Classifications

• • G—PHYSICS
  • G01—MEASURING; TESTING
  • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
  • G01S7/00—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
  • G01S7/02—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S13/00
  • G01S7/03—Details of HF subsystems specially adapted therefor, e.g. common to transmitter and receiver
  • G01S7/032—Constructional details for solid-state radar subsystems
• • G—PHYSICS
  • G01—MEASURING; TESTING
  • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
  • G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
  • G01S13/02—Systems using reflection of radio waves, e.g. primary radar systems; Analogous systems
  • G01S13/06—Systems determining position data of a target
  • G01S13/42—Simultaneous measurement of distance and other co-ordinates
  • G01S13/44—Monopulse radar, i.e. simultaneous lobing
  • G01S13/4463—Monopulse radar, i.e. simultaneous lobing using phased 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
  • H01Q3/00—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system
  • H01Q3/26—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the relative phase or relative amplitude of energisation between two or more active radiating elements; varying the distribution of energy across a radiating aperture
• • G—PHYSICS
  • G01—MEASURING; TESTING
  • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
  • G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
  • G01S13/02—Systems using reflection of radio waves, e.g. primary radar systems; Analogous systems
  • G01S2013/0236—Special technical features
  • G01S2013/0245—Radar with phased array antenna
  • G01S2013/0254—Active array antenna
• • G—PHYSICS
  • G01—MEASURING; TESTING
  • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
  • G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
  • G01S13/02—Systems using reflection of radio waves, e.g. primary radar systems; Analogous systems
  • G01S2013/0236—Special technical features
  • G01S2013/0272—Multifunction radar

