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US3803617A - High efficiency multifrequency feed - Google Patents

High efficiency multifrequency feed
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Publication number
US3803617A
US3803617AUS00244158AUS24415872AUS3803617AUS 3803617 AUS3803617 AUS 3803617AUS 00244158 AUS00244158 AUS 00244158AUS 24415872 AUS24415872 AUS 24415872AUS 3803617 AUS3803617 AUS 3803617A
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United States
Prior art keywords
horn
frequency band
high efficiency
feed system
arms
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Expired - Lifetime
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US00244158A
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J Fletcher
J Ajioka
G Tsuda
W Leeper
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National Aeronautics and Space Administration NASA
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National Aeronautics and Space Administration NASA
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Priority to US00244158ApriorityCriticalpatent/US3803617A/en
Priority to CA167,786Aprioritypatent/CA977047A/en
Priority to DE2316842Aprioritypatent/DE2316842C3/en
Priority to BR732624Aprioritypatent/BR7302624D0/en
Priority to GB1738573Aprioritypatent/GB1355030A/en
Priority to JP48041489Aprioritypatent/JPS5224369B2/ja
Priority to FR7313570Aprioritypatent/FR2180114B1/fr
Priority to IT49428/73Aprioritypatent/IT988143B/en
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Publication of US3803617ApublicationCriticalpatent/US3803617A/en
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Abstract

The apparatus of the present invention relates to antenna systems and particularly to compact and simple antenna feeds which can transmit and receive simultaneously in at least three frequency bands, each with high efficiency and polarization diversity. The feed system is especially applicable for frequency bands having nominal frequency bands with the ratio 1:4:6. By way of example, satellite communications telemetry bands operate in frequency bands 0.8 - 1.0 GHz, 3.7 - 4.2 GHz and 5.9 - 6.4 GHz. In addition, the antenna system of the invention has monopulse capability for reception with circular or diverse polarization at frequency band 1.

