EP0004215B1 - Mehrmode Mikrowellenstrahler und Monopulsantenne mit einem solchen Strahler - Google Patents
Mehrmode Mikrowellenstrahler und Monopulsantenne mit einem solchen Strahler Download PDFInfo
- Publication number
- EP0004215B1 EP0004215B1 EP79400100A EP79400100A EP0004215B1 EP 0004215 B1 EP0004215 B1 EP 0004215B1 EP 79400100 A EP79400100 A EP 79400100A EP 79400100 A EP79400100 A EP 79400100A EP 0004215 B1 EP0004215 B1 EP 0004215B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- horn
- plane
- source
- mode
- opening
- 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
Links
- 230000005684 electric field Effects 0.000 claims description 2
- 238000003475 lamination Methods 0.000 claims 4
- 230000001902 propagating effect Effects 0.000 claims 3
- 238000005286 illumination Methods 0.000 description 17
- 230000005284 excitation Effects 0.000 description 5
- 230000014509 gene expression Effects 0.000 description 4
- 239000002184 metal Substances 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 230000005855 radiation Effects 0.000 description 2
- 238000010276 construction Methods 0.000 description 1
- 230000001627 detrimental effect Effects 0.000 description 1
- 230000037213 diet Effects 0.000 description 1
- 235000005911 diet Nutrition 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 229940082150 encore Drugs 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 230000003287 optical effect Effects 0.000 description 1
- 238000005192 partition Methods 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
Images
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q25/00—Antennas or antenna systems providing at least two radiating patterns
- H01Q25/04—Multimode antennas
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q19/00—Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic
- H01Q19/06—Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using refracting or diffracting devices, e.g. lens
- H01Q19/08—Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using refracting or diffracting devices, e.g. lens for modifying the radiation pattern of a radiating horn in which it is located
Definitions
- the present invention relates to a multimode microwave source for single-pulse antennas in which several radiation patterns are implemented simultaneously; the shapes of these diagrams are directly involved in the overall performance of the radar system using such antennas.
- the source of this Figure 1 is made up of two plane moders E ME1 and ME2 placed side by side and separated by a common vertical partition. Each of these moders is excited by two pairs of guides 1, 10 and 2, 20 which receive the fundamental mode, and which each lead into a guide 3, 30 of length L1 between the planes PO and P1.
- the plane PO is what is called a discontinuity plane at the level of which higher, propagative or evanescent modes are formed, the length L1 and the dimensions of the guides 3, 30 being such that only the desired modes, in this case by example, the odd modes H11 and E11 and the even modes H12 and E12, propagate until the opening of the moder E thus constituted, that is to say the plane P1, the fundamental mode of excitation being the mode H10.
- the set between the planes P1 and P3 constitutes superimposed plane H planes, the plane P2 being the plane of discontinuity where the higher modes are formed.
- the opening of the source, which is in the plane P3, radiates according to a global law of illumination produces partial laws of illumination obtained in the vertical plane and in the horizontal plane.
- Such a source has drawbacks in the use which must be made of it as the primary source of a multimode antenna for which an increase in performance is requested, mainly in bandwidth. Indeed, it has a weight and longitudinal dimensions in particular, too large. Excessive longitudinal dimensions may, when the location of its installation is already planned, require a displacement of the antenna reflector in a direction such that the inertia of the assembly tends to increase, which has a detrimental effect on the servo mechanisms in particular.
- An object of the present invention is to produce a multimode source of reduced length and of lightened structure, which removes these constraints and makes it possible to produce a monopulse antenna with the desired performance.
- This reduction in size, combined with a reduced weight, is particularly advantageous for the construction of Cassegrain type antennas mounted on turrets where increased inertia problems arise due to the limitation of the space available between the reflector and the site axis.
- a multimode microwave source for a monopulse antenna according to the invention is characterized by the means set out in the characterizing part of claim 1.