Definitions

• the present invention relates to radar architectures. It relates more particularly to the architecture of electronic scanning radars, comprising an antenna capable of exploring an area of the space deposit and site by electronic scans of one or more digitally controlled beams.
• multi-mission radars we generally mean radars capable of carrying out several types of functions during the same operating phase (monitoring, detection, tracking), the realized function being able to be different according to the portion of the space considered. to perform different missions at different times, to order different missions or to take on different roles within a larger surveillance structure.To have a multi-mission radar allows both to reduce the number of radars needed operations, and to increase the operational performance of the systems implemented.
• multi-mission radar is also, in a known manner, intimately linked to the notion of electronic scanning, a feature that can be implemented both in the context of a rotating antenna and a fixed antenna.
• the need for flexibility in the management of space and time, which characterize multi-mission radars requires at least the means to achieve an electronic scan in two planes, a horizontal plane (scanning in a bearing or azimuth) and a vertical plane (sweep in elevation or elevation).
• the search for the multi-mission character leads to the development of radar equipment having the capacity to simultaneously form several observation beams pointed in different directions of space and generally intended for the execution of different tasks.
• the definition of a new radar generally requires the definition of a new antenna specifically adapted to the needs, as well as that of the interconnection of this antenna with the various subassemblies. in particular responsible for the synthesis of the transmitted signal and the demodulation of the signal picked up by this antenna.
• An object of the invention is to propose a means for simplifying the design of multimission radars based on the implementation of active electronic scanning antenna Another goal is to allow the realization of radars whose operational capabilities can be changed without physical modification. Another goal is to allow the realization of evolving radars which can integrate new functions not included in the initial definition and whose different functions can be updated without the need to modify from a material point of view the -sets and / or interfaces between the different subsets.
• the invention relates to a modular radar architecture, characterized in that it comprises a plurality of identical elementary radar units in parallel, each unit comprising itself:
• a standard radiating surface comprising N radiating elements, capable of radiating and picking up microwave waves
• microwave transmission and detection means for generating and transmitting to the radiating elements a hyper-frequency wave of given shape and power as well as for amplifying the microwave waves picked up by the radiating elements,
• reception means for performing the video band transposition of the collected microwave waves and the digitization of the video signals obtained
• digital processing means for conditioning the digital signals provided by the receiving means
• the architecture according to the invention also comprises:
• a plurality of elementary radar units - a subset responsible for the general synchronization of the structure, supplying each subset with an identical set of reference signals,
• the different subsets are interconnected by an appropriate data and signal exchange structure.
• FIG. 1 a block diagram specifying the decomposition into functional zones of a conventional passive electronic scanning antenna radar
• FIG. 2 a block diagram specifying the decomposition into functional zones of an active antenna radar
• FIG. 3 a block diagram specifying the decomposition into functional zones of a radar defined on the basis of the architecture according to the invention
• FIG. 4 a block diagram making it possible to present the different types of subassemblies constituting the architecture according to the invention
• FIGS. 6 and 7 illustrations relating to a first example of implementation of the architecture according to the invention
• FIG. 8 an illustration relating to a second exemplary implementation of the architecture according to the invention
• FIGS. 9 and 10 illustrations relating to a third example. implementation of the architecture according to the invention.
• subassemblies to radiate or pick up electromagnetic waves.
• a scanning radar equipped with a passive antenna it is for example subassemblies January 1 comprising all the elements allowing a radiating element 12, or a set of radiating elements forming a radiating source constituting the antenna for radiating the electromagnetic wave generated by the transmitter 13 as well as those for transmitting to the receiver 14 the electromagnetic waves picked up by the radiating element 12.
• Such a subset 1 1 is considered as naturally parallelizable in that its integration into the system is achieved by connecting it to the inputs / outputs of the system provided for this purpose; the addition or deletion of a module of this type to modify the overall operation of the system having no impact on the intrinsic function of other subsets of the same type.
• the C-Class mainly consists of digital functional subsystems, performing functions of processing signals received after digitization or digital data processing and management, functions that are implemented by "multinode” digital processing machines capable of performing various operations, known to those skilled in the art, such as pulse compression, doppler filtering 1 6, management of waveforms, etc.
• node ie “processing node”
• processing node is meant here a processor, mono or multinoyau (or “core” according to the English name), with its external memory (SRAM and / or DRAM) and its communication links with the communication network or internodes allowing the various nodes of the machine to exchange information
• the number and size of the machines implemented depend essentially on the number of types of functions performed as well as the computing capacity of these machines. nes. Adding or removing such functional subsets is therefore done by activating or deactivating calculation routines and / or adding a processing node. This operation generally has no impact on the architecture integrating the machines used, provided that it has the necessary flexibility.
• Class B is for developed radars currently the part of the system with the least provisions to undergo changes without requiring major revisions.
• Class B machines are also machines that perform more specific functions of each designed radar. It includes in particular all analog functional subsystems such as synthesizers 17 whose function is, in general, to provide the other subsets synchronization signals and clock signals, signals generally specific to the sub-system. together for which they are intended.