Description

United States Patent [191 Fletcher et al.
[111 3,803,617 [451 Apr. 9, 1974 HIGH- EFFICIENCY MULTIFREQUENCY FEED [22] Filed: Apr. 14, 1972 [21] Appl. No.: 244,158
51 1m. c1. ..H01q1/00 58 Field ofSearch 343/729, 730,786, 797, 343/853, 854
[56] References Cited UNITED STATES PATENTS Raburn 343/730 Primary Examiner-Eli Lieberman Attorney, Agent, or Firm-Leonard Rawicz; Neil B. Siegel; Robert F. Kempf 5 7] ABSTRACT The apparatus of the present invention relates to antenna systems and particularly to compact and simple antenna feeds which can transmit and receive simultaneously in at least three frequency bands, each with high efficiency and polarization diversity. The feed system is especially applicable for frequency bands having nominal frequency bands with the ratio 1:416. By way of example, satellite communications telemetry bands operate in frequency bands 0.8 1.0 GHZ, 3.7 4.2 GHz and 5.9 6.4 GHz. In addition, the antenna system of the invention has monopulse capability for reception with circular or diverse polarization at frequency band 1.
14 Claims, 12 Drawing Figures SHEET 1 BF 7 PATENTED APR 9 974 PATENTEDAPR 91974 SHEET 3 BF 7 P liv l I! "A 8 I :8 as? Fig.3.
PATENTEDAPR slam 3303517 SHEET 6 BF 7 P Fig.6. I f m r J 50 v sl v 52 Two Poinf Fed Dipole Model Showing Currenr Disirlbuiion 369 @FEZIFigT.
Higher Frequency Horn Feed Serves As Central Portion Of Two Point Fed Dipole MI Fig.8.
A PF
Two Poinis Of Dipole Fed With |80 4- Port Hybrid 57 (eg.Magic Tee Or Rarrace) Diagram Showing High Freq. Horn As Part Of Law Freq. Dipoie HIGH EFFICIENCY MULTIFREQUENCY FEED BACKGROUND OF THE INVENTION Conventional techniques comprise the use of nested horns or nested dipole clusters. In the case of nested horns, a high frequency horn is nested inside an intermediate frequency horn which, in turn is nested inside SUMMARY OF THE INVENTION The present invention circumvents the problems of mutual blockage and mutual coupling by using a single common aperture for the 6 and 4 GHz frequency bands and a crossed dipole for the 1 GHz frequency band. The crossed dipole is not a conventional dipole in that each dipole is excited at two points with edges of a 6/4 GHz horn. as the central portion of the dipole. To achieve a high efficiency, the primary pattern of the feed must illuminate the reflector or lens without an undue amount of spillover or without being too directive so as to under illuminate the reflector or lens. The net result is that the feed pattern for all three frequency bands must be nearly identical in all planes and have a common center of phase. This is achieved in the 6/4 GHz common horn by multimoding at 6 CH2 so that its effective aperture is less (about three-fourths linear dimension) than the physicalaperture of the 6/4 GI-I2 horn while at the 4 GHz frequency it is not multimoded so that it has its full physical aperture. This results in the 6 GHz and 4 GHz frequency bands having similar feed patterns for proper reflector or lens illumination. A crossed set of two 2-point feed strip dipoles are used for the 1 GHz frequency band.
One or more quarter wavechokes surrounding the 6/4 GHz horn aperture prevent coupling to the 1 GHz frequency wave dipole. Also, a choke is built into the dipole wings to further prevent coupling with 4 GHz frequencies. The 6 GHz frequencies are sufficiently far removed from the 1 GHz frequency band so that the coupling to the l GHz dipole is sufficiently suppressed by the choke around the horn alone. Separation between the 6 GHz and 4 GHz frequencies is achieved with conventional diplexers. Lastly, the two feed points of the dual feedpoint dipole are connected with a hybrid (e.g., a magic tee). When the difference port is used, the currents in the dipole wings are in phase resulting in a good sum" pattern. When the sum port of the hybrid is used, the currents in the dipole wings are in anti-phase creating a null pattern. Hence, for certain polarizations, the sum port of the hybrid can be used for monopulse tracking applications. This type of tracking is especially applicable in circularly polarized systems.
BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 shows a plan view of a C band UHF aperture of a high efficiency multifrequency feed in accordance with the present invention;
FIG. 2 shows a cross-sectional view of the C Band UHF aperture of FIG. 1;
FIGS. 3-5 illustrate the feed patterns'for the H, E and diagonal planes for each of the frequency bands of the apparatus of FIGS. 1 and 2;
FIG. 6 illustrates a schematic of a two point pole model showing current distribution;
FIG. 7 illustrates a schematic showing the manner in which a higher frequency horn feed serves as a central portion of the two point fed dipole in the illustration of FIG. 6;
FIG. 8 illustrates the manner in which the two point fed dipole of FIG. 7 is fed by the use of a 4-Pont Hybrid; and
FIGS. 9-l2 show alternative configurations of the plan view of the aperture of the multifrequency feed of FIGS. 1 and 2.
fed di- DESCRIPTION Referring to FIGS. 1 and 2 of the drawings, there is shown a plan view of the aperture and across-section 22 thereof, respectively, of the high efficiency multifrequency feed antenna system of the present invention. In particular, asquare horn 10 having dimensions suitable to provide a 6 GHz and 4 GHz common aperture extends through the central portion of aconductive ground plane 12. On the back side ofground plane 12 relative to the antenna aperture, thesquare horn 10 extends into amultimode step section 14 dimensioned for 6 GHz whichsection 14 terminates in aflange 15. Themultimode step section 14 is symmetrically disposed about the center line through horn l0. Surrounding the outer periphery ofhorn 10 at the lip thereof is disposed achoke section 16 primarily designed to inhibit the flow of 4 GHz energy thereacross.
