US3641578A - Discone antenna - Google Patents

Discone antenna Download PDF

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US3641578A
US3641578A US56830A US3641578DA US3641578A US 3641578 A US3641578 A US 3641578A US 56830 A US56830 A US 56830A US 3641578D A US3641578D A US 3641578DA US 3641578 A US3641578 A US 3641578A
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port
coaxial lines
energy
phase
coaxial
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William M Spanos
Michael S Polgar
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TDK Micronas GmbH
ITT Inc
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Deutsche ITT Industries GmbH
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    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q21/00Antenna arrays or systems
    • H01Q21/24Combinations of antenna units polarised in different directions for transmitting or receiving circularly and elliptically polarised waves or waves linearly polarised in any direction
    • H01Q21/26Turnstile or like antennas comprising arrangements of three or more elongated elements disposed radially and symmetrically in a horizontal plane about a common centre

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  • ABSTRACT A multimode discone antenna providing simultaneously, without interference, rightand left-hand circularly polarized omnidirectional patterns and a vertically polarized omnidirectional pattern.
  • Four coaxial cables are disposed parallel to each other with the outer conductors electrically coupled together.
  • An extension of the central conductor of each coaxial line is extended downward from the upper end of and at a given angle less than to the associated one of the coaxial are excited in phase by second energy, a vertically polarized omnidirectional pattern.
  • An embodiment of a feed arrangement is disclosed enabling the four coaxial lines to be excited in phase by the second energy and simultaneously to enable each of the four coaxial lines to be excited by the different orthogonally related first energy.
  • An object of the present invention is to provide a multimode antenna suitable for utilization in satellite systems.
  • Another object of the present invention is to provide a multimode discone antenna capable of having simultaneously a vertically polarized omnidirectional pattern, a right-hand circularly polarized omnidirectional pattern and a left-hand circularly polarized omnidirectional pattern.
  • Still another object of the present invention is to provide a multimode discone antenna capable of utilization with satellite systems, LOS communication systems and/or navigation systems.
  • a feature of the present invention is the provision of a multimode discone antenna capable of having simultaneously a vertically polarized omnidirectional pattern, a right-hand circularly polarized omnidirectional pattern and a left-hand circularly polarized omnidirectional pattern comprising four coaxial transmission lines disposed in a parallel relationship, each of the coaxial lines including an inner conductor and an outer conductor; first means to electrically and physically interconnect the outer conductors of all the coaxial lines; and four first members each coupled to the center conductor of a different one of a coaxial line and extending downwardly from an end of, and at a given angle less than 90 to, the associated one ofthe coaxial lines.
  • Another feature of the present invention is the provision of four second members each coupled to the free end of a different one of the above-mentioned first members and extending downwardly and toward the associated one of the coaxial lines at an angle less than 180 and greater than 90".
  • a further feature of the present invention is the provision of a disc and a second means to electrically connect the disc to the above-mentioned first means and to physically support the disc spaced from the end of, and orthogonal to, the abovementioned coaxial lines.
  • Still a further feature of this invention is the provision of a multimode discone antenna as described above wherein each of the four coaxial lines are excited by in-phase energy and simultaneously each of the coaxial lines are excited by different orthogonally related energy.
  • FIG. I is a perspective view of a multimode discone antenna and its feed arrangement in accordance with the principles of the present invention.
  • FIG. 2 is atop view of FIG. I;
  • FIG. 3 is a schematic illustration of the electric field and current configuration for in-phase excitation of the coaxial lines of FIGS. 1 and 2;
  • FIG. 4 is the elevational pattern resulting from the electric field and current configuration as illustrated in FIG. 3;
  • FIG. 5 is a schematic illustration of the electric field and current configuration when the four coaxial lines of FIGS. 1
  • FIG. 6 illustrates the elevational pattern resulting from the electric field and current configuration illustrated in FIG. 5.
  • dual circular refers to right and left hand circularly polarized radiation.
