scanning and analysis capability |
EP3827228A1 (fr) | 2018-07-24 | 2021-06-02 | Fluke Corporation | Systèmes et procédés pour capteurs d'imagerie acoustique détachables et attachables |
KR102616879B1 (ko) * | 2019-08-19 | 2023-12-26 | 삼성전자주식회사 | 복합 방열 부재를 포함하는 전자 장치 및 그 제조 방법 |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0718907A1 (fr) * | 1994-12-23 | 1996-06-26 | Daimler-Benz Aerospace Aktiengesellschaft | Réseau d'antennes à commande de phase et procédé pour sa fabrication |
EP0726612A1 (fr) * | 1995-02-03 | 1996-08-14 | Gec-Marconi Avionics (Holdings) Limited | Dispositif d'antenne |
JPH09130319A (ja) * | 1995-10-30 | 1997-05-16 | Nippon Hoso Kyokai <Nhk> | 移動体sng装置 |
US5940031A (en) * | 1996-09-05 | 1999-08-17 | 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 |
Family Cites Families (6)
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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 |
US5644277A (en) * | 1995-02-27 | 1997-07-01 | Hughes Aircraft Company | Three-wire-line vertical interconnect structure for multilevel substrates |
-
2002
- 2002-01-09 DE DE10200561A patent/DE10200561B4/de not_active Expired - Fee Related
- 2002-11-16 DE DE50206215T patent/DE50206215D1/de not_active Expired - Lifetime
- 2002-11-16 AT AT02025792T patent/ATE322090T1/de not_active IP Right Cessation
- 2002-11-16 EP EP02025792A patent/EP1328042B1/fr not_active Expired - Lifetime
- 2002-11-16 ES ES02025792T patent/ES2258588T3/es 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
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0718907A1 (fr) * | 1994-12-23 | 1996-06-26 | Daimler-Benz Aerospace Aktiengesellschaft | Réseau d'antennes à commande de phase et procédé pour sa fabrication |
EP0726612A1 (fr) * | 1995-02-03 | 1996-08-14 | Gec-Marconi Avionics (Holdings) Limited | Dispositif d'antenne |
JPH09130319A (ja) * | 1995-10-30 | 1997-05-16 | Nippon Hoso Kyokai <Nhk> | 移動体sng装置 |
US5940031A (en) * | 1996-09-05 | 1999-08-17 | 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 |
Non-Patent Citations (1)
Title |
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PATENT ABSTRACTS OF JAPAN vol. 1997, no. 09 30 September 1997 (1997-09-30) * |
Cited By (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2004013934A1 (fr) * | 2002-08-01 | 2004-02-12 | Raytheon Company | Cadre d'interconnexion dielectrique comprenant un protecteur d'interferences electromagnetiques et absorbeur d'hydrogene pour modules emetteurs/recepteurs en mosaique |
EP2159875A1 (fr) * | 2008-08-28 | 2010-03-03 | Thales Nederland B.V. | Antenne de réseau comprenant un moyen de suppression de l'effet de couple dans les espaces diélectriques entre les éléments de son radiateur sans établir de contacts galvaniques |
EP2159876A1 (fr) * | 2008-08-28 | 2010-03-03 | Thales Nederland B.V. | Antenne de réseau comprenant un moyen pour établir des contacts galvaniques entre les éléments de son radiateur tout en permettant leur expansion thermique |
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. |
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. |
EP2418345A1 (fr) * | 2009-03-24 | 2012-02-15 | Raytheon Company | Articulation à translation |
US9441404B2 (en) | 2009-03-24 | 2016-09-13 | Raytheon Company | Translating hinge |
WO2010111012A3 (fr) * | 2009-03-24 | 2010-11-18 | Raytheon Company | Articulation de translation |
US8270169B2 (en) | 2009-03-24 | 2012-09-18 | Raytheon Company | Translating hinge |
WO2010116357A1 (fr) * | 2009-04-05 | 2010-10-14 | Elta Systems Ltd | Antenne à balayage électronique et son procédé de production |
US9590317B2 (en) | 2009-08-31 | 2017-03-07 | Commscope Technologies Llc | Modular type cellular antenna assembly |
WO2011026034A3 (fr) * | 2009-08-31 | 2015-11-19 | Andrew Llc | Ensemble antenne cellulaire de type modulaire |
US11652278B2 (en) | 2009-08-31 | 2023-05-16 | Commscope Technologies Llc | Modular type cellular antenna assembly |
US8971056B2 (en) | 2009-10-09 | 2015-03-03 | Eads Deutschland Gmbh | Hermetically sealed radio-frequency front end |
WO2011042000A1 (fr) * | 2009-10-09 | 2011-04-14 | Eads Deutschland Gmbh | Frontal haute fréquence hermétique étanche |
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 |
EP2840647A1 (fr) * | 2013-08-22 | 2015-02-25 | Alcatel Lucent | Module d'antenne |
CN111541001A (zh) * | 2020-07-08 | 2020-08-14 | 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 |
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 |
Also Published As
Publication number | Publication date |
---|---|
DE50206215D1 (de) | 2006-05-18 |
ES2258588T3 (es) | 2006-09-01 |
US20030218566A1 (en) | 2003-11-27 |
JP2004028980A (ja) | 2004-01-29 |
DE10200561B4 (de) | 2006-11-23 |
US6876323B2 (en) | 2005-04-05 |
DE10200561A1 (de) | 2003-07-24 |
ATE322090T1 (de) | 2006-04-15 |
JP4156382B2 (ja) | 2008-09-24 |
EP1328042B1 (fr) | 2006-03-29 |
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