US3247512A - Microwave antenna - Google Patents

Microwave antenna Download PDF

Info

Publication number
US3247512A
US3247512A US345222A US34522264A US3247512A US 3247512 A US3247512 A US 3247512A US 345222 A US345222 A US 345222A US 34522264 A US34522264 A US 34522264A US 3247512 A US3247512 A US 3247512A
Authority
US
United States
Prior art keywords
radiating
planar array
array
energy
beams
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 - Lifetime
Application number
US345222A
Inventor
Diamond Maurice
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.)
Laboratory For Electronics Inc
Original Assignee
Lab For Electronics Inc
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 Lab For Electronics Inc filed Critical Lab For Electronics Inc
Priority to US345222A priority Critical patent/US3247512A/en
Application granted granted Critical
Publication of US3247512A publication Critical patent/US3247512A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q25/00Antennas or antenna systems providing at least two radiating patterns
    • H01Q25/004Antennas or antenna systems providing at least two radiating patterns providing two or four symmetrical beams for Janus application

Definitions

  • Airborne Doppler radar systems which cmploy an antenna for transmitting directional beams of microwave energy toward the surface of the earth and receiving Doppler shifted signals reflected therefrom.
  • One known type of such antenna is the so-called Luneberg lens antenna, wherein a wide angle dielectric lens co operates with a number of feed horns to produce the desired beams.
  • Another known type of antenna which pro prises a plurality of directional beams is the so-called planar antenna, as for example, the antenna described in the application for patent (assigned to the same assignee as this application) Serial No. 193,717, entitled Microwave Antenna, filed May 10, 1962, in the name of Alan J. Simmons, wherein a plurality of parallel sections of: waveguides support a plurality of radiating slots to produce a beam when such sections are energized with microwave energy.
  • neither type may be used when it is desired to produce beams of other shapes. Further, neither type is well adapted to the simultaneous transmission of more than one beam or to changes in the polarization of the energy in the propagated beam or beams.
  • Another object of this invention is to provide an improved beam forming antenna which is adapted to produce beams of microwave energy of diifering cross-sectional shapes.
  • Another object of this invention is to provide an improved beam forming antenna which is adapted to produce beams of microwave energy wherein the polarization of such energy may be easily controlled.
  • Still another object of this invention is to provide an improved beam forming antenna which accomplishes the foregoing objects with compact, known elements.
  • an antenna comprising a first and second planar array orthogonally disposed with respect to each other.
  • the beam forming radiating elements of the first such array are preferably disposed parallel to each other and spaced from each other to allow the radiating slots in the radiating elements of the second such array to be disposed between the radiating elements of the first.
  • the two arrays may be energized either simultaneously or sequentially making it possible to form, at any time, either a single beam, or a plurality of beams, and to control the polarization thereof. Further the shape of the beams may be controlled within wide limits by changing the arrangelit Gil
  • FIG. 1 is a simplified view taken from below of an antenna according to the invention (a portion of the structure being broken away in order to illustrate normally hidden elements), which antenna is adapted to provide three elliptical beams symmetrically disposed with respect to a line perpendicular to the plane of each array; and
  • FIG. 2 is a block diagram of a system according to an alternative embodiment of the invention.
  • an antenna comprises a first planar array 10 and a second planar array 12 preferably in contact with one another and energized through wave guides 13, 14, 15.
  • the latter elements are connected through a radio frequency switch 16 of any conventional design to a transmitter/receiver 17. Signals out of the receiver portion of the last named element are, when the antenna is a portion of a Doppler radar system, fed to a tracker unit 18 and thence to an indicator 19.
  • the planar array 10 consists of a feed guide 21 integrally attached to and extending from the wave guide 13 and a plurality of radiating guides 23 affixed to the feed guide 21 as shown.
  • the radiating guides 23 are parallel to each other and spaced as shown, there being a convcntional matched load (unnumbered) affixed to the free end of each radiating guide 23 to prevent unwanted reflections.
  • the spacing between adjacent radiating guides 23 is not critical, so long as such spacing is less than one half wavelength of the frequency of the signal radiated from the planar array 12.
  • the radiating slots 24 in the radiating guides 23 are arranged in the form of an approximate parallelogram as shown by the dotted line 1 to produce an elliptical beam when electromagnetic energy is passed through waveguide 13 to the planar array 10.
  • planar array 12 is similar to the planar array 10 except that the radiating guides 23 of the former array are orthogonal to those of the latter.
  • planar array 12 includes two feed guides 21a, 21b fed, respectivcly, by waveguides 14, 15.
  • the radiating slots (unnumbered) of planar array 12 are arranged between the radiating guides 23 so as to form an approximate parallelogram which is a mirror image (partially illustrated by dotted line 2) of the approximate parallelogram (dotted line 1) formed by the radiating slots 24 of array 10. That is to say the approximate parallelogram shape formed by the radiating slots in array 12 is the parallelogram of array 16 reversed or flipped over.
  • planar array 10 radiates energy in a conventional manner. That is, when the radio frequency switch 16 is actuated so that energy passes through waveguide 13 to feed guide 21, such energy is distributed among the various radiating guides 23 and is radiated through the radiating slots 24.
