US2430568A - Antenna system - Google Patents
Antenna system Download PDFInfo
- Publication number
- US2430568A US2430568A US447891A US44789142A US2430568A US 2430568 A US2430568 A US 2430568A US 447891 A US447891 A US 447891A US 44789142 A US44789142 A US 44789142A US 2430568 A US2430568 A US 2430568A
- Authority
- US
- United States
- Prior art keywords
- plane
- parabolic
- wires
- overlapping
- radiation
- 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
Links
Images
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q3/00—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system
- H01Q3/24—Arrangements 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 orientation by switching energy from one active radiating element to another, e.g. for beam switching
- H01Q3/245—Arrangements 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 orientation by switching energy from one active radiating element to another, e.g. for beam switching in the focal plane of a focussing device
Definitions
- This invention relates to devices for radiating electromagnetic waves and more particularly for radiating such waves alternately in different directions and with variable directivity.
- Waves having lengths of the order of '50 centimeters and less may be concentrated conveniently by means of parabolic reflectors.
- the directivity of such arrangements is a function of the particular design and is not ordinarily readily Variable. Also when it is necessary to change the direction of maximum radiation, the structure must be moved bodily.
- Another object is to provide improved radiating means of variable directivity.
- FIG. 1 is a perspective View of a radiating structure embodying the invention
- Figs. 2 and 3 are perspective representations of radiation patterns which may be produced by the structure shown in Fig, 1
- Fig. 4 is a schematic perspective View of a system for energizing the device of Fig. 1.
- a rectangular plate or grid l of conductive material supports four ribs 3 which are parabolically curved and located in positions defining the traces of an intersection of two parabolic cylinders at right angles to each other.
- a plurality of wires 5 and ll! of conductive material are stretched at spaced intervals between the ribs 3 in positions corresponding to those of elements of respective parabolic cylindrical surfaces.
- Wave guides 1 and 3 extend through the member I at each side of its center and substantially at right angles thereto and terminate a relatively short distance from a plate 9 of conductive material supported preferably at the center of the mouth of the parabolic structure.
- the plate 9 may be fiat or dished; if it is flat, it should be positioned at the focus of the parabola; if dished, it should be so placed that it reflects energy from the wave guides 1 and 8 in such a way as to simulate a source located at the focus.
- an ultra high frequency oscillator energizes an antenna l3 which is supported at the end of a wave guide, l5.
- the antenna l3 may be arranged to be rotatable from the vertical position t the horizontal position as indicated by the dotted line, in order to rotate correspondingly the .plane of polarization of the energy transmitted through the wave guide l5.
- the wave guide I5 is bifurcated a short distance from the oscillator II to form the two guides I and 8.
- disks 1 l and IQ of conductive material are supported in the respective guides in planes at right angles to each other On a shaft 2
- is continuousl rotated by a motor 23.
- the plate 9 In the operation of the device, energy conducted through one of the wave guides l and 8 strikes the plate 9 and is reflected to the surfaces defined by the wires 5.
- the plate 9 thus acts like a source of energy substantially in the plane of the focus of the parabolic reflector and slightly to one side of the center, depending on which wave guide is delivering the energy.
- overlapping radiation lobes may be established alternately, as illustrated in Figs. 2 and 3 which are hereinafter described.
- the invention has been described as a device for radiating directively electromagnetic waves alternately in overlapping lobes and with controllable directivity.
- a reflector is arranged at or near the focus of a larger parabolic reflector. Energy is transmitted through a wave guide to the smaller reflector and thence to the parabolic reflector, producing a beam, or lobe of radiation.
- overlapping beams are produced.
- plane polarized waves are used and the parabolic reflector is made of groups of parallel wires arranged to concentrate the radiation predominantly in planes lying parallel to the plane of wavepolarization, which may be rotated to give either broad or sharp overlapping.
- a device for radiating electromagnetic waves including two groups of conductive wires disposed in positions corresponding respectively to the elements of a pair of intersecting parabolic cylinders, a plate of conductive material positioned within the space defined by the intersection of said cylinders, and wave guide means terminating near said plate and directed so that energy transmitted through said Wave guide means is reflected by said plate to said conductive wires.
