US2253501A - Resonant antenna system - Google Patents
Resonant antenna system Download PDFInfo
- Publication number
- US2253501A US2253501A US163241A US16324137A US2253501A US 2253501 A US2253501 A US 2253501A US 163241 A US163241 A US 163241A US 16324137 A US16324137 A US 16324137A US 2253501 A US2253501 A US 2253501A
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- cylinder
- chamber
- antenna
- axis
- waves
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q19/00—Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic
- H01Q19/10—Combinations 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
- H01Q19/12—Combinations 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 wherein the surfaces are concave
- H01Q19/13—Combinations 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 wherein the surfaces are concave the primary radiating source being a single radiating element, e.g. a dipole, a slot, a waveguide termination
Description
Aug. 26, 1941. w. L. BARROW v@sormm' AMENNA SYSTEM Filed Sept. 10, 1937 a Sheets-Sheet 1 M A.. TA N m w M Patented Aug. 26, 1941 UNITED STATES PATENT OFFICE 2,253,501 RESONANT ANTENNA SYSTEM Newton, Mass, assignor to Wilmer Lanier Barrow,
Research Corporation,
poration of New York. Application September 10, 1937, Serial No. 163,241 6 Claims. (01. 250-41) The present invention relates to electric communication, and more'particularly to directive radio communication, particularly at ultra-high frequencies, or very short waves.
' An object of the invention is to provide a new and improved electric system for transmitting and receiving intelligence over long distances at ultra-high frequencies.
Another object is to provides, new and improved directive reflector for ultra-high-frequency waves in free space.
.A further object is to provide lanew and improved hollow space-resonant cavity or chamber, particularly a chamber or cavity with cylindrical walls.
Still another object is to utilize the walls of the said space-resonant cavity or chamber to reflect ultra-high frequency waves.
Other and further objects will be described hereinafter and will be particularly pointed out in the appended claims.
The invention wfll now be explained more fully in connection with the accompanyin draw-v ings, in which Fig, 1 is a diagrammatic view of a. transmitting system embodying the invention, the reflector being shown in perspective; Fig. '2 is a diagrammatic plan of the cylindrical reflector, with explanatory symbols; Figs. 3 to 6 are views of modifications; Fig. '7 is a view similar to Fig. 1 of a receiving system; and Fig. 8 is a view of a further modification.
The. radio-transmitting system diagrammatically shown for illustrative purposes in Fig. 1 comprises a radio-frequency oscillator 2, connected with a modulator 3, and which may be modulated in any desired way, as by means of a microphone 4. The modulated output may be fed to a'radio-i'requency amplifier 8 that may be coupled to a circuit 8 having parallel-line output leads l and I2. Sending apparatus will be connected to the biconductor leads in and I2.
The leads l0 and I! are shown connected to an exciting linear rod antenna ll, disposed in and substantially along the axis of a. hollow resonant cylindrical chamber or cavity IQ of substantially circular cross section and the walls of which are constituted of suitable wave-reflecting material, as hereinafter described. The wires l0 and I! are shown extending into the cylinder it through an opening 9. The sending apparatus will be adjusted to excite in the antenna ll modulated ultra-high-frequency electromagnetic waves of a frequency corresponding to the resonant frequency of the chamber. These waves will have rectively radiated out New York, N. Y., a corelectric lines of force substantially parallel to the axis of the cylinder.
The cylinder is may be constituted of sheet metal, such as copper or aluminum, or it may be constituted of other material if its inner wall is otherwise rendered a conductor of the said waves, so as to reflect them. The cylinder may be constituted of a thin-walled dielectric pipe 83 the outer surface of which is constituted of conducting material, such as the metal deposit 84 of Fig. 3. The chief purpose of the dielectric 83 here is to support the metal deposit 84. In some cases, indeed, the cylinder It may be bonstituted wholly of dielectric material, though the eflect is less pronounced than when conducting cylinders are employed. The interior of the cylinder I6, being open to the atmosphere, is naturally a non-conductor.
