GB1355030A - Antenna feed system - Google Patents

Antenna feed system

Info

Publication number
GB1355030A
GB1355030A GB1738573A GB1738573A GB1355030A GB 1355030 A GB1355030 A GB 1355030A GB 1738573 A GB1738573 A GB 1738573A GB 1738573 A GB1738573 A GB 1738573A GB 1355030 A GB1355030 A GB 1355030A
Authority
GB
United Kingdom
Prior art keywords
horn
ghz
section
arms
bands
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
GB1738573A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Raytheon Co
Original Assignee
Hughes Aircraft Co
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Hughes Aircraft Co filed Critical Hughes Aircraft Co
Publication of GB1355030A publication Critical patent/GB1355030A/en
Expired legal-status Critical Current

Links

Classifications

    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • General Physics & Mathematics (AREA)
  • Waveguide Aerials (AREA)
  • Aerials With Secondary Devices (AREA)
  • Variable-Direction Aerials And Aerial Arrays (AREA)

Abstract

1355030 Aerials HUGHES AIRCRAFT CO 11 April 1973 [14 April 1972] 17385/73 Heading H4A An aerial feed system operative simultaneously in first, second and third increasingly higher frequency bands comprises a horn defining a common radiating aperture for signals within the second and third bands, the latter signals being multimoded by means coupled to the horn. Two arms extend outwardly in opposite directions from the periphery of the horn and, in conjunction with the horn, are resonant within the first frequency band. The arms are fed at their ends nearest the horn, which is surrounded by a cavity also resonant within the first frequency band. As described, the first, second, and third frequency bands are respectively of the orders of 1, 4 and 6 GHz. A square crosssection horn 10 provides a common aperture for the 4 and 6 GHz signals, which are fed to it via a multi-mode step section 14. A 4 GHz choke section 16 surrounds the said aperture, and a dielectric material disc 18 extends radially outwards from the lip thereof, and is supported at its outer periphery by posts 24, which are mounted on a ground plane 12. Dipole arms 20 to 23 extend outwards on the disc 18 from the centres of the sides of the horn 10, and are formed with 4 GHz choke sections. Coaxial feed lines 30 to 33 operating in the 1 GHz band extend from connectors 34 to 37 alongside the horn 10, their centre conductors being connected to respective ones of the dipole arms 20 to 23, and their outer conductors being connected to the outer periphery of the choke section 16 and to the ground plane 12. A 1 GHz resonant cavity is formed by metal bands 26, 28 around the posts 24, and by the ground plane 12. Lastly, a metal cylinder 40 terminating in a flange 42 is disposed outside the posts 24. A cover which is transparent to radiation may be supported on the flange 42. The arrangement provides two crossed dipoles operating in the first (1 GHz) frequency band each comprising two outer arms and a central portion utilizing the periphery of the higher frequency horn (Fig. 7, not shown). The two feeders of a dipole may be connected to respective ports of a 180 degree four-port hybrid to provide sum and difference outputs, for monopulse applications (Fig. 8, not shown). In another mode of operation, the crossed dipoles may be fed in phase quadrature, to provide circularly polarized radiation. It is stated that the feed patterns of the system are nearly identical for each of the three frequency bands (Figs. 3, 4, 5, not shown). A second embodiment is generally similar to the first embodiment, but the horn is surrounded with a double choke section (Fig. 9, not shown). In a third embodiment a circular cross-section horn, having a double choke section, is used (Fig. 10, not shown). In fourth and fifth embodiments, square cross-section horns are used, but are provided with re-entrant portions located, respectively, at the corners and at the centres of the sides of the square (Figs. 11, 12, not shown). The dipole arms extend outwardly from these reentrant portions, and are thus diagonally located in the fourth embodiment.
GB1738573A 1972-04-14 1973-04-11 Antenna feed system Expired GB1355030A (en)

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)

Publication Number Publication Date
GB1355030A true GB1355030A (en) 1974-06-05

Family

ID=22921594

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1738573A Expired GB1355030A (en) 1972-04-14 1973-04-11 Antenna feed system

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)

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1555307A (en) * 1975-06-17 1979-11-07 Marconi Co Ltd Dipole radiotors
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
FR2391570A1 (en) * 1977-05-18 1978-12-15 Thomson Csf DEVICE FOR CORRECTING THE RADIATION OF MULTI-FREQUENCY AIRCRAFT AND AERIALS INCLUDING SUCH A DEVICE
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
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
DE3544092A1 (en) * 1985-12-13 1987-06-19 Licentia Gmbh Multi-band antenna for the GHz band
US4740795A (en) * 1986-05-28 1988-04-26 Seavey Engineering Associates, Inc. Dual frequency antenna feeding with coincident phase centers
US4843399B1 (en) * 1986-07-30 1994-04-05 Narco Avionics Inc Portable navigational communications transceiver
US5041840A (en) * 1987-04-13 1991-08-20 Frank Cipolla Multiple frequency antenna feed
US5255003B1 (en) * 1987-10-02 1995-05-16 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
DE19608622A1 (en) * 1996-03-06 1997-09-11 Sel Alcatel Ag Aerial system with two aerials
US5990838A (en) * 1996-06-12 1999-11-23 3Com Corporation Dual orthogonal monopole antenna system
US6121939A (en) * 1996-11-15 2000-09-19 Yagi Antenna Co., Ltd. Multibeam antenna
FR2773271B1 (en) * 1997-12-31 2000-02-25 Thomson Multimedia Sa ELECTROMAGNETIC WAVE TRANSMITTER / RECEIVER
US6297782B1 (en) * 2000-07-26 2001-10-02 Gabriel Electronics Incorporated Modular hub array antenna
CN103700924B (en) * 2013-12-05 2015-07-15 清华大学 Circularly polarized angle diversity antenna
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

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3205499A (en) * 1956-08-30 1965-09-07 Avco Mfg Corp Dual polarized horn antenna
US3325817A (en) * 1964-06-01 1967-06-13 Hughes Aircraft Co Dual frequency horn antenna

Also Published As

Publication number Publication date
JPS4921045A (en) 1974-02-25
IT988143B (en) 1975-04-10
DE2316842A1 (en) 1973-10-18
FR2180114B1 (en) 1977-02-04
DE2316842B2 (en) 1978-05-24
DE2316842C3 (en) 1979-01-18
BR7302624D0 (en) 1974-07-11
CA977047A (en) 1975-10-28
US3803617A (en) 1974-04-09
JPS5224369B2 (en) 1977-06-30
FR2180114A1 (en) 1973-11-23

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PCNP Patent ceased through non-payment of renewal fee