GB1081518A - Antenna system - Google Patents

Antenna system

Info

Publication number
GB1081518A
GB1081518A GB43316/65A GB4331665A GB1081518A GB 1081518 A GB1081518 A GB 1081518A GB 43316/65 A GB43316/65 A GB 43316/65A GB 4331665 A GB4331665 A GB 4331665A GB 1081518 A GB1081518 A GB 1081518A
Authority
GB
United Kingdom
Prior art keywords
mode
line
outputs
waveguide
probes
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
GB43316/65A
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 GB1081518A publication Critical patent/GB1081518A/en
Expired legal-status Critical Current

Links

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q21/00Antenna arrays or systems
    • H01Q21/0006Particular feeding systems
    • H01Q21/0012Radial guide fed arrays
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q25/00Antennas or antenna systems providing at least two radiating patterns
    • H01Q25/04Multimode antennas
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q3/00Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system
    • H01Q3/26Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the relative phase or relative amplitude of energisation between two or more active radiating elements; varying the distribution of energy across a radiating aperture
    • H01Q3/30Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the relative phase or relative amplitude of energisation between two or more active radiating elements; varying the distribution of energy across a radiating aperture varying the relative phase between the radiating elements of an array
    • H01Q3/34Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the relative phase or relative amplitude of energisation between two or more active radiating elements; varying the distribution of energy across a radiating aperture varying the relative phase between the radiating elements of an array by electrical means
    • H01Q3/40Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the relative phase or relative amplitude of energisation between two or more active radiating elements; varying the distribution of energy across a radiating aperture varying the relative phase between the radiating elements of an array by electrical means with phasing matrix

Landscapes

  • Variable-Direction Aerials And Aerial Arrays (AREA)

Abstract

1,081,518. Aerials. HUGHES AIRCRAFT CO. Oct. 12, 1965 [Nov. 2, 1964], No. 43316/65. Heading H4A. [Also in Division H1] In an aerial system, the radiating elements of a linear array are connected by feeders of equal lengths to pick-up probes spaced evenly around the periphery of a radial transmission line to which is coupled a mode excitation device so that the fundamental and at least one higher mode may be set up, causing signals in the probes which result in beams from the array each directed at an angle which is dependent upon the order of the generating mode. As described, a radial transmission line 10, Fig. 1, comprises two spaced-apart circular plates (22), (24), Fig. 2 (not shown), which are fed by a circular waveguide (18), a coupling cavity (30) being provided. Around the periphery are disposed equally spaced probe assemblies 12, comprising pick-up probes 13 which are connected by cables 14 of equal lengths to the equally spaced radiating elements 15 of a linear array 16, said elements being mounted in a trough (17), Fig. 4 (not shown), and separated from each other by partitions (19). Successive pick-up probes (13) are connected to successive elements (15), for example, adjacent probes to adjacent elements (Fig. 11, not shown) or alternate probes to adjacent elements (Fig. 12, not shown). The upper end of the circular waveguide 18 is connected to a feed mechanism 20 comprising a mode excitation device 21 which has waveguide arms 34, 35, 36, 37 and a tuning extension (31), Fig. 2 (not shown), containing an adjustable plug (32). The waveguide arms 34, 35 and 36, 37 are connected, respectively, to the outputs of magic tees 38 and 41, whose sum inputs are connected to the outputs of a magic tee 44, and whose difference inputs are connected to the outputs of a magic tee (47), Fig. 3 (not shown). When a signal is applied to the sum input (45) of the magic tee (44), outputs in phase are delivered to the waveguide arms (34), (35), (36), (37) and the TM 01 mode is excited in the circular waveguide (18), causing the fundamental TEM mode to be generated in the radial transmission line (10). The pick-up probes 13 are excited in phase and a beam (60), Fig. 13 (not shown), is developed normal to the linear array 16. If a signal is applied to the difference input (46), Fig. 3 (not shown), of the magic tee (44), the outputs to the waveguide arms (34), (35) and (36), (37), respectively, are in anti-phase and a TE 11 mode is excited in the circular waveguide (18). Similarly, when a signal is applied to the difference input (49) of the magic tee (47), a TE 11 mode is excited in the circular waveguide (18), but it is orthogonal to that excited by a signal applied to input (46) of the magic tee (44). The two TE 11 modes develop higher order circumferential modes (m = Π1) in the radial transmission line (10), which correspond to beams (61), (62), Fig. 13 (not shown), angularly displaced on each side of the broadside beam (60). The same considerations apply for reception. In another embodiment, Fig. 5 (not shown), the radial transmission line (10), is fed by a coaxial line (76) from a mode excitation section (75), Fig. 6 (not shown), comprising two rectangular waveguide arms (80), (82) leading into a coaxial segment (77) by suitable transition sections. The segment (77) is connected to the coaxial line (76) and the arms (80), (82) are connected to the outputs (73), (74) of an E- plane folded magic tee (70). When a signal is applied to the sum input (72) of the magic tee (70), outputs in phase appear in the arms (80), (82) of the mode excitation section (75) and a TE 11 mode is developed in the line (76) (Fig. 8, not shown). When a signal is applied to the difference input (71), however, outputs in antiphase appear in the arms (80), (82) and the TEM mode is developed in the line (76). An orthogonal TE 11 mode may be fed to the radial transmission line from the other side thereof. In a further embodiment, the excitation system for the radial transmission line (10) comprises a coaxial line (100), Fig. 10 (not shown), feeding from the top, and a circular waveguide (102) feeding from the bottom. The TEM mode and a TE 11 mode are developed in the line (100) and an orthogonal TE 11 mode in the waveguide (102). Axial septa (103); (104) within the feeders (100), (102) are at right angles to each other and prevent the escape of either TE 11 mode into the feeder for the orthogonal mode. In a further embodiment, a transmitter (90), Fig. 9 (not shown), is connected to the first port of a circulator (91) and a coaxial line feeder (92) for the radial transmission line (10) is connected to the second port thereof. The TEM mode is excited in the line (92), which sets up equi-phase signals in the elements of the linear array, resulting in the transmission of a broadside beam. During reception, however, as well as the TEM mode in the coaxial line (92), orthogonal TE 11 modes are developed in an oppositely disposed circular waveguide (95) and are separated from each other in an orthogonal mode transducer (96). The " inphase " signal corresponding to the TEM mode is passed from the second to the third port of the circular (91), and thence by a line (93) to one input of a 1: 2 power divider (94). A signal having a phase relation which can be designated as cos # is obtained from one output of the mode transducer (96) and is applied to the other input of the 1: 2 power divider (94), the output of which is then equivalent to a (1 + cos #) = 2# 2 cos - aerial aperture distribution. 2
GB43316/65A 1964-11-02 1965-10-12 Antenna system Expired GB1081518A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US408205A US3290682A (en) 1964-11-02 1964-11-02 Multiple beam forming antenna apparatus

