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US1910147A - Antenna system - Google Patents

Antenna system Download PDF

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Publication number
US1910147A
US1910147A US173833A US17383327A US1910147A US 1910147 A US1910147 A US 1910147A US 173833 A US173833 A US 173833A US 17383327 A US17383327 A US 17383327A US 1910147 A US1910147 A US 1910147A
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US
United States
Prior art keywords
antenna
wave
conductors
length
vertical
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
US173833A
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English (en)
Inventor
Bruce Edmond
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.)
AT&T Corp
Original Assignee
Bell Telephone Laboratories Inc
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Filing date
Publication date
Application filed by Bell Telephone Laboratories Inc filed Critical Bell Telephone Laboratories Inc
Application granted granted Critical
Publication of US1910147A publication Critical patent/US1910147A/en
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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

  • This invention relates to wave transmission, and especially to antennae adapted for short wave radio communication.
  • One fundamental aspect of the invention Vlies in connecting the vertical antennae by means of conductors in such manner that phases are taken into account throughout the system with resulting increase in eiiiciency.
  • This aspect of the invention may be better understood by considering a simple receiving antenna array comprising verticals connected lin series by horizontally connected wires.
  • the arrangement maybe such, in accordance with this invention, that a current pulse set up by the space wave inthe uppermost elemental section of the first vertical wire, for example, is just one wave length of the wire from the lowermost elemental section of the second vertical, so that there will be an add ino" of the current in the verticals in phase.
  • the verticale are one-half wave length high and one-half wave length apart. This additive effect may be obtained in other forms of antennae of this general type by having corresponding elemental sections somewhat differently spaced as will be hereinafter described.
  • Tn another aspect the invention pertains to the choice of antenna height, the preferred form of antenna being one in which the height is one-half wave length.
  • l f 1 Another aspect of the invention relates t0 the proper impedance termination of the an? C65 tenna array to obtain a desireddirectional effect by preventing undesired reflections.
  • the invention provides an antenna array of the type mentioned above, but fo-ld- 'p ed back upon itself, so'as in general to obtain i compactness, and, in certainicases, the elimination of grounds.
  • Figs. 1, 3, 5, 6 and 7 of the 'drawings show five different systems of the type described above; Figs. 2A, 2B, 4A and 4B are diagrams for facilitating explanation of the invention; and Fig. 8 shows the polar directional characteristics of the 'system of Fig. 7
  • the sinusoid shows the space distribution of the electric or the magnetic t 70 ield strength of an advancing electromagnetic wave at a given' instant of time t.
  • the heavy yvertical and horizontal lines represent a series of vertical orupright inductor wires r I u a half wave-length high and spaced by a half wave-length and horizontal wires f of that length connecting ⁇ the vertical wires.
  • the wires are all in a kplane perpendicular to the/wave front, and the electric field of the oncoming wave is parallel 'to the vertical f3 wires.
  • the electromagnetic wave may be such as would be sent 'from a vertical transmitting antenna wire.
  • the arrows on the conductors show the direction of current flow at the given time t. Interconnecting the inductors or verticale u by conductors j", as shown, securesthe benefit of the cumulative effect of the verticals.
  • This system satisfies cach of two conditions which it is desirableK to fulfill, namely that the'height L be of90 proper value to produce the optimum effective induced voltage in each of the verticals, and that the height h and the spacing of the verticals in the direction of the wave motion, and the length of the horizontal wires f have values such that the resultant currents, one of which is produced'by each vertical, are directly in phase at any point in the line so that the cumulative effect just mentioned is a maximum. (For the present it is assumed that the current Wave velocity in the Wire is equal to the space Wave velocity in the surrounding medium.)
  • Fig. 2A represents a lossless Wire u divided into small elements 1, 2, 3, etc.,each having the same induced voltage in time phase With each other.
  • Acurrent pulse from, say, element 3 travels toward point P With the speed of light. By the time it reaches P, it lags behind the instantaneous induced voltage in time phase an amount depending on the distance traveled.
  • Fig. 2B shows the vector addition of these current pulses originating in elements 1, 2, 3, etc. which, for a lossless line, traces along the circumference of a circle.
  • the resultant current IP Will be a maximum when it is the diameter of the circle.
  • this arrangement also satisfies the second condition (with separation of verticals u equal to half of the wave-length because-any elemental length in one vertical has a corresponding elementary length, in the next vertical, just one Wire Wave-length away, as illustrated in Fig. 1 by a and al, likewise I) and b1.
  • the elemental lengths a and al are here referred to as corresponding elemental lengths because, o r in the sense that, they are the same distance from the entrance ends of their respective verticals I at any given instant, or in other Words the same distance from those ends of their respective verticals which at each instant are given equal potentials relative to the other ends by the action of portions of the space Wave one-half Wavelength apart.