  • hemisphericaF present in the above table has reference to a rightand left-hand circularly polarized omnidirectional pattern.
  • FIGS. 1 and 2 there is illustrated therein a multimode discone antenna in accordance with the'principles of the present invention including four coaxial transmission lines 1-4, each of which includes an outer conductor 5 and an inner conductor 6.
  • the outer conductors 5 of coaxial lines l-4 are interconnected electrically and physically by members7 and 8.
  • a member 9 extending downward from the upper end of coaxial lines 14 and at a given angle less than to the associated one of coaxial lines l-4.
  • the structure just described provides a hemispherical antenna pattern when each of the pairs of coaxial lines 1 and 4 and coaxial lines 2 and 3 are excited in a balanced relationship and these pairs of coaxial lines are orthogonally excited by a given energy for transmission from the antenna structure, or
  • radiating elements 9 when hemispherically radiated energy is received by radiating elements 9.
  • the radiating elements 9 in the form of wire or rods is equivalent to the cone of a discone antenna and due to its hemispherical antenna pattern provides the multifunction of providing both rightand left-hand circular polarization with an omnidirectional pattern. This arrangement as just described would be suitable for UHF satellite communication as indicated in the above table.
  • second members 10 are coupled to the free end of each of the members 9 and arranged to extend downwardly and toward the associated one of coaxial lines 14 at an angle between members 9 and 10 less than and greater than 90.
  • the angle between each of the members 9 and 10 enables variation of space consideration and also impedance considerations in the antenna structure as well as the shape of the antenna pattern.
  • a disc 11 is disposed orthogonal to the parallel coaxial lines l-4.
  • Disc 11 is electrically connected to the outer conductors 5 of coaxial lines 1-4 by physical connection to members 7 and 8 via feed member 12 which is physically coupled to the center of disc 11.
  • Feeder 12 also provides an electrical connection between the outer conductors of coaxial lines 1-4 and disc 11.
  • Current-flows on outer conductor 5 of coaxial lines 14 due to inphase excitation thereof which could cause the coaxial lines to radiate and disturb the desired patterns.
  • a high impedance to this current flow and, hence, elimination of the unwanted radiation is provided by the one-quarter wavelength choke 19 having the end 20 thereof in electrical contact with outer conductor 5 of coaxial lines,l-4.
  • Disc 11 has a diameter approximately equal to 0.7 D, where the dimension D is illustrated in FIG. 2, at the operating frequency while wires 9 and 10 each have a length greater than a quarter wavelength.
  • Another important dimension is the space between the ends of coaxial lines 1-4 and disc 11 as provided by the length of member 12 and also the diameter of member 12.
  • the spacing, as provided by the length of member 12, and the diameter of member 12 may be adjusted to control the impedance levels of the antenna structure of this invention.
  • coaxial lines 1-4 To provide transmission of vertically polarized omnidirectional energy, coaxial lines 1-4 must each be energized by the desired energy in-phase and upon reception of vertically polarized omnidirectional energy coaxial transmission lines again will be excited in-phase by the received energy.
  • FIG. 3 illustrates by virtue of the solid arrows the electrical field configuration when the antenna structure and, particularly, the coaxial lines 1-4 are excited in-phase.
  • the dotted arrows illustrated the current flow present in the diagonally related members 9 and 10.
  • FIG. 4 illustrates the elevational antenna pattern resulting from the electric field and current configuration as illustrated in FIG. 3.
  • FIG. 5 illustrates by the solid arrows the electric field configuration when the antenna structure and, particularly, coaxial lines 1 and 4 and coaxial lines 2 and 3 are excited in a balanced relationship and these pairs are orthogonally excited through means of quadrature hybrid by the desired energy.
  • the dotted arrows illustrate the current flow present in diagonallyrelated members 9 and 10 of FIG. 1.
  • FIG. 6 illustrates the elevational antenna pattern for the circularly polarized portion of the antenna structure shown in FIGS. 1 and 2.
  • the feed arrangement for the antenna structure of this invention as shown in FIG. 1 used for both transmission and reception includes two balanced hybrids 13 and 14 and a quadrature hybrid 15.
  • the feed arrangement operates as follows.
  • the energy to be transmitted with vertical polarization is applied to port 16 and fed in common to the in-phase port of balanced hybrids l3 and 14.
  • This inphase excitation of the coaxial lines 14 will result in the figure-eight elevational antenna pattern provided by members 9 and 10disc l l.