• synthesizers 17 whose function is, in general, to provide the other subsets synchronization signals and clock signals, signals generally specific to the sub-system. together for which they are intended.
• transmitter subassemblies 13 and receiver 14 or the subset 18 responsible for climate conditioning system There are also transmitter subassemblies 13 and receiver 14 or the subset 18 responsible for climate conditioning system.
• Such a radar system comprising a large number of functional subassemblies of class B, is therefore inherently immature, so that, for example, two radars with distinct functional characteristics can not be designed from the same hardware structure, even if they have identical basic functionalities.
• Their implementation uses separate hardware devices (transmitter, receiver, synchronization signal generation module, or interconnection structure for example) personalized and specific to each system and therefore not interchangeable.
• FIG. 2 is then considered which shows the distribution, in the three structural classes defined above, of the various constituent sub-assemblies of an active-antenna electronic scanning radar as it can be developed at present.
• such radars are generally designed by starting from a simple adaptation of the architectures developed to realize radar with electronic scanning passive antenna.
• the proportion of subsets belonging to class B thus remains important, as illustrated in the figure.
• it is generally sufficient to modify the transmission chain by replacing the single transmitter 13 (for example an electronic power tube) and the distribution circuit 19 of the microwave to the radiating elements 22, by sending circuits
• the single transmitter 13 for example an electronic power tube
• the distribution circuit 19 of the microwave to the radiating elements 22
• This type of approach has the immediate advantage of limiting the technological risks incurred when it is decided to design an active antenna radar.
• the development costs are further limited to the development part needed to integrate new radiating sources each comprising a transmission module.
• This approach also increases, in a natural way, the number of subassemblies belonging to the class A of the modules with natural parallelization by integrating the modules participating in the emission. The emitted power thus becomes a modulable characteristic, since the function is proportional to the number of transmission channels implemented.
• such an approach does not in itself make it possible to envisage the parallelization of the reception functions.
• each subassembly 31 constitutes an autonomous assembly that integrates all the means allowing radiation and microwave wave capture but also the means for generating, demodulating and conditioning these waves.
• a radar structure advantageously consists of an association of independent subassemblies which can be configured separately and arranged to achieve the desired operational functions.
• FIG. 4 which presents a schematic diagram showing the different types of subsets defining a radar architecture according to the invention.
• the architecture is here presented in a partial way, focusing on the subsets responsible for performing the functions relating to the transmission, reception, local synthesis of the main synchronization signals, the synthesis of the emitted waveform and radar signal processing, objects of the invention claimed herein.
• Subassemblies located downstream of these subsets, which are in particular responsible for the processing of the data developed from the received signals are not here, for the sake of clarity, not shown.
• the radar architecture according to the invention mainly comprises: a first type 41 of sub-assembly, or "Building-Block" according to the English terminology, consisting of an elementary radar unit, or mini-radar;
• a second type of subassembly 42 consisting of a signal generator intended for overall synchronization
• a third type 43 of a subassembly consisting of one or more parallel signal processing machines (computers).
• the first type of subassembly 41 an elementary radar unit, comprises mainly: a radiating face 41 having N radiating elements mounted on a supporting structure (substrate),
• microwave circuits 412, or TR modules each comprising a solid state emitter device associated with a microwave phase shifter, and a microwave reception head itself comprising an amplifier and limiter device low noise,
• N receiver modules 413 also comprising a circuit for digitizing the video signal
• a module 414 for the local digital processing of the received signals, after digitization This device makes it possible, in particular, to condition the signals received by the various elements of the radiating face. By conditioning means, among other operations, the combination with the desired amplitudes and phases, after digitization, of the signals picked up by the radiating elements constituting the radiating face, a combination making it possible to constitute one or more primary reception beams in the direction or directions ( s) desired.
• a module 415 a local waveform and synchronization generator, whose role is to synthesize all of the synchronization signals and analog reference signals from the common signals generated by the single subset.
• -etemble 41 thus comprises all the resources necessary to transmit and receive a microwave on N channels. It also includes the resources for processing the waves received on all the N channels and, among other operations, combining the different paths together to form different beams that can be pointed in different directions. That is why it is defined here as an active, independent, or mini-radar elementary radar unit.
• the second type of subassembly 42 comprises all the means making it possible to coordinate a plurality of subassemblies 41, that is to say to associate in their operation several elementary radar units, to form a larger radar system.
• it comprises means for synthesizing, on the one hand high-level synchronization signals, and on the other hand to synthesize one or more reference local oscillators.
• these generic reference signals are advantageously identical for all the subsets to which they are provided.
• the particular synchronization signals necessary for the individual operation of each of the elementary units 41 are synthesized locally at the level of the units from the synchronization signals supplied by the subset 42.
• the general synchronization signals are distributed to the various subsets via point-to-point links 421 (electrical, optical, etc.).
• the third type of subassembly 43, data management and global digital processing module) comprises one or more parallel numerical machines (computers), arranged so as to be able to perform all the operations of digital processing of the signals delivered by the elementary radar units 41 as well as so as to be able to develop and deliver to these same elementary radar units the information, commands, necessary for each unit to determine its own mode of operation.