- a system for alternately establishing overlapping radiation lobes comprising two coaxial spaced reflectors, one of said reflectors including two groups of conductive wiresin positions corresponding to the elements of a pair of intersecting parabolic cylinders, the wires of one of said groups being at right angles to those of the other of said groups, and a plurality of separate wave guide means extending through said parabolic cylindrical reflector with their axes parallel to the axis of said reflectors and terminating near the surface of the other of said reflectors, whereby alternate energization of said wave guides in one plane of polarization produces radiation lobes overlapping throughout a relatively small angle,
Landscapes
- Aerials With Secondary Devices (AREA)
- Variable-Direction Aerials And Aerial Arrays (AREA)
Description
Nov, 11, 1947. w. D. HERSl -I BERGER ANTENNA SYSTEM Zinnentor HBERGER F IMLIAMDIE'RS :2 II" 5: v
Filed June 22, 1942 Patented Nov. 11, 1947 2,430,568 ANTENNA sYs'rEM William D. Hershberger, Haddonfield, N. 5., assignor to Radio Corporation of America, a corporation of Delaware Application June 224, 1942, Serial No. 447,891
2 Claims.
This invention relates to devices for radiating electromagnetic waves and more particularly for radiating such waves alternately in different directions and with variable directivity.
Waves having lengths of the order of '50 centimeters and less may be concentrated conveniently by means of parabolic reflectors. The directivity of such arrangements is a function of the particular design and is not ordinarily readily Variable. Also when it is necessary to change the direction of maximum radiation, the structure must be moved bodily.
It is an object of this invention to provide an improved means for radiating short electromagnetic waves alternately in different directions without the necessity of mechanically moving said means.
Another object is to provide improved radiating means of variable directivity.
These and other and incidental objects will become apparent to those skilled in the art upon consideration of the following description, with reference to the accompanying drawing, of which Fig. 1 is a perspective View of a radiating structure embodying the invention, Figs. 2 and 3 are perspective representations of radiation patterns which may be produced by the structure shown in Fig, 1, and Fig. 4 is a schematic perspective View of a system for energizing the device of Fig. 1.
Referring to Fig. 1, a rectangular plate or grid l of conductive material supports four ribs 3 which are parabolically curved and located in positions defining the traces of an intersection of two parabolic cylinders at right angles to each other. A plurality of wires 5 and ll! of conductive material are stretched at spaced intervals between the ribs 3 in positions corresponding to those of elements of respective parabolic cylindrical surfaces. Wave guides 1 and 3 extend through the member I at each side of its center and substantially at right angles thereto and terminate a relatively short distance from a plate 9 of conductive material supported preferably at the center of the mouth of the parabolic structure.
The plate 9 may be fiat or dished; if it is flat, it should be positioned at the focus of the parabola; if dished, it should be so placed that it reflects energy from the wave guides 1 and 8 in such a way as to simulate a source located at the focus.
Referring to Fig. 4, an ultra high frequency oscillator, generally designated in the drawing by the block II, energizes an antenna l3 which is supported at the end of a wave guide, l5. The antenna l3 may be arranged to be rotatable from the vertical position t the horizontal position as indicated by the dotted line, in order to rotate correspondingly the .plane of polarization of the energy transmitted through the wave guide l5. The wave guide I5 is bifurcated a short distance from the oscillator II to form the two guides I and 8.
To provide alternate transmission through the wave guides land 8, disks 1 l and IQ of conductive material are supported in the respective guides in planes at right angles to each other On a shaft 2|. The shaft 2| is continuousl rotated by a motor 23.
In the operation of the device, energy conducted through one of the wave guides l and 8 strikes the plate 9 and is reflected to the surfaces defined by the wires 5. The plate 9 thus acts like a source of energy substantially in the plane of the focus of the parabolic reflector and slightly to one side of the center, depending on which wave guide is delivering the energy. By supplying energy to first one and then the other of the guides 1 and 8, overlapping radiation lobes may be established alternately, as illustrated in Figs. 2 and 3 which are hereinafter described.
- The ability of spaced conductors to reflect electromagnetic waves having wavelengths greater than 21! times the conductor spacing depends upon the polarization of the waves striking the.
conductors. If the electric vector lies in a direction substantially parallel to the wires, reflection occurs. If the electric vector lies at right angles to the wires, very little reflection takes place. This phenomenon is utilized in the structure described above by employing plane polarized waves. If the plane of polarization is horizontal, the horizontally extending wires 5 (Fig. 1) function as elements of a parabolic cylindrical reflector lying horizontally, and the vertically disposed wires ID are of no effect. The radiation is thereby concentrated in relatively wide, flat lobes, with a considerable angle a of overlapping, as illustrated in Fig. 2. Conversely, if the plane of polarization is vertical, the radiation lobes are narrow and high, and overlap only within a relatively small angle, as shown in Fig. 3. Thus it is possible to change the angular width of the overlapping portion of the two radiation lobes by merely rotating the plane of polarization of the wave through an angle of ninety degrees.