  • the resultant of the energy from the radiating slots 24 is a beam, the inclination of which to the plane of the planar array 10 and the shape of which is dependent on the number and disposition of the radiating slots 24.
  • the polarization of the energy in the main beam radiated from the planar array 10 is, however, always in a plane substantially parallel to the radiating guides 23 of that array although the polarization of energy in the sidelobes may not necessarily be so polarized.
  • planar array 12 When the planar array 12 is energized from eith r Waveguide 14 or 15, a beam is radiated in either one of two directions, depending upon which of the two waveguides is energized. Since the energy propagated from the planar array 12 must pass between the radiating guides 23 of planar array 10 and since, as noted hereinbefore, the spacing between adjacent ones of the radiating guides 23 of planar array 10 is less than one-half of the wavelength of the frequency of such radiated energy, it follows that the radiating guides 23 of planar array 10 affect any energy radiated from planar array 12. That is, the radiating guides 23 of planar array 10 selectively attenuate portions of the energy radiated from planar array 12 in accordance with the polarization of such energy.
  • the antenna just described is intended to be energized so as to produce, sequentially, any one of three beams.
  • beams from the planar array 10 are, for practical purposes independent of beams from the planar array 12. That is, since the plane of polarization of energy in any beam from the planar array 10 is in space quadrature with the plane of polarization of energy in any beam from the planar array 12, the beams from the two planar arrays are decoupled from one another even though the two planar arrays are energized simultaneously. It follows, then, that the two planar arrays may be so enc rgized as to form beams simultaneously, if desired, without appreciable cross-talk. Such beams would be particularly useful in a system such as the one described in the application filed November 5, 1963, Serial No. 321,500, by James L. Burrows entitled Doppler Radar System" (which application is assigned to the same assignee as this application).
  • a transmitter 30 (which may be either a conventional continuous wave or pulsed transmitter) is connected to a conventional turnstile junction 32, as, for example, the 'type shown and described in U.S. Patent No. 2,858,535, issued October 28, 1958, entitled Microwave Polarization Apparatus, to produce a circularly polarized micro wave signal in a conventional dual mode transducer 34 which is connected in a known manner to a first and a second transmission line 36, 38.
  • the orthogonal components of the circularly polarized microwave signal are divided by the dual mode transducer 34 so that one component passes down the first transmission line 36 and the other passes down the second transmission line 38.
  • a conventional phase shifter 40 may be inserted in the transmission line 38 so that the phase of the signal appearing at the feed port (here marl-Led A) of a planar array 10 is in time quadrature with the phase of the signal appearing at the corresponding feed port of a planar array 12 (here marked 3
  • the planar arrays 10', 12 are identical with the planar arrays 10, 12 of FIG. 1 except that the distribution of It is evident, however, that 5 lit the radiating slots in the former are similar so that the beams propagated by the two beams arc of the same shape and are coaxial with each other.
  • the energy in the resultant beam from the planar arrays 10', 12 is circularly polarized.
  • the direction of polarization i.e. left hand or right hand may be made to be the same as the direction of polarization of the energy entering the dual mode transducer 34 by adjustment of the phase shifter 40.
  • the contemplated system utilizes passive decoupling means between the transmitter 30 and the receiver 42, in that the turnstile junction 32, once adjusted, performs the function of a conventional duplexer.
  • This advantage is, however, ancillary to the main advantage of the just described system. That is, the use of the double planar array permits precise and stable control of the shape of the propagated beam.
  • radio frequency switches may be incorporated in the system shown in FIG. 2 to permit switching to other feed ports of the arrays 10', 12' whenever it is desired to produce beams in different directions from the beam formed when feed ports A, B are energized.
  • the crosssectional shape of the beams may be changed as desired simply by changing the distribution of the radiating slots in the arrays 10', 12' and that the polarization of the beams may be readily changed from circular polarization of one hand to circular polarization of the other hand or to elliptical polarization of any degree. Since the foregoing and many other changes not mentioned are obvious, it is felt that the invention should not he restricted to the illustrated embodiments, but rather should be limited only by the spirit and scope of the appended claims.
  • an antenna comprising:
  • each such member having radiating slots formed therein;
  • a second planar array having a plurality of parallel, spaced radiating members, each such member having radiating slots formed therein, the radiating members of the second planar array being disposed orthogonal to the radiating members of the first array and the radiating slots of the second array being interposed between the radiating members of the first array;
  • (c) means for sequentially energizing the first and the second planar array to generate the plurality of beams.
  • a microwave antenna for producing a plurality of beams of microwave energy comprising:
  • a second planar array similar to the first planar array, but disposed orthogonally thereto on the side thereof opposite to the side from which the microfirst and the second planar array are disposed to produce Wave energy is radiated; and, substantially plane-polarized energy in spaced quadrature.
  • (-0) means for feeding microwave energy to the first and the second planar array to produce the desired References Clted y Exammel' plurality of beams of microwave energy. 5 UNITED STATES PATENTS 3.

