GB1605279A - Aerials - Google Patents

Aerials Download PDF

Info

Publication number
GB1605279A
GB1605279A GB4786472A GB4786472A GB1605279A GB 1605279 A GB1605279 A GB 1605279A GB 4786472 A GB4786472 A GB 4786472A GB 4786472 A GB4786472 A GB 4786472A GB 1605279 A GB1605279 A GB 1605279A
Authority
GB
United Kingdom
Prior art keywords
reflectors
aerial
aerials
axis
wavelength
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
GB4786472A
Inventor
N D Dover
R Essam
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.)
BAE Systems Electronics Ltd
Original Assignee
Marconi Co Ltd
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 Marconi Co Ltd filed Critical Marconi Co Ltd
Priority to GB4786472A priority Critical patent/GB1605279A/en
Publication of GB1605279A publication Critical patent/GB1605279A/en
Expired legal-status Critical Current

Links

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q21/00Antenna arrays or systems
    • H01Q21/06Arrays of individually energised antenna units similarly polarised and spaced apart
    • H01Q21/061Two dimensional planar arrays
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q19/00Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic
    • H01Q19/10Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using reflecting surfaces
    • H01Q19/18Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using reflecting surfaces having two or more spaced reflecting surfaces
    • H01Q19/185Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using reflecting surfaces having two or more spaced reflecting surfaces wherein the surfaces are plane

Landscapes

  • Aerials With Secondary Devices (AREA)

Description

(54) IMPROVEMENTS IN OR RELATING TO AERIALS (71) We, THE MARCONI COMPANY LIMITED. of Marconi Housc, Ncw Street, Chelmsford, CM1 1PL, Essex, a British Company, do hereby declare the invention, for which we pray that a patent may be granted to us, and the method y which it is to be performed, to be particularly described in and by the following statement: This invention relates to aerials.
According to the invention, an aerial for radiating and/or receiving electromagnctic waves of a predetermined wavelength I comprises two plane reflectors of different sizes mounted parallel to each other and spaced apart hy a distance substantially equal to N1/2, where N is a positive integer, along a common axis of symmetry, so as to form a resonant structure and an antenna positioned on said axis between said reflectors for exciting vibrations of wavelength I in said resonant structure, thereby causing an output beam of electromagnetic radiation of wavelength I to be produced, directed generally along said axis in the direction of the smaller of said reflectors, said antenna being formed hy a slot in an otherwise closed end of a waveguide which passes along said axis through the larger of said re@lec@@ Preferable @ri@@flectors are circular in shape and preferably they have diameters substantially equal to 21 and 0.41 respectively.
Preferably also said antenna is positioned substantially midway between said reflectors. the invention also provides an aerial array comprising two or more aerials each in accordance with the present invention, mounted together on a common support member. Such aerial arrays are suitable for use with radar or direction-finding equipment @@@ the @@@@ principl The invention @@ls particular application in a tracking radar system for a homing head of a missile.
One embodiment of the @@@@ntion will now be described, by way of example. with reference to the accompanying drawing. of which: Figures I and 7 are respectively a sectional elevation and a plan view of an elementary aerial; ind Figure 3 is a plan view of an aerial array.
Referring to Figures I and 2, the aerial comprises two circular metal reflectors 10 and 12, having diameters respectively equal to 21 and ().41 where 1 is the operating wavelength of the aerial. The larger reflector 10 carrics a tubular metal rim 14, having a depth of 0.51.
The smaller reflector 12 is mounted on this rim 14, by means of a pair of dielectric supports 16.
In this way, the reflectors 10 and 12 are fixed parallel to each other and spaced apart by a distance approximately equal to 0.51, along a common axis IX of symmetry. The two reflectors it), 12 thus form a resonant structure for clcctromagnctic vibrations of wavelength l A rectangular waveguide 20 passes along the axis 18, through the larger reflector 10, and terminates in a slot 22, approximately 0.5l in length. which acts as an exciting antenna for the aerial The Icngth of the waveguide 20 which projects between the reflectors 10 and 12 is approximately equal to 0.25l, so that the exciting slot 22 lics substantially mid-way between the reflectors 10 and 12.
In operation, electromagnetic guided waves are fed down the waveguide 20. These waves are radiated from the s@@ 22, and excite electromagne@ @ib@@ wavelength @ between the reflectors are 12. these vibrations cause an output beam of electromagnetic waves to be produced, directed generally along the axis 18 in the direction of the smaller reflector 12.
Such an aerial providers a high gain factor and yet is simple in construction and is therefore both chcap to produce and reliable in operation.
The rim 14 is not essential, but serves to increase the gain of the aerial still further.
In @odi@@@@tion of the element @@rial, the spacing of the reflectors 10 and 12 may be increased by an integral number of half wavelength. Thus, in general, the spacing between the reflectors is substantially equal to @@@@l@re N is a positive integer.
Referring now to Figure 3, four elementary aerials 24, 26, 2X and 30. each of which is constructed as shown in Figures I and 2, are mounted side-by-side on a common support 32 in a square formation to provide an aerial array suitable for use in a static-split radar system.
The support 32 may be mounted on gimbals (not shown) so that it can be tilted so as to permit the aerial array to track a target.
What we claim is: 1. An aerial for radiating and/or receiving electromagnetic waves of predetermined wavelength 1 comprising two plane reflectors of different sizes mounted parallel to each other and spaced apart by a distance substantially equal to No/2, where N is a positive integer, along a common axis of symmetry, so as to form a resonant structure, and an antenna positioned on said axis between said reflectors for exciting vibrations of wavelength 1 in said resonant structure, thereby causing an output beam of electromagnetic radiation of wavelength I to be produced, directed generally along said axis in the direction of the smaller of said reflectors, said antenna being formed by a slot in an otherwise closed end of a waveguide which passes along said axis through the larger of said reflectors.

