US3803617A - High efficiency multifrequency feed - Google Patents

High efficiency multifrequency feed Download PDF

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Publication number
US3803617A
US3803617A US00244158A US24415872A US3803617A US 3803617 A US3803617 A US 3803617A US 00244158 A US00244158 A US 00244158A US 24415872 A US24415872 A US 24415872A US 3803617 A US3803617 A US 3803617A
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horn
frequency band
high efficiency
feed system
arms
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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 US00244158A priority Critical patent/US3803617A/en
Priority to CA167,786A priority patent/CA977047A/en
Priority to DE2316842A priority patent/DE2316842C3/en
Priority to BR732624A priority patent/BR7302624D0/en
Priority to GB1738573A priority patent/GB1355030A/en
Priority to JP48041489A priority patent/JPS5224369B2/ja
Priority to FR7313570A priority patent/FR2180114B1/fr
Priority to IT49428/73A priority patent/IT988143B/en
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    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q25/00Antennas or antenna systems providing at least two radiating patterns
    • H01Q25/02Antennas or antenna systems providing at least two radiating patterns providing sum and difference patterns
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO 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
    • G01S13/00Systems 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
    • G01S13/02Systems using reflection of radio waves, e.g. primary radar systems; Analogous systems
    • G01S13/06Systems determining position data of a target
    • G01S13/42Simultaneous measurement of distance and other co-ordinates
    • G01S13/44Monopulse radar, i.e. simultaneous lobing
    • G01S13/4409HF sub-systems particularly adapted therefor, e.g. circuits for signal combination
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q5/00Arrangements for simultaneous operation of antennas on two or more different wavebands, e.g. dual-band or multi-band arrangements
    • H01Q5/40Imbricated or interleaved structures; Combined or electromagnetically coupled arrangements, e.g. comprising two or more non-connected fed radiating elements
    • H01Q5/45Imbricated 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