Landscapes

  • Variable-Direction Aerials And Aerial Arrays (AREA)

Description

April 19, 1966 M. DIAMOND MICROWAVE ANTENNA '& Sheets-Sheet 1 Filed Feb. 17, 1964 FIG.
INVENTOR. MAURICE DRAMOND [:T ORNEY April 1966 M. DIAMOND 3,247,512
MICROWAVE ANTENNA Filed Feb. 17, 1964 2 Sheets-Sheet 2 T NS IL To TRANSMITTER UR T E RECEIVER UTILIZATION JUNCTION q CIRCUITS FIG. 2
INVENTOR. MAURICE DIAMOND A RN Y United States Patent 0 3,247,512 MICROWAVE ANTENNA Maurice Diamond, Framingham, Mass., assignoito Laboratory for Electronics, Inc., Boston, Mass., at corporation of Delaware Filed Feb. 17, 1964, Ser. No. 345,222 4 Claims. (Cl. 343-9) This invention pertains generally to antennas and particularly to an antenna for radiating high frequency electromagnetic energy in any one of a plurality of beams.
Airborne Doppler radar systems are known which cmploy an antenna for transmitting directional beams of microwave energy toward the surface of the earth and receiving Doppler shifted signals reflected therefrom. One known type of such antenna is the so-called Luneberg lens antenna, wherein a wide angle dielectric lens co operates with a number of feed horns to produce the desired beams. Another known type of antenna which pro duces a plurality of directional beams is the so-called planar antenna, as for example, the antenna described in the application for patent (assigned to the same assignee as this application) Serial No. 193,717, entitled Microwave Antenna, filed May 10, 1962, in the name of Alan J. Simmons, wherein a plurality of parallel sections of: waveguides support a plurality of radiating slots to produce a beam when such sections are energized with microwave energy.
While both the justmentioned types of antennas are satisfactory when it is desired to produce pencil beams (meaning beams having a circular cross-section), neither type may be used when it is desired to produce beams of other shapes. Further, neither type is well adapted to the simultaneous transmission of more than one beam or to changes in the polarization of the energy in the propagated beam or beams.
Therefore, it is a primary object of this invention to provide an improved beam forming antenna which is adapted to produce one or more independent beams of microwave energy at the same time.
Another object of this invention is to provide an improved beam forming antenna which is adapted to produce beams of microwave energy of diifering cross-sectional shapes.
Another object of this invention is to provide an improved beam forming antenna which is adapted to produce beams of microwave energy wherein the polarization of such energy may be easily controlled.
Still another object of this invention is to provide an improved beam forming antenna which accomplishes the foregoing objects with compact, known elements.
These and other objects of this invention are accomplished by an antenna comprising a first and second planar array orthogonally disposed with respect to each other. The beam forming radiating elements of the first such array are preferably disposed parallel to each other and spaced from each other to allow the radiating slots in the radiating elements of the second such array to be disposed between the radiating elements of the first. The two arrays may be energized either simultaneously or sequentially making it possible to form, at any time, either a single beam, or a plurality of beams, and to control the polarization thereof. Further the shape of the beams may be controlled within wide limits by changing the arrangelit Gil
Patented Apr. 19, 1956 ment of the radiating slots in each array or by changing the manner in which each radiating element is energized. For a more complete understanding of this invention reference is now made to the drawings illustrating the invention and to the following detailed description.
In the drawings:
FIG. 1 is a simplified view taken from below of an antenna according to the invention (a portion of the structure being broken away in order to illustrate normally hidden elements), which antenna is adapted to provide three elliptical beams symmetrically disposed with respect to a line perpendicular to the plane of each array; and
FIG. 2 is a block diagram of a system according to an alternative embodiment of the invention.
Referring now to FIG. 1, it may be seen that one embodiment of an antenna according to this invention comprises a first planar array 10 and a second planar array 12 preferably in contact with one another and energized through wave guides 13, 14, 15. The latter elements, in turn, are connected through a radio frequency switch 16 of any conventional design to a transmitter/receiver 17. Signals out of the receiver portion of the last named element are, when the antenna is a portion of a Doppler radar system, fed to a tracker unit 18 and thence to an indicator 19.