Modulated electromagnetic waves will be produced by the exciting rod ll.- The walls of the cylinder will, by reflection concentrate the energy upon the linear antenna it to produce linearly polarized standing waves in the chamber or cavity within the cylinder IS. A condition of linearly polarized space resonance will thus be produced in the cylindrical reflector that will materially alter the radiation resistance of the antenna, thus introducing a change in the impedance of the antenna, since it depends upon the nature and the conditions of the medium surrounding the cylindrical-reflector system. The space-resonance effects in the cylinder will depend upon the phase relations between the original and the reflected waves within the cylinder, with the consequent production of a directional pattern for the radiation field. Considerable of the linearly polarized wave energy of the said resonant frequency will he diof the chamber into space through an opening 20, produced by cutting a section out of the cylindrical wall of the chamber or cavity I6, along sides 22 and 24 substantially parallel to the axis of the cylinder. The space-resonance eitects between the antenna and the cylindrical reflector I! increase the strength of the radiation. The cylindrical chamber or cavity thusconstitutes a directive electromagnetic radiator or the electromagnetic energy transmitted to the antenna ll. Not all of the energy is so radiated into space, because of. refiections from the said opening and because of the standing waves that are set up in the cylinder.
Similar action will take place for absorption of such waves, in reception. A modulated space modulating the received and reflected waves.
The detector is coupled to a suitable amplifier 35 that, in turn, is connected to a loud speaker 38.
The term hollow resonant conducting chamber, or its equivalent, will be used in this specifica tion to denote a substantially non-conducting space within a conducting cylindrical shell of substantially circular cross section, the cross dimensionoi the cylindrical shell being about equal to or greater than one-half of the free-space wavelength of the oscillations in the non-conducting space, and the dimension parallel to the axis of the cylindrical shell, which is the dimension substantially parallel to the electric lines of force of the oscillatory waves within the cavity, being of any desired suitable value. In the drawings, this last-named dimension is parallel to the exciting rod H.
The exciting rod I 4 may be supported in the cylinder in any desired way, as by means of an insulating member or members (not shown, for clearness).
The resonant chamber or cavity of the present invention may thus be connected to free outside space, and the antenna H to sending or receiving apparatus, for purposes of either radiating waves into, or absorbing them from, space. The said resonant modulated high-frequency electromagnetic-wave energy may be taken from the antenna l4 and radiated to outside space, or it may be received from outside space and delivered to the antenna H for demodulation by the receiving system.
The invention may also'be employed with concentric or coaxial-line systems, as in Figs. 4 and 5. As illustrated in Fig. 4, one of the wires, as the wire In, may be connected to the tubular portion l8 of the coaxial system, and the other wire, as the wire i2, may be continuously extended axially into the tubular portion l8, as illustrated at IS. The conductor I3 is shown supported in and spaced from the walls of the tube l8 by insulating members l9. The tubular portion I8 will constitute the outer tubular conductor of the coaxial line and the conductor iii the inner conduetor. The members l8 and I3 are connected to the antenna ll in the sameway as the conductors l and I2 01' Fig. 1.
Because of spurious radiation from the para]- lel-wire transmission line, and because energy was taken off from this line to form spurious currents on both the outside and the inside surfaces of the reflector it, which spurious currents was increased, there appeared to caused unwanted radiation, the radiationpattern was somewhat distorted. The coaxial. line l8, it was found to be more satisfactory than the parallel-wire ieeder, illustrated at l0, I2
of Fig. 1; it minimized this spurious radiation and distortion from the feeder line and the reflector l8, resulting in more regular. radiation patterns and improved performance of the resonant radiating system.
The resonant cylindrical chamber or cavity 98, as illustrated in Fig. 5, may be closed at its ends, and the exciting rod 26 and its cooperating tube 25 of the coaxial line may be disposed substantially axially of the cylinder 98. The conditions of space resonance produced by the standing waves in the closed chamber will be rendered manifest in a corresponding change in load on the section of the concentric line 25, 26, with marked effect on the radiation or absorption of the radio waves.
The closed ends of the cylinder may be provided also with the arrangement illustrated in Fig. 1, as shown at 35 and 36 in Fig. 6.
The field pattern around the cylindrical reflector and system, that is, the magnitude and the direction of the field at any point in space produced by the radiating antenna l4 (and similar considerations apply for reception), will vary with the angle 0 subtended at the axis of the cylinder by the opening 20.
The oscillator 2 should be capable of producing a reasonably strong field at a wave length low enough so that the physical size of the reflector l6 shall not be economically prohibitive. The wave transmitted or received may be in a wave band from between less than a meter to ten meters, in order to keep the dimensions of the apparatus small. The antenna Il may be any desired length. It may be small compared to the wave-length, it may be a half wave-length, or it may be longer, if desired, but it should extend throughout the major portion of the axis of the cylinder, in order that substantially all parts of the inner walls of the cylinder may cooperate to return the radiations of the rod antenna back upon the rod antenna.
