GB2303266A - Sidelobe supression radar - Google Patents
Sidelobe supression radar Download PDFInfo
- Publication number
- GB2303266A GB2303266A GB9613343A GB9613343A GB2303266A GB 2303266 A GB2303266 A GB 2303266A GB 9613343 A GB9613343 A GB 9613343A GB 9613343 A GB9613343 A GB 9613343A GB 2303266 A GB2303266 A GB 2303266A
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- United Kingdom
- Prior art keywords
- antenna
- channel
- output
- elements
- deriving
- 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.)
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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
- 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
-
- 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
- G01S7/28—Details of pulse systems
- G01S7/2813—Means providing a modification of the radiation pattern for cancelling noise, clutter or interfering signals, e.g. side lobe suppression, side lobe blanking, null-steering arrays
-
- 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
- G01S2013/0263—Passive array antenna
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)
- Variable-Direction Aerials And Aerial Arrays (AREA)
Abstract
A method and apparatus are provided for determining whether a signal received the main channel 2 (e.g. a monopulse sun channel) of an antenna 1 was incident on the antenna 1 in a direction corresponding to a high gain main lobe. A sidelobe suppression signal is generated from signals received from other channels 3, 4, 12 at least some of which (eg monopulse difference channels) are derived from antenna elements whose output generates the main channel. The signal is categorised as originating from a direction corresponding to the high gain main lobe, or alternatively a sidelobe, of the main channel by comparing the value of the signal received on the main channel with that of sidelobe suppression signal generated from the signals received on the other channels. One of the other channels 12 may be connected to an omni-directional guard antenna 11.
Description
RADAR APPARATUS
The present invention relates to radar apparatus and provides a means and method of determining whether a signal received by a main channel, particularly but not exclusively a sum channel, of an antenna of the apparatus has been received from a direction within a high gain main lobe of the antenna or whether it has been received from a direction lying outside the main lobe.
Many radar systems employ highly directional antennas, typically slotted planar waveguide array or phased array antennas, comprising a large number of antenna elements the outputs of which are summed to provide a sum channel output, which output has a characteristic gain pattern comprising a, normally central, main lobe and a number of sidelobes, the sidelobes typically decreasing in amplitude the greater the angle from the main lobe.
In addition to a sum channel, a radar antenna may also have one or more difference channel outputs. These are obtained by separately summing the outputs of the antenna elements in different regions of the antenna, typically four quadrants, and taking the difference between the signal received from two regions. This provides an interferometric technique which can provide an angular discriminant for tracking purposes.
A signal received from a small target in a direction corresponding to the main lobe of a sum channel of an antenna will provide a signal of similar intensity to a larger target in a direction lying outside the main lobe. Therefore it is not possible to use returned signal strength to determine whether a target lies in a direction of the main lobe or not.
The simplest way of determining the direction in which the target lies relative to the antenna is to scan the antenna noting the position of the main lobe when the maximum signal is received, the direction of the main lobe at this instant corresponding to the direction of the target. This however is often impracticable to implement or is ineffective, especially if the apparatus is operating in a mode such that its measurements of range and/or doppler frequency are ambiguous.
Guard antennas are widely used in primary and secondary radar applications to provide a means of distinguishing between main beam and sidelobe radar echoes. Guard antennas are normally relatively small in comparison with the main antenna and have a wide angle beam of substantially uniform gain relative to the main antenna However guard antennas may sometimes be integral with the main antenna. The signals received from the main antenna and guard antenna are compared, Figure 1 of the attached drawings illustrating a comparison of the relative gain of the two antennas. If the signal received from the main antenna M(z) is greater than the signal received from the guard antenna G(z) then the target must be located in a direction corresponding to the main lobe of the main antenna, and vice versa.This can be expressed as:
main antenna gain M(z) > guard antenna gain G(z) = within the main beam
main antenna gain M(z) < guard antenna gain G(z) = outside the main beam where z defines the angle at which the comparison is made.
In practice, conventional antenna configurations typically use a large, high gain main antenna and a small, broad beam wide-angle guard antenna. This type of implementation often provides inadequate G(z)/M(z) gain margin in the region A of the close-in sidelobes of the main antenna, as illustrated in Figure 2, where the gain of the guard antenna G(z) is less than the gain of the main antenna M(z) .