The planar array 10 consists of a feed guide 21 integrally attached to and extending from the wave guide 13 and a plurality of radiating guides 23 affixed to the feed guide 21 as shown. The radiating guides 23 are parallel to each other and spaced as shown, there being a convcntional matched load (unnumbered) affixed to the free end of each radiating guide 23 to prevent unwanted reflections. It is here noted that the spacing between adjacent radiating guides 23 is not critical, so long as such spacing is less than one half wavelength of the frequency of the signal radiated from the planar array 12. Further it is noted that the radiating slots 24 in the radiating guides 23 are arranged in the form of an approximate parallelogram as shown by the dotted line 1 to produce an elliptical beam when electromagnetic energy is passed through waveguide 13 to the planar array 10.
The planar array 12 is similar to the planar array 10 except that the radiating guides 23 of the former array are orthogonal to those of the latter. In addition, planar array 12 includes two feed guides 21a, 21b fed, respectivcly, by waveguides 14, 15. Still further, the radiating slots (unnumbered) of planar array 12 (which correspond here to the radiating slots 24 in array 10) are arranged between the radiating guides 23 so as to form an approximate parallelogram which is a mirror image (partially illustrated by dotted line 2) of the approximate parallelogram (dotted line 1) formed by the radiating slots 24 of array 10. That is to say the approximate parallelogram shape formed by the radiating slots in array 12 is the parallelogram of array 16 reversed or flipped over. The array 12 is energized from either waveguide 14 or waveguide 15 depending on the condition of the radio frequency switch In operation, planar array 10 radiates energy in a conventional manner. That is, when the radio frequency switch 16 is actuated so that energy passes through waveguide 13 to feed guide 21, such energy is distributed among the various radiating guides 23 and is radiated through the radiating slots 24. The resultant of the energy from the radiating slots 24 is a beam, the inclination of which to the plane of the planar array 10 and the shape of which is dependent on the number and disposition of the radiating slots 24. Further, when the radiating slots 24 are disposed as shown, the polarization of the energy in the main beam radiated from the planar array 10 is, however, always in a plane substantially parallel to the radiating guides 23 of that array although the polarization of energy in the sidelobes may not necessarily be so polarized.
When the planar array 12 is energized from eith r Waveguide 14 or 15, a beam is radiated in either one of two directions, depending upon which of the two waveguides is energized. Since the energy propagated from the planar array 12 must pass between the radiating guides 23 of planar array 10 and since, as noted hereinbefore, the spacing between adjacent ones of the radiating guides 23 of planar array 10 is less than one-half of the wavelength of the frequency of such radiated energy, it follows that the radiating guides 23 of planar array 10 affect any energy radiated from planar array 12. That is, the radiating guides 23 of planar array 10 selectively attenuate portions of the energy radiated from planar array 12 in accordance with the polarization of such energy. Energy polarized in a plane Orthogonal to the radiating guides 23 of planar array 10 is not attenuated, whereas energy polarized in a plane parallel to the radiating guides 23 is, for all practical purposes, completely attenuated. The result then is that the energy in any beam originating at planar array 12 is polarized in a direction orthogonal to the radiating guides 23 of planar array 10.
It should be noted here that the antenna just described is intended to be energized so as to produce, sequentially, any one of three beams. beams from the planar array 10 are, for practical purposes independent of beams from the planar array 12. That is, since the plane of polarization of energy in any beam from the planar array 10 is in space quadrature with the plane of polarization of energy in any beam from the planar array 12, the beams from the two planar arrays are decoupled from one another even though the two planar arrays are energized simultaneously. It follows, then, that the two planar arrays may be so enc rgized as to form beams simultaneously, if desired, without appreciable cross-talk. Such beams would be particularly useful in a system such as the one described in the application filed November 5, 1963, Serial No. 321,500, by James L. Burrows entitled Doppler Radar System" (which application is assigned to the same assignee as this application).
