EP1325537A1 - Perfectionnement aux sources d'emission / reception d'ondes electromagnetiques pour antenne a multireflecteurs - Google Patents
Perfectionnement aux sources d'emission / reception d'ondes electromagnetiques pour antenne a multireflecteursInfo
- Publication number
- EP1325537A1 EP1325537A1 EP01976390A EP01976390A EP1325537A1 EP 1325537 A1 EP1325537 A1 EP 1325537A1 EP 01976390 A EP01976390 A EP 01976390A EP 01976390 A EP01976390 A EP 01976390A EP 1325537 A1 EP1325537 A1 EP 1325537A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- network
- source according
- radiating elements
- source
- longitudinal radiation
- 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
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q21/00—Antenna arrays or systems
- H01Q21/28—Combinations of substantially independent non-interacting antenna units or systems
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q11/00—Electrically-long antennas having dimensions more than twice the shortest operating wavelength and consisting of conductive active radiating elements
- H01Q11/02—Non-resonant antennas, e.g. travelling-wave antenna
- H01Q11/08—Helical antennas
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q13/00—Waveguide horns or mouths; Slot antennas; Leaky-waveguide antennas; Equivalent structures causing radiation along the transmission path of a guided wave
- H01Q13/20—Non-resonant leaky-waveguide or transmission-line antennas; Equivalent structures causing radiation along the transmission path of a guided wave
- H01Q13/24—Non-resonant leaky-waveguide or transmission-line antennas; Equivalent structures causing radiation along the transmission path of a guided wave constituted by a dielectric or ferromagnetic rod or pipe
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q5/00—Arrangements for simultaneous operation of antennas on two or more different wavebands, e.g. dual-band or multi-band arrangements
- H01Q5/40—Imbricated or interleaved structures; Combined or electromagnetically coupled arrangements, e.g. comprising two or more non-connected fed radiating elements
- H01Q5/45—Imbricated or interleaved structures; Combined or electromagnetically coupled arrangements, e.g. comprising two or more non-connected fed radiating elements using two or more feeds in association with a common reflecting, diffracting or refracting device
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q5/00—Arrangements for simultaneous operation of antennas on two or more different wavebands, e.g. dual-band or multi-band arrangements
- H01Q5/40—Imbricated or interleaved structures; Combined or electromagnetically coupled arrangements, e.g. comprising two or more non-connected fed radiating elements
- H01Q5/45—Imbricated or interleaved structures; Combined or electromagnetically coupled arrangements, e.g. comprising two or more non-connected fed radiating elements using two or more feeds in association with a common reflecting, diffracting or refracting device
- H01Q5/47—Imbricated or interleaved structures; Combined or electromagnetically coupled arrangements, e.g. comprising two or more non-connected fed radiating elements using two or more feeds in association with a common reflecting, diffracting or refracting device with a coaxial arrangement of the feeds
Definitions
- the present invention relates to a source antenna
- E E / reception
- I / O source which can be placed at the focal point of an antenna system and more particularly at the focal point of a Cassegrain type double reflector antenna.
- I / O source A possible application for this I / O source is found in satellite communication systems using C, Ku or Ka bands.
- the propeller network for reception and the longitudinal radiation source for transmission.
- the losses from the printed supply network doubly affect the link budget.
- the merit factor G / T of the antenna is reduced due on the one hand to the reduction in the gain G of the antenna, and on the other hand, to the increase in the noise temperature T of the system linked to dissipative losses from the supply network.
- the solution proposed in patent application 00 07424 makes it possible, by using a network of propellers preferably to a network of patches, to improve the factor
- FIG. 1 which schematically represents a Cassegrain structure comprising a main reflector 1, a source 2 and a secondary reflector 3 facing the source 2, the secondary lobes mainly come from: i) diffraction by the secondary reflector 3.
- the diffracted energy has an absolute level in dB equal to (G-Edge).
- G is the gain of the primary source defined essentially by its directivity.
- Edge is around 20 dB.
- the level of the secondary lobes resulting from this diffraction is of the order of the value of (G-Edge), ii) of the secondary lobes I radiated by the same source 2 and not intercepting the secondary reflector 3. If the primary source 1 has a level of secondary lobes equal in dB to SLL, then the absolute level of the secondary lobes of the antenna system originating from the secondary lobes of the primary source is equal to (G-SLL).