Relative to the 1 GHz frequency band, adielectric disc 18 extends radialy outwards from the outer lip ofchoke section 16 for a sufficient distance to support UHF chokeddipole arms 20, 21, 22 and 23 which extend outwards from the center of the four sides ofhorn 10. The outer periphery ofdielectric disc 18 is supported bymetallic posts 24 which extend to theground plane 12. A UHF cavity is formed bymetal bands 26, 28 disposed about the central portion andadjacent ground plane 12, respectively, of themetallic posts 24. The extremity of the center leg of the UHF choked dipole arms 20-23nearest horn 10 are fed by the respective center conductors of coaxial lines 30-33, respectively. The coaxial lines 3033 extend through theground plane 12 parallel to the center line ofhorn 10 and are terminated by connectors 34-37, respectively. The outer conductors of coaxial lines 30-33 are electrically connected to the outer periphery ofchoke section 16 and to theground plane 12. Lastly, ametal cylinder 40 terminating in aflange 42 is disposed symmetrically aboutmetallic posts 24.Metal cylinder 40 is attached toground plane 12 and has a height slightly greater than the dimension ofsquare horn 10 which extends through theground plane 12. Theflange 42 provides a support for a radome if desired.
In the operation of the multifrequency prime focus feed of the present invention, the 4 GHz and 6 GHz frequency band signals are fed through themultimode step section 14 to thehorn 10. Contemporary multimoding techniques are employed to obtain the mu ltimoding at the 6 G Hz frequency band and single moding at the 4 GHz frequency band. In particular, the mode exciters coupled toflange 15 are designed for both the 4 GHz and 6 GHz frequency bands and the common aperture of horn is dimensioned to be below cutoff for the higher modes at 4 GI-lz. The separation of the 4 GHz and 6 GHz frequency bands is achieved with conventional diplexers, not shown.Quarter wave choke 16 surrounding the 6/4 GI-Iz horn 10 aperture prevents coupling from the 4 GHz and 6 GHz frequency bands to the 1 GHz frequency dipoles 20-23. Also, there is a choke built into each ofthe dipoles 20-23 to further prevent coupling with the 4 GI-Iz frequencies. The 6 GHz frequencies are sufficiently far removed that coupling to the 4 GHz dipoles 20-23 is suf ficiently suppressed by thechoke 16 around thehorn 10 alone. 7
Referring to FIGS. 6-8, there is illiistrated the manner in whichopposite dipoles 20, 22 and 21, 23 operate. In particular, FIG. 6 illustrates a two point feddipole having segments 50, 51, and52 driven byvoltage sources 53, 54 which supply a signal voltage, V. When voltage sources 53, 54 drive thedipole segments 50, 51, 52 in phase, the current, I, increases from the left extremity, as shown in the drawing, to a, maximum alongcenter segment 51 and then decreases to zero at the right extremity ofsegment 52. This current distribution is similar to that of a typical dipole, with the exception that it is fed at two points instead of one.
Proceeding to FIG. 7, thecenter segment 51 of FIG. 6 is replaced with thehorn 10. In this case, the current that previously flowed through thecenter segment 51 divides and flows around opposite sides of thehorn 10.
Lastly, FIG. 8 shows thedipoles 50, 52 replaced with the chokeddipoles 23, 21, respectively, and thevoltage sources 53, 54 provided bycoaxial lines 33, 31, as in FIG. 1. Thecoaxial lines 31, 33 are, in turn, fed with a 180 four-port hybrid 56. When fed through a sum input (2) 57 thereof, the voltages at the outputs ofcoaxial lines 31, 33 are in anti-phase, creating a null pattern. Alternatively, when fed through the difference input (A) 58, the voltages at the outputs ofcoaxial lines 31, 33 are in phase, resulting in a good sum pattern. Hence, for a particular polarization, the sum and null patterns can be used for monopulse tracking applications. Lastly, in a normal mode of operation, the remainingdipoles 20, 22 are fed in phase with a hybrid (not shown) which, in turn, may be fed 90 out of phase relative to the signal applied tohybrid 56, thereby to generate a circularly polarized output signal.
In the multifrequency antenna feed system it is desirable that the feed pattern for each of the three frequency bands be nearly identical in all planes and have a common'center of phase. In the 6/4 common born 10 this is achieved by multimoding at 6 GI-Iz so that its effective aperture is less by about three-fourths linear dimension than the physical aperture of the 6/4 GI-Iz horn 10, while at the 4 GHz frequency it is not multimoded so that it has its full physical aperture. This results in the 6 Gl-Iz and 4 GHz frequency bands having similar feed patterns for proper reflectoror lens illumination. The horn-dipole assembly is contained in a l GI-Iz cavity formed byground plane 18, and themetal bands 26, '28 whose parameters are adjusted to shape the 1 GHz patterns without afiecting the 6 and 4 GHz patterns.
Referring to FIGS. 3-5, there is illustrated measured horizontal, vertical, and diagonal patterns for the 4 GI-Iz, 6 GHz, and 1 GHz frequency bands developed by the antenna system of FIGS. 1 and 2, respectively. In particular, FIG. 3 illustrates ahorizontal pattern 60, avertical pattern 61, and adiagonal pattern 62 for the 4 GHz frequency band; FIG. 4 illustrates ahorizontal pattern 63, avertical pattern 64, and adiagonal pattern 68 for the 1 GHz frequency band. As can be seen from these figures, the feed patterns of the antenna system of FIGS. 1 and 2 is nearly identical in all planes for each of the three frequency bands, as is required for antenna feeds of this type. Although the described embodiment of the invention was designed for the 3.7 4.2 GHZ band, the 5.9 6.4 GHz band and the 0.8 1 GHzband, the principles embodied therein are applicable to other frequency bands.