If the wave length is about two meters, for example, with the radius r of the reflector [6 also about two meters, the antenna H and the height of the reflector l6 may be about one meter or one-half wave-length. The radiation from the outside surface of the cylinder l6 itself should be eliminated, or reduced to a minimum, as by preventing the occurrence of capacitance between the cylinder IG and the transmission line, and also by matching the impedance of the line to the antenna.
The angle 0 will enter as a factor in determining the characteristics of the field pattern because of the phenomenon of diffraction around the edges 22 and 24 of the opening 20, the dimensions of which opening 20 may be. comparable to a wave length of the oscillations from the antenna H. The diffraction pattern of the field will thus vary with the width of the opening 20, or with the angle 0. Itis because of the fact that the dimensions are comparable to the length of the electromagnetic wave that the radiation pattern produced has directive characteristics.
It was found that, for angles 0 less than about Gildegrees, the radiation field outward .through the opening 20 is less intensethan field-1,130 the right and the left thereof, which latter are presumably caused by diflraction. As the angle 0 be a critical angle, less than about degrees. at which the radiation from the system assumed the shape of a wide central beam, with the said diffraction lobes tunable in other ways wave length. Most satisfactory results, however, were obtained with the one-quarter wave-length radius, the field being then strongest, and more of the energy then appearing in the radiated beam.
The variation of the radius may be effected by using different sizes of cylinders H5, or by bending the cylinder to a new radius. The chamber or cavity may also to vary its resonant characteristics.
The resonant cylindrical cavity may be joined to two oppositely disposed conducting flaring electro-magnetic wave-guiding sides or extensions I04 and I06, one extending from each side of the opening 20, substantially parallel to the axis of the cylinder as shown in Fig. 8. Radiating systems of this kind can produce a beam which is more or less confined in the plane in which the flaring occurs, without materially affecting the directivity in the plane at right angles to this plane.
It will be undertsood that the invention is not limited to the exact embodiments thereof that are illustrated and described herein, but that further modifications may be made by persons skilled in the art without departing from the spirit and scope of the invention, as defined in the appended claims.
What is claimed is:
1. An electric system comprising a hollow resonant cylindrical chamber of substantially circular cross section provided in its wall with an opening the sides of which are substantially parallel to the axis of the cylinder, a rod antenna disposed in the chamber substantially along the axis of the cylinder and extending throughout the major portion of the length of the cylinder, and means for exciting or absorbing in the antenna electromagnet waves of a frequency corresponding to the resonant frequency of the chamber and having electric lines of force substantially parallel to the axis of the cylinder to produce, by reflecting from the walls of the cylinder, linearly polarized standing waves in the cylindrical chamber to create a condition of linearly polarized space resonance therein, whereby linearly polarized energy of the said resonant frequency will be directively radiated out of the chamber or absorbed into the chamber through the opening.
2. An electric system comprising a hollow resonant. cylindrical chamber of substantially circular cross section closed at its ends and provided in its wall with an opening the are substantially parallel to the axis of the cylinder,- a rod antenna disposed in-the chamber substantially along the axis of the cylinder and extending throughout the major portion of the length of the cylinder, a coaxial-line system connected to the chamber and to the rod antenna, and means for exc'ting or absorbing in the antenna electromagnetic waves of a frequency corresponding to the resonant frequency of the chamber and having electric lines of force substantially parallel to the axis of the cylinder to produce, by reflection from the walls of the cylinder, linearly polarized standing waves in the cylindrical chamber to create a condition of linearly polarized space resonance therein, whereby linearly polarized energy of the said resonant frequency will be directively radiated out of the chamber or absorbed into the chamber through the opening.
3. An electric system comprising a hollow ressides of which be rendered adjustable or 1 parallel to the axis of the cylinder, sending apchamber and onant cylindrical chamber of substantially circular cross section provided in its wall with an opening'the sides of which are substantially parallel to the axis of the cylinder, an absorbing rod.
antenna disposed in the chamber substantially along the axis of the cylinder and extending throughout the major portion of the length of the cylinder, means for absorbing from space in the antenna modulated ultra-'high-frequency electro-magnetic waves of a frequency corresponding to the resonant frequency of the chamber and having electric lines of force substantially parallel'to the axis of the cylinder to produce, by reflection from the walls of the cylinder, linearly polarized standing waves in the cylindrical chamber to create a condition of linearly polarized space resonance therein, and means for demodulating the absorbed and reflected waves.