- One solution to reduce the lobes of a Cassegrain system is to reduce G.
- the focal length 2 'of the antenna system is located between the main reflector 1 and the secondary reflector 3.
- the present invention aims to remedy this problem by proposing an E / R source structure having its phase center between the main reflector and the secondary reflector without inducing blocking for the functioning of the antenna system with two reflectors. It thus makes it possible to reduce the secondary lobes of the antenna system.
- the present invention also aims to propose a new E / R source structure which makes it possible to reduce the secondary lobes of emission and reception sources.
- an antenna system with double reflector has a perfectly defined focal point and requires for E / R sources a perfect coincidence of their phase centers.
- the present invention also aims to provide an E / R source structure which makes it possible to perfectly match the phase centers of the transmission and reception sources.
- the subject of the present invention is therefore a source of emission / reception (E / R) of electromagnetic waves for a multi-reflector antenna of the Cassegrain type comprising means with longitudinal radiation operating in a first frequency band and a network of n radiating elements. of the traveling wave type operating in a second frequency band with the n radiating elements arranged symmetrically around the longitudinal radiation means, the network and the longitudinal radiation means having a substantially common phase center, characterized in that the network of n radiating elements is excited by a waveguide of rectangular cross section.
- the network of n radiating elements is a circular network and the guide forms a cavity in the form of a “pineapple slice”.
- ⁇ g ⁇ 0 [ ⁇ r - ( ⁇ O / ⁇ c) 2 ] "% with ⁇ c the cut-off wavelength of the rectangular guide for the fundamental mode TE01, ⁇ O the wavelength in vacuum and ⁇ r the permittivity of the filling dielectric material the guide.
- ⁇ c 2a ( ⁇ r) Vl where a is the width of the rectangular guide.
- the longitudinal radiation antenna which can be constituted either by a “polyrod” excited by a circular or square guide or by a long helix excited by a coaxial line, located in the center of the array has a sort rear cavity which allows:
- FIG. 1 already described is a schematic representation of '' a Cassegrain system according to the prior art
- Figure 2 already described is a schematic representation corresponding to that of Figure 1 and explaining one of the problems that the invention seeks to solve
- Figure 3 is a schematic representation of a Cassegrain system comprising a source according to the present invention
- Figures 4a and 4b respectively represent a sectional view and a top view of a source system according to an embodiment of the present invention
- FIG. 1 already described is a schematic representation of '' a Cassegrain system according to the prior art
- Figure 2 already described is a schematic representation corresponding to that of Figure 1 and explaining one of the problems that the invention seeks to solve
- Figure 3 is a schematic representation of a Cassegrain system comprising a source according to the present invention
- Figures 4a and 4b respectively represent a sectional view and a top view of a source system according to an embodiment of the present invention
- FIG. 5 is a detailed sectional view of a propeller used in the system of FIGS. 4,
- FIG. 6 is a curve giving the results of the coupling of the rectangular guide to the propellers as a function of the frequency
- FIG. 7 is a view identical to that of FIG. 4a representing the system produced for simulation
- FIGS. 8, 9 and 10 are curves giving results of simulations carried out with the source system of FIG. 7,
- FIG. 11 represents another embodiment of a source system according to the present invention.
- FIG. 3 schematically shows a sectional view of the E / R source 10 which is the subject of the invention, placed at the focal point FP of an antenna system with double reflector situated between the two reflectors 1 and 3.
- the source / transmit antenna object of the invention has, compared to more conventional solutions using waveguide technology, the following advantages, namely: space, weight and cost reduced at the same time as '' good electrical insulation between the transmission and reception channels thanks to physical insulation between the two channels.
- i) It makes it possible to further reduce the losses of the source consisting of the propeller network thanks to the very low losses of its supply network using a rectangular guide singlemode, known for these minimum losses, and the length of which is reduced on average to the half-perimeter of the circular network.
- ii) It provides a low-cost solution to the problem of excessively high side lobes of Cassegrain type double reflector antennas:
- Figures 4a and 4b respectively show a sectional view and a top view of the source system object of the invention.
- Figures 4a and 4b respectively show a sectional view and a top view of the source system object of the invention.