If to overcome the above problem the gain G(z) of the guard antenna is modified such that it has a gain pattem as illustrated in Figure 3, then while the gain pattem is sufficient such as to ensure the gain of the guard antenna is greater than the gain of the main antenna in the close-in sidelobe regions A, the gain of the guard antenna falls below that of the main antenna in the far-out regions B such that it is not possible to determine from a comparison of the main antenna and guard antenna signals whether a signal has been received in a direction corresponding to the main lobe of the main antenna C or whether that signal has been received from the far-out regions B.
One way in which it has been proposed to overcome this problem is to employ two guard antennas, the first being a small wide-angle antenna having a uniform gain G (z), as illustrated in Figure 4, and the second, a larger directional antenna, having a gain GXz).
By summing the power output of the two guard antennas the desired guard antenna gain is achieved, as shown by the broken line in Figure 4. If the signal received from the main antenna is greater than that of the combined channel of the guard antennas then the signal can unambiguously be classified as having been received in a direction corresponding to the main beam of the main antenna. The problem with this arrangement however is that it is necessary to employ both a small wide-angle guard antenna and also a larger directional guard antenna, substantially increasing the cost of such an arrangement, and often more importantly the bulk of the radar apparatus.
According to the present invention there is provided radar apparatus comprising an antenna having a plurality of antenna elements from which a plurality of output signals can be derived having different gain characteristics;
means for deriving from a first set of plurality of antenna elements a first output channel having a relatively high gain main lobe;
means for deriving from a second set of the plurality of antenna elements a second output channel having a different gain pattern, at least some of the plurality of antenna elements being common to the first and second sets;
means for deriving one or more further output channels each having a different gain pattern to the first and second output channels; and
a discriminator for generating a sidelobe suppression signal from the signals received on the second and one or more further output channels, the discriminator determining that the direction from which a signal is received by the antenna is in the main lobe of the first channel by comparison of the signal received on the first channel with the value of the sidelobe suppression.
The present invention arises from the realisation that channels other than the main channel of an antenna, the difference channel for example, have a high gain in the region corresponding to the relatively high gain sidelobes of the sum channel but have a null on the antenna boresight, the peak of the sum channel response. The difference channel for example can thus be used to provide at least in part the desired sidelobe suppression signal.
Preferably the antenna comprises a plurality of elements interconnected as a number of arbitrary groups, the output signals from the groups being combined in different manners such as to produce the first and second output channels.
Detailed examination of typical antenna patterns have now shown that the difference channel gain patterns possess the desirable gain margins for generating sidelobe suppression signals on or near the principal or cardinal planes of the antenna, but normally have inadequate gain in regions well off the boresight and in the intercardinal planes. By contrast small low gain guard antennas provide good coverage of sum channel sidelobes in the far-out and intercardinal regions, but generally show inadequate gain margin in the close-in sidelobe regions, and it is preferable that the apparatus further comprises such a guard type antenna having a wide beam relatively uniform gain pattern, the output of which is combined with the output of the second channel to provide the sidelobe suppression signal. This may be done by analogue or digital processing means.
It may be advantageous if the discriminator applies scaling factors to the second output channel and a further output channel to set their relative gains in the most suitable position relative to the first channel.
Depending on the application to which the antenna is put, it may be desirable for the second channel to be a ring difference channel, as this channel particularly possesses the desired gain margins.
Advantageously the antenna comprises a slotted planar waveguide array or phased array antenna consisting of a plurality of elements interconnected such as to define two groups, the output signals of the two groups being summed to obtain a sum channel, and differenced to obtain a difference channel. Preferably the antenna configuration comprises an antenna divided into four quadrants, each quadrant being defined by having a plurality of antenna elements the outputs of which are summed, the apparatus comprising means for generating from the difference in output of two pairs of horizontally separated quadrants an azimuth difference channel, and means for generating from the difference in output of two pairs of vertically separated quadrants an elevation difference channel. Advantageously each channel has a respective receiver associated with it.Alternatively the elevation difference channel and azimuth difference channel may be alternately switched to a common receiver.
According to a second aspect of the present invention there is provided a method of determining whether a signal received by radar apparatus is received from a direction within a high gain main lobe of a first channel of an antenna of the radar apparatus, the method comprising:
deriving a first output channel from a first set of a plurality of elements of the antenna with a relatively high gain pattern having a main lobe;
deriving from a second set of the plurality of elements of the antenna, a second output channel having a different gain pattern, some elements being common to the first and second sets;
deriving one or more further output channels each having a different gain pattern to the first and second output channels;;
generating a sidelobe suppression signal, the value of which is determined at least in part from the signal received on the second and one or more further output channels; and
determining that the direction from which a signal is received by the antenna is in the main lobe of the first channel by comparison of the value of a signal received on the first channel with the value of the sidelobe suppression signal.