  • the circular polarization pattern for transmission is simultaneously provided by exciting port 17 of quadrature hybrid 15 with left-hand circularly polarized signal and port 18 of quadrature hybrid 15 with right-hand circularly polarized signal.
  • the energy applied to ports 17 and 18 is coupled from port 22 of hybrid 15 to the balanced port of hybrid 14 resulting in a +90 phase shift for left-hand circularly polarized signal (a 0 phase shift for right-hand circularly polarized signal) for excitation of transmission line 3 and a 90 phase shift for left-hand circularly polarized signal (a 180 phase shift for right-hand circularly polarized signal) for excitation of transmission line 2.
  • the resultant excitation of coaxial lines 1-4 with different balanced and orthogonal energy results in a circularly polarized signal radiated from the antenna structure including members 9 and 10.
  • a multimode vertically polarized omnidirectional pattern, a right-hand circularly polarized omnidirectional pattern and a left-hand circularly polarized omnidirectional pattern comprising:
  • each of said coaxial lines including an inner conductor and an outer conductor: first means to electrically and physically interconnect said outer conductors of all said coaxial lines: fourth first members each coupled to said center conductor of a different one of said coaxial lines and extending downward from an end of and at a given angle less than 90 to the associated one of said coaxial lines: four second members each coupled to the free end of a different one of said first members and extending downwardly and toward the associated one of said coaxial lines at an angle less than and greater than 90: a disc; and second means to electrically connect said disc to said first means and to physically support said disc spaced from said end of and orthogonal to said coaxial lines.
  • An antenna according to claim 1 wherein: said disc has a diameter approximately equal to 0.7 D at the operating frequency of said antenna, where D is the distance between the free ends of diagonally related ones of said first members; and each of said first and second members have a length greater than one-quarter wavelength at said operating frequency. 4.
  • second iii-phase port a third port coupled to said center conductor of a third of said coaxial lines and a fourth port coupled to said center conductor of a fourth of said coaxial lines diagonally disposed with respect to said third of said coaxial lines, said third port being responsive to said first energy having a -90 phase relationship with said first energy at said first port, said fourth port being responsive to said first energy having a +90 phase relationship with said first energy at said first port and said third and fourth ports simultaneously being responsive to said in-phase second energy;
  • a quadrature hybrid having a fifth port, a sixth port, a 0 phase port coupled to said first balanced port and a 90 port coupled to said second balanced port.
  • a multimode discone antenna capable of having simultaneously a vertically polarized omnidirectional pattern, a right-hand circularly polarized omnidirectional pattern and a left-hand circularly polarized omnidirectional pattern comprising:
  • each of said coaxial lines including an inner conductor and an outer conductor;
  • said disc has a diameter approximately equal to 0.7 D at the operating frequency of said antenna, where D is the distance between the free ends of diagonally related ones of said first members;
  • each of said first members have a length greater than onequarter wavelength at said operating frequency.
  • a first balanced hybrid having a first balanced port.
  • a first inphase port a first port coupled to said center conductor of a first of said coaxial lines and a second port coupled to said center conductor of a second of said coaxial lines diagonally disposed with respect to said first of said coaxial lines, said first port being responsive to first energy, said second port being responsive to said first energy having a 180 phase relationship with said first energy at said first port and said first and second ports simultaneously being responsive to in-phase second energy;
  • a second balanced hybrid having a second balanced port
  • second in-phase port a third port coupled to said center conductor of a third of said coaxial lines and a fourth port coupled to said center conductor of a fourth of said coaxial lines diagonally disposed with respect to said third of said coaxial lines, said third port being responsive to said first energy having a phase relationship with said first energy at said first port, said fourth port being responsive to said first energy having a +90 phase relationship with said first energy at said first port and said third and fourth ports simultaneously being responsive to said in-phase second energy;
  • a quadrant hybrid having a fifth port, a sixth port, a 0 phase port coupled to said first balanced port and a 90 port coupled to said second balanced port.