• parallel numerical machines computers
• the local digital processing devices 414 located at the level of the elementary radar units 41 and the module 43 cooperates according to the following general principle:
• Each module 414 of local digital processing mainly performs the processing and the association of the digital data corresponding to the N receive channel that the elementary radar unit to which it belongs. This association aims to combine the digital data of the different reception channels to form a given number M of beams pointing different directions of space; digital beam formation using techniques known to those skilled in the art and not developed here. In doing so, the flow rate of the data produced at the output of treatment is incidentally reduced.
• each module 414 transmits data to the global processing module 43 which recombines the data from the different elementary radar units to form one or more global beams representing the signal generally received by the radar in a given direction.
• the recombined data forming each global beam are processed separately by conventional radar signal processing methods.
• the distribution of the digital processing tasks of the signals received between the local processing modules 414 and the global processing module 43 can vary from one configuration to another in order to optimize the processing. computational load overall and consequently the processing time and the number of calculation units used.
• the architecture of this third type of subassembly 43 is defined so that the overall building block capacity can be modulated by simply adding or removing one or more processing nodes without the need to retouch at the interfaces between the different building blocks.
• the implementation of the different computers is carried out so that an operation contributing to the realization of a more general operation of treatment can be performed by one or the other machine depending on the composition Exactly the subset 43, the execution of a function can thus be advantageously distributed over all the machines present in the subset for a given configuration.
• the digital data 431 from or to the other subsets are conveyed by a dedicated communication bus.
• the three types of subassemblies constituting the architecture according to the invention advantageously make it possible, by themselves, to constitute radar structures corresponding to various operational requirements and having characteristics for this purpose.
• functional data in terms of angular precision and worn for example.
• the desired number of elementary radar structures (mini-radars) 41 are assembled by assembling the radiating faces in particular by arranging them on a mechanical structure of reception. 51 so as to constitute a global antenna having the desired geometry. It is also generally necessary to add a single subassembly 43 intended to perform the overall processing of the signals supplied by the elementary radar structures 41, as well as a single subassembly 42 intended to supply the general synchronization signals.
• This structure of digital data exchange, analogue reference signals (local oscillators) and synchronization signals can obviously be implemented in different ways, both from the point of view of the technical realization and from the point of view of the material organization of the exchanges and that from the point of view of the exchange protocols implemented.
• the conditions required for its design are simply those related to the need to maintain the architecture according to the invention a highly evolutionary character.
• the exchange structure must make it possible to integrate a variable number of elementary radar units and to make the mode of operation of each of these units completely configurable and to provide the module 42 with the information necessary to exploit the data provided by each unit.
• elementary radar units 41 taking into account how each of the units is configured.
• the radar architecture according to the invention is therefore a modular architecture in which the characteristic elements constituted by the elementary radar units 41 operate with a high degree of autonomy relative to each other. to others, which makes the overall operation of the architecture advantageously parameterizable.
• Radar equipment designed according to this architecture is by nature evolving both in terms of the range of functionalities achieved and the overall performance achieved. Changing the operational performance of the equipment can be easily modified by adding or removing one or more elementary radar units 41 (typically the number of units 41 may vary from 1 to a few hundred), as well as by modifying the data processing routines implemented by the device devices.
• This architecture therefore responds well to the problem which consists in particular in designing scalable multi-mission radar equipment that can, from a given configuration, evolve in a simple way to various configurations, according to new operational requirements.
• FIGS. 6 and 7, illustrate a first example of application of the modular radar architecture according to the invention.
• An important advantage of the radar architecture according to the invention consists in the great modularity of the assembly.
• This modularity advantageously finds its application in this first example of implementation, in which the problem to be solved consists in finding the means of widening the emission lobe of the radar.
• the use of a radar whose structure is in accordance with the architecture according to the invention makes it possible to propose a simple and adapted solution.
• the problem posed here can be advantageously solved by implementing an operating mode in which the elementary radar units are parameterized so as to constitute an antenna 61 divided into several zones, two zones 61 and 62 on FIG. 6, each zone forming a transmission sub-antenna of smaller size. Each sub-antenna is also associated, a central frequency of own emission and a given bandwidth.
• the global antenna is divided into two sub-antennas, each sub-antenna being respectively associated with the central transmission frequencies fe 1 and fe 2 .
• the passbands B 'of the transmitted waves have a width that is substantially equal and of a value such that, taking into account the values of the frequencies f ⁇ i and fe 2 , and of the width of the bandwidth B of the receivers of the elementary radar units, the waves emitted by each of the two sub-antennas have disjointed bandwidths. It is thus advantageously possible, without modifying the physical structure of the radar, to have two transmitters, each of size equal to half the size of the overall antenna and thus producing a transmission pattern advantageously widened in the field. compared to that of the global antenna.
