EP0080507A1 - Antennes a large bande passante - Google Patents

Antennes a large bande passante

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Publication number
EP0080507A1
EP0080507A1 EP19820902227 EP82902227A EP0080507A1 EP 0080507 A1 EP0080507 A1 EP 0080507A1 EP 19820902227 EP19820902227 EP 19820902227 EP 82902227 A EP82902227 A EP 82902227A EP 0080507 A1 EP0080507 A1 EP 0080507A1
Authority
EP
European Patent Office
Prior art keywords
antenna
line
invention defined
elements
impedance
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.)
Withdrawn
Application number
EP19820902227
Other languages
German (de)
English (en)
Inventor
Richard D. Snyder
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.)
Individual
Original Assignee
Individual
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Filing date
Publication date
Application filed by Individual filed Critical Individual
Publication of EP0080507A1 publication Critical patent/EP0080507A1/fr
Withdrawn legal-status Critical Current

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Classifications

    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q9/00—Electrically-short antennas having dimensions not more than twice the operating wavelength and consisting of conductive active radiating elements
    • H01Q9/04—Resonant antennas
    • H01Q9/16—Resonant antennas with feed intermediate between the extremities of the antenna, e.g. centre-fed dipole
    • 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
    • H01Q19/22—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 a secondary device in the form of a single substantially straight conductive element
    • H01Q19/24—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 a secondary device in the form of a single substantially straight conductive element the primary active element being centre-fed and substantially straight, e.g. H-antenna
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q21/00—Antenna arrays or systems
    • H01Q21/06—Arrays of individually energised antenna units similarly polarised and spaced apart
    • H01Q21/08—Arrays of individually energised antenna units similarly polarised and spaced apart the units being spaced along or adjacent to a rectilinear path
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q9/00—Electrically-short antennas having dimensions not more than twice the operating wavelength and consisting of conductive active radiating elements
    • H01Q9/04—Resonant antennas
    • H01Q9/30—Resonant antennas with feed to end of elongated active element, e.g. unipole

Definitions

  • This invention relates to dipole or Hertzian and Marconi or monopole type antennae which exhibit broad ⁇ band characteristics, and to broadband parasitic antenna 10 elements and to antenna arrays which employ such antennae and elements.
  • the standard, or reference, antenna is one-half electrical wave length long. It is divided at the center, and the feed lines are connected one to each leg. Mounted one-quarter wave length, or multiple thereof, above a perfectly conductive ground, such an antenna pre ⁇ sents a 73 ohm radiation resistance at the feed point. If the frequency is increased, the impedance seen by the feed line is a combination of resistance and inductive reactance. If the frequency is decreased, the impedance presented to the feed line is a combination of resistive and compacitive reactance.
  • the transmitter output circuit is a resonant circuit or untuned network set to the transmission fre ⁇ quency.
  • the effective output circuit is untuned with attendant high SWR generated on the feed line.
  • the result can be generation and radiation of har ⁇ monic signals, excessive and damaging voltages and circu ⁇ lating currents, and reduction of efficiency and radiated energy.
  • the transmitter can be protected by the inclusion of "matching" networks in the transmission feed line from the transmitter to the antenna, but the use of a matching network solves only part of the problem. In practice, it is necessary to retune the transmitter or the matching network when changing transmitting frequency more than two or three percent.
  • the amount of returning that is required when changing frequency across a radio service band can be re ⁇ substituted by the use of a "broadband" antenna.
  • a "broadband" antenna Such an an- tenna incorporates variations from the standard dipole or Marconi antenna the effect of which is to minimize the in ⁇ crease in reactive impedance at the antenna feed point with frequency at frequencies higher and lower than the resonant frequency.
  • An antenna exhibits characteristics similar to those exhibited by a lumped resonant circuit and, just as- in the lumped resonant circuit, the change in antenna impedance with frequency is minimized if the Q of the system is low. The Q is reduced if the antenna conduc ⁇ tors are increased in diameter relative to antenna length. It is also known that the band width, the frequency devia ⁇ tion that can be accommodated without undue increase in reactance, increases as radiation resistance increases.
  • the reference dipole exhibits exactly 73 ohms radia ⁇ tion resistance only in free space high above a perfect ground.
  • radiation resistance is decreased by an increase in radiator diameter relative to length, by reflective objects mounted near the antenna, and by a decrease in antenna height below one-quarter wave length, particularly below 5 MHz.
  • the double apelooka is formed by a length of coaxial cable the outer braid of which is severed and separated at the midpoint along its length.
  • the braid at each side of the separation is connected to a respectively associated side of the feed line.
  • the center conductor and the outer shield braid are connected together.
  • the antenna is tuned by the addition of lengths of wire to each end of the coaxial section so that the combination of braid and end section is electri- cally one-quarter wave length long in air.
  • Each half of the coaxial cable is also one-quarter wave length long electrically, but, because the propogation velocity is less in the coaxial cable, it is physically shorter by the length of the end section.
  • the end sections are formed of open wire transmission line.
  • the band width limitations of the dipole antenna extend to the Marconi antenna.