Thus the invention has been described as a device for radiating directively electromagnetic waves alternately in overlapping lobes and with controllable directivity. A reflector is arranged at or near the focus of a larger parabolic reflector. Energy is transmitted through a wave guide to the smaller reflector and thence to the parabolic reflector, producing a beam, or lobe of radiation. By employing two or more wave guides directed at points ofi the center of the smaller reflector, overlapping beams are produced. In order to control the amount of the overlap, plane polarized waves are used and the parabolic reflector is made of groups of parallel wires arranged to concentrate the radiation predominantly in planes lying parallel to the plane of wavepolarization, which may be rotated to give either broad or sharp overlapping.
I claim as my invention:
1. A device for radiating electromagnetic waves including two groups of conductive wires disposed in positions corresponding respectively to the elements of a pair of intersecting parabolic cylinders, a plate of conductive material positioned within the space defined by the intersection of said cylinders, and wave guide means terminating near said plate and directed so that energy transmitted through said Wave guide means is reflected by said plate to said conductive wires.
2. A system for alternately establishing overlapping radiation lobes comprising two coaxial spaced reflectors, one of said reflectors including two groups of conductive wiresin positions corresponding to the elements of a pair of intersecting parabolic cylinders, the wires of one of said groups being at right angles to those of the other of said groups, and a plurality of separate wave guide means extending through said parabolic cylindrical reflector with their axes parallel to the axis of said reflectors and terminating near the surface of the other of said reflectors, whereby alternate energization of said wave guides in one plane of polarization produces radiation lobes overlapping throughout a relatively small angle,
and alternate energization of said wave guides in a plane of polarization at right angles to said first-mentioned plane produces radiation lobes overlapping throughout a relatively wide angle.
WILLIAM D. HERSHBERGER.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PA I'EN I S Number Name Date 2,206,923 Southworth July 9, 1940 2,095,083 Renatus Oct. 5, 1937 2,270,314 Kraus Jan. 20, 1942 2,232,559 Rice Feb. 18, 1941 2,002,181 Ilberg May 21, 1935 1,299,397 Conklin et a1. Apr. 1, 1919 2,217,321 Runge et al. Oct. 8, 1940 FOREIGN PATENTS Number Country Date 804,966 France Aug. 17, 1936 582,007 Germany Aug. 7, 1933
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US447891A US2430568A (en) | 1942-06-22 | 1942-06-22 | Antenna system |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US447891A US2430568A (en) | 1942-06-22 | 1942-06-22 | Antenna system |
Publications (1)
Publication Number | Publication Date |
---|---|
US2430568A true US2430568A (en) | 1947-11-11 |
Family
ID=23778156
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US447891A Expired - Lifetime US2430568A (en) | 1942-06-22 | 1942-06-22 | Antenna system |
Country Status (1)
Country | Link |
---|---|
US (1) | US2430568A (en) |
Cited By (24)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2505424A (en) * | 1946-08-27 | 1950-04-25 | Tomlinson I Moseley | Radar scanner antenna feed |
US2534716A (en) * | 1945-10-08 | 1950-12-19 | Emmett L Hudspeth | Inflatable radar reflector buoy |
US2545472A (en) * | 1944-07-31 | 1951-03-20 | Kline Morris | Radio system |
US2570197A (en) * | 1949-06-16 | 1951-10-09 | John I Bohnert | Dual purpose antenna |
US2572088A (en) * | 1945-12-22 | 1951-10-23 | Sperry Corp | Ultra high frequency coded transmitter system utilizing stored energy received by the system |