Referring to FIGS. 9-12, there are illustrated other possible configurations of the multifrequency feed. More particularly, FIG. 9 shows an aperture view withdouble choke slots 70, 71' surrounding the periphery ofhorn 10.Choke slot 70, for example, could be designed to impede the 4 GHz frequency band and chokeslot 71 designed to impede the 6 CH2 frequency band. Referring to FIGS. 10, 11, acircular horn 72 and acrossedhorn 73 are shown, respectively, in place of thesquare horn 10. In the case of the crossed-hom 73, the choked dipole arms 20-23 emanate from the inside corners thereof. Lastly, FIG. 12 illustrates ahorn 74 having indentations adapted to accommodate coaxial lines 30-33. Achoke slot 75 about the periphery of thehorn 74 follows the aforementioned indentations.
What is claimedis:
1. A high efficiency antenna feed system capable of transmitting and receiving simultaneously in first, sec- 0nd, and third increasingly higher frequency bands, said antenna feed system comprising means including a horn for providing a common radiating aperture for signals within said second and third frequency bands;
means coupled to said horn for multimoding at said third frequency band therein;
means surrounding said horn for providing a cavity for said first frequency band;
first and second arms resonant in conjunction with said horn at said first frequency band and extending outwards from opposite sides of the periphery thereof; and
means coupled to the respective extremities of said arms nearest said horn for energizing said arms.
2. The high efficiency antenna feed system as defined in claim 1 additionally including means disposed about the periphery of said horn for isolating said first frequency band from said second and third frequency bands.
3. The high efficiency antenna feed system as defined inclaim 2 wherein said rneans disposed about the periphery of said born for isolating said first frequency band from said second and third frequency bands constitutes a slot formed of conductive material, said slot being one quarter wavelength deep at said second frequency band, thereby to provide a choke.
4. The high efficiency antenna feed system as defined inclaim 2 wherein said means disposed about the periphery of said horn for isolating said first frequency band from said second and third frequency bands constitutes first and second parallel slots formed of conductive material, said first slot being one quarter wavelength deep at said second frequency band and said second slot being one quarter wavelength deep at said third frequency band, thereby to provide first and second chokes at said second and third frequency bands, respectively.
5. The high efficiency antenna feed system as defined in claim 1 wherein said first and second arms extending outwards from opposite sides of the periphery of said horn are choked thereby to isolate said first frequency band from said second frequency band.
6. The high efficiency antenna feed system as defined in claim 1 additionally including third and fourth arms resonant in conjunction with said horn at said first frequency band and extending outwards from opposite sides of the periphery thereof midway between said first and second arms.
7. The high efficiency antenna feed system as defined inclaim 6 wherein said first, second, third, and fourth arms extending outwards from the periphery of said horn are choked thereby to isolate said first frequency band from said second frequency band.
8. The high efficiency antenna feed system as defined in claim 7 wherein said means surrounding said horn for providing a cavity for said first frequency band includes means for providing a ground plane outwards from the exterior of the rear portion of said horn normal to the axis of rotation thereof, a plurality of metallic posts disposed intermediate said ground plane and the plane of said first, second, third, and fourth arms at periodic intervals along the circumference of a circle of predetermined radius and having a center coinciding with the axis of rotation of said horn, and first and second parallel metallic bands disposed about said plurality of metallic posts.
9. The high efficiency antenna feed system as defined in claim 1 wherein said first and second arms extending outwards from opposite sides of the periphery of said horn are connected to first and second arms, respectively, of a four-part hybrid junction, having said first and second arms, a sum arm, and a difference arm.
10. The high efficiency antenna feed system as defined in claim 1 wherein the cross-sectional configuration of said horn is square.
11. The high efficiency antenna feed system as defined in claim 1 wherein the cross-sectional configuration of said horn is circular.
12. The high efficiency antenna feed system as defined in claim 1 wherein the cross-sectional configuration of said horn constitutes the outer configuration of first and second crossed identical rectangles.
13. The high efficiency antenna feed system as defined in claim 1 wherein the cross-sectional configuration of said horn is square with indentations in the center portions of each side thereof.
14. A high efficiency antenna feed system capable of transmitting and receiving simultaneously in first, second, and third increasingly higher frequency bands, said antenna feed system comprising a ground plane;
a horn disposed through said ground plane for providing a common radiating aperture for signals within said second and third frequency bands;
a step section connected to the input of said horn for multimoding at said third frequency band therein;
first, second, third, and fourth arms resonant in conjunction with said horn at said first frequency band extending outwards from quadrature points of the periphery thereof;
a plurality of metallic posts extending between said ground plane and the plane of said first, second, third, and fourth arms along the circumference of a circle disposed about said horn;
first and second parallel metallic bands disposed about said plurality of metallic posts thereby to provide a cavity resonant at said first frequency band; and
means coupled to the respective extremities of said first, second, third, and fourth arms nearest said horn for energizing said arms.