  • the Marconi antenna in most common forms, is an odd number of electrical quarter waves long and is mounted vertically.
  • the earth reflects radio waves in a manner similar to reflection of light by a mirror.
  • an "image" of the antenna can be considered to exist below ground.
  • the combination of the antenna and its image re-ulate a dipole except that the contribution of the image portion to radiation resistance measured at the center point of the dipole (base of the Marconi portion) depends upon the conductivity of earth.
  • the analogy to mirror reflec ⁇ tion is exact.
  • the mirror can accomplish reflec- tion of three dimensional objects, although it occupies only a plane, so the image antenna is reflected from a plane in the earth. That action can be simulated by elec ⁇ trical conductors extending radially in a plane from the bas of a Marconi vertical antenna whether the plane of the radial conductors lies at or above the surface of the earth.
  • ground plane embraces both the earth and the simulated earth.
  • the vertical antenna is one-quarter wave length long, and the ground plane is a perfect conductor, the radiation resistance is half of that of the standard dipole. In practice, perfect conductivity in the ground plane is not achieved, and it is customary in antenna design to assume a ground plane resistance that reduces radiation resistance to 25 ohms which is one-half of what is assumed in dipole design.
  • the invention provides a dipole antenna which incorporates two matching stubs, one associated with each leg of the dipole.
  • the stubs intro ⁇ Jerusalem reactance to oppose the off-frequency reactance of the dipole antenna.
  • Each stub is formed by a length of coaxial cable whose outer braid constitutes part of the antenna radiator itself.
  • the stubs are one-quarter electrical wave length long, or nearly so, and are shorted at their outer ends. They are connected in parallel with one another and with the antenna by being cross-connected to the feed point.
  • an antenna so ar- ranged can be operated at a standing ratio less than two to one with a standing wave ratio change of no more than 0.5 over a band width as much as fifteen to twenty percent of band center frequency.
  • the antenna system presents to the balun a resistive impedance of about 50 ohms (2 to 1 SWR) at midfrequency, and a nearly resistive impedance of about 200 ohms (2 to 1 SWR) at band edges. It presents a complex impedance of about 100 plus or minus j 40 ohms (1.5 to 1 SWR at the midfrequencies between band center and upper and lower band edge fre ⁇ quencies (see Figs. 7, 8 and 9).
  • Antenna system impedances of that order result from an arrangement in which the legs are formed from 5 coaxial cable having an effective surge impedance of about 25 ohms.
  • the coaxial sections are shorted at their outer ends, and each has electrical length of one-quarter wave length.
  • the center conductor of each cable section is con ⁇ nected at the feed point to the braid of the opposite cable 10 section.
  • the radiator itself is formed by the outer braid of the two cable sections and wire end extensions which increase the overall electrical length of the radiator to one-half wave length in air.
  • the antenna of the invention is not arranged to achieve minimum possible standing wave ratio at band center. Instead, the invention combines a center frequency mismatch comparable to the mismatch at band
  • the antenna and compensation stubs is one-fourth at resonant frequency of the nearly resistive impedance at band edge frequencies, and about one-half of the complex impedance at the upper and lower frequencies midway between resonant frequency and band edge frequencies.
  • the antenna 30 in the preferred embodiment has an effective characteristic impedance of 100 ohms or twice the value of the combined impedance of the antenna and compensation system at reso ⁇ nant frequency.
  • the antenna system presents a 50 ohm load at the feed point at resonant fre ⁇ quency.
  • OSPI impedance . is increased to about 200 ohms, and at the mid- frequencies, between resonance and band edges, the complex impedance is about 100 plus or minus j 40 ohms. Those values are achieved by making the stubs of 25 ohm surge impedance cable. Alternatively, cable of higher surge impedance values may be substituted and the required feed point surge impedance reached by the addition of conven- tional stubs having appropriate characteristic impedance.
  • feed point impedance can be made by changing the length of the matching stubs, but the electrical length should not differ from mid-frequency quarter wave length by more than about five percent. Greater deviation results in excessive impedance and attendant SWR at the opposite band edge.
  • the basic structure of the invention is an antenna leg a portion of which is formed by a two- conductor transmission line one conductor of which is free to radiate and the other of which is not.
  • the trans ⁇ mission line conductors are shorted together at one end of the line whereby the non-radiating conductor combines with the other conductor of the line .to form an impedance modi ⁇ fying stub, and said other conductor of the line forms part of the antenna leg.
  • the transmission line exhibits 25 ohms surge impedance and is a coaxial line or cable.
  • antenna elements constructed according to the inven- tion, and short circuited at one end will serve as broad band passive radiators - as directors and reflectors in directive antenna systems.
  • To provide improved and broadband vertical antennae and passive radiators or parasitic elements, and to provide improved directive beam antennae and broad ⁇ side and colinear and other antennae arrays are other ob ⁇ jects of the invention.