Referring now to FIG. 2, an arrangement for utilizing the antenna illustrated in FIG. 1 to produce a beam of circularly polarized microwave energy is shown. Thus, a transmitter 30 (which may be either a conventional continuous wave or pulsed transmitter) is connected to a conventional turnstile junction 32, as, for example, the 'type shown and described in U.S. Patent No. 2,858,535, issued October 28, 1958, entitled Microwave Polarization Apparatus, to produce a circularly polarized micro wave signal in a conventional dual mode transducer 34 which is connected in a known manner to a first and a second transmission line 36, 38. As is known, the orthogonal components of the circularly polarized microwave signal are divided by the dual mode transducer 34 so that one component passes down the first transmission line 36 and the other passes down the second transmission line 38. A conventional phase shifter 40 may be inserted in the transmission line 38 so that the phase of the signal appearing at the feed port (here marl-Led A) of a planar array 10 is in time quadrature with the phase of the signal appearing at the corresponding feed port of a planar array 12 (here marked 3 The planar arrays 10', 12 are identical with the planar arrays 10, 12 of FIG. 1 except that the distribution of It is evident, however, that 5 lit the radiating slots in the former are similar so that the beams propagated by the two beams arc of the same shape and are coaxial with each other.
It will be apparent now that the energy in the resultant beam from the planar arrays 10', 12 is circularly polarized. The direction of polarization, i.e. left hand or right hand may be made to be the same as the direction of polarization of the energy entering the dual mode transducer 34 by adjustment of the phase shifter 40.
Since energy reflected back to the planar arrays 10', 12, is, in the normal case, reversed 180 in polarity, such energy recombines in the dual mode transducer 34 to produce energy having a circular polarization opposite to the direction of polarization of the energy from the transmitter 30. The received energy then passes through the turnstile junction 32 to a receiver 42 and thence to utilization circuits, as the tracker unit 18 of FIG. 1.
It may be seen from the foregoing that the contemplated system utilizes passive decoupling means between the transmitter 30 and the receiver 42, in that the turnstile junction 32, once adjusted, performs the function of a conventional duplexer. This advantage is, however, ancillary to the main advantage of the just described system. That is, the use of the double planar array permits precise and stable control of the shape of the propagated beam.
It will be immediately evident to those having skill in the art that conventional radio frequency switches may be incorporated in the system shown in FIG. 2 to permit switching to other feed ports of the arrays 10', 12' whenever it is desired to produce beams in different directions from the beam formed when feed ports A, B are energized. Further, it will be evident that the crosssectional shape of the beams may be changed as desired simply by changing the distribution of the radiating slots in the arrays 10', 12' and that the polarization of the beams may be readily changed from circular polarization of one hand to circular polarization of the other hand or to elliptical polarization of any degree. Since the foregoing and many other changes not mentioned are obvious, it is felt that the invention should not he restricted to the illustrated embodiments, but rather should be limited only by the spirit and scope of the appended claims.
I claim:
1. In an airborne Doppler navigator having a plurality of beams of electromagnetic energy, each illuminating a different area of the terrain beneath an aircraft, an antenna, comprising:
(a) a first planar array having a plurality of parallel,
spaced radiating members, each such member having radiating slots formed therein;
(h) a second planar array having a plurality of parallel, spaced radiating members, each such member having radiating slots formed therein, the radiating members of the second planar array being disposed orthogonal to the radiating members of the first array and the radiating slots of the second array being interposed between the radiating members of the first array; and,
(c) means for sequentially energizing the first and the second planar array to generate the plurality of beams.
2. A microwave antenna for producing a plurality of beams of microwave energy comprising:
(a) a first planar array including a plurality of radiating waveguides disposed adjacent to one another in a parallel relationship, the distance between each pair of such waveguides being less than one-half the Wavelength of the microwave energy radiated therefrom;
(b) a second planar array, similar to the first planar array, but disposed orthogonally thereto on the side thereof opposite to the side from which the microfirst and the second planar array are disposed to produce Wave energy is radiated; and, substantially plane-polarized energy in spaced quadrature. (-0) means for feeding microwave energy to the first and the second planar array to produce the desired References Clted y Exammel' plurality of beams of microwave energy. 5 UNITED STATES PATENTS 3. A microwave antenna as in claim 2 wherein the first and the second planar array are in substantially oontinuous electrical contact with one another at the over- 0 ms y lappmg thereof' CHESTER L. JUSTUS, Primary Examiner.
4. A microwave antenna as in claim 3 wherein the m radiating elements in the radiating waveguides of the R BENNETT, 1483mm"! Exflmmeli