  • the far ends of the line or antenna may be free, as shown.V
  • an antenna With its ends grounded as about to be described may be employed.
  • the total length of the antenna is an integral odd multiple of half of a Wire Wave length and when the ends are groimded the total length of the antenna is an integral even multiple Vof half of a Wire Wave length.
  • the load is preferably connected at the midpoint of one of the half Wave-length horizontal Wires f, at the center of the Wave collector, as shown in Fig. 1.
  • the impedance which the load presents to the Wave collector should be as high as possible and therefore may Well be an anti-resonant circuit, as shown at 10, tuned to the Wave length A.
  • the anti-resonant circuit is coupled to a radio receiver (or transmitter) 11 by a resonant circuit 12.
  • the system is bi-directional and the outputs due to signal field strengths in the broadside directions directions perpendicular to the plane of the antennae), are negligible.
  • Such an antenna is preferably built for a definite frequency and a definite direction of reception, for use in point to point communication, for example.
  • the output voltage maximum of one or more verticale of an antenna of this type, if the antenna were lossless, would be directly proportional to the wave length for which it was designed.
  • the antenna system of Fig. 1 is bi-directional, meaning that it responds readily to waves from either horizontal direction in the plane of the antenna.
  • the system of Fig. 1 is equally responsive tor these two opposite directions.
  • One way in which asymmetry, or lack of equality, of responsiveness for the two directions may be obtained is by rearranging the spacing of the'wires ofA half wave-length ⁇ height, while maintaining the alternate ones of those wires at a. wave length apart and maintaining the lengths of the horizontal connecting wires equal to the distances between the verticale which they connect.
  • Vhen the spacing of the wires u of half wavelength height is, by way of example, alternately a quarter and three quarters of the wave-length, as shown in Fig.
  • the antenna is responsive to waves from only one of the two opposite horizontal directions in its plane, provided the reflections from the far end are absorbed by properly terminating that end as shown at 15 in Fig. 3.
  • An antenna having this directional property will be referred to in this specification as a unidirectional antenna.
  • the action i of the proper termination can be explained by reference to Figs. 4A and 4B, each of which represents a single section.
  • Figs. 3 A and 4B, horizontal quart-er wave-length conductors f or three-.quarter wave-length conductors f connect adjacent verticals.
  • the resultant effective voltage induced in a vertical u can be represented by a lumped voltage centrally located in that vertical, as at @l and e2.
  • a vector picture of the currents and voltages for each vertical is drawn below the vertical. It is seen that the voltages phase difference between verticals is a quarter period. Assuming the velocity of the current pulses as the speed of light, one complete period elapses for a current pulse to travel directly from el to receiver R, likewise a quarter period is necessary between e2 and R. For the current pulses arriving at R via the far end reflection, e1 to R requires effectively two complete periods while e2 to R requires two and three-quarter periods. Figs.
  • a multiple section antenna such as that in Fig. 3 may be folded back upon itself and the terminating impedances connected between wires, as shown in Fig. 6, thus eliminating the necessity of ground connections.
  • Fig. 6 illustrates how this scheme may be enlarged.
  • the theoretical vpolar directional characteristics-tor the antenna system of Fig. 7 are given inFig. 8.
  • the symbol e in Fig. 8 represents field strength.
  • Figs. 6 and 7 as in the case of Figs. 3 and 5, the antenna lies in a plane containing the direction of theelectric force in the wave front- 'of the .wave to be received (or transmitted) and peints from the receiver ing wave.
  • Fig. 3 illustrates an alterna- ⁇ 100 nant circuit, which will make the combination effectively a pure resistance.
  • the theoretical Asurge impedance contains a small re- V12, respectively, of Fig. 1 but adjusted to simulate the impedance l5.
  • rIlhe electrical lengths or ⁇ wire wave lengths of the elements 10,10 and-15 are substantially zero or negligibly small.
  • the electrical lengths ofthe conductors connecting elements 10 and l5 between a onehalf wave length vertical conductor u and earth are substantially zero or negligibly small.
  • the elements l5 and l0 are connected at the center of one-half Wave length horizontal conductors f2 which connect the lower ends of two of the onehalf wave length vertical wires u.
  • conductors f and f are horizontal one-quarter wave length and three-quarter wave length conductors respectively, each connecting two vertical wires u.
  • f Fig. 8 is the calculated polar directional characteristic for the antenna system of Fig.
  • the wires u are vertical and the wires f, f and f horizontal
  • the principle of the invention is independent cf the absolute direction of the wires u and f, f and f.
  • the wires u are parallel to the direction of the electric force in the wave front, or in other words. are parallel to the axis of polarization of the waves to be received by, or radiated from, the antenna, and the wires f, f and f are perpendicular to the axis of polarization.
  • the term height as used in this specification and in the claims is not restricted to vertical dimensions.
  • integral multiple7 of a quantity includes unity as the multiplier involved.
