US2380333A - High frequency antenna - Google Patents

High frequency antenna Download PDF

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Publication number
US2380333A
US2380333A US470763A US47076342A US2380333A US 2380333 A US2380333 A US 2380333A US 470763 A US470763 A US 470763A US 47076342 A US47076342 A US 47076342A US 2380333 A US2380333 A US 2380333A
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United States
Prior art keywords
elements
antenna
lines
assemblies
plane
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Expired - Lifetime
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US470763A
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English (en)
Inventor
Marvel W Scheldorf
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General Electric Co
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General Electric Co
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Publication date
Priority to BE475639D priority Critical patent/BE475639A/xx
Application filed by General Electric Co filed Critical General Electric Co
Priority to US470763A priority patent/US2380333A/en
Application granted granted Critical
Publication of US2380333A publication Critical patent/US2380333A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q11/00—Electrically-long antennas having dimensions more than twice the shortest operating wavelength and consisting of conductive active radiating elements
    • H01Q11/02—Non-resonant antennas, e.g. travelling-wave antenna
    • H01Q11/04—Non-resonant antennas, e.g. travelling-wave antenna with parts bent, folded, shaped, screened or electrically loaded to obtain desired phase relation of radiation from selected sections of the antenna

Definitions

  • the transmitter In radio transmitter systems, the transmitter is usually located at a point relatively remote from the studio or other source of program. In
  • a horizontally polarized antenna comprising two separate horizontally disposed radiating assemblies each having a plurality of sections arranged colinearly or end to end.
  • the separate assemblies are separated or spaced apart a distance of three quarters of a wavelength and connected together in such a way that the phase of the currents in the two assemblies differs by 270.
  • This spacing and current relationship causes one radiating assembly to act as a director with respect to the other and produces the desired unidirectional radiation characteristic.
  • phase inverting sections are used between them when more than two matching lines and two concentric interconnecting lines are provided between the two radiating of the plane of the assemblies.
  • a third adjustable impedance matching line is connected betweer the common driving point on the interconnecting lines and the, transmission line to the transmitter.
  • Fig. 1 is a perspective view partly broken away of a complete antenna system embodying the principles of my invention
  • Fig. 2 is a diagrammatic representation illustrating certain phases of operation of a system of the general type embodying my invention
  • Figs. 3 and l are enlarged views of the phase inverting means illustrated in Fig. 1
  • Figs. 5 and 6 are enlarged views illustrating the connections from the signal source to the antenna
  • Figs. 1 is a perspective view partly broken away of a complete antenna system embodying the principles of my invention
  • Fig. 2 is a diagrammatic representation illustrating certain phases of operation of a system of the general type embodying my invention
  • Figs. 3 and l are enlarged views of the phase inverting means illustrated in Fig. 1
  • Figs. 5 and 6 are enlarged views illustrating the connections from the signal source to the antenna
  • Figs. 1 is a perspective view partly broken away of a complete antenna system embodying the principles of my invention
  • Fig. 2 is a diagrammatic
  • a horizontally mounted high frequency antenna system comprising two separate radiating assemblies in and H each having five colincolinear sections are used. These phase invertducting members approximately one-half wavelength long, bent or folded back upon themselves to provide adjacent parallel members, the free ends engaging adjacent antenna elements. The resulting arrangement approximates a onequarter wavelength transmission line.
  • Fig. 2 where colinear elements l2 are connected by phase inverting means l3.
  • phase inverting means l3 When such a system is energized, standing waves appear as indicated by the curved lines in Fig. 2 and the direction of currents through the system is as shown by the solid arrows.
  • the current flowing in the adjacent parallel sections of the phase inverting means I3 are in opposite directions the electric fields created thereby tend to cancel and radiation from the phase inverters is minimized.