  • Figure 1 is a diagram of a reference dipole antenna connected by a balun and coaxial feed line to a radio transmitter;
  • FIG. 2 is a diagram of an antenna system incorporating the invention
  • FIG. 3 is a diagram of a modification of the antenna system of Figure 2;
  • Figure 4 is a graph in which the relation ⁇ ship of standing wave ratio to frequency for systems according to the invention are compared with that of prior art systems;
  • Figure 5 is a graph of the changes in standard dipole antenna resistive and reactive im ⁇ pedance with antenna length
  • Figure 6 is a diagram of a second modifi ⁇ cation of the antenna system of Figure 2;
  • FIGS 7, 8 and 9 are diagrams of the antenna system of the invention referred to the antenna side of the balun transformer showing the equivalent circuits at frequencies fo. fi and f ⁇ . and fLO and fjil. respectively;
  • Figure 10 is a schematic diagram of a modi ⁇ fied dipole antenna system according to the inven- • tion
  • Figure 11 is a schematic diagram of a Marconi type antenna system according to the inven ⁇ tion
  • Figure 12 is a schematic diagram of two modified Marconi type antenna systems according to the invention.
  • Figure 13 shows schematic diagrams of Marconi forms of the passive or parasitic radiator elements of the invention.
  • Figures 14. 15 and 16 are schematic diagrams of dipole forms of the passive or para ⁇ sitic radiator elements of the invention.
  • Figure 17 is a schematic diagram of an an- tenna array employing dipole radiators and dipole parasitic radiators
  • Figure 18 is a schematic diagram of an antenna array employing Marconi type radiators and Marconi type parasitic elements.
  • Figure 19 is a schematic diagram of a vari ⁇ ation of the antenna shown in Figure 10.
  • the preferred forms of the invention employ a radiation element, examples of which are shown in Figure 13, which is nominally one-quarter wave length long elec ⁇ trically at the design center frequency for operation.
  • That element comprises an extension conductor connected to the outer end of a length of two-conductor transmission line.
  • One conductor of the line does not radiate, and the velocity of current flow in the non-radiating conductor is less than in the other conductor and extension conduc ⁇ tor.
  • the element exhibits two elec- trical lengths, one along the path of the non-radiating conductor and the other along the path formed ' by the radiating conductor of the line and the extension.
  • the inner conductor can be made to serve as a non-radiat ⁇ ing matching stub for the outer conductor of the element of which it is a part, or of another element.
  • coaxial cable will be used herein to mean transmission lines having at least two con ⁇ ductors one of which can radiate and the other of which cannot.
  • the term describes coaxial line and coaxial cable and certain wave guides and other special forms that function in similar manner.
  • the terms "radiator” and “transmitter” will be used in connection with explanations of applications for the invention with the understanding that receiving and receivers and transceivers and the like are also intended because broadbanding of antennae is also important in the reception of signals.
  • coaxial cable the basic element of the invention is a length of coaxial cable and an extension conductor connected to the outer conductor of the cable.
  • extension conductor connected to the outer conductor of the cable.
  • the invention is not limited to straight forms.
  • the basic element is one-quarter electrical wave length long, but it can be extended to odd multiples of one-quarter wave length.
  • two of the basic elements are employed, usually in a straight line * or V-shaped configuration.
  • the basic element When the basic element is employed as a radiating or receiving element of an antenna system, energy is fed to it, or derived from it, at the end of the coaxial cable opposite the end at which the extension conductor is con ⁇ nected.
  • the inner and outer conductors of the line are shorted together at the end at which the extension conductor is connected.
  • the extension conductor may not be connected to the center conductor of the coaxial cable and the short is made at the other end of the line. This causes the element to "look longer" (more inductive) elec ⁇ trically at lower than band-center frequencies, and to "look shorter” (more capacitive) electrically at higher than band- center frequencies. In this way, conjugate reactive com ⁇ pensation is achieved for the radiating element over a
  • the coaxial segment of each side of the dipole serves as the stub for the other leg of the dipole.
  • the coaxial section serves as the stub for the leg of which it forms a part.
  • the inner and outer conductors of the coaxial cable may be shorted to ⁇ gether at the end opposite the end to which the extension conductor is connected in some applications, including some in which the element is to serve as a parasitic ele- ment. That is true even when two elements are arranged end to end to form a dipole parasitic reflector or director.
  • the usually preferred form has the inner and outer conductors of the coaxial section shorted at the end to which the extension is connected.
  • the reference antenna 10 is shown in diagrammatic form in Figure 1. It consists of two conductor legs 12 and 14, each one electrical quarter wave long at the operating frequency. The legs are arranged end to end in a straight line and are mounted horizontally in free space or in air one-quarter wave length, or a multiple thereof, above a perfectly conductive ground plane. When constructed of conductors approaching infinitely small diameter, such an antenna exhibits 73 ohms resistive radiation impedance at the center feed point 16. That impedance is exhibited when
  • the antenna is driven at the frequency for which the antenna is one-half electrical wave longth long.
  • the resistive impedance is above or below 73 ohms.
  • the antenna exhibits complex impedance.
  • the impedance has resistive and induc ⁇ tive components, and at lower frequency, the impedance has resistive and capacitive components.
  • the wave length is relatively short, other special antenna configurations are feasible.
  • one-quarter wave length is ten meters. As frequency is decreased, wave length increases, and at or below 5 MHz it becomes increasingly difficult to erect the antenna at least one-quarter wave length above ground.