Definitions

  • 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.
  • satellite communications telemetry bands operate in frequency bands 0.8 1.0 GHZ, 3.7 4.2 GHz and 5.9 6.4 GHz.
  • the antenna system of the invention has monopulse capability for reception with circular or diverse polarization at frequency band 1.
  • 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.
  • 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.
  • 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.
  • One or more quarter wavechokes surrounding the 6/4 GHz horn aperture prevent coupling to the 1 GHz frequency wave dipole.
  • 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.
  • 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.
  • the sum port of the hybrid 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.
  • 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
  • FIGS. 9-l2 show alternative configurations of the plan view of the aperture of the multifrequency feed of FIGS. 1 and 2.
  • FIGS. 1 and 2 of the drawings there is shown a plan view of the aperture and a cross-section 22 thereof, respectively, of the high efficiency multifrequency feed antenna system of the present invention.
  • a square horn 10 having dimensions suitable to provide a 6 GHz and 4 GHz common aperture extends through the central portion of a conductive ground plane 12.
  • the square horn 10 On the back side of ground plane 12 relative to the antenna aperture, the square horn 10 extends into a multimode step section 14 dimensioned for 6 GHz which section 14 terminates in a flange 15.
  • the multimode step section 14 is symmetrically disposed about the center line through horn l0.
  • a choke section 16 Surrounding the outer periphery of horn 10 at the lip thereof is disposed a choke section 16 primarily designed to inhibit the flow of 4 GHz energy thereacross.
  • a dielectric disc 18 extends radialy outwards from the outer lip of choke section 16 for a sufficient distance to support UHF choked dipole arms 20, 21, 22 and 23 which extend outwards from the center of the four sides of horn 10.
  • the outer periphery of dielectric disc 18 is supported by metallic posts 24 which extend to the ground plane 12.
  • a UHF cavity is formed by metal bands 26, 28 disposed about the central portion and adjacent ground plane 12, respectively, of the metallic posts 24.
  • the extremity of the center leg of the UHF choked dipole arms 20-23 nearest horn 10 are fed by the respective center conductors of coaxial lines 30-33, respectively.
  • the coaxial lines 3033 extend through the ground plane 12 parallel to the center line of horn 10 and are terminated by connectors 34-37, respectively.
  • the outer conductors of coaxial lines 30-33 are electrically connected to the outer periphery of choke section 16 and to the ground plane 12.
  • a metal cylinder 40 terminating in a flange 42 is disposed symmetrically about metallic posts 24.
  • Metal cylinder 40 is attached to ground plane 12 and has a height slightly greater than the dimension of square horn 10 which extends through the ground plane 12.
  • the flange 42 provides a support for a radome if desired.
  • the 4 GHz and 6 GHz frequency band signals are fed through the multimode step section 14 to the horn 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.
  • the mode exciters coupled to flange 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 the choke 16 around the horn 10 alone. 7
  • FIG. 6 illustrates a two point fed dipole having segments 50, 51, and52 driven by voltage sources 53, 54 which supply a signal voltage, V.
  • voltage sources 53, 54 drive the dipole segments 50, 51, 52 in phase
  • the current, I increases from the left extremity, as shown in the drawing, to a, maximum along center segment 51 and then decreases to zero at the right extremity of segment 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.
  • the center segment 51 of FIG. 6 is replaced with the horn 10.
  • the current that previously flowed through the center segment 51 divides and flows around opposite sides of the horn 10.
  • FIG. 8 shows the dipoles 50, 52 replaced with the choked dipoles 23, 21, respectively, and the voltage sources 53, 54 provided by coaxial lines 33, 31, as in FIG. 1.
  • the coaxial lines 31, 33 are, in turn, fed with a 180 four-port hybrid 56.
  • the voltages at the outputs of coaxial lines 31, 33 are in anti-phase, creating a null pattern.
  • the difference input (A) 58 when fed through the difference input (A) 58, the voltages at the outputs of coaxial lines 31, 33 are in phase, resulting in a good sum pattern.
  • the sum and null patterns can be used for monopulse tracking applications.
  • the remaining dipoles 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 to hybrid 56, thereby to generate a circularly polarized output signal.
  • the feed pattern for each of the three frequency bands be nearly identical in all planes and have a common'center of phase.
  • 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.
  • the horn-dipole assembly is contained in a l GI-Iz cavity formed by ground plane 18, and the metal bands 26, '28 whose parameters are adjusted to shape the 1 GHz patterns without afiecting the 6 and 4 GHz patterns.
  • 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.
  • FIG. 3 illustrates a horizontal pattern 60, a vertical pattern 61, and a diagonal pattern 62 for the 4 GHz frequency band
  • FIG. 4 illustrates a horizontal pattern 63, a vertical pattern 64, and a diagonal pattern 68 for the 1 GHz frequency band.
  • 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.
  • 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.
  • FIG. 9 shows an aperture view with double choke slots 70, 71' surrounding the periphery of horn 10.
  • Choke slot 70 could be designed to impede the 4 GHz frequency band and choke slot 71 designed to impede the 6 CH2 frequency band.
  • a circular horn 72 and a crossedhorn 73 are shown, respectively, in place of the square horn 10.
  • the choked dipole arms 20-23 emanate from the inside corners thereof.
  • FIG. 12 illustrates a horn 74 having indentations adapted to accommodate coaxial lines 30-33.
  • a choke slot 75 about the periphery of the horn 74 follows the aforementioned indentations.
  • 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;
  • 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;
  • 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.
  • 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.
  • 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.
  • 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.
  • 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.
  • 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;
  • first and second parallel metallic bands disposed about said plurality of metallic posts thereby to provide a cavity resonant at said first frequency band

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 a cross-section 22 thereof, respectively, of the high efficiency multifrequency feed antenna system of the present invention. In particular, a square horn 10 having dimensions suitable to provide a 6 GHz and 4 GHz common aperture extends through the central portion of a conductive ground plane 12. On the back side of ground plane 12 relative to the antenna aperture, the square horn 10 extends into a multimode step section 14 dimensioned for 6 GHz which section 14 terminates in a flange 15. The multimode step section 14 is symmetrically disposed about the center line through horn l0. Surrounding the outer periphery of horn 10 at the lip thereof is disposed a choke section 16 primarily designed to inhibit the flow of 4 GHz energy thereacross.
Relative to the 1 GHz frequency band, a dielectric disc 18 extends radialy outwards from the outer lip of choke section 16 for a sufficient distance to support UHF choked dipole arms 20, 21, 22 and 23 which extend outwards from the center of the four sides of horn 10. The outer periphery of dielectric disc 18 is supported by metallic posts 24 which extend to the ground plane 12. A UHF cavity is formed by metal bands 26, 28 disposed about the central portion and adjacent ground plane 12, respectively, of the metallic posts 24. The extremity of the center leg of the UHF choked dipole arms 20-23 nearest horn 10 are fed by the respective center conductors of coaxial lines 30-33, respectively. The coaxial lines 3033 extend through the ground plane 12 parallel to the center line of horn 10 and are terminated by connectors 34-37, respectively. The outer conductors of coaxial lines 30-33 are electrically connected to the outer periphery of choke section 16 and to the ground plane 12. Lastly, a metal cylinder 40 terminating in a flange 42 is disposed symmetrically about metallic posts 24. Metal cylinder 40 is attached to ground plane 12 and has a height slightly greater than the dimension of square horn 10 which extends through the ground plane 12. The flange 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 the multimode step section 14 to the horn 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 to flange 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 the choke 16 around the horn 10 alone. 7
Referring to FIGS. 6-8, there is illiistrated the manner in which opposite dipoles 20, 22 and 21, 23 operate. In particular, FIG. 6 illustrates a two point fed dipole having segments 50, 51, and52 driven by voltage sources 53, 54 which supply a signal voltage, V. When voltage sources 53, 54 drive the dipole segments 50, 51, 52 in phase, the current, I, increases from the left extremity, as shown in the drawing, to a, maximum along center segment 51 and then decreases to zero at the right extremity of segment 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, the center segment 51 of FIG. 6 is replaced with the horn 10. In this case, the current that previously flowed through the center segment 51 divides and flows around opposite sides of the horn 10.
Lastly, FIG. 8 shows the dipoles 50, 52 replaced with the choked dipoles 23, 21, respectively, and the voltage sources 53, 54 provided by coaxial lines 33, 31, as in FIG. 1. The coaxial 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 of coaxial 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 of coaxial 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 remaining dipoles 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 to hybrid 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 by ground plane 18, and the metal 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 a horizontal pattern 60, a vertical pattern 61, and a diagonal pattern 62 for the 4 GHz frequency band; FIG. 4 illustrates a horizontal pattern 63, a vertical pattern 64, and a diagonal 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 with double choke slots 70, 71' surrounding the periphery of horn 10. Choke slot 70, for example, could be designed to impede the 4 GHz frequency band and choke slot 71 designed to impede the 6 CH2 frequency band. Referring to FIGS. 10, 11, a circular horn 72 and a crossedhorn 73 are shown, respectively, in place of the square 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 a horn 74 having indentations adapted to accommodate coaxial lines 30-33. A choke slot 75 about the periphery of the horn 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 in claim 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 in claim 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 in claim 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)