Claims (14)

14. A high efficiency antenna feed system capable of transmitting and receiving simultaneously in first, second, and third increasingly higher frequency bands, said antenna feed system comprising a ground plane; a horn disposed through said ground plane for providing a common radiating aperture for signals within said second and third frequency bands; a step section connected to the input of said horn for multimoding at said third frequency band therein; first, second, third, and fourth arms resonant in conjunction with said horn at said first frequency band extending outwards from quadrature points of the periphery thereof; a plurality of metallic posts extending between said ground plane and the plane of said first, second, third, and fourth arms along the circumference of a circle disposed about said horn; first and second parallel metallic bands disposed about said plurality of metallic posts thereby to provide a cavity resonant at said first frequency band; and means coupled to the respective extremities of said first, second, third, and fourth arms nearest said horn for energizing said arms.
US00244158A1972-04-141972-04-14High efficiency multifrequency feedExpired - LifetimeUS3803617A (en)

Priority Applications (8)

Application NumberPriority DateFiling DateTitle
US00244158AUS3803617A (en)1972-04-141972-04-14High efficiency multifrequency feed
CA167,786ACA977047A (en)1972-04-141973-04-03High efficiency multifrequency feed
DE2316842ADE2316842C3 (en)1972-04-141973-04-04 Multi-frequency antenna for three frequency bands
GB1738573AGB1355030A (en)1972-04-141973-04-11Antenna feed system
BR732624ABR7302624D0 (en)1972-04-141973-04-11 HIGH EFFICIENCY MULTIPLE FREQUENCY POWER SUPPLY
JP48041489AJPS5224369B2 (en)1972-04-141973-04-13
FR7313570AFR2180114B1 (en)1972-04-141973-04-13
IT49428/73AIT988143B (en)1972-04-141973-04-13 MULTIFREQUENCY POWER SUPPLY D HIGH PERFORMANCE ANTENNA

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US00244158AUS3803617A (en)1972-04-141972-04-14High efficiency multifrequency feed

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US3803617Atrue US3803617A (en)1974-04-09

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US00244158AExpired - LifetimeUS3803617A (en)1972-04-141972-04-14High efficiency multifrequency feed

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JP (1)JPS5224369B2 (en)
BR (1)BR7302624D0 (en)
CA (1)CA977047A (en)
DE (1)DE2316842C3 (en)
FR (1)FR2180114B1 (en)
GB (1)GB1355030A (en)
IT (1)IT988143B (en)

Cited By (17)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
US4028708A (en)*1975-10-101977-06-07The United States Of America As Represented By The Secretary Of The NavyAntenna feed for dual beam conical scan tracking radar
US4109254A (en)*1975-06-171978-08-22The Marconi Company Ltd.Dipole radiators for feeding a parabolic reflector
US4207573A (en)*1977-05-181980-06-10Thomson-CsfDual-frequency antenna system with common reflector illuminated by different feeds
US4675685A (en)*1984-04-171987-06-23Harris CorporationLow VSWR, flush-mounted, adaptive array antenna
US4740795A (en)*1986-05-281988-04-26Seavey Engineering Associates, Inc.Dual frequency antenna feeding with coincident phase centers
US4843399A (en)*1986-07-301989-06-27Narco Avionics, Inc.Portable navigational communications transceiver
US4862187A (en)*1988-10-241989-08-29Microwave Components And Systems, Inc.Dual band feedhorn with two different dipole sets
US5003321A (en)*1985-09-091991-03-26Sts Enterprises, Inc.Dual frequency feed
US5038151A (en)*1989-07-311991-08-06Loral Aerospace Corp.Simultaneous transmit and receive antenna
US5041840A (en)*1987-04-131991-08-20Frank CipollaMultiple frequency antenna feed
US5255003A (en)*1987-10-021993-10-19Antenna Downlink, Inc.Multiple-frequency microwave feed assembly
EP0860893A1 (en)*1997-02-241998-08-26AlcatelConcentric set of microwave antennas
US5990838A (en)*1996-06-121999-11-233Com CorporationDual orthogonal monopole antenna system
US6297782B1 (en)*2000-07-262001-10-02Gabriel Electronics IncorporatedModular hub array antenna
US6388633B1 (en)*1996-11-152002-05-14Yagi Antenna Co., Ltd.Multibeam antenna
CN103700924A (en)*2013-12-052014-04-02清华大学Circularly polarized angle diversity antenna
CN107946746A (en)*2017-10-162018-04-20西安雷通科技有限责任公司UHF/S dual-frequency range satellite communications and wireless communication system