• the signals emitted by the two sub-antennas having a frequency spectrum covered by the bandwidth of the receivers, the entirety of the energy radiated in a direction of space and reflected by a target is received by the receiver. antenna so that the reception of the signal is carried out without loss although the beam is widened on transmission.
• This concept can naturally be extended to the constitution of more than two transmit antennas and on both axes (azimuth and elevation).
• the important advantage obtained by the decomposition of the architecture according to the invention into a plurality of elementary radar units synchronized at high level by a general synchronization module particularly sensitive when the desired configuration requires to be able to drive each radiating sources separately.
• the preceding example represents only one use among others of this advantageous characteristic of the invention.
• an advantageous application of the architecture according to the invention consists in using this architecture to produce an active electronic scanning radar using a fixed antenna with four radiating panels, such as that illustrated in FIG.
• Such an antenna makes it possible, for example, to obtain a refresh time of the incompatible scanning of a conventional rotating system (order of magnitude: 0.1 s instead of 1 s)
• the architecture according to the invention proves particularly advantageous in that it makes it possible to produce an antenna whose adjacent panels, 81 and 82 for example, emit waves of frequencies Fe 1 and Fe 2 different from each other. so that the reception performed by each of the two panels considered, is not affected by the signal transmitted by one of the adjacent faces and this using a single unit 42 for the four faces.
• the architecture according to the invention proves particularly advantageous in that it makes it possible to produce an antenna whose adjacent panels, 81 and 82 for example, emit waves of frequencies Fe 1 and Fe 2 different from each other. so that the reception performed by each of the two panels considered, is not affected by the signal transmitted by one of the adjacent faces and this using a single unit 42 for the four faces.
• the elementary radar units are divided into four panels 81 to 84 placed back to back so as to form an antenna of parallelepipedal shape, the panels 81 and 83 on the one hand and 82 and 84 on the other hand form two groups of opposing panels (A and C on the one hand, B and D on the other hand), the emission frequency being the same (respectively Fei and Fe 2 ) for the two panels of one same group.
• FIGS. 9 and 10 illustrate a second example of application of the modular radar architecture according to the invention.
• This example illustrates how the architecture according to the invention advantageously makes it possible, in a simple manner, to realize a radar equipment capable of performing recognition, identification, and detected and non-cooperative detection functions ("NCTR" or "Non Cooperative” function Target Recognition "according to the Anglo-Saxon denomination).
• NCTR recognition, identification, and detected and non-cooperative detection functions
• Target Recognition According to the Anglo-Saxon denomination.
• the advantageous characteristic put forward by this application consists in the possibility offered of being able to define the waveform applied to each of the units 41 constituting the radar antenna independently of one unit to another.
• the realization of the NCTR function assumes that the radar used is capable of transmitting and receiving a modulated wave over a very wide band.
• the conventional "narrow band" approximation no longer works as soon as the antenna exceeds a size substantially greater than one meter. There is therefore a need to compensate for propagation delays in the antenna. These delays are mainly a function of the position of the sensor considered and the misalignment of the antenna beam formed. Thus, for example, for an antenna 5 meters in diameter, the catch-up at the periphery with respect to the center of the antenna can reach a maximum value of +/- 5 ns.
• this compensation is not easy and often, a specific compensation for each source constituting the antenna is impossible by design.
• this correction operation can be advantageously implemented simply as well on reception as on transmission.
• the radar architecture according to the invention provides a reception and digitization device on each reception channel of each elementary radar unit.
• the compensation may advantageously be performed as a simple digital correction operation of the signal received on each channel.
• the correction can thus be performed digitally in a simple and precise manner.
• the emitted wave it is advantageous to proceed in the manner illustrated by FIGS. 9 and 10.
• the emitted microwave pulse is synthesized by modulating the local oscillator OL 1 provided by the general synchronization module 42, by a signal Fl consisting of a local oscillator OL 2 in intermediate frequency itself modulated a ramp linear frequency frequency R, frequency deviation varying between - ⁇ f and + ⁇ f on a time interval equal to ⁇ t.
• a frequency ramp extending over a range of 300 MHz (-150 MHz to +150 MHz) is applied during a time interval equal to 30 ⁇ s corresponding to the duration of the transmitted pulse.
• the synthesis of the signal R is carried out in the same way for all the elementary radar units 41, so that the frequency of the modulation ramp R is zero in the middle of the duration of the pulse transmitted in accordance with FIG. the curve 101 of FIG. 10.
• the synthesis of the signal R is carried out differently for each unit 41; so that for some units 41, the passage of the signal R by a zero frequency occurs for a time before or after the instant t 0 corresponding to the middle of the transmitted RF pulse.
• the frequency deviation of the signal R is no longer centered on a zero frequency, but shifted by a difference in frequency ⁇ f positive or negative, according to the curve 102 of FIG. 10.
• This frequency difference ⁇ f is translated at the level of the microwave wave emitted by the corresponding time shift ⁇ t, this time difference being measured with respect to a general synchronization signal of the emissions sent identically to all the units 41.
• the microwave pulses emitted by a given elementary radar unit may appear on time, in advance or late.
• the architecture according to the invention therefore advantageously makes it possible to generate separately, for each radiating element, a delay, variable at emission between -5 ns and +5 ns in the example of FIG. 9, making it possible to compensate for the variations of propagation time appearing between the different radiating sources according to their positions on the antenna.
• the problems related to the implementation of the function WHR are thus naturally resolved by the use of the architecture according to the invention.
• the architecture according to the invention also makes it possible to perform functions for refining angular measurements, of the monopulse deviation type.