  • the quantity may be an integral multiple of itself.
  • The'dimensions mentioned above for the length, spacing, height, etc. of the component parts of the antenna may be increased by any integral multiple of one wave length, since the phase relations of the voltages and currents in the system will not be thereby altered.
  • difference of sign or sense is not regarded as a dierence of direction, although in referring to the directional characteristics of the antenna opposite signs or senses of direction are regarded as opposite directions.
  • An antenna for space wave communication comprising inductors spaced in a direction of propagation of the space waves past said antenna, and current conducting means connecting said inductors, the electrical length of said antenna between corresponding elementary lengths of any two of said inductors differing an odd integral multiple of a half wave length from the spacing, measured in space wave lengths, of the two inductors in said direction, at the frequency of said waves.
  • an antenna for space wave communication and terminal apparatus for said antenna, said antenna comprising portions spaced in a direction of propagation of the space Waves past said antenna, and current paths connecting said portions" in series with each other and said terminal apparatus, the difference between the electrical lengths of said antenna betwen corresponding elementary lengths of adjacent ones of said portions on the lone hand and said terminal apparatus on the other hand,
  • An antenna comprising a plurality of elements extending in two right-angularly related directions, occupying a common plane,jand series connected in zig-zag form and therefore comprising in part a series of parallel non-colinear elements, the spacing of said parallel elements being so related to the electrical length of a cyclically repeated unit of the antenna as a whole that, with respect to any two points separated by such a unit length, the phase difference between currents induced from a space wave Whose front is parallel with said parallel element will be the same as the corresponding phase dilference between currents at the same point resulting from propagation of a Wave along the antenna between such points.
  • an antenna for radio wave communication comprising a conductor having a height approximately an odd integral multiple of half of the wave length
  • An antenna comprising a plurality of sections, each section comprising two conductors and a third conductor positioned at right angles to said two conductors and connecting said two conductors in series, said two conductors being spaced a quarter space Wave length apart, and another conductor connecting two of said sections in series, the electrical lengths of said two conductors of each section and said last mentioned conductor being such that the time required for current to iow from the electrical center of one of said two conductors of one of said two sect-ions to the electrical center of the corresponding one of said two conductors of the other section is such that at said center points said current is in the same phase relation to the space wave identified with the current.
  • An antenna system for radio wave communication comprising conductors each having a height approximately half of the wave length of the communication wave, and connecting conductors, at right angles to said first conductors, joining said first conductors in series, the spacing of said iirst conductors being alternately a quarter wave length and three quarters of a wave length.
  • An antenna comprising conductors extending in a given direction, and means in a plane at right angles to said conductors connecting said conductors in series, said conductors being so spaced apart, and the length of said antenna between corresponding elementary lengths of said conductors being such that direct propagations in said conductors identified with a space wave moving in a given direction are cumulative at a given point in said antenna, and direct propagations in said conductors identiied with a space Wave moving in another direction are differential at said point.
  • An antenna system having an asymmetrical directional characteristic comprising a plurality of antenna members connected by conductors having substantially no antenna characteristics, and means terminating the antenna system in an impedance equal to the surge impedance of such system.
  • an antenna system comprising a plurality of antenna members connected by conductors having substantially no antenna characteristics, in which direct and reliected propagations identified with a space wave moving in a given direction are cumulative and dierential, respectively, at a point in said antenna, and direct and reiiected propagations identified with a space wave moving in another direction are differential and cumulative, respectively, at said point, and means rendering said reflected propagations substantially zero.
  • An antenna comprising a plurality of main conductors, each approximately onehalf wave length in height, and auxiliary conductors positioned vat right angles to and connecting said main conductors in series, said main conductors being so spaced that the successive spacings are unequal and that at the center points of alternate main 'conductors the current is in the same space relation to the space wave identified with the current.
  • An antenna'for radio wave communication comprising a plurality of main conductors, each approximately one half a Wave length in height, and auxiliary conductors positioned at right angles to and connecting said main conductors in series, said main conductors being so spacedthat the successive spacings are unequal and alternate conductors are separated by a distance of approximately one wave length in the direction of propagation of the communication Wave.