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
FR2442519A1 (en)*1978-11-241980-06-20Thomson Csf PRINTED MONOPULSE PRIMER SOURCE FOR AIRPORT RADAR ANTENNA AND ANTENNA COMPRISING SUCH A SOURCE
DE3544092A1 (en)*1985-12-131987-06-19Licentia GmbhMulti-band antenna for the GHz band
DE19608622A1 (en)*1996-03-061997-09-11Sel Alcatel AgAerial system with two aerials
FR2773271B1 (en)*1997-12-312000-02-25Thomson Multimedia Sa ELECTROMAGNETIC WAVE TRANSMITTER / RECEIVER

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US3205499A (en)*1956-08-301965-09-07Avco Mfg CorpDual polarized horn antenna

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US3325817A (en)*1964-06-011967-06-13Hughes Aircraft CoDual frequency horn antenna

Patent Citations (1)

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US3205499A (en)*1956-08-301965-09-07Avco Mfg CorpDual polarized horn antenna

Cited By (19)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
US4109254A (en)*1975-06-171978-08-22The Marconi Company Ltd.Dipole radiators for feeding a parabolic reflector
US4028708A (en)*1975-10-101977-06-07The United States Of America As Represented By The Secretary Of The NavyAntenna feed for dual beam conical scan tracking radar
US4207573A (en)*1977-05-181980-06-10Thomson-CsfDual-frequency antenna system with common reflector illuminated by different feeds
US4675685A (en)*1984-04-171987-06-23Harris CorporationLow VSWR, flush-mounted, adaptive array antenna
US5003321A (en)*1985-09-091991-03-26Sts Enterprises, Inc.Dual frequency feed
US4740795A (en)*1986-05-281988-04-26Seavey Engineering Associates, Inc.Dual frequency antenna feeding with coincident phase centers
US4843399A (en)*1986-07-301989-06-27Narco Avionics, Inc.Portable navigational communications transceiver
US5041840A (en)*1987-04-131991-08-20Frank CipollaMultiple frequency antenna feed
US5255003A (en)*1987-10-021993-10-19Antenna Downlink, Inc.Multiple-frequency microwave feed assembly
US4862187A (en)*1988-10-241989-08-29Microwave Components And Systems, Inc.Dual band feedhorn with two different dipole sets
US5038151A (en)*1989-07-311991-08-06Loral Aerospace Corp.Simultaneous transmit and receive antenna
US5990838A (en)*1996-06-121999-11-233Com CorporationDual orthogonal monopole antenna system
US6388633B1 (en)*1996-11-152002-05-14Yagi Antenna Co., Ltd.Multibeam antenna
US6864850B2 (en)1996-11-152005-03-08Yagi Antenna Co., Ltd.Multibeam antenna
EP0860893A1 (en)*1997-02-241998-08-26AlcatelConcentric set of microwave antennas
US6297782B1 (en)*2000-07-262001-10-02Gabriel Electronics IncorporatedModular hub array antenna
CN103700924A (en)*2013-12-052014-04-02清华大学Circularly polarized angle diversity antenna
CN107946746A (en)*2017-10-162018-04-20西安雷通科技有限责任公司UHF/S dual-frequency range satellite communications and wireless communication system
CN107946746B (en)*2017-10-162019-11-22西安雷通科技有限责任公司UHF/S dual-frequency range satellite communication and wireless communication system

Also Published As

Publication numberPublication date
JPS5224369B2 (en)1977-06-30
JPS4921045A (en)1974-02-25
IT988143B (en)1975-04-10
DE2316842C3 (en)1979-01-18
DE2316842A1 (en)1973-10-18
CA977047A (en)1975-10-28
BR7302624D0 (en)1974-07-11
FR2180114A1 (en)1973-11-23
GB1355030A (en)1974-06-05
FR2180114B1 (en)1977-02-04
DE2316842B2 (en)1978-05-24

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