One embodiment of the invention will now be described by way of example only with reference to Figures 5 to 8 of the accompanying drawings, of which:
Figure 5 is a schematic diagram of radar apparatus in accordance with the present invention;
Figure 6 illustrates the segmentation of the antenna of Figure 5;
Figure 7 is a plot of the typical gain characteristics of a ring difference channel of an array antenna along a transverse plane; and
Figure 8 shows a comparison of the gain characteristics between an augmented guard channel and the sum channel of the main antenna.
Referring to Figure 5, there is illustrated radar apparatus comprising a phased array antenna 1 having: a sum channel 2; an azimuth difference channel 3; and an elevation difference channel 4. Each channel has a respective amplifier 5, 6, 7 and receiver 8, 9, 10. The apparatus further comprises a wide-angle guard antenna 11 for providing a guard channel 12 to amplifier 13 and receiver 14. Signals from receivers 5, 6, 7 and 10 are fed into a discriminator 15 which, as described in more detail below, validates that a signal has been received from a direction corresponding to the main lobe of the sum channel antenna.
Referring to Figure 6 there is schematically illustrated the front face of the antenna 1 of
Figure 5. Each of the segments A to D comprises a plurality of antenna elements, the elements of each quadrant being connected to a common output. The outputs from each quadrant are interconnected such as to provide the following channels.
Sum channel S=A+B +C+D Azimuth difference channel DA = A + D - (B + C)
Elevation difference channel DE = A + B - (C + D).
In operation, signals received from the azimuth difference channel 3 and elevation difference channel 4 are alternately fed to discriminator 15. In addition the discriminator receives a signal from sum channel 2 and also from guard channel 12. The discriminator 15 generates a ring difference signal by digitally adding the azimuth and elevation difference channel voltage signals in phase quadrature. The gain characteristics of the resultant ring difference channel (in one axis only) are illustrated in Figure 7.
The discriminator digitally combines the signal power amplitude of the guard signal from receiver 14 with that of the ring difference signal to provide an augmented guard signal, in effect a sidelobe suppression signal. The gain characteristics of the augmented guard signal G,(z) compared to the gain characteristics of the main sum channel M(z) are illustrated in Figure 8. When the signal received from the sum channel receiver 8 is compared with the value of the augmented guard signal, the discriminator determines that the signal has been received by the antenna 1 in a direction within the main lobe of the sum channel of the antenna if the two signals comply with predetermined rations, or some other similar criteria..
The embodiment illustrated above is given by way of example only but many variations of this apparatus can be made within the scope of the claims appended hereto. In particular, the ring difference signal can be formed before the receivers by adding the elevation and azimuth difference channels in phase quadrature. This could be implemented by the waveguide structure. The power amplitudes of the ring difference channel and guard channel can then be combined after detection by the receivers to form an augmented guard signal. This arrangement allows three receiver channels to be used but may preclude the use of the difference channels for tracking. Another variation may use the azimuth or elevation difference channel alone, possibly selecting the appropriate channel according to circumstances.
Claims (21)
1. Radar apparatus comprising:
an antenna having a plurality of antenna elements from which a plurality of output signals can be derived having different gain characteristics;
means for deriving from a first set of the plurality of antenna elements a first output channel having a relatively high gain main lobe;
means for deriving from a second set of the plurality of antenna elements a second output channel having a different gain pattern, at least some of the plurality of antenna elements being common to the first and second sets;
means for deriving one or more further output channels having a different gain pattern to the first and second output channels; and
a discriminator for generating a sidelobe suppression signal from the signals received on the second and one or more further output channels, the discriminator determining that the direction from which a signal is received by the antenna is in the main lobe of the first channel by comparison of the signal received on the first channel with the value of the sidelobe suppression signal.
2. Apparatus as claimed in claim 1 wherein at least one of the one or more further output channels is derived from antenna elements none of which are comprised in the first set.
3. Apparatus as claimed in claim 2 wherein at least one of the one or more further output channels is derived from a separate antenna.
4. Apparatus as claimed in any preceding claim wherein one of the one of more further channels is derived from the output of a guard antenna.