  • the. antenna illustrated in Fig. 1 is provided with phase inverting means l3 similar to those described above and illustrated in Fig. 2 but which are disposed in such a configuration, as illustrated in Fig. 3, that voltages induced in the parallel portions 13a and l3b of the inverters by the current flowing in the elements 12 cause currents to flow which are in opposition and therefore substantially cancel. Accordingly, radiation from the inverters I3 is substantially prevented. The reason for this substantial cancellation will be clear from an inspection of Fig. 4. Any radiation caused by current flow in sections l2 causes opposing voltages in diametrically opposite portions of the inverter loops as generally indicated by the arrows at, a.
  • the assemblies l and II are center fed by introducing a driving voltage at substantially the midpoint of the center section of each of the assemblies. This may be accomplished by providing substantially one-quarter wavelength sections 12a and Rh so that the middle section of each of the assemblies is open at substantially the midpoint thereof.
  • the assemblies I0 and II are then connected at the adjacent ends of the mid-sections l2a and I2!) by interconnecting lines I4 and i5 terminating at each end in adjustable impedance matching lines l1 and I8,
  • the lines l4 and I5 are preferably of the coaxial cable type except at the points of connection to the. transmission line and to the matching lines in order to minimize radiation therefrom and provide weather protection.
  • the impedance of the matching lines ll, l8, which are electrically connected to the elements I20. and I222, may be adjusted by the means shown in Fig. 5.
  • the members or elements Ma and I2b may be slotted as indicated by the numeral 2
  • the other ends of the matching lines l1, l8 may be adjustably connected to the concentric bars or straps 23 provided at one end with an enlarged portion orboss 24 having a suitable opening to receive lateral extending portions 25 of the matching lines.
  • Suitably threaded fastening means indicated by the numeral 26 may be provided for clamping the matching lines at correct position is determined the members 22 and 26 may be tightened.
  • the matching lines are provided with a configuration similar to that of the phase inverters in order to prevent radiation therefrom in the same manner as previously described and should be slightly less than one-quarter wave-length long, the exact length being determined by experiment.
  • the concentric lines I4, l5 lie in the same plane as the radiating assemblies 10 and II it has been found that energy radiated from the assemblies i0 and II is reflected from the lines l4, IS in horizontal directions and radiation in undesired horizontal directions is increased.
  • the connecting lines are disposed out of the plane of the radiating assemblies. For convenience of erection of the antenna system, these lines are preferably disposed below the assemblies. Any energy reflected from the lines is therefore upward and not effective in the horizontal plane.
  • the assemblies are spaced three-fourths of a wavelength apart and the transmission line 30 is connected to the feed lines I4, l5 at a point such that the distance from the point of connection to the directing assembly I0 is onequarter of a wavelength shorter than the distance from the point of connection to the radiating assembly II. If the assemblies are thus connected the phase of thecurrent in the assemblies l0 and H differs by 270 which is the equivalent of a difference of or a quarter wavelength, in the opposite direction and the assembly nearest the point of connection acts as a director for the other assembly.
  • the transmission line preferably terminates in adjustable impedance means.
  • the transmission line may be terminated in conductors 32 and 33 which may be adjustably connected to the lines ll, [5 by means of suitable adjusting straps or bars 3
  • the outer conductor of the transmission line 30 is normally grounded.
  • an electrically conductive cylinder 36 larger in diameter than the transmission line and approximately one-quarter wavelength long.
  • the lower end of the cylinder is connected electrically to the outer member 31 of the transmission line and is open at the upper end.
  • the effect of this assembly is to introduce a high impedance between ground and the extreme end of the outer conductor 33 of the transmission line.
  • the adjustable members 34 and 35 and the end of the transmission line 30 are housed in a suitable housing 38 which is preferably of electrically conductive material disposed in engagement with the outer members 39 and 40 of the lines I4, l5, thereby grounding the outer members 39 and 40 of the lines l4 and I5, respectively, through the housing and the cylinder 36.