4. An electric system omprising a hollow resonant cylindrical chamber of substantially circular cross section provided in its wall with an opening the sides of which are substantially paratus, an exciting rod antenna disposed in the chamber substantially along the axis of the cylinder and extending throughout the major portion of the length of the cylinder, and means for connecting the sending apparatus to the rod antenna to excite inthe antenna modulated ultrahigh-frequency electromagnetic waves of a frequency corresponding to the resonant frequency of the chamber and having electric lines of force substantially parallel to the axis of the cylinder to produce, by reflection from the walls of the cylinder, linearly polarized standing waves inv the cylindrical chamber to create a condition of linearly polarized space resonance therein, whereby linearly polarized modulated ultrahigh-frequency energy of the said resonant frequency will be directively radiated out of the chamber through the opening.
5. An electric system comprising a hollow resonant cylindrical chamber of substantially circular cross section closed at one end and pro vided in its wall with an opening the sides of which are substantially parallel to the axis of the cylinder, a rod antenna disposed in the chamber substantially along the axis of the cylinder and extending throughout the major portion of the length of the cylinder, and means for exciting or absorbing in the antenna electromagnetic waves of a frequency corresponding to the resonant frequency of the chamber and having electric lines of force substantially parallel to the axis of the cylinder to produce, by reflection from the walls of the cylinder, linearly standing waves in the cylindrical chamber to create a condition of linearly polarized space resonance therein, whereby linearly polarized energy of the said resonant frequency will be directively radiated out of the chamber or absorbed into the chamber through the opening. 6. An electric system comprising a hollow reonant cylindrical chamber of substantially circular cross section provided in its wall with an opening the sides of which are substantially parallel to the axis of the cylinder, a rod antenna disposed in the chamber substantially along the axis of the cylinder and extending throughout the major portion of the length of the cylinder, and means for exciting or absorbing in the antenna electromagnetic waves of a frequency corresponding to the resonant frequency of the having electric lines of force subpolarized chamber or absorbed into the chamber through the opening, the chamber being provided with two oppositely disposed electromagnetic-wave-guiding extensions, one extending from each side of the opening substantially parallel to the axis of the cylinder.
WILMER. LANIER, BARROW.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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US163241A US2253501A (en) | 1937-09-10 | 1937-09-10 | Resonant antenna system |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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US163241A US2253501A (en) | 1937-09-10 | 1937-09-10 | Resonant antenna system |
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US2253501A true US2253501A (en) | 1941-08-26 |
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US163241A Expired - Lifetime US2253501A (en) | 1937-09-10 | 1937-09-10 | Resonant antenna system |
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Cited By (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2433368A (en) * | 1942-03-31 | 1947-12-30 | Sperry Gyroscope Co Inc | Wave guide construction |
US2452767A (en) * | 1946-04-02 | 1948-11-02 | John D Kraus | Broad-band antenna |
US2453751A (en) * | 1944-08-26 | 1948-11-16 | Philco Corp | Antenna reflector system |
US2460287A (en) * | 1938-01-17 | 1949-02-01 | Univ Leland Stanford Junior | Radiating electromagnetic resonator |
US2460286A (en) * | 1938-01-17 | 1949-02-01 | Univ Leland Stanford Junior | Radiating electromagnetic resonator |
US2468751A (en) * | 1942-01-16 | 1949-05-03 | Sperry Corp | Object detecting and locating system |
US2469419A (en) * | 1943-10-26 | 1949-05-10 | Sperry Corp | Energy directing apparatus |
US2475563A (en) * | 1944-02-25 | 1949-07-05 | Raytheon Mfg Co | Transmission system |
US2510290A (en) * | 1947-06-10 | 1950-06-06 | Rca Corp | Directional antenna |