5. Apparatus as claimed in any preceding claim wherein the sidelobe suppression signal corresponds to the complete sidelobe region associated with the first output channel.
6. Apparatus as claimed in any preceding claim comprising means for deriving a plurality of output channels, each having a different gain pattern to the first output channel, from respective sets of antenna elements, each set comprising at least some of the antenna elements of the first set of antenna elements, the discriminator generating the sidelobe suppression signal at least in part from said plurality of output channels.
7. Apparatus as claimed in any preceding claim wherein the second set of antenna elements itself comprises a plurality of subsets of antenna elements each subset incorporating at least some of the antenna elements of the first set, the antenna having a waveguide geometry such as to generate the second output channel from the subsets of antenna elements comprised in the second set.
8. Apparatus as claimed in any preceding claim wherein the antenna comprises a plurality of sets of elements each interconnected as a number of arbitrary groups, the output signals from the groups being combined in different manners such as to produce the first and second output channels.
9. Apparatus as claimed in any preceding claim wherein the antenna is a phased array antenna.
10. Apparatus as claimed in any preceding claim wherein the first channel is a sum channel of the antenna.
11. Apparatus as claimed in any preceding claim wherein the antenna is divided into four quadrants, each quadrant being defined by having a plurality of antenna elements the outputs of which are summed, the apparatus comprising means for generating from the difference in output of two pairs of horizontally separated quadrants an azimuth difference channel, and means for generating from the difference in output of two pairs of vertically separated quadrants an elevation difference channel.
12. Apparatus as claimed in claim 11 comprising means for summing in phase quadrature the output of the elevation difference channel and azimuth difference channel to produce a ring difference channel.
13. Apparatus as claimed in claim 11 or 12 wherein the elevation difference channel and azimuth difference channel are alternatively switched to a common receiver.
14. Apparatus substantially as hereinbefore described with reference to Figures 5 to 8 and as illustrated in Figures 5 and 6 of the accompanying drawings.
15. A method of determining whether a signal received by radar apparatus is received from a direction within a high gain main lobe of a first channel of an antenna of the radar apparatus, the method comprising:
deriving a first output channel from a first set of a plurality of elements of the antenna with a relatively high gain pattern having a main lobe;
deriving from a second set of the plurality of elements of the antenna. a second output channel having a different gain pattern. some elements being common to the first and second sets;
deriving one or more further output channels each having a different gain pattem to the first and second output channels;
generating a sidelobe suppression signal, the value of which is determined at least in part from the signal received on the second and one or more further output channels; and
determining that the direction from which a signal is received by the antenna is in the main lobe of the first channel by comparison of the value of a signal received on the first channel with the value of the sidelobe suppression signal.
16. A method as claimed in claim 15 comprising deriving the one or more further output channels from antenna elements none of which are comprised in the first set.
17. A method as claimed in claim 15 or 16 comprising deriving at least one of the one or more output channels from a separate guard antenna.
IS A method as c]ined in any one of clams 15 to 17 wherein the sidelobes suppression signal corresponds to the complete sidelobe region associated with the main lobe of the first output channel.
19. A method as claimed in any one of claims 15 to 18 comprising deriving a plurality of output channels from respective sets of antenna elements, each having a different gain pattern to the first output channel. each set comprising at least some of the antenna elements of the first set, and generating the sidelobe suppression signal at least in part from said plurality of output channels.
20. A method as claimed in any one of claims 15 to 19 comprising deriving the second output channel from a plurality of subsets of elements comprised in the second set of elements, each subset incorporating at least some of the elements of the first set, and combining the output of the subsets to generate the second channel.