  • Coaxial cable is much more common and much more convenient than open wire transmission line, so a coaxial feed line 18 has been selected for illustration in Figure 1. It is possible for radiation to occur from the outer conductor of a coaxial line, but not from the inner con ⁇ ductor. For that reason, coaxial cables are called un ⁇ balanced lines.
  • the antenna itself is symmetrical, or balanced. It is usual to interconnect the unbalanced feed line with a balanced antenna through a transformer 20 to prevent feed line outer conductor radiation. That trans ⁇ former can have any turns ratio needed to match the surge
  • the output stage of the transmitter 22 ordinarily includes an impedanc matching network by which the impedance of the feed line 18 can be matched to the plate resistance or equivalent impe ⁇ dance of the last stage in the transmitter.
  • the input network of receivers is similar.
  • the overall length of the radiator is one-half wave length.
  • the velocity of electrical energy in a wire is approximately ninety-five percent of the velocity in a vacuum or free space so that the physical length of the antenna is given by the expression "the velocity of light in meters per second times 0.95, all divided by the opera- ting frequency of the antenna in Hertz.”
  • the band center frequency at 3.75 MHz has been labelled fg.
  • the upper and lower band edges at 4.0 MHz and 3.5 MHz have been labelled f-t- ⁇ - and fL0 > respectively.
  • the frequency 3.62 MHz, approximately midway between f ⁇ ,o and f ⁇ , is called the midlow frequency and is labelled fl.
  • 3.87 MHz is called the r ⁇ dhigh frequency and is labelled £- .
  • the numerals represent standing wave ratios.
  • Ratios from one to three are shown. Many modern commercially available transmitters cannot be operated safely at standing wave ratios exceeding two to one. If the transmitter 22 in Figure 1 had that limi- tation, and if the antenna 10 was cut to center frequency f ⁇ , it would not be possible to retune the transmitter if its. operating frequency were changed from fo to a value approaching f or f2- That is because the standing wave ratio curve for the reference antenna, the curve 28 formed of short dashed lines, rises rapidly above two to one at frequencies approaching fl and at frequencies approaching f2. In practice, to ensure optimum operation, the trans ⁇ mitter output would be retuned at even lesser frequency excursions from £Q .
  • the curve 30 formed of long dashes in Figure 4 represents the standing wave ratio curve that can be ex ⁇ pected with the double apelooka antenna. It is more shallow than curve 28, but rises above a standing wave ratio of two to one before reaching the band edges. Consequently, the transmitter 22 could be operated safely into a double apelooka antenna across a wider but still insufficient por ⁇ tion of the 3.5 MHz to 4.0 MHz band without retuning. Also, the change in the standing wave ratio over the band width is greater than 1.0, so that much reloading is still required if optimum efficiency and minimum heating is to be achieved. That difficulty is overcome in an antenna which exhibits standing wave ratio variation of the form depicted by curve 32.
  • Curve 32 describes the kind of standing wave ratio uniformity that can be achieved over a service band using an antenna according to the invention. It is, in fact, a description of the standing wave ratio that is achieved in the system depicted in Figure 2.
  • the Figure 2 system includes two compensation stubs, 40 at the right and 42 at the left. At their inner ends, those stubs are cross-connected to a balun transformer generally designated 44. At its outer end, the stub 40 has its center conductor and braid interconnected by a conductor 46, and the two are connected to a wire end extension 48.
  • the stub 42 has its braid con ⁇ nected to the center conductor by a connector 50.
  • the braid and center connector are connected to a wire end extension 52.
  • the radiating portion of the antenna is form by two legs each one-quarter electrical wave length long in air. One leg is formed by the combination of end wire extension 52 and the outer conductor or braid of stub 42. The other leg is formed by the combination of end wire extension 48 and the outer conductor or braid of compensa ⁇ tion stub 40.
  • the stub 40 and the stub 42 are lengths of coaxial cable having a surge impedance of 25 ohms.
  • the center conductor of stub 40 is connected by a conductor 56 to terminal 58 of the balun 44.
  • Terminal 58 is also connected to the outer conductor of stub 42.
  • the inner conductor of stub 42 is connected by a line 60 to terminal 62 of the balun 44 which terminal is also con ⁇ nected to the outer conductor, the braid, of stub 40.
  • Terminals 58 and 62 of the balun are interconnected by windings 64 and 66 of the balun.
  • the terminals 58 and 62 are the output terminals of the balun.
  • One is connected to the leg formed by extension 52 and the outer conductor of stub 42. That one is connected to terminal 58.
  • Terminal 62 is connected to the radiating leg formed by the outer conductor of stub 40 and extension 48.
  • the radiating legs of the antennae are represented by a feed point impedance which is connected across secondary terminals 58 and 62.
  • the stubs 40 and 42 are connected in parallel with one another across those same secondary terminals.
  • the feed point impedance of the radiator and the impedance of the stub 40 and the impe ⁇ dance of the stub 42 are all connected in parallel with one another across the secondary terminals 58 and 62 which can be called the feed point for the antenna system.