- a multimode source according to the invention mainly comprises a waveguide 12 forming a cavity extending by a horn 13 whose mouth 16 constitutes the opening radiating from the source.
- a certain number of feeding guides four in this case 9, 90, 10, 100 excite the fundamental mode H10.
- the total length of this source is equal to L and the dimensions of its rectangular opening are a for its large dimension and b for its small dimension, here vertical.
- the guides 9 and -10 are adjacent to each other by a common vertical wall 11. They are arranged in an upper horizontal plane, while the guides 90 and 100 adjacent by a vertical wall 110, are arranged in a plane lower horizontal.
- the guides constitute the feed for a plane moder H.
- These guides can be grouped two by two vertically constituting excitation guides 9, 90 and 10, 100 of two plane moders E.
- the feed guides open into the cavity 12, in a plane ⁇ 1, which is a discontinuity plane at the level of which higher modes of the excitation mode transmitted by the guides are formed, excitation mode which is generally the fundamental mode .
- the length L of the source according to the invention is chosen so that the phasing of the modes H10 and EH12 takes place on the opening 16 for the central frequency.
- the EH12 mode conveniently represents the E12 and H12 modes created in the plane of discontinuity ⁇ 1, from the fundamental H10 excitation mode. These modes E12 and H12 have the same cut-off frequency and the same phase speed and their superposition can be considered as a single mode.
- the field on the opening 16 in the sum track is of the form: and on the way to difference:
- T ' i and T' 3 represent respectively the amplitudes relative to the modes H10 and EH12, y is a coordinate value along the dimension b.
- FIG. 4 shows the structure of the moderator according to the invention in the plane E
- FIG. 5 the law of illumination obtained in the opening 16 in the plane E.
- the resulting amplitude of field 19 is the sum of the amplitude of the EH12 mode, curve 17, representing the function cos 2 ⁇ (y / b) and the amplitude of the fundamental mode H10, curve 18.
- FIG. 6 represents the moderator which constitutes the source in the plane H perpendicular to the plane E with represented in particular all the supply guides 9 and 10, adjacent to each other by the wall 11, located in a horizontal plane which has been called superior.
- T1 and T3 respectively represent the amplitudes relating to the fundamental mode H10 and to the mode-H30 generated in the mouth of the horn 13 by the bars 14 and 15, and x is the coordinate along the dimension a.
- the H30 mode is already generated in the discontinuity plane ⁇ 2 at the junction of the straight guide 12 and the horn 13, but it is then evanescent. It becomes propagative in the cornet, beyond a plane marked by ⁇ 3, but with a very low level.
- the mode ratio a is modified and therefore the law of illumination in the opening.
- the bars In making the moderator, the bars must have a relatively small diameter, less than one tenth of the wavelength. As for the location of the bars, we can admit that we have:
- the bars can be replaced by metal strips without modifying the results. If their width is close to ⁇ / 4, their presence does not mismatch the horn. In any case, in order to avoid a mismatching of the horn due to the presence of the bars, provision is made in this case for a second pair of bars 140-150 identical to the first but located ⁇ / 4 behind in the mouth of the horn.
- FIG. 7 shows the illumination on the opening in the absence of the bars or lamellae while FIG. 8 shows this illumination when the bars or lamellae are present.
- Curve 20 gives the resulting amplitude of the field in the opening of the moderator in the plane H.
- plane H which represents a footprint in length less than that of the source represented in FIG. 1 constituted by a plane moder E, a transition and a plane moder H.
- the footprint in length is found thus reduced by approximately 2.5 to 3 times.
- the bandwidth is greater than that obtained with a conventional multimode source.
- the bandwidth obtained is around 15% against 7% roughly. This is due to the fact that the upper mode is generated in the very opening of the moder, the phasing being constant whatever the frequency.
- the flared shape of the horn in plane H gives a quadratic phase to the law of illumination resulting in a primary diagram having a constant opening in the band of frequencies to be covered.