  • FIGS. 7, 8 and 9 are illustrated representative radiation patterns obtained when employing inverters of the type shown in Fig. 2 and when the interconnecting lines lie in the plane of the assemblies I and I I. These figures represent such a. system adjusted for minimum side lobes 43 and minimum back lobes 42, respectively. However, when side lobes are reduced, the back lobe is considerable and vice versa. i
  • Fig. 9 shows a typical radiation pattern for the antenna system illustrated in Fig. 1. It will be noted that there is very little radiation in the direction opposite from the desired beam and all the side lobes are relatively small. Such an arrangement is particularly adapted to use in studio-to-transmitter links for frequency modulation systems because a, very large proportion of the radiated energy is transmitted in a narrow beam which, of course, is directed at the point of transmission.
  • the narrowness of the beam of the antenna or the above described type is dependent upon the number of elements l2. While five have been illustrated, any desired number may 'be employed.
  • a high frequency antenna system compristenna at the ends thereof, whereby voltages induced in said members at opposite sides of said loop by current flowing in said elements are in substantial opposition and substantially no current flows in said members as a result of such induced voltages and radiation therefrom is substantially prevented.
  • said members being formed in loops at right angles to said elements, the opposite ends of said conductor engaging adjacent elements of said antenna at the ends thereof, whereby voltages induced in said members at opposite sides of said loops by current flowing in said elements are in substantial opposition and substantially no current flows in said members as a result of such induced voltages and radiation therefrom is substantially prevented, said loops being so positioned in their respective planes that a line drawn through the center thereof and the axis of said elements lies at an angle of the order of forty-five degrees with respect to the horizontal.
  • a high frequency antenna system comprising at least three colinear elements, each of said elements being approximately one-half wave length long, phase inverting means connecting adjacent elements and comprising a conductor approximately one-half Wavelength long doubled on itself to provide two substantially parallel members of substantially the same length with the opposite ends of said conductor engaging adjacent elements at the ends thereof, said parallel members having the form of an approximately circular substantially closed loop at right angles to said elements.
  • a directive antenna having at least two coaxial elements extending in adjacent end-to-end relation, said elements operating in phase with respect to waves in space, the adjacent ends of said elements being connected together by a coning at least three colinear elements, each of said elements being approximately one-half wavelength long, phase inverting means connecting adjacent elements and comprising a conductor approximately one-half wavelengthlong doubled upon itself to provide two substantially parallel members of substantially the same length, 891d parallel members being formed in loops at right angles to said elements, the opposite ends of said conductor engaging adjacent elements of said anductor having a length substantially equal to half of a wavelength at the frequency at which said antenna operates, said conductor having successive portions along its length from one end to the other extending in opposite directions with respect to each other and successivesections of each of said portions extending in opposite directions in a plane at right angles to said coaxial elements whereby said conductors are substantially equally and oppositely influenced by desired waves in space thereby to reduce the action of' said antennawith respect to waves propagated in undesired directions.
  • a directive antenna comprising a pair of coaxialelements arranged end to end, adjacent ends of said elements bein connected together by a conductor having a length equal to half of a Wavelengthat the frequency at which said antenna operates, said conductor being folded on itself at its midpoint, said midpoint lying adjacent to said elements, and the portions of said conductor opposite said midpoint extending therefrom about respective loops to, said ends of the respective elements, said loops lying in a plane at right angles to said elements.
  • a directive antenna comprising a pair of coaxial elements arranged end to end, adjacent ends of said elements being connected together by a conductor folded on itself at its midpoint, said midpoint lying adjacent said elements, and the portions of said conductor opposite said midpoint being formed in loops at right angles to said elements, said loops having a peripheral length equal to a quarter of the operating wavelength of said antenna.
  • a directive antenna having coaxial elements spaced in end-to-end relation in a colinear array, radio apparatus connected to the midpoint of said array, and means to operate all of said elements in phase, said means comprising conductors connected between adjacent ends of adjacent elements, said conductors having a length equal to half a wavelength at the frequency at which said antenna operates, each of said conductors being folded upon itself at its midpoint and formed in a loop in a plane at right angles to said array.