  • the combined length of the outer conductor of stub 40 and extension 48 are one- quarter wave length long electrically in air at frequency fg.
  • the combined electrical length of the outer conductor of stub 42 and extension 52 is one-quarter wave length in air at frequency fg.
  • the physical length of each of those two lengths is approximately ninety-five percent of a quarter wave length in free space.
  • Each of the stubs 40 and 42 is also one electrical quarter wave length long at frequency fg.
  • the velocity constant for representative coaxial cable is sixty-six percent of the velocity in free space.
  • the physical length of the stubs 40 and 42 is less than the physical length of the radiating legs, notwithstanding that their electrical lengths are essentially equal.
  • the radiator impedance will be resis ⁇ tive and have a value of about 50 ohms. It is less than the theoretical value of 73 ohms because of the larger conductor diameter and nearness or proximity to earth ground. Twenty-five ohms, and 25 ohms, connected in parallel, is equivalent to 12.5 ohms, and that is the equi ⁇ valent compensating surge impedance presented to the an ⁇ tenna feed point. However, the feed point impedance of the antenna system remains essentially 50 ohms at fg.
  • the feed line employs a 50 ohm coaxial cable which is shown in Figure 2 and identified by the reference numeral 68. It is not required In the invention that that line have any prescribed operational length.
  • the balun 44 has a turns ratio that will limit the maximum mismatch between the impedance of the antenna system and the surge impedance of the coaxial feed line to a ratio of less than 2 to 1, and the feed line 68 need not be a multiple of half wave lengths long, except for purposes of accurately measuring feed point SWR at the transmitter output with conventional apparatus, but can have any length.
  • Most transmitters have output circuit adjustability to accommodate that small degree of mismatch.
  • the transmitter 70 of Figure 2 has that kind of adjustability.
  • the input terminals of the balun are numbered 72 and 74, respectively.
  • Terminal 74 is connected to the junction of balun windings 64 and 66 and to earth ground.
  • Input terminal 72 is at the end of a third balun winding 76 whose other end is connected to terminal 58.
  • windings 64 and 76 constitute the primary windings of the balun
  • the combination of windings 64 and 66 constitute the secondary circuit of the balun.
  • the three windings are trifilar windings on a toroidal core. The black dot on each winding indicates magnetic polarity according to established conventions.
  • the turns ratio between pri ⁇ mary and secondary is selected such that the impedance of the antenna system appears to be about 25 ohms from the primary side of the balun at fg, and so that the impedance of the feed line 68 appears to be about 100 ohms when looking from the secondary side of the balun at fg.
  • the impedance transformation ratio across the transformer is essentially 2 to 1.
  • the standing wave ratio in the feed line 68 is approximately 2 to 1 at fg. That figure is improved as the radiation resistance of the antenna is increased in operating excursions from fg toward f and f£, to approximately 1.5 to 1. Excursions in operating frequency beyond fi and f degrades SWR which approaches 2 to 1 again at band edge frequencies of ⁇ ⁇ .Q and fjn-
  • Figure 5 is a graph on which is plotted the variation in resistive impedance and reactance impedance that appears across a reference dipole antenna in which the ratio of conductor length to conductor diameter is about 1000.
  • the reactance is near zero. It becomes positive or inductive at longer wave lengths or higher frequencies.
  • the reactance becomes nega- tive or capacitive at shorter wave lengths or lower fre ⁇ quencies.
  • the graph also shows that the resistive compon ⁇ ent of feed point impedance increases as wave length is increased or frequency is increased, whereas the feed point resistance is reduced.somewhat at shorter wave lengths or lower frequencies.
  • the standing wave ratio will be slightly different at frequencies below mid-frequency than it is at frequencies above mid-frequency, and, indeed, that is reflected in the shape of the curve 32 in Figure 4 where the region 80 describes a slightly different standing wave ratio than does region 82 above mid-frequency.
  • OMPl not exactly the inverse of the compensation stub reactance means that complete cancellation can occur at only one set of frequencies. It is preferred to make the compensation stubs of coaxial cable having a surge impedance of 25 ohms because the reactance curve for their 12.5 ohms equivalent places the reactance cancellation points at frequencies that differ from mid-frequency by plus and minus 6 to 7 percent of mid-frequency, as shown in Figure 4 near f-r ⁇ and fjji band edges.
  • the resistive feed point impedance at frequen ⁇ cies six to seven percent above and below resonant fre- quency is near four times the resistive impedance at re ⁇ sonant frequency. That number varies, as does radiation resistance, with antenna height, radiator diameter, and, to some extent, with ground conductivity.
  • the cable surge impedance and turns ratio in the balun that are described as preferred in the embodiment of Figure 2 assume a band edge resistive impedance of about 200 ohms. Looking from the primary side of the balun, that impedance looks like about 100 ohms which is twice the surge impedance of trans ⁇ mission line 68 so that the standing wave ratio at band edges is again essentially 2.0 to 1.
  • the system 100 employs an antenna system like that of Figure 2 except that, in this case, the stubs 102 and 104 are formed of coaxial cable whose, stub surge impedance is 50 ohms. In parallel, they present a 25 ohm surge impedance stub across the feed point of the antenna system. That value is effectively reduced by the inclusion of a third set of 50 ohm stubs 106.