Landscapes

• Engineering & Computer Science (AREA)
• Radar, Positioning & Navigation (AREA)
• Remote Sensing (AREA)
• Computer Networks & Wireless Communication (AREA)
• Physics & Mathematics (AREA)
• General Physics & Mathematics (AREA)
• Radar Systems Or Details Thereof (AREA)

Applications Claiming Priority (2)

Publications (1)

Family

ID=39166425

Family Applications (1)

Country Status (8)

Families Citing this family (6)

Family Cites Families (28)

• 2007
  • 2007-08-03 FR FR0705709A patent/FR2919731A1/fr not_active Withdrawn
• 2008
  • 2008-07-31 EP EP08786693A patent/EP2174159A1/de not_active Withdrawn
  • 2008-07-31 KR KR1020107002456A patent/KR20100045987A/ko not_active Withdrawn
  • 2008-07-31 CA CA2694916A patent/CA2694916A1/en not_active Abandoned
  • 2008-07-31 AU AU2008285746A patent/AU2008285746A1/en not_active Abandoned
  • 2008-07-31 US US12/671,879 patent/US20110032141A1/en not_active Abandoned
  • 2008-07-31 WO PCT/EP2008/060068 patent/WO2009019191A1/fr not_active Ceased
• 2010
  • 2010-02-03 ZA ZA201000805A patent/ZA201000805B/xx unknown

Non-Patent Citations (1)

Also Published As

Similar Documents

Legal Events