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US173833A 1927-01-10 1927-03-09 Antenna system Expired - Lifetime US1910147A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB764/27A GB272117A (en) 1927-01-10 1927-01-10 Improvements in antenna systems

Publications (1)

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US1910147A true US1910147A (en) 1933-05-23

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US173833A Expired - Lifetime US1910147A (en) 1927-01-10 1927-03-09 Antenna system

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US (1) US1910147A (de)
DE (1) DE561827C (de)
FR (1) FR629045A (de)
GB (1) GB272117A (de)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2433804A (en) * 1943-04-23 1947-12-30 Rca Corp Frequency-modulated pulse radio locating system
US3465343A (en) * 1965-10-11 1969-09-02 Control Data Corp Multi-hop ramp feed for wire-grid lens antenna
US3851131A (en) * 1973-06-28 1974-11-26 Canadian Patents Dev Multimode microwave cavities for microwave heating systems
US5285210A (en) * 1990-05-08 1994-02-08 Nippon Sheet Glass Co., Ltd. Double loop antenna with reactance elements
US5517206A (en) * 1991-07-30 1996-05-14 Ball Corporation Broad band antenna structure
US6426730B1 (en) * 1999-12-27 2002-07-30 Mitsubishi Denki Kabushiki Kaisha Multi-frequency array antenna
US6842156B2 (en) 2001-08-10 2005-01-11 Amplifier Research Corporation Electromagnetic susceptibility testing apparatus

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE755343C (de) * 1935-03-06 1953-05-18 Telefunken Gmbh Richtstrahlantennenanordnung

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2433804A (en) * 1943-04-23 1947-12-30 Rca Corp Frequency-modulated pulse radio locating system
US3465343A (en) * 1965-10-11 1969-09-02 Control Data Corp Multi-hop ramp feed for wire-grid lens antenna
US3851131A (en) * 1973-06-28 1974-11-26 Canadian Patents Dev Multimode microwave cavities for microwave heating systems
US5285210A (en) * 1990-05-08 1994-02-08 Nippon Sheet Glass Co., Ltd. Double loop antenna with reactance elements
US5517206A (en) * 1991-07-30 1996-05-14 Ball Corporation Broad band antenna structure
US6426730B1 (en) * 1999-12-27 2002-07-30 Mitsubishi Denki Kabushiki Kaisha Multi-frequency array antenna
US6842156B2 (en) 2001-08-10 2005-01-11 Amplifier Research Corporation Electromagnetic susceptibility testing apparatus

Also Published As

Publication number Publication date
GB272117A (en) 1927-06-09
DE561827C (de) 1932-10-19
FR629045A (fr) 1927-11-03

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