  • the equivalent surge impedance of these 50 ohm stubs is 12.5 ohms on the primary side of the balun 108.
  • the added stubs would reduce the com- bined feed point effective stub surge impedance to essen ⁇ tially 12.5 ohms.
  • the trans ⁇ former 108 which is assumed to have an impedance transfor ⁇ mation ratio of 1 to 2. Therefore, so that it will have the same electrical effect as a 25 ohm stub on the secon ⁇ dary side of the transformer, the stubs 106 are constructed of four 50 ohm coaxial cables in parallel on the primary side of the balun.
  • the antenna of Figure 3 is cumbersome in its construction and will perform somewhat differently than does the antenna of Figure 2, primarily due to increases in antenna system losses due to the use of four stubs 106 connected across the primary side of the balun to achieve the 12.5 ohm equivalent compensation surge impedance across the antenna feed point. Performance of the two systems can be brought more into conformity by omitting the stubs 106 and substituting for them a third stub of 50 ohm cable in parallel with stub 102, and a fourth stub of 50 ohm cable in parallel with stub 104 as shown in Figure 6.
  • Figure 2 is preferred due to constructional simplicity and less tendency to sag because it is less heavy.
  • Figure 6 has been included to show that the required compensating stub impedance can be achieved by connecting several stubs In parallel. In this case, two 50 ohm stubs 200 and 202 are connected in parallel to replace a single 25 ohm stub. Similarly, stubs 204 and 206 are made of 50 ohm cable and they replace a single 25 ohm stub.
  • the electrical length of the stubs is the same as the electrical length of the radiating legs. That is not essential to successful operation of the antenna; although the average standing wave ratio across the band will be in ⁇ creased somewhat, it is possible to flatten the standing wave ratio curve across one-half of the service band by cutting the stubs to an electrical length which differs in small degree from the electrical length of the radiators whereby to add capacitive or inductive reactance to feed point impedance at center frequency.
  • the electrical length should not be changed by more than about five percent of center frequency wave length because greater differential will result in excessive standing wave ratios at opposite band edges and changes with antenna environ ⁇ mental differences that are difficult to predict.
  • the stubs are cut to a length that represents one-quarter electrical wave length of what is to be the center operating frequency of the antenna.
  • the end extensions are made longer than required to make the radiating legs approximately one elec- trical quarter wave length long at that frequency.
  • the antenna is then installed in that form, and standing wave ratio measurements are made to determine its performance in the actual environment in which the antenna will remain. If the graph of standing wave ratio with frequency has a center hump, that suggests that the radiation resistance of the antenna should be adjusted, the height can be ad ⁇ justed up or down and/or the ends of the dipole can be lowered or raised in inverted V form.
  • the process for adjusting and tuning antennae is substantially the same as the process used for adjusting and tuning the standard dipole antennae. It is preferred, because the operation of the two legs of the dipole is thus made more uniform, that the coaxial line of each leg serve as the reactance modifying stub for the other. However, that is not essential. It has been discovered that the coaxial line can serve as the matching stub for its own leg. That can be done in either of two ways.
  • the reactive impedance of the stubs is achieved by removing the short circuit at the outer end of the coaxial cable section and shorting the inner and outer conductors of the cables at the inner end as shown in Figure 10.
  • the inner conduc ⁇ tors 300 and 302 have been represented by dashed lines to show that end extension conductors 304 and 306 are connected to the conductors 300 and 302 at the outer ends of cables 309 and 311, respectively.
  • the balun or matching trans ⁇ former 312 comprises three windings 314, 316 and 318 magnetically coupled as indicated by the black dot conven ⁇ tion.
  • the inner and outer conductors at the inner end of cable 309 are connected to the transformer at a secondary terminal between coils.314 and 316.
  • the two conductors of cable 311 are shorted at the inner end and connected to the secondary terminal at the outer end of the balun winding 318
  • the input terminals are located at the outer end of coil 314 and at the junction of coils 316 and 318.
  • the cir- cuit configuration of Figure 10 differs from that of Fig ⁇ ure 2 in the position of the short circuits and in the fact that the center conductors are not cross-connected across the secondary winding of the balun transformer.
  • the stubs and antennae are connected in series in the circuit con- figuration of Figure 10.
  • each coaxial cable serve as the stub for the leg of which it is a part is illustrated in Figures 11 through 14.
  • the antenna system of Figure 11 is derived from the arrangement of Figure 2. It is equivalent to half of the antenna system of Figure 2. Physically and electrically, only one leg 320 and half of an output side 330 of a balun transformer, like the one shown in Figure 2, are employed. To complete the system, the balun output is connected across the two coaxial cable conductors at the inner end of the cable. One side of this connection, the center conductor side in this example, is connected to a ground plane 324. Doing that will supply the ground plane "image" to form a Marconi type antenna. It is not essential, but in practice such an antenna is usually mounted vertically.
  • FIG. 12 Another form of Marconi antenna is shown in Fig ⁇ ure 12.