21. A method substantially as hereinbefore described with reference to Figures 5 to 8 of the accompanying drawings.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB9613343A GB2303266B (en) | 1995-07-07 | 1996-06-26 | Radar apparatus |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GBGB9513936.6A GB9513936D0 (en) | 1995-07-07 | 1995-07-07 | Radar apparatus |
GB9613343A GB2303266B (en) | 1995-07-07 | 1996-06-26 | Radar apparatus |
Publications (3)
Publication Number | Publication Date |
---|---|
GB9613343D0 GB9613343D0 (en) | 1996-08-28 |
GB2303266A true GB2303266A (en) | 1997-02-12 |
GB2303266B GB2303266B (en) | 2000-01-19 |
Family
ID=26307348
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB9613343A Expired - Lifetime GB2303266B (en) | 1995-07-07 | 1996-06-26 | Radar apparatus |
Country Status (1)
Country | Link |
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GB (1) | GB2303266B (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1067396A2 (en) * | 1999-07-09 | 2001-01-10 | TRW Inc. | Self-guarding monopulse antenna |
WO2005116680A1 (en) * | 2004-05-28 | 2005-12-08 | Telefonaktiebolaget Lm Ericsson (Publ) | A method and arrangement for identifying side-lobe signals |
FR2888332A1 (en) * | 2005-07-08 | 2007-01-12 | Thales Sa | Bistatic radioelectric detection barrier for protecting geographical zone, has reception unit comparing echo level received from waves emitted by directive and non directive emission antennae to identify echo in direction of secondary lobe |
WO2014077946A1 (en) * | 2012-11-14 | 2014-05-22 | Raytheon Company | Antenna system having guard array and associated techniques |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1017966A (en) * | 1962-04-10 | 1966-01-26 | Csf | Improvements in radar systems |
GB1316562A (en) * | 1971-03-01 | 1973-05-09 | Cossor Ltd A C | Secondary radar systems |
US4023172A (en) * | 1959-12-17 | 1977-05-10 | Numax Electronics Incorporated | Monopulse system for cancellation of side lobe effects |
US4298872A (en) * | 1980-05-27 | 1981-11-03 | Hughes Aircraft Company | Sidelobe blanking system |
US4959653A (en) * | 1989-08-23 | 1990-09-25 | Massachusetts Institute Of Technology | Adaptive sidelobe blanker |
EP0540249A1 (en) * | 1991-10-24 | 1993-05-05 | National Space Development Agency Of Japan | Processing method for antenna patterns |
GB2285549A (en) * | 1987-06-12 | 1995-07-12 | Thomson Csf | Method for extracting targets from a radar signal and radar capable of implementing this method |
-
1996
- 1996-06-26 GB GB9613343A patent/GB2303266B/en not_active Expired - Lifetime
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4023172A (en) * | 1959-12-17 | 1977-05-10 | Numax Electronics Incorporated | Monopulse system for cancellation of side lobe effects |
GB1017966A (en) * | 1962-04-10 | 1966-01-26 | Csf | Improvements in radar systems |
GB1316562A (en) * | 1971-03-01 | 1973-05-09 | Cossor Ltd A C | Secondary radar systems |
US4298872A (en) * | 1980-05-27 | 1981-11-03 | Hughes Aircraft Company | Sidelobe blanking system |
GB2285549A (en) * | 1987-06-12 | 1995-07-12 | Thomson Csf | Method for extracting targets from a radar signal and radar capable of implementing this method |
US4959653A (en) * | 1989-08-23 | 1990-09-25 | Massachusetts Institute Of Technology | Adaptive sidelobe blanker |
EP0540249A1 (en) * | 1991-10-24 | 1993-05-05 | National Space Development Agency Of Japan | Processing method for antenna patterns |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1067396A2 (en) * | 1999-07-09 | 2001-01-10 | TRW Inc. | Self-guarding monopulse antenna |
EP1067396A3 (en) * | 1999-07-09 | 2001-05-16 | TRW Inc. | Self-guarding monopulse antenna |
WO2005116680A1 (en) * | 2004-05-28 | 2005-12-08 | Telefonaktiebolaget Lm Ericsson (Publ) | A method and arrangement for identifying side-lobe signals |
FR2888332A1 (en) * | 2005-07-08 | 2007-01-12 | Thales Sa | Bistatic radioelectric detection barrier for protecting geographical zone, has reception unit comparing echo level received from waves emitted by directive and non directive emission antennae to identify echo in direction of secondary lobe |
WO2007006678A1 (en) | 2005-07-08 | 2007-01-18 | Thales | Bistatic radioelectric device for producing an intrusion detecting barrier |
WO2014077946A1 (en) * | 2012-11-14 | 2014-05-22 | Raytheon Company | Antenna system having guard array and associated techniques |
US9160072B2 (en) | 2012-11-14 | 2015-10-13 | Raytheon Company | Antenna system having guard array and associated techniques |
Also Published As
Publication number | Publication date |
---|---|
GB2303266B (en) | 2000-01-19 |
GB9613343D0 (en) | 1996-08-28 |
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Legal Events
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PE20 | Patent expired after termination of 20 years |
Expiry date: 20160625 |