US2539680A (en) * | 1945-11-26 | 1951-01-30 | Rca Corp | Ultra high frequency antenna |
US2540757A (en) * | 1944-06-16 | 1951-02-06 | Henry J Riblet | Antenna |
US2573461A (en) * | 1942-06-27 | 1951-10-30 | Rca Corp | Antenna |
US2611867A (en) * | 1946-08-31 | 1952-09-23 | Alford Andrew | Slotted winged cylindrical antenna |
US2624843A (en) * | 1945-06-07 | 1953-01-06 | Redheffer Raymond | Radio wave radiating system |
US2628311A (en) * | 1948-11-04 | 1953-02-10 | Rca Corp | Multiple slot antenna |
US2632851A (en) * | 1944-03-23 | 1953-03-24 | Roland J Lees | Electromagnetic radiating or receiving apparatus |
US2642529A (en) * | 1949-07-29 | 1953-06-16 | Int Standard Electric Corp | Broadband loop antenna |
US2659003A (en) * | 1946-04-30 | 1953-11-10 | Dorne Arthur | Antenna mountable in small spaces |
US2695958A (en) * | 1944-07-31 | 1954-11-30 | Bell Telephone Labor Inc | Directive antenna system |
US2696681A (en) * | 1942-11-11 | 1954-12-14 | John P Sheridan | Navigation trainer for radio homing |
US2711440A (en) * | 1944-10-09 | 1955-06-21 | Rines Robert Harvey | Microwave scanning system |
US2799017A (en) * | 1946-08-31 | 1957-07-09 | Alford Andrew | Slotted cylindrical antennas |
US3066293A (en) * | 1956-03-16 | 1962-11-27 | Ross A Davis | Antenna system with output means in parallel with resonating means |
US3099836A (en) * | 1960-05-16 | 1963-07-30 | Lockheed Aircraft Corp | V-strip antenna with artificial dielectric lens |
US3177491A (en) * | 1960-12-02 | 1965-04-06 | Portenseigne Ets Marcel | Cavity antenna with flared horn |
US4965869A (en) * | 1987-06-23 | 1990-10-23 | Brunswick Corporation | Aperture antenna having nonuniform resistivity |
-
1937
- 1937-09-10 US US163241A patent/US2253501A/en not_active Expired - Lifetime
Cited By (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2460287A (en) * | 1938-01-17 | 1949-02-01 | Univ Leland Stanford Junior | Radiating electromagnetic resonator |
US2460286A (en) * | 1938-01-17 | 1949-02-01 | Univ Leland Stanford Junior | Radiating electromagnetic resonator |
US2468751A (en) * | 1942-01-16 | 1949-05-03 | Sperry Corp | Object detecting and locating system |
US2433368A (en) * | 1942-03-31 | 1947-12-30 | Sperry Gyroscope Co Inc | Wave guide construction |
US2573461A (en) * | 1942-06-27 | 1951-10-30 | Rca Corp | Antenna |
US2696681A (en) * | 1942-11-11 | 1954-12-14 | John P Sheridan | Navigation trainer for radio homing |
US2469419A (en) * | 1943-10-26 | 1949-05-10 | Sperry Corp | Energy directing apparatus |
US2475563A (en) * | 1944-02-25 | 1949-07-05 | Raytheon Mfg Co | Transmission system |
US2632851A (en) * | 1944-03-23 | 1953-03-24 | Roland J Lees | Electromagnetic radiating or receiving apparatus |
US2540757A (en) * | 1944-06-16 | 1951-02-06 | Henry J Riblet | Antenna |
US2695958A (en) * | 1944-07-31 | 1954-11-30 | Bell Telephone Labor Inc | Directive antenna system |
US2453751A (en) * | 1944-08-26 | 1948-11-16 | Philco Corp | Antenna reflector system |
US2711440A (en) * | 1944-10-09 | 1955-06-21 | Rines Robert Harvey | Microwave scanning system |
US2624843A (en) * | 1945-06-07 | 1953-01-06 | Redheffer Raymond | Radio wave radiating system |
US2539680A (en) * | 1945-11-26 | 1951-01-30 | Rca Corp | Ultra high frequency antenna |
US2452767A (en) * | 1946-04-02 | 1948-11-02 | John D Kraus | Broad-band antenna |
US2659003A (en) * | 1946-04-30 | 1953-11-10 | Dorne Arthur | Antenna mountable in small spaces |
US2611867A (en) * | 1946-08-31 | 1952-09-23 | Alford Andrew | Slotted winged cylindrical antenna |
US2799017A (en) * | 1946-08-31 | 1957-07-09 | Alford Andrew | Slotted cylindrical antennas |
US2510290A (en) * | 1947-06-10 | 1950-06-06 | Rca Corp | Directional antenna |
US2628311A (en) * | 1948-11-04 | 1953-02-10 | Rca Corp | Multiple slot antenna |
US2642529A (en) * | 1949-07-29 | 1953-06-16 | Int Standard Electric Corp | Broadband loop antenna |
US3066293A (en) * | 1956-03-16 | 1962-11-27 | Ross A Davis | Antenna system with output means in parallel with resonating means |
US3099836A (en) * | 1960-05-16 | 1963-07-30 | Lockheed Aircraft Corp | V-strip antenna with artificial dielectric lens |
US3177491A (en) * | 1960-12-02 | 1965-04-06 | Portenseigne Ets Marcel | Cavity antenna with flared horn |
US4965869A (en) * | 1987-06-23 | 1990-10-23 | Brunswick Corporation | Aperture antenna having nonuniform resistivity |
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