  • the reactance of the stub was achieved by removing the short circuit from the outer end of the coaxial cable stub and short circuiting the inner end of the cable section instead.
  • the center conductor and outer conductor at the inner end of the coaxial section are connected to one output terminal of the balun and the other output terminal of the balun is connected to what corresponds to the other leg of the
  • the extension conductor 340 is con ⁇ nected to the outer end of the conductor 342 of cable section 344.
  • the two cable conductors are connected to ⁇ gether at the cable's inner end by a short circuit 346.
  • the short is connected to one output terminal of balun 348 at the junction between the two coils of the balun.
  • the other output terminal of the balun at the other end of the coil 350 and one input terminal are connected to the ground plane 352.
  • the other input terminal is connected to the other end of balun coil 354.
  • the invention requires that the stub exhibit reactance opposing the reactance exhibited by the antenna leg with which it is associated. That effect can be a- chieved by arranging for current flow in opposite directions in the leg and stub as in Figures 2 and 11, or by reversing stub configuration between shorted circuit termination to open circuit termination, as in Figures 10 and 12.
  • Antenna elements to which energy is supplied by a transmitter or from which energy is removed as by a receiver are called active or driven elements.
  • the legs of the antenna systems in Figures 1, 2, 3, 6, 10, 11 and 12 are driven elements.
  • the legs or elements shown in Figures 13, 14 and 15 are passive or parasitic elements. They are not connected to an energy source or load, but, when placed in a field of radio waves, energy from the field is induced in the passive element causing current flow in the passive element. If the element is an odd multiple of one-quarter electrical wave lengths long, if th element is resonant at the frequency of the radio energy, standing waves of voltage and current are developed and the energy that was absorbed is radiated away. Termed parasitic, such elements are employed in directive arrays.
  • the driven element or elements are placed in parallel with, and in juxtaposition to, the driven element or elements.
  • the spacing between parasi and driven elements determines whether the parasitic elemen will serve to aid or oppose radiation from the driven ele ⁇ ment. If re-radiation from the parasitic element tends to cancel radiation from the driven element, the parasitic element is called a reflector. If re-radiation reinforces the driven element output, the parasitic element is called director. If the driven and parasitic elements are ar ⁇ ranged in a plane with reflectors on one side of the driven element and directors on the other side, more of the output energy from the driven element will be directed in the direction of the plane on the side toward the directors tha will be radiated in other directions. Antenna systems of that kind are called beams.
  • two or more beams are arrang in a common plane in juxtaposition so that they are direc- tive in the same direction, they are called a colinear array. If they are juxtaposed in parallel planes and are directive in like direction, they are called a stacked array.
  • a number of juxtaposed driven elements arranged in a plane are called a broadside array when spaced and phased to cancel the radiation of adjacent elements, and are called an endfire array when spaced and phased to rein ⁇ force the radiation of adjacent elements.
  • FIG. 17 depicts a colinear array formed by two beams each of which includes four driven elements arranged as two dipoles, and eight parasitic elements arranged as one dipol reflector and three dipole directors.
  • the array of Figure 18 is formed by a parallel two-section, Marconi broadside array each section of which is formed by four sets of juxta- posed driven elements.
  • each section the driven elements are spaced to cancel radiation of the next element.
  • the two sections are spaced so that radiation in the broadside direction is reinforced.
  • a parasitic reflector at each end of each section tends to cancel end fire radiation from the section.
  • the symbol numbered 400 in Figures 17 and 18 represent any drive element of the kind shown among Figures 2, 3, 6, 10 and 11.
  • the symbol 402 in Figures 17 and 18 represent any parasitic element of the kind shown In Figures 13, 14 and 15 of the drawing.
  • the efficiency of re-radia tion can be increased by short circuiting the coil 330. If the coil is shorted so that the outer conductor is connecte directly to the ground plane 324, the inner and outer con ⁇ ductors at the inner end of coaxial line 320 will be shorte In that circumstance, the line will be shorted at both ends and the coaxial line will not be effective as an impedance modifier. However, if the short is removed from one end or the other of the line, it will be effective. As voltage an current change in the outer conductor of the line, the electrical stress, the voltage gradient across the dielec- tive of the line, is changed. As an incident to that stress current is caused to flow in the center conductor and that flow is in a direction opposite to flow in the outer conduct
  • the antenna element of Figure 11 in parasitic form is shown in two forms in Figure 13.
  • the balun has been omitted and the coaxial line's inner conductor is connected to ground plane 500 in both forms.
  • Element 502 has the line conductors shorted at the inner end of the line
  • element 504 has the line conductors shorted at the outer end of the line.
  • These same two forms of parasitic elements are shown in dipole configuration in Figures 14 and 15.
  • two elements, like element 502 of Figure 13 are arranged on a common line with the inner end of one connected to the inner end of the other. Instead of being connected to a ground plane, the short circuit at the in ⁇ ner end of each coaxial line is' connected to the short cir- cuit of the other by a conductor 508.
  • That conductor 508 may be connected to the ground plane if desired, and that has an advantage in the construction of a beam antenna. There is no need to insulate the inner ends of the elements from the boom on which the elements are mounted if the boom is made of metal and is grounded.