Publications (1)

Publication Number Publication Date
GB1081518A true GB1081518A (en) 1967-08-31

Family

ID=23615282

Family Applications (1)

Application Number Title Priority Date Filing Date
GB43316/65A Expired GB1081518A (en) 1964-11-02 1965-10-12 Antenna system

Country Status (3)

Country Link
US (1) US3290682A (en)
DE (1) DE1466127A1 (en)
GB (1) GB1081518A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2000095A1 (en) * 1968-01-09 1969-08-29 Emerson Electric Co LENS POWER SUPPLY SYSTEM IN PHASE ELEMENTS NETWORK

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3863255A (en) * 1971-06-11 1975-01-28 Itt Nonrotating tacan antenna
US4446463A (en) * 1982-02-24 1984-05-01 The United States Of America As Represented By The Secretary Of The Navy Coaxial waveguide commutation feed network for use with a scanning circular phased array antenna
JPS59178801A (en) * 1983-03-29 1984-10-11 Fujitsu Ltd Resonator type power distribution and combination device
JPS6018007A (en) * 1983-07-12 1985-01-30 Fujitsu Ltd Microwave power amplifier
US4590446A (en) * 1984-06-28 1986-05-20 Trw Inc. Radial waveguide power divider/combiner
WO1987002186A1 (en) * 1985-10-03 1987-04-09 Hughes Aircraft Company Non-reactive radial line power divider/combiner with integral mode filters
JPS63501675A (en) * 1985-10-03 1988-06-23 ヒユ−ズ・エアクラフト・カンパニ− Broadband high isolation radial line power splitter/combiner
US4929955A (en) * 1988-03-07 1990-05-29 E-Systems, Inc. Circular waveguide amplitude commutator
US4926145A (en) * 1988-12-16 1990-05-15 Flam & Russell, Inc. Radial power combiner/divider with mode suppression

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2000095A1 (en) * 1968-01-09 1969-08-29 Emerson Electric Co LENS POWER SUPPLY SYSTEM IN PHASE ELEMENTS NETWORK

Also Published As

Publication number Publication date
DE1466127A1 (en) 1969-01-16
US3290682A (en) 1966-12-06

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