Landscapes
- Variable-Direction Aerials And Aerial Arrays (AREA)
- Waveguide Aerials (AREA)
- Aerials With Secondary Devices (AREA)
Claims (3)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7805337 | 1978-02-24 | ||
FR7805337A FR2418551A1 (fr) | 1978-02-24 | 1978-02-24 | Source hyperfrequence multimode et antenne comportant une telle source |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0004215A1 EP0004215A1 (de) | 1979-09-19 |
EP0004215B1 true EP0004215B1 (de) | 1986-05-28 |
Family
ID=9205012
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP79400100A Expired EP0004215B1 (de) | 1978-02-24 | 1979-02-16 | Mehrmode Mikrowellenstrahler und Monopulsantenne mit einem solchen Strahler |
Country Status (4)
Country | Link |
---|---|
US (1) | US4241353A (de) |
EP (1) | EP0004215B1 (de) |
DE (1) | DE2967598D1 (de) |
FR (1) | FR2418551A1 (de) |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2477785A1 (fr) * | 1980-03-07 | 1981-09-11 | Thomson Csf | Source hyperfrequence multimode et antenne comportant une telle source |
FR2498820A1 (fr) * | 1981-01-23 | 1982-07-30 | Thomson Csf | Source hyperfrequence bi-bande et antenne comportant une telle source |
DE3381303D1 (de) * | 1983-06-18 | 1990-04-12 | Ant Nachrichtentech | Viertornetzwerk fuer mikrowellenantennen mit monopulsnachfuehrung. |
WO1986003344A1 (en) * | 1984-11-19 | 1986-06-05 | Hughes Aircraft Company | High gain-area-product antenna design |
GB2171561B (en) * | 1985-02-24 | 1989-01-11 | Philips Electronic Associated | Antenna |
US4764775A (en) * | 1985-04-01 | 1988-08-16 | Hercules Defense Electronics Systems, Inc. | Multi-mode feed horn |
US4712110A (en) * | 1985-12-26 | 1987-12-08 | General Dynamics, Pomona Division | Five-port monopulse antenna feed structure with one dedicated transmit port |
US6452561B1 (en) * | 2001-03-28 | 2002-09-17 | Rockwell Collins, Inc. | High-isolation broadband polarization diverse circular waveguide feed |
EP1993166B1 (de) * | 2007-05-14 | 2020-10-07 | Saab AB | Antennenvorrichtung |
WO2020180220A1 (en) | 2019-03-04 | 2020-09-10 | Saab Ab | Dual-band multimode antenna feed |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CH257862A (de) * | 1942-06-23 | 1948-10-31 | Lorenz C Ag | Mit Trichter versehener Hohlraumresonator. |
US2825062A (en) * | 1945-07-09 | 1958-02-25 | Chu Lan Jen | Antenna |
US3573838A (en) * | 1968-10-28 | 1971-04-06 | Hughes Aircraft Co | Broadband multimode horn antenna |
US3701163A (en) * | 1971-11-09 | 1972-10-24 | Us Navy | Multi-mode, monopulse feed system |
DE2626926C2 (de) * | 1976-06-16 | 1983-08-25 | AEG-Telefunken Nachrichtentechnik GmbH, 7150 Backnang | Hohlleiterprimärstrahler mit rechteckigem Querschnitt für eine Reflektorantenne mit Strahlschwenkung |
-
1978
- 1978-02-24 FR FR7805337A patent/FR2418551A1/fr active Granted
-
1979
- 1979-02-16 DE DE7979400100T patent/DE2967598D1/de not_active Expired
- 1979-02-16 EP EP79400100A patent/EP0004215B1/de not_active Expired
- 1979-02-21 US US06/013,272 patent/US4241353A/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
DE2967598D1 (en) | 1986-07-03 |
FR2418551B1 (de) | 1981-12-31 |
EP0004215A1 (de) | 1979-09-19 |
FR2418551A1 (fr) | 1979-09-21 |
US4241353A (en) | 1980-12-23 |
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