  • the parasitic dipole of Figure 15 is derived from the form of the element 504 in Figure 13 and from the interconnection arrangement of Figure 2.
  • two elements similar to element 504 of Figure 13 are arranged in dipole form.
  • the outer conductor 510 of element 512 is connected to extension conductor 514 and to the inner conductor of the coaxial line at the outer end of the line.
  • the center conductor is con- nected by conductor 516 to the outer conductor 518 of the coaxial line of element 520.
  • the outer conductor 510 of the element 512 is connected by a conductor 522 to the center conductor of the coaxial line of element 520.
  • That center conductor is shorted to outer conductor 518 and extension conductor 524 at the outer end of the coaxial line of element 520.
  • the coaxial line of element 520 serves as the stub for element 512
  • the coaxial line of element 512 serves as the stub for element 520.
  • a major advantage of the invention is that the relative impedance of the primary leg and of the stub may be altered merely by changing the relative length of the extension conductor and the coaxial transmission line. Reversing the position of the short circuit extends the range of relative impedance difference that is possible by changing relative length, and the boundaries of the range can be adjusted by selection of the transmission line surge impedance.
  • the length of the transmission line portion, and of the extension conductor portions of these several active and parasitic antenna elements, are selected according to the principles explained in connection with the develop ⁇ ment above of the elements of Figure 2.
  • pre ⁇ ferred elements employed 25 ohm coaxial line.
  • the pre ⁇ ferred embodiments of the remaining figures also are formed using 25 ohm lines unless otherwise noted.
  • element 504 has its end extension 530 connected to the center con- ductor of line 532 at the outer end of the line, and the line conductors are shorted at the inner end.
  • element 504 has its extension conductor 534 connected to the outer conductor of line 536 at the outer end of the line and the line conductors are shorted at their outer end.
  • the part of the antenna leg formed by the stub experiences cur ⁇ rent flow which can be characterized as the composite of antenna current and stub current.
  • element 360 has been added in Figure 12.
  • the outer end of its line 362 is shorted and connected to the end extension 364.
  • Comparison of Figures 11 and 12 shows that the same con ⁇ figuration, element 320 in Figure 11 and element 360 in Figure 12, can be driven by connecting either the inner or outer conductor of the line to the energy source.
  • Figure 12 The two elements of Figure 12 are duplicated and arranged in line with their inner ends in proximity in Figures 10 and 19 to form dipoles to Illustrate that element 344 can be used in a dipole as in Figure 10, and that element 360 can be used in a dipole as in Figure 19.
  • the two passive elements of Figure 13 are dupli ⁇ cated In Figures 14 and 16, and arranged in line with their inner ends in proximity to show that both element forms can be used in a dipole arrangement.
  • An important modification of the invention is to incorporate a reactor, either an inductor or a capacitor, in the end extension portion of the antenna or parasitic element to alter its physical length without altering its electrical length. It is intended that the antenna and parasitic element forms, with and without such odifications. are represented by the symbols used in the drawings to
  • Inclusion of capacitive reactance is useful in the case of vertical elements to permit lowering of the physical height.
  • In ⁇ clusion of inductive reactance, in the form of a loading coil, is useful in the case of horizontal antennae to permit shorter physical length.

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Abstract

L'excursion de la frequence de travail que des elements d'un systeme d'antenne peuvent controler sans qu'il ne se produise de serieux desaccords de la ligne de transmission est augmentee lorsque l'antenne est construite de maniere telle que les parties interieures (40, 42) de ses jambes (40, 48 et 42, 50) sont formees d'une ligne de transmission co-axiale connectee de maniere que le conducteur exterieur fait partie du radiateur et que les conducteurs interieur et exterieur de la ligne agissent de concert pour former des adaptateurs de compensation dont l'impedance varie avec la frequence de maniere a supprimer ou a s'opposer a la reactance que presentent les jambes de l'antenne lors du changement de frequence. Les adaptateurs sont connectes en serie ou en parallele avec le point d'alimentation de l'antenne et les elements parasites. L'impedance d'onde est selectionnee de maniere que les elements commandes par l'antenne (presque resistifs) et la source de signaux, ainsi que les elements parasites faisant l'objet de la presente invention, sont en desaccord aux frequences d'extremites de bande et a la frequence de bande centrale selon des valeurs approximativement analogues. L'impedance est selectionnee de maniere que l'antenne (quelque peu reactive) et la source de signaux se trouvent dans une situation plus proche de l'accord a des frequences a mi-chemin entre la frequence de bande centrale et les frequences laterales de la bande.
EP19820902227 1981-06-05 1982-06-01 Antennes a large bande passante Withdrawn EP0080507A1 (fr)

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US27074681A 1981-06-05 1981-06-05
US270746 1981-06-05

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Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2321454A (en) * 1941-11-22 1943-06-08 Rca Corp Multiple section antenna
US2313046A (en) * 1942-03-26 1943-03-09 Bruce Malcolm Radio antenna system
US3656167A (en) * 1969-11-25 1972-04-11 Plessey Co Ltd Dipole radio antennae

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO8204358A1 *

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