  • each of said elements having a length equal to half a wavelength at the frequency at which the antenna operates, adjacent ends of adjacent elements being connected together by a nonradiating conductor having an electrical length equal to half said wavelength, said conductor being doubled on itself at its midpoint, the halves thereof extending from said midpoint first in one direction and then in the opposite direction in a plane at right angles to said radiating elements whereby electromotive forces induced in the oppositely extending portions of said halves by fields produced by said elements neutralize each other thereby preventing the production of currents in said conductor which produce undesired radiation therefrom.
  • An antenna comprising a plurality of coaxial elements arranged end to end, each of said elements having a length equal to half the operating wavelength, conductors joining adjacent ends of adjacent of said elements, said conductors each being folded on itself at its midpoint and formed in a loop extendin from said midpoint to the respective ends of said elements, said loop lying in a plane at right angles to said elements, high frequency apparatus, and connections extending from the midpoint of the middle of said elements to said apparatus, said connections being formed in a loop parallel to said first mentioned loops, and the peripheral length of all of said loops being adjusted for maximum directivity of said antenna.
  • a directive antenna comprising two parallel arrays, each array comprising a plurality of coaxial half wavelength elements arranged end to end, means to energize all of said elements of each array in phase, said means comprising transmission lines extending to each array, having lengths proportioned to reduce maximum effect of said antenna in the plane of said arrays, the conductors of said transmission'lines being disposed out of said plane defined by said arrays thereby to reduce the effect of said conductors on the directivity characteristics of said array in said plane.
  • a directive antenna comprising two parallel arrays, each array comprising a plurality of coaxial half wavelength elements arranged end to end, means to energize all of said elements of each array in phase, and to energize the different arrays in phase relation to produce maximum eifect in the plane defined bysaid arrays said means comprising transmission lines extending to each array, the conductors of said array, the conductors of said transmission lines transmission lines being disposed out of said plane defined by said arrays thereby to reduce the effect of said conductors on the directivity characteristics of said array and the portion of each of said conductors adjacent said arrays extending about a loop in a plane at right angles to the array to reduce the induction of current therein by waves in space.
  • a directive antenna comprising two parallel arrays, each array comprising a plurality of coaxial half wavelength elements arranged end to end, means to energize all of said elements in phase to produce maximum radiation in the plane defined by said arrays, said means comprising transmission lines extending to each being disposed out of said plane defined by said arrays thereby to reduce the effect of said conductors on the directivity characteristics of said array in said plane and the portion of each of said conductors adjacent said arrays extending about a loop in a plane at right angles to the respective array to reduce the induction of current therein by waves in space, the adjacent elements of each array beingconnected together by conductors each doubled on itself at its midpoint and formed in a loop parallel with said first loop and the peripheral length of all of said loops being adjusted for optimum directivity of said antenna.
  • a directive antenna comprising two parallel arrays, each array comprising a plurality of half wavelength elements arranged end to end, adjacent ends of the elements in each array being connected together by conductors of length to maintain said elements in phase, each of said conductors being doubled on itself at its midpoint and formed in a loop at right angles to said elements, the centers of said loops lying in a plane intersecting the plane defined by the arrays at an angle of forty-five degrees at the position of the elements joined by the respective loops.
  • An antenna system comprising two assemblies arranged in parallel space relation, each assembly comprising a number of colinear elements arranged end to end, high frequency apparatus connected to each of said assemblies through respective transmission lines differing in length by an odd multiple of a quarter of a wave length of the wave on which said antenna operates whereby said antenna has maximum effect in a direction at right angles to said assemblies and in the plan of said assemblies, and said lines lying substantially entirely out of the plane of said assemblies thereby to have minimum effect upon the field pattern of said antenna in space.