Claims (1)

1. IN AN AIRBORNE DOPPLER NAVIGATOR HAVING A PLURALITY OF BEAMS OF ELECTROMAGNETIC ENERGY, EACH ILLUMINATING A DIFFERENT AREA OF THE TERRAIN BENEATH AN AIRCRAFT, AN ANTENNA, COMPRISING: (A) A FIRST PLANAR ARRAY HAVING A PLURALITY OF PARALLEL, SPACED RADIATING MEMBERS, EACH SUCH MEMBER HAVING RADATING SLOTS FORMED THEREIN; (B) A SECOND PLANAR ARRAY HAVING A PLURALITY OF PARALLEL, SPACED RADIATING MEMBERS, EACH SUCH MEMBER HAVING RADIATING SLOTS FORMED THEREIN, THE RADIATING MEMBERS OF THE SECOND PLANAR ARRAY BEING DISPOSED ORTHOGONAL TO THE RADIATING MEMBERS OF THE FIRST ARRAY AND THE RADIATING SLOTS OF THE SECOND ARRAY BEING INTERPOSED BETWEEN THE RADIATING MEMBERS OF THE FIRST ARRAY; AND, (C) MEANS FOR SEQUENTIALLY ENERGIZING THE FIRST AND THE SECOND PLANAR ARRAY TO GENERATE THE PLURALITY OF BEAMS.
US345222A 1964-02-17 1964-02-17 Microwave antenna Expired - Lifetime US3247512A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US345222A US3247512A (en) 1964-02-17 1964-02-17 Microwave antenna

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US345222A US3247512A (en) 1964-02-17 1964-02-17 Microwave antenna

Publications (1)

Publication Number Publication Date
US3247512A true US3247512A (en) 1966-04-19

Family

ID=23354102

Family Applications (1)

Application Number Title Priority Date Filing Date
US345222A Expired - Lifetime US3247512A (en) 1964-02-17 1964-02-17 Microwave antenna

Country Status (1)