US2603749A (en) * | 1946-04-08 | 1952-07-15 | Bell Telephone Labor Inc | Directive antenna system |
US2638547A (en) * | 1945-09-18 | 1953-05-12 | Us Navy | Electromagnetic wave controlling apparatus |
US2683855A (en) * | 1949-11-30 | 1954-07-13 | Raytheon Mfg Co | Frequency converter |
US2735982A (en) * | 1956-02-21 | Radio frequency power comparator | ||
US2820214A (en) * | 1949-05-28 | 1958-01-14 | John P O'neill | Sonar transducers |
US2913723A (en) * | 1956-01-23 | 1959-11-17 | Csf | Variable pattern radar aerial |
US2922160A (en) * | 1950-04-27 | 1960-01-19 | Lester C Van Atta | Split paraboloidal reflector |
US2926349A (en) * | 1957-03-29 | 1960-02-23 | Jack H Jensen | Corner reflector antenna |
US2935745A (en) * | 1958-03-12 | 1960-05-03 | Melpar Inc | Air navigation antenna device |
US2940078A (en) * | 1956-08-07 | 1960-06-07 | Hollandse Signaalapparaten Bv | Directive aerial |
US2942264A (en) * | 1958-03-31 | 1960-06-21 | Ryan Aeronautical Co | Coaxial antenna |
US2942265A (en) * | 1958-03-31 | 1960-06-21 | Ryan Aeronautical Co | Enclosed coaxial antenna |
US2982961A (en) * | 1957-03-20 | 1961-05-02 | Calvin C Jones | Dual feed antenna |
US2982962A (en) * | 1953-08-19 | 1961-05-02 | Gen Railway Signal Co | Antenna system |
US3045239A (en) * | 1949-12-14 | 1962-07-17 | Westinghouse Electric Corp | Parabolic feed system |
US3085204A (en) * | 1958-09-03 | 1963-04-09 | Carlyle J Sletten | Amplitude scanning |
US3096519A (en) * | 1958-04-14 | 1963-07-02 | Sperry Rand Corp | Composite reflector for two independent orthogonally polarized beams |
US3173145A (en) * | 1962-12-17 | 1965-03-09 | Ite Circuit Breaker Ltd | Conical scanning produced by a.m. modulator feeding plural horns with reflector |
WO2000021158A1 (en) * | 1998-10-06 | 2000-04-13 | Hittite Microwave Corporation | Miniature skewed beam horn antenna |
Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1299397A (en) * | 1917-05-12 | 1919-04-01 | Oliver Earle Conkin | Light-projection apparatus. |
DE582007C (en) * | 1933-08-07 | Ernst Gerhard Dr | Arrangement for the emission of several independent and different beam cones of electrical waves | |
US2002181A (en) * | 1930-10-29 | 1935-05-21 | Telefunken Gmbh | Transmitter |
FR804966A (en) * | 1935-04-17 | 1936-11-06 | Telefunken Gmbh | Improvements to transmit and receive antennas for ultra-short directed waves |
US2095083A (en) * | 1934-11-17 | 1937-10-05 | Telefunken Gmbh | Directional antenna system |
US2206923A (en) * | 1934-09-12 | 1940-07-09 | American Telephone & Telegraph | Short wave radio system |
US2217321A (en) * | 1935-06-01 | 1940-10-08 | Telefunken Gmbh | Beam antenna |
US2232559A (en) * | 1936-01-29 | 1941-02-18 | Gen Electric | Short wave radio transmitter |
US2270314A (en) * | 1940-01-31 | 1942-01-20 | John D Kraus | Corner reflector antenna |
-
1942
- 1942-06-22 US US447891A patent/US2430568A/en not_active Expired - Lifetime
Patent Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE582007C (en) * | 1933-08-07 | Ernst Gerhard Dr | Arrangement for the emission of several independent and different beam cones of electrical waves | |
US1299397A (en) * | 1917-05-12 | 1919-04-01 | Oliver Earle Conkin | Light-projection apparatus. |
US2002181A (en) * | 1930-10-29 | 1935-05-21 | Telefunken Gmbh | Transmitter |
US2206923A (en) * | 1934-09-12 | 1940-07-09 | American Telephone & Telegraph | Short wave radio system |
US2095083A (en) * | 1934-11-17 | 1937-10-05 | Telefunken Gmbh | Directional antenna system |
FR804966A (en) * | 1935-04-17 | 1936-11-06 | Telefunken Gmbh | Improvements to transmit and receive antennas for ultra-short directed waves |
US2217321A (en) * | 1935-06-01 | 1940-10-08 | Telefunken Gmbh | Beam antenna |
US2232559A (en) * | 1936-01-29 | 1941-02-18 | Gen Electric | Short wave radio transmitter |
US2270314A (en) * | 1940-01-31 | 1942-01-20 | John D Kraus | Corner reflector antenna |