1. 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 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 in claim 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 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 in claim 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 in claim 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.
US00244158A 1972-04-14 1972-04-14 High efficiency multifrequency feed Expired - Lifetime US3803617A (en)

Priority Applications (8)

Application Number Priority Date Filing Date Title
US00244158A US3803617A (en) 1972-04-14 1972-04-14 High efficiency multifrequency feed
CA167,786A CA977047A (en) 1972-04-14 1973-04-03 High efficiency multifrequency feed
DE2316842A DE2316842C3 (en) 1972-04-14 1973-04-04 Multi-frequency antenna for three frequency bands
GB1738573A GB1355030A (en) 1972-04-14 1973-04-11 Antenna feed system
BR732624A BR7302624D0 (en) 1972-04-14 1973-04-11 HIGH EFFICIENCY MULTIPLE FREQUENCY POWER SUPPLY
JP48041489A JPS5224369B2 (en) 1972-04-14 1973-04-13
FR7313570A FR2180114B1 (en) 1972-04-14 1973-04-13
IT49428/73A IT988143B (en) 1972-04-14 1973-04-13 MULTIFREQUENCY POWER SUPPLY D HIGH PERFORMANCE ANTENNA

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US00244158A US3803617A (en) 1972-04-14 1972-04-14 High efficiency multifrequency feed

Publications (1)

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US3803617A true US3803617A (en) 1974-04-09

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US00244158A Expired - Lifetime US3803617A (en) 1972-04-14 1972-04-14 High efficiency multifrequency feed

Country Status (8)

Country Link
US (1) US3803617A (en)
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 (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4028708A (en) * 1975-10-10 1977-06-07 The United States Of America As Represented By The Secretary Of The Navy Antenna feed for dual beam conical scan tracking radar
US4109254A (en) * 1975-06-17 1978-08-22 The Marconi Company Ltd. Dipole radiators for feeding a parabolic reflector
US4207573A (en) * 1977-05-18 1980-06-10 Thomson-Csf Dual-frequency antenna system with common reflector illuminated by different feeds
US4675685A (en) * 1984-04-17 1987-06-23 Harris Corporation Low VSWR, flush-mounted, adaptive array antenna
US4740795A (en) * 1986-05-28 1988-04-26 Seavey Engineering Associates, Inc. Dual frequency antenna feeding with coincident phase centers
US4843399A (en) * 1986-07-30 1989-06-27 Narco Avionics, Inc. Portable navigational communications transceiver
US4862187A (en) * 1988-10-24 1989-08-29 Microwave Components And Systems, Inc. Dual band feedhorn with two different dipole sets
US5003321A (en) * 1985-09-09 1991-03-26 Sts Enterprises, Inc. Dual frequency feed
US5038151A (en) * 1989-07-31 1991-08-06 Loral Aerospace Corp. Simultaneous transmit and receive antenna
US5041840A (en) * 1987-04-13 1991-08-20 Frank Cipolla Multiple frequency antenna feed
US5255003A (en) * 1987-10-02 1993-10-19 Antenna Downlink, Inc. Multiple-frequency microwave feed assembly
US5990838A (en) * 1996-06-12 1999-11-23 3Com Corporation Dual orthogonal monopole antenna system
US6297782B1 (en) * 2000-07-26 2001-10-02 Gabriel Electronics Incorporated Modular hub array antenna
US6388633B1 (en) * 1996-11-15 2002-05-14 Yagi Antenna Co., Ltd. Multibeam antenna
CN103700924A (en) * 2013-12-05 2014-04-02 清华大学 Circularly polarized angle diversity antenna
CN107946746A (en) * 2017-10-16 2018-04-20 西安雷通科技有限责任公司 UHF/S dual-frequency range satellite communications and wireless communication system