Country Link
US (1) US3247512A (en)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3471857A (en) * 1967-05-24 1969-10-07 Singer General Precision Planar array antenna arrangements
US3518689A (en) * 1967-03-06 1970-06-30 North American Rockwell Frequency-sensitive cross-scanning antenna
FR2069945A1 (en) * 1969-12-12 1971-09-10 Labo Cent Telecommunicat
US3623111A (en) * 1969-10-06 1971-11-23 Us Navy Multiaperture radiating array antenna
FR2117831A1 (en) * 1970-12-18 1972-07-28 Toyota Motor Co Ltd
FR2497002A1 (en) * 1980-12-23 1982-06-25 United Technologies Corp MULTIMODE DIRECTIVE ANTENNA
JPS61127202A (en) * 1984-11-27 1986-06-14 Nec Corp Waveguide type power distributer
US4958166A (en) * 1988-08-22 1990-09-18 General Dynamics Corp., Pomona Division Amplitude monopulse slotted array
US5923290A (en) * 1995-03-31 1999-07-13 Kabushiki Kasiha Toshiba Array antenna apparatus
EP2869396B1 (en) * 2013-11-04 2020-07-22 Thales Power divider including a T-coupler in the E-plane, radiating network and antenna including such a radiating network
USD1113876S1 (en) * 2020-04-24 2026-02-17 Battelle Memorial Institute Radio frequency aperture

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2851681A (en) * 1955-03-16 1958-09-09 Sperry Rand Corp Diversity polarization radar system
US2865020A (en) * 1956-08-13 1958-12-16 Gen Precision Lab Inc Aircraft vertical velocity and drift angle measuring system

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2851681A (en) * 1955-03-16 1958-09-09 Sperry Rand Corp Diversity polarization radar system
US2865020A (en) * 1956-08-13 1958-12-16 Gen Precision Lab Inc Aircraft vertical velocity and drift angle measuring system

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3518689A (en) * 1967-03-06 1970-06-30 North American Rockwell Frequency-sensitive cross-scanning antenna
US3471857A (en) * 1967-05-24 1969-10-07 Singer General Precision Planar array antenna arrangements
US3623111A (en) * 1969-10-06 1971-11-23 Us Navy Multiaperture radiating array antenna
FR2069945A1 (en) * 1969-12-12 1971-09-10 Labo Cent Telecommunicat
FR2117831A1 (en) * 1970-12-18 1972-07-28 Toyota Motor Co Ltd
FR2497002A1 (en) * 1980-12-23 1982-06-25 United Technologies Corp MULTIMODE DIRECTIVE ANTENNA
US4376281A (en) * 1980-12-23 1983-03-08 United Technologies Corporation Multimode array antenna
JPS61127202A (en) * 1984-11-27 1986-06-14 Nec Corp Waveguide type power distributer
US4958166A (en) * 1988-08-22 1990-09-18 General Dynamics Corp., Pomona Division Amplitude monopulse slotted array
US5923290A (en) * 1995-03-31 1999-07-13 Kabushiki Kasiha Toshiba Array antenna apparatus
EP2869396B1 (en) * 2013-11-04 2020-07-22 Thales Power divider including a T-coupler in the E-plane, radiating network and antenna including such a radiating network
USD1113876S1 (en) * 2020-04-24 2026-02-17 Battelle Memorial Institute Radio frequency aperture

Similar Documents

Publication Publication Date Title
US4868574A (en) Electronically scanned radar system
US3305867A (en) Antenna array system
US3448450A (en) Pulse radar for determining angles of elevation
US4129872A (en) Microwave radiating element and antenna array including linear phase shift progression angular tilt
US4845506A (en) Antenna system
US5283587A (en) Active transmit phased array antenna
US3906508A (en) Multimode horn antenna
US3623114A (en) Conical reflector antenna
EP0126626B1 (en) Resonant waveguide aperture manifold
US3281851A (en) Dual mode slot antenna
US4063243A (en) Conformal radar antenna
US3247512A (en) Microwave antenna
US4348679A (en) Multi-mode dual-feed array radar antenna
US5337058A (en) Fast switching polarization diverse radar antenna system
US3419870A (en) Dual-plane frequency-scanned antenna array
US3430242A (en) Bidirectional electronically scanned antenna system
US3646559A (en) Phase and frequency scanned antenna
US3270336A (en) Eliminating multiple responses in a grating lobe antenna array
US3484784A (en) Antenna array duplexing system
US4376281A (en) Multimode array antenna
US3508275A (en) Doppler array with interleaved transmitting and receiving slotted waveguides
US3093826A (en) Antenna system
US4091387A (en) Beam forming network
GB2356096A (en) Radar antenna system
US3636563A (en) Aerial arrangements