- FIG. 4a shows a sectional view and a top view of the source system object of the invention.
- the network of n radiating elements of the traveling wave type consists of eight helices 11. They are placed on the circumference of a circle of diameter D operating in a second frequency band. They are mounted on the upper face 15a of a waveguide 15 in the form of a “pineapple slice”.
- the longitudinal radiation antenna located in the middle of the array is a “polyrod” 12
- the rear cavities 13 and 14 to reduce the radiation of the side lobes for the "polyrod” and for the propeller network are conical.
- the rectangular waveguide 15 in the form of a “pineapple slice” is excited by a coaxial line 16.
- the radiating helices 11 are in turn coupled by probe 17 to the cavity in rectangular guide.
- FIG. 5 shows the detail and the dimensioning of a propeller 11 excited at 12 GHz mounted on a waveguide 15 of polygonal cross section, more particularly rectangular with dimensions a and b.
- FIG. 6a presents simulations showing the result of the coupling of the rectangular guide to the propellers according to the invention as well as the adaptation of the cavity as a guide, at the central frequency of 12 GHz.
- 4 propellers such as 11- 2, 1 1-3, 11-4, 11-5 compared to port A1
- the dimensioning of the rectangular guide 15 is done as follows:
- ⁇ g is the guided wavelength at the operating frequency
- ⁇ ⁇ ⁇ 0 [ ⁇ r - ( ⁇ p / ⁇ ç] 'V2 ⁇ (II);
- ⁇ c is the cut-off wavelength of the rectangular guide for TE10 mode and ⁇ O is the wavelength in vacuum ;
- ⁇ c 2a ( ⁇ r ) 1/2 ;
- a is the width of the rectangular guide
- ⁇ r permittivity of the dielectric material filling the guide -
- the directivity of the primary source varies between + / - 20 ° and +/- 30 ° at -20 dB
- These directivity values are obtained for average diameters D such as: 1, 3 ⁇ 0 ⁇ D ⁇ 1, 9 ⁇ j (III); ⁇ 0 being the wavelength in a vacuum
- equations (I) and (III) make it possible to deduce a relation between ⁇ g and ⁇ 0 . Taking this relation into account in (II), we deduce a.
- the height b of the rectangular guide is chosen to be approximately half its width. So let b -a / 2.
- the magnitudes ⁇ , ⁇ and h are adjusted so as to reduce the level of the secondary lobes of the propeller network.
- the diameter d c is given by the dimensioning of the rectangular guide 15, and more particularly by its width a.
- the depth d is such that the phase center FP of the "polyrod »12 (which is approximately 1/3 the length of the polyrod) coincides with the phase center FH of the propeller network 11 (ie in the middle of the propeller network and approximately 1/3 of the length of l 'propeller).
- the point Fp is at a height of approximately Lp / 3 where Lp is the total length of the polyrod 12 counted from the origin.
- the dimensions of each of the propellers 11 operating in longitudinal mode at the central frequency, as well as those of the central polyrod in according to the desired directivities, are given by conventional formulas known to those skilled in the art.
- the shape of the rear cavity of the central polyrod can be modified.
- the rear cavity can have a cylindrical shape or the like.
- FIG. 7 represents a particular embodiment of the transmission / reception source which is the subject of the invention.
- the transmission part consists of the polyrod 12 and operates in the 14-14.5 GHz band.
- the conical cavity made it possible for this configuration to obtain the best result.
- the adaptation of the polyrod in the targeted band (14-14.5 GHz) as well as the radiation patterns obtained in the presence of the conical cavity are given in Figure 8.
- the source consists of a propeller 12 mounted in a conical cavity 13 and coupled by a probe 17 to the supply Tx.
- the polarizations of the sources on emission and on reception are circular and can be of the same direction or of opposite direction.
- the propeller 12 ′ can be positioned in a cylindrical cavity like the polyrod.