  • An antenna system comprising two assemblies arranged in parallel space relation, each assembly comprising a number of colinear elements arranged end to end, high frequency apparatus connected to each of said assemblies through respective transmission lines differing in length by an odd multiple of a quarter of a wave length of the wave on which said antenna operates whereby said antenna has maximum effect in a direction at right angles to said assemblies and in the plane of said assemblies, said lines lying substantially entirely out of the plane of said assemblies and each conductor thereof extending to its respective assembly about a loop in a plane at right angles to the respective assembly whereby voltages induced in opposite sides of said loop by waves on which operates whereby said antenna has maximum effect in a direction at right angles to said assemblies and in the plane of said assemblies, and said lines lying substantially entirely out of the plane of said assemblies, each of said lines comprising a pair of conductors extending at the antenna end thereof about a loop to the respective assembly, said loops lying at right angles to the respective assembly whereby voltages induced in said conductors at opposite sides of said loops by desired waves in space are oppos
  • An antenna system comprising two assemblies arranged in parallel space relation, each assembly comprising a number of colinear elements arranged end to end,high frequency apparatus connected to each of said assemblies through respective transmission lines differing in length by an odd multiple of a quarter of a wave length of the wave on which said antenna operates whereby said antenna has maximum effect in a direction at right angles to said assemblies and in the plane of said assemblies, and said lines lying substantially entirely out of the plane of said assemblies, each of said lines comprising apair of conductors extending at the antenna end thereof about a loop to the respective assembly, said loops lying at right angles to the respective assembly whereby voltages induced in said conductors at opposite sides of said loops by desired waves in space are opposing and the circumferences of said loops and the spacing between said conductors being adjusted to match the impedance of said lines to that of said assembly.
  • An antenna comprising two parallel assemblies, each assembly comprising an odd number of colinear elements arranged end to end, each of said elements having a length equal to half of a wavelength of the wave on which said antenna operates, and the middle element of each assembly being broken at its midpoint, high frequency apparatus connected through respective transmission lines to each assembly, said lines comprising conductors extending about loops at right angles to the respective assembly to opp0- site sides of said break, conductors connecting adjacent ends of adjacent elements of each assembly, said conductors each having a length equal to a half wavelength and doubled at its midpoint on ital!
  • said lines having length sufliciently different from each other to pr-duce maximum effect of said antenna in a direction in the plane of said assemblies, said lines lying outside of said plane to reduce the eflect thereof on the space pattern of said antenna in said plane and all said conductors extending about loops having opposingvoltages induced therein at opposite sides of the respective loop by desired waves in space thereby to neutralize and reduce the efiect of said conductors on said space pattern.
  • An antenna comprising two parallel assemblies, each assembly comprising an odd number of colinear elements arranged end to end, each of said elements having a length equal to half of a wavelength of the wave on which said anteniia operates, and the middle element of each assembly being broken at its midpoint, high frequency ap-' paratus connected through respective transmission lines to each assembly, said lines comprising conductors extending about loops at right angles to the respective assembly to opposite sides of said break, conductors connecting adjacent ends of adjacent elements of each assembly, said conductors each having a length equal to a half wavelength and doubled at its midpoint on itself and extending from said midpoint about a loop parallel with said first mentioned loops, said lines having length sufliciently difierent from each other to produce maximum effect of said antenna in a direction in the line of said assemblies, said lines lying outside of said plane to reduce the effect thereof on the space pattern of said antenna in said plane and said loops having centers outside said plane and in a direction from the respective assembly in a plane at right angles thereto to reduce the

