GB889460A - Improvements in or relating to antenna array - Google Patents

Improvements in or relating to antenna array

Info

Publication number
GB889460A
GB889460A GB41937/59A GB4193759A GB889460A GB 889460 A GB889460 A GB 889460A GB 41937/59 A GB41937/59 A GB 41937/59A GB 4193759 A GB4193759 A GB 4193759A GB 889460 A GB889460 A GB 889460A
Authority
GB
United Kingdom
Prior art keywords
array
junction
branch
branches
aerial
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
GB41937/59A
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.)
Algemene Nl Radio Unie N V
Original Assignee
Algemene Nl Radio Unie N V
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 Algemene Nl Radio Unie N V filed Critical Algemene Nl Radio Unie N V
Publication of GB889460A publication Critical patent/GB889460A/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

Landscapes

  • Variable-Direction Aerials And Aerial Arrays (AREA)
  • Waveguide Aerials (AREA)
  • Radar Systems Or Details Thereof (AREA)

Abstract

889,460. Radar; radio direction-finding; aerials. ALGEMENE NEDERLANDSE RADIO UNIE N.V. Dec. 9, 1959 [Dec. 11, 1958], No. 41937/59. Class 40(7). The invention relates to an aerial system for direction-finding and radar purposes which is suitable for automatic tracking and which avoids the received signal having a null value when the aerial system is correctly aligned on the target. The system comprises a centrally fed linear array of aerial elements connected as branches of a first "magic T" junction, the E and H branches of this junction being connected by waveguides to the similar branches of a second "magic T" to the output branches of which are connected identical amplifiers or detectors. In a simple embodiment comprising a slot array the two aerial array branches 1, 2, feed a junction having E and H branch outlets 3 and 4 respectively. These are connected to the corresponding branches 5 and 6 of a second junction whose arms 7 and 8 contain probes or detector crystals 9 and 10. The array may be either resonant or non-resonant. In either case an in-phase connection of the array sections, as by the H branch feeder, will provide a single main lobe pattern symmetrical about an axis perpendicular to the array. Out of phase connection of the two array sections, as by the E branch feeder, on the other hand provides a two-lobed pattern. with a null on the above mentioned axis. It should be noted that the pattern lobes on each side of this null are in opposite phase. The E branch coupling feeds outputs of opposite sign to detectors 9 and 10 whilst the H branch coupling feeds them with in-phase signals. For auto-follow purposes the detector outputs are subtracted and the resultant signal used to drive the motor aligning the aerial system. Provided the target is initially within the single lobe pattern to give an output over the H branch coupling tracking can be effected. For searching purposes the single lobe pattern may be broadened by providing micro-wave switches disconnecting the outer parts of the array. Communication is possible during tracking due to the finite (but equal) outputs from detectors 9 and 10. Aerial systems according to the invention may be used in point-to-point communication links and in radar systems. Fig. 3 shows an embodiment for radar use. In this the H branch coupling is considerably modified. The H connection 16 from the first junction leads past a short slot hybrid 22 to a T.R. cell 24 and on past a second short slot hybrid 25 to a matching impedance termination 26. The H connection 27 from the second junction is arranged parallel and includes hybrid 25, a second T.R. cell 23 and hybrid 22. It is terminated by connection to transmitter magnetron 21. A transmitter pulse causes T.R. cells 23 and 24 to fire and energy is directed through slot 22 to feed the aerial system sections in phase. Received signals are below the power necessary to cause the cells to fire and pass to the second "magic T" junction exactly as described for the previous embodiment. A klystron 28, or other source of hetrodyning radiations, may be coupled to the H branch of this second junction through a directional coupler 29. To protect detectors 19 and 20 during transmission a micro-wave switch 17, controlled by the transmitter modulating arrangement is inserted in the E branch connection. Fig. 4 shows an aerial system for determining bearings in spherical co-ordinates having two mutually perpendicular centre-fed arrays 30, 31, and 36, 37 coupled at different levels to a turnstile junction 32. In-phase signals from the array at the same level and out-ofphase signals from the other array are derived from pairs of outputs 33, 34 and 38, 39 and may be used to provide error signals for tracking.
GB41937/59A 1958-12-11 1959-12-09 Improvements in or relating to antenna array Expired GB889460A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
NL234115 1958-12-11

Publications (1)

Publication Number Publication Date
GB889460A true GB889460A (en) 1962-02-14

Family

ID=19751470

Family Applications (1)

Application Number Title Priority Date Filing Date
GB41937/59A Expired GB889460A (en) 1958-12-11 1959-12-09 Improvements in or relating to antenna array

Country Status (6)

Country Link
US (1) US3136993A (en)
BE (1) BE585365A (en)
CH (1) CH387716A (en)
DE (2) DE1441556A1 (en)
FR (1) FR1242660A (en)
GB (1) GB889460A (en)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1291750A (en) * 1961-03-17 1962-04-27 Csf Flat antenna for single pulse radar
DE1293252B (en) * 1962-08-17 1969-04-24 Deutsche Bundespost Rotatable directional antenna system
US3340532A (en) * 1963-09-30 1967-09-05 Walter L Glomb Tracking receiver
US3430247A (en) * 1967-09-05 1969-02-25 North American Rockwell Centerfed travelling wave array having a squinted aperture
US4203114A (en) * 1978-11-13 1980-05-13 Anaren Microwave, Inc. Digital bearing indicator
US4359742A (en) * 1980-12-23 1982-11-16 United Technologies Corporation Dual switch multimode array antenna
US9711870B2 (en) * 2014-08-06 2017-07-18 Waymo Llc Folded radiation slots for short wall waveguide radiation
CN114823251B (en) * 2022-04-08 2023-04-14 电子科技大学 Axial cascade relativistic magnetron based on branch feed structure frequency locking and phase locking

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB589136A (en) * 1943-06-05 1947-06-12 Western Electric Co Improvements in or relating to directive radio systems
US2817835A (en) * 1945-11-29 1957-12-24 Jr Harvey R Worthington Lobe comparison systems
US2825057A (en) * 1946-06-18 1958-02-25 Jr Harvey R Worthington Simultaneous lobe matching device
US2821701A (en) * 1948-04-01 1958-01-28 Jr Clyde E Vogeley Automatic radar tracking-system
NL195059A (en) * 1955-02-23
DE1015502B (en) * 1955-02-24 1957-09-12 Telefunken Gmbh Directional antenna system for carrying out a spatial bearing
US2981948A (en) * 1956-05-29 1961-04-25 Hughes Aircraft Co Simultaneous lobing array antenna system

Also Published As

Publication number Publication date
FR1242660A (en) 1960-09-30
US3136993A (en) 1964-06-09
BE585365A (en) 1960-04-01
DE1441556B2 (en) 1970-08-13
CH387716A (en) 1965-02-15
DE1157675B (en) 1963-11-21
DE1441556A1 (en) 1969-10-02

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