Abstract
Description
Claims
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0013213 | 2000-10-12 | ||
FR0013213 | 2000-10-12 | ||
PCT/FR2001/003132 WO2002031920A1 (fr) | 2000-10-12 | 2001-10-11 | Perfectionnement aux sources d'emission / reception d'ondes electromagnetiques pour antenne a multireflecteurs |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1325537A1 true EP1325537A1 (fr) | 2003-07-09 |
EP1325537B1 EP1325537B1 (fr) | 2004-06-02 |
Family
ID=8855380
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP01976390A Expired - Lifetime EP1325537B1 (fr) | 2000-10-12 | 2001-10-11 | Perfectionnement aux sources d'emission / reception d'ondes electromagnetiques pour antenne a multireflecteurs |
Country Status (10)
Country | Link |
---|---|
US (1) | US6861998B2 (fr) |
EP (1) | EP1325537B1 (fr) |
JP (1) | JP4090875B2 (fr) |
KR (1) | KR20030040513A (fr) |
CN (1) | CN1254883C (fr) |
AU (1) | AU2001295677A1 (fr) |
DE (1) | DE60103653T2 (fr) |
ES (1) | ES2222394T3 (fr) |
MX (1) | MXPA03002670A (fr) |
WO (1) | WO2002031920A1 (fr) |
Families Citing this family (141)
Publication number | Priority date | Publication date | Assignee | Title |
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DE102005002505A1 (de) * | 2005-01-19 | 2006-07-27 | Robert Bosch Gmbh | Vorrichtung zum Aussenden und Empfangen elektromagnetischer Strahlung |
US7388559B1 (en) * | 2006-12-21 | 2008-06-17 | The Boeing Company | Reflector antenna |
KR100961221B1 (ko) * | 2007-12-05 | 2010-06-03 | 위월드 주식회사 | 듀얼 편파 헬릭스 급전기를 이용한 송수신 겸용 ade안테나 시스템 |
US9281561B2 (en) * | 2009-09-21 | 2016-03-08 | Kvh Industries, Inc. | Multi-band antenna system for satellite communications |
US9966648B2 (en) | 2012-08-27 | 2018-05-08 | Kvh Industries, Inc. | High efficiency agile polarization diversity compact miniaturized multi-frequency band antenna system with integrated distributed transceivers |
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US20150270615A1 (en) * | 2013-10-10 | 2015-09-24 | Michael Andrew Neenan | High Frequency GPS GNN GLONASS Antenna |
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US5041840A (en) * | 1987-04-13 | 1991-08-20 | Frank Cipolla | Multiple frequency antenna feed |
GB9900411D0 (en) * | 1999-01-08 | 1999-02-24 | Cambridge Ind Ltd | Multi-frequency antenna feed |
US6320553B1 (en) * | 1999-12-14 | 2001-11-20 | Harris Corporation | Multiple frequency reflector antenna with multiple feeds |
-
2001
- 2001-10-11 JP JP2002535203A patent/JP4090875B2/ja not_active Expired - Lifetime
- 2001-10-11 WO PCT/FR2001/003132 patent/WO2002031920A1/fr active IP Right Grant
- 2001-10-11 DE DE60103653T patent/DE60103653T2/de not_active Expired - Lifetime
- 2001-10-11 CN CNB018172288A patent/CN1254883C/zh not_active Expired - Fee Related
- 2001-10-11 EP EP01976390A patent/EP1325537B1/fr not_active Expired - Lifetime
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- 2001-10-11 MX MXPA03002670A patent/MXPA03002670A/es active IP Right Grant
- 2001-10-11 AU AU2001295677A patent/AU2001295677A1/en not_active Abandoned
- 2001-10-11 US US10/398,834 patent/US6861998B2/en not_active Expired - Fee Related
- 2001-10-11 KR KR10-2003-7004642A patent/KR20030040513A/ko not_active Application Discontinuation
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DE60103653D1 (de) | 2004-07-08 |
WO2002031920A1 (fr) | 2002-04-18 |
JP4090875B2 (ja) | 2008-05-28 |
JP2004511940A (ja) | 2004-04-15 |
ES2222394T3 (es) | 2005-02-01 |
KR20030040513A (ko) | 2003-05-22 |
US20040021612A1 (en) | 2004-02-05 |
US6861998B2 (en) | 2005-03-01 |
MXPA03002670A (es) | 2003-06-24 |
CN1470089A (zh) | 2004-01-21 |
EP1325537B1 (fr) | 2004-06-02 |
DE60103653T2 (de) | 2005-06-09 |
CN1254883C (zh) | 2006-05-03 |
AU2001295677A1 (en) | 2002-04-22 |
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