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US470763A 1942-12-31 1942-12-31 High frequency antenna Expired - Lifetime US2380333A (en)

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Cited By (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2455403A (en) * 1945-01-20 1948-12-07 Rca Corp Antenna
US2471215A (en) * 1945-09-27 1949-05-24 Pye Ltd Radio antenna
US2472106A (en) * 1943-09-20 1949-06-07 Sperry Corp Broad band antenna
US2558145A (en) * 1948-05-20 1951-06-26 Jr Wesley C Mock Antenna
US2566287A (en) * 1950-09-16 1951-08-28 Jr Lewis H Finneburgh Television antenna system
US2578973A (en) * 1946-12-11 1951-12-18 Belmont Radio Corp Antenna array
US2580798A (en) * 1947-05-22 1952-01-01 Kolster Muriel Broad-band antenna system
US2648768A (en) * 1948-12-29 1953-08-11 Rca Corp Dipole antenna
US2648771A (en) * 1946-10-01 1953-08-11 Emi Ltd Resonant aerial
US2655599A (en) * 1953-03-10 1953-10-13 Jr Lewis H Finneburgh All band television antenna
US2700105A (en) * 1954-07-26 1955-01-18 Winegard Co Tv antenna array
US2752486A (en) * 1950-10-18 1956-06-26 Rca Corp Ultra high frequency oscillation injection equalizer
US2755467A (en) * 1946-05-15 1956-07-17 Leonard J Eyges Broadband linear array
US2772413A (en) * 1956-03-30 1956-11-27 Trio Mfg Co Composite dipole multi-channel television antenna
US2953624A (en) * 1953-07-05 1960-09-20 Perrone Arrigo Spacer for twin and multiple conductors of high voltage aerial transmission lines
US3805269A (en) * 1971-06-14 1974-04-16 Matsushita Electric Ind Co Ltd Diverse type dipole antennas on common mount
US4186403A (en) * 1975-07-08 1980-01-29 Arthur Dorne Antenna formed of non-uniform series connected sections
US20060139229A1 (en) * 2004-12-28 2006-06-29 Cisco Technology, Inc. Hooked stub collinear array antenna
AU2018386614B2 (en) * 2017-12-21 2021-08-12 Huawei Technologies Co., Ltd. Antenna and terminal

Cited By (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2472106A (en) * 1943-09-20 1949-06-07 Sperry Corp Broad band antenna
US2455403A (en) * 1945-01-20 1948-12-07 Rca Corp Antenna
US2471215A (en) * 1945-09-27 1949-05-24 Pye Ltd Radio antenna
US2755467A (en) * 1946-05-15 1956-07-17 Leonard J Eyges Broadband linear array
US2648771A (en) * 1946-10-01 1953-08-11 Emi Ltd Resonant aerial
US2578973A (en) * 1946-12-11 1951-12-18 Belmont Radio Corp Antenna array
US2580798A (en) * 1947-05-22 1952-01-01 Kolster Muriel Broad-band antenna system
US2558145A (en) * 1948-05-20 1951-06-26 Jr Wesley C Mock Antenna
US2648768A (en) * 1948-12-29 1953-08-11 Rca Corp Dipole antenna
US2566287A (en) * 1950-09-16 1951-08-28 Jr Lewis H Finneburgh Television antenna system
US2752486A (en) * 1950-10-18 1956-06-26 Rca Corp Ultra high frequency oscillation injection equalizer
US2655599A (en) * 1953-03-10 1953-10-13 Jr Lewis H Finneburgh All band television antenna
US2953624A (en) * 1953-07-05 1960-09-20 Perrone Arrigo Spacer for twin and multiple conductors of high voltage aerial transmission lines
US2700105A (en) * 1954-07-26 1955-01-18 Winegard Co Tv antenna array
US2772413A (en) * 1956-03-30 1956-11-27 Trio Mfg Co Composite dipole multi-channel television antenna
US3805269A (en) * 1971-06-14 1974-04-16 Matsushita Electric Ind Co Ltd Diverse type dipole antennas on common mount
US4186403A (en) * 1975-07-08 1980-01-29 Arthur Dorne Antenna formed of non-uniform series connected sections
US20060139229A1 (en) * 2004-12-28 2006-06-29 Cisco Technology, Inc. Hooked stub collinear array antenna
US7098861B2 (en) * 2004-12-28 2006-08-29 Cisco Technology, Inc. Hooked stub collinear array antenna
AU2018386614B2 (en) * 2017-12-21 2021-08-12 Huawei Technologies Co., Ltd. Antenna and terminal
US11251534B2 (en) 2017-12-21 2022-02-15 Huawei Technologies Co., Ltd. Antenna and terminal

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