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JPS5816602Y2 (en) * 1978-03-16 1983-04-04 シャープ株式会社 air conditioner
FR2442519A1 (en) * 1978-11-24 1980-06-20 Thomson Csf PRINTED MONOPULSE PRIMER SOURCE FOR AIRPORT RADAR ANTENNA AND ANTENNA COMPRISING SUCH A SOURCE
DE3544092A1 (en) * 1985-12-13 1987-06-19 Licentia Gmbh Multi-band antenna for the GHz band
DE19608622A1 (en) * 1996-03-06 1997-09-11 Sel Alcatel Ag Aerial system with two aerials
FR2773271B1 (en) * 1997-12-31 2000-02-25 Thomson Multimedia Sa ELECTROMAGNETIC WAVE TRANSMITTER / RECEIVER

Citations (1)

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US3205499A (en) * 1956-08-30 1965-09-07 Avco Mfg Corp Dual polarized horn antenna

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US3325817A (en) * 1964-06-01 1967-06-13 Hughes Aircraft Co Dual frequency horn antenna

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US3205499A (en) * 1956-08-30 1965-09-07 Avco Mfg Corp Dual polarized horn antenna

Cited By (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4109254A (en) * 1975-06-17 1978-08-22 The Marconi Company Ltd. Dipole radiators for feeding a parabolic reflector
US4028708A (en) * 1975-10-10 1977-06-07 The United States Of America As Represented By The Secretary Of The Navy Antenna feed for dual beam conical scan tracking radar
US4207573A (en) * 1977-05-18 1980-06-10 Thomson-Csf Dual-frequency antenna system with common reflector illuminated by different feeds
US4675685A (en) * 1984-04-17 1987-06-23 Harris Corporation Low VSWR, flush-mounted, adaptive array antenna
US5003321A (en) * 1985-09-09 1991-03-26 Sts Enterprises, Inc. Dual frequency feed
US4740795A (en) * 1986-05-28 1988-04-26 Seavey Engineering Associates, Inc. Dual frequency antenna feeding with coincident phase centers
US4843399A (en) * 1986-07-30 1989-06-27 Narco Avionics, Inc. Portable navigational communications transceiver
US5041840A (en) * 1987-04-13 1991-08-20 Frank Cipolla Multiple frequency antenna feed
US5255003A (en) * 1987-10-02 1993-10-19 Antenna Downlink, Inc. Multiple-frequency microwave feed assembly
US4862187A (en) * 1988-10-24 1989-08-29 Microwave Components And Systems, Inc. Dual band feedhorn with two different dipole sets
US5038151A (en) * 1989-07-31 1991-08-06 Loral Aerospace Corp. Simultaneous transmit and receive antenna
US5990838A (en) * 1996-06-12 1999-11-23 3Com Corporation Dual orthogonal monopole antenna system
US6388633B1 (en) * 1996-11-15 2002-05-14 Yagi Antenna Co., Ltd. Multibeam antenna
US6864850B2 (en) 1996-11-15 2005-03-08 Yagi Antenna Co., Ltd. Multibeam antenna
US6297782B1 (en) * 2000-07-26 2001-10-02 Gabriel Electronics Incorporated Modular hub array antenna
CN103700924A (en) * 2013-12-05 2014-04-02 清华大学 Circularly polarized angle diversity antenna
CN107946746A (en) * 2017-10-16 2018-04-20 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) * 2017-10-16 2019-11-22 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 number Publication date
DE2316842C3 (en) 1979-01-18
JPS4921045A (en) 1974-02-25
IT988143B (en) 1975-04-10
CA977047A (en) 1975-10-28
BR7302624D0 (en) 1974-07-11
DE2316842A1 (en) 1973-10-18
FR2180114A1 (en) 1973-11-23
GB1355030A (en) 1974-06-05
DE2316842B2 (en) 1978-05-24
JPS5224369B2 (en) 1977-06-30
FR2180114B1 (en) 1977-02-04

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