Cited By (24)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2735982A (en) * | 1956-02-21 | Radio frequency power comparator | ||
US2545472A (en) * | 1944-07-31 | 1951-03-20 | Kline Morris | Radio system |
US2638547A (en) * | 1945-09-18 | 1953-05-12 | Us Navy | Electromagnetic wave controlling apparatus |
US2534716A (en) * | 1945-10-08 | 1950-12-19 | Emmett L Hudspeth | Inflatable radar reflector buoy |
US2572088A (en) * | 1945-12-22 | 1951-10-23 | Sperry Corp | Ultra high frequency coded transmitter system utilizing stored energy received by the system |
US2603749A (en) * | 1946-04-08 | 1952-07-15 | Bell Telephone Labor Inc | Directive antenna system |
US2505424A (en) * | 1946-08-27 | 1950-04-25 | Tomlinson I Moseley | Radar scanner antenna feed |
US2820214A (en) * | 1949-05-28 | 1958-01-14 | John P O'neill | Sonar transducers |
US2570197A (en) * | 1949-06-16 | 1951-10-09 | John I Bohnert | Dual purpose antenna |
US2683855A (en) * | 1949-11-30 | 1954-07-13 | Raytheon Mfg Co | Frequency converter |
US3045239A (en) * | 1949-12-14 | 1962-07-17 | Westinghouse Electric Corp | Parabolic feed system |
US2922160A (en) * | 1950-04-27 | 1960-01-19 | Lester C Van Atta | Split paraboloidal reflector |
US2982962A (en) * | 1953-08-19 | 1961-05-02 | Gen Railway Signal Co | Antenna system |
US2913723A (en) * | 1956-01-23 | 1959-11-17 | Csf | Variable pattern radar aerial |
US2940078A (en) * | 1956-08-07 | 1960-06-07 | Hollandse Signaalapparaten Bv | Directive aerial |
US2982961A (en) * | 1957-03-20 | 1961-05-02 | Calvin C Jones | Dual feed antenna |
US2926349A (en) * | 1957-03-29 | 1960-02-23 | Jack H Jensen | Corner reflector antenna |
US2935745A (en) * | 1958-03-12 | 1960-05-03 | Melpar Inc | Air navigation antenna device |
US2942264A (en) * | 1958-03-31 | 1960-06-21 | Ryan Aeronautical Co | Coaxial antenna |
US2942265A (en) * | 1958-03-31 | 1960-06-21 | Ryan Aeronautical Co | Enclosed coaxial antenna |
US3096519A (en) * | 1958-04-14 | 1963-07-02 | Sperry Rand Corp | Composite reflector for two independent orthogonally polarized beams |
US3085204A (en) * | 1958-09-03 | 1963-04-09 | Carlyle J Sletten | Amplitude scanning |
US3173145A (en) * | 1962-12-17 | 1965-03-09 | Ite Circuit Breaker Ltd | Conical scanning produced by a.m. modulator feeding plural horns with reflector |
WO2000021158A1 (en) * | 1998-10-06 | 2000-04-13 | Hittite Microwave Corporation | Miniature skewed beam horn antenna |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US2430568A (en) | Antenna system | |
US2754513A (en) | Antenna | |
US3231892A (en) | Antenna feed system simultaneously operable at two frequencies utilizing polarization independent frequency selective intermediate reflector | |
US2908002A (en) | Electromagnetic reflector | |
US2594409A (en) | Directive antenna | |
US3189907A (en) | Zone plate radio transmission system | |
US2977594A (en) | Spiral doublet antenna | |
US3916416A (en) | 360{20 {0 Azimuth scanning antenna without rotating RF joints | |
US2413085A (en) | Antenna system | |
US2840819A (en) | Reflecting surfaces | |
US2790169A (en) | Antenna | |
US3102265A (en) | New aerial system radiating several beams | |
US2527222A (en) | Scanning antenna | |
ES361117A1 (en) | Bidirectional electronically scanned antenna system | |
US2721263A (en) | Curved throat scan horn for the transmission of electromagnetic energy | |
US2522562A (en) | Antenna system | |
US2991473A (en) | Scanning antenna system for horizontally and vertically polarized waves | |
US2867801A (en) | High frequency radio aerials | |
US3277490A (en) | Broadband conical scan feed for parabolic antennas | |
US2187618A (en) | Radio beacon system | |
US2545472A (en) | Radio system | |
US2570197A (en) | Dual purpose antenna | |
US2888674A (en) | Dual lens antenna for tracking and searching | |
US2656464A (en) | Feed locus for semiparabolic reflector | |
US2942266A (en) | Antenna with means for preventing re-radiation into feed guide |