Claims (1)

  1. 2. An aerial according to Claim 1, wherein said reflectors are circular in shape.
    3. An aerial according to Claim 2 wherein said reflectors have diameters substantially equal to 21 and 0.41 respectively.
    4. An aerial according to Claim 1, Claim 2 or Claim 3, wherein said antenna is positioned substantially midway between said reflectors.
    5. An aerial array comprising two or more aerials mounted together on a common support member, each of these aerials being in accordance with any one of the preceding claims.
    6. An aerial array according to Claim 6, wherein there are four of said aerials mounted side-by-side in a square formation.
    7. An acrial substantially as hereinbefore described with reference to Figures 1 and 2 of the accompanying drawing.
    8. An aerial array substantially as hereinbefore described with reference to Figures 1. 2 and 3 of the accompanying drawing.
GB4786472A 1972-10-17 1972-10-17 Aerials Expired GB1605279A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB4786472A GB1605279A (en) 1972-10-17 1972-10-17 Aerials

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB4786472A GB1605279A (en) 1972-10-17 1972-10-17 Aerials

Publications (1)

Publication Number Publication Date
GB1605279A true GB1605279A (en) 1987-10-21

Family

ID=10446513

Family Applications (1)

Application Number Title Priority Date Filing Date
GB4786472A Expired GB1605279A (en) 1972-10-17 1972-10-17 Aerials

Country Status (1)

Country Link
GB (1) GB1605279A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2655204A1 (en) * 1989-11-27 1991-05-31 Matsushita Electric Works Ltd WAVEGUIDE SUPPLY NETWORK ANTENNA.

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2655204A1 (en) * 1989-11-27 1991-05-31 Matsushita Electric Works Ltd WAVEGUIDE SUPPLY NETWORK ANTENNA.

Similar Documents

Publication Publication Date Title
US3755815A (en) Phased array fed lens antenna
US5268680A (en) Combined infrared-radar detection system
US3936835A (en) Directive disk feed system
US3189907A (en) Zone plate radio transmission system
DE60040862D1 (en) DIELECTRIC RESONATOR ANTENNA WITH VARIOUS CROSS-SECTION SHAPES, CONTROLLABLE RADIATION ELEMENTS AND MULTIPLE SUPPLY
US2846678A (en) Dual frequency antenna
US2408373A (en) Antenna
GB1425142A (en) Antenna system for radiating multiple planar beams
US3750182A (en) Suppressed sidelobe equal beamwidth millimeter horn antenna
US2595271A (en) Antenna lobe shifting device
US2871477A (en) High gain omniazimuth antenna
US2169553A (en) Directive radio system
US2643338A (en) Conical scan antenna
WO2018096307A1 (en) A frequency scanned array antenna
JP2002151943A (en) Divergent dome lens for microwave, and antenna including the lens
GB1434986A (en) Antenna system
US2187618A (en) Radio beacon system
GB1605279A (en) Aerials
US2888674A (en) Dual lens antenna for tracking and searching
US2591695A (en) High-frequency radiator apparatus and resonator
US2567220A (en) Scalloped limacon pattern antenna
US2939141A (en) Omnirange beacon antennas
US2440210A (en) Antenna
US3064258A (en) Directive antenna scanning and tracking device and applications thereof
US2820221A (en) Directional aerials

Legal Events

Date Code Title Description
CSNS Application of which complete specification have been accepted and published, but patent is not sealed