Abstract

A multimode discone antenna providing simultaneously, without interference, right- and left-hand circularly polarized omnidirectional patterns and a vertically polarized omnidirectional pattern. Four coaxial cables are disposed parallel to each other with the outer conductors electrically coupled together. An extension of the central conductor of each coaxial line is extended downward from the upper end of and at a given angle less than 90* to the associated one of the coaxial lines. This arrangement, when the two pairs of diagonally disposed coaxial lines are excited in a balanced relationship and the pairs are excited orthogonally by first energy, provides simultaneously both right- and left-hand circularly polarized omnidirectional patterns. When a disc is electrically connected to the outer conductors of the four coaxial lines and is physically supported in spaced and orthogonal relation to the upper end of the four coaxial lines, the antenna, in addition, simultaneously provides, when each of the four coaxial lines are excited in phase by second energy, a vertically polarized omnidirectional pattern. An embodiment of a feed arrangement is disclosed enabling the four coaxial lines to be excited in phase by the second energy and simultaneously to enable each of the four coaxial lines to be excited by the different orthogonally related first energy.

Description

United States Patent Spanos et al.
[54] DISCONE ANTENNA [72] Inventors: William M. Spanos, Wayne; Michael S.
Polgar, Ocean Port, both of NJ.
[22] Filed: July 21, 1970 [21] ApplNo; 56,830
52 us. Cl ..343/'173,333/11 343/846 lines- This arrangement when the Pails f diagonally 343/854 disposed coaxial lines are excited in a balanced relationship 51 1 t. Cl. ..H01 1 4s H01 13 00, H01 21 00 and the? am excited by fir-"energy, Pmides issi Field of Search "334 3/796-86 2 8416 simulmnmusly fightand left-hand circularly 1001mm 3/ 4 808 9 77 5 omnidirectional patterns. When a disc iS electrically con- I nected to the outer conductors of the four coaxial lines and is f "mes physically supported in spaced and orthogonal relation to the [56] Re e cued upper end of the four coaxial lines, theantenna, in addition,
UNITED STATES PATENTS simultaneously provides, when each of the four coaxial lines 2,511,899 6/1950 Brown ..'.343/797 X Primary ExaminerEli Lieberman Assistant ExaminerMarvin Nussbaum Att0rneyC. Cornell Remsen, .lr., Walter J. Baum, Paul W. Hemminger, Charles L. Johnson, In, Philip M. Bolton, Isidore Togut, Edward Goldberg and Menotti J. Lombardi, Jr.
[ Feb. 8, 1972 ABSTRACT A multimode discone antenna providing simultaneously, without interference, rightand left-hand circularly polarized omnidirectional patterns and a vertically polarized omnidirectional pattern. Four coaxial cables are disposed parallel to each other with the outer conductors electrically coupled together. An extension of the central conductor of each coaxial line is extended downward from the upper end of and at a given angle less than to the associated one of the coaxial are excited in phase by second energy, a vertically polarized omnidirectional pattern. An embodiment of a feed arrangement is disclosed enabling the four coaxial lines to be excited in phase by the second energy and simultaneously to enable each of the four coaxial lines to be excited by the different orthogonally related first energy.
8 Claims, 6 Drawing Figures LEFT HAND ClRCUl-QRLY RICH 1' HAND C18 C04 AEL Y Q 0 -90 +9o (-90") (+9d)(|80) V 0 BALANCED BALmfo H B D l3 urea/0 )4 l llwums A l/VPHASE PORT Pom- BALANCED ,2 PORT (90) 2 (9) 1 liaAuwceo 0, 2! 3 0 FORT P6 1 QUAORATURE HYBRID VRT/CALLY OMV$$IQE2I8IVAL I? onr DISCONE ANTENNA BACKGROUND OF THE INVENTION This invention relates to antennas and more particularly to discone antennas.
Because of existing space limitations and a need for greater numbers of antennas to provide radiating means for a multiplicity of services, the trend in antenna design is toward compact multipurpose radiators which provide more than one function. For example, in mobile applications, requirements exist for providing radio communications and navigation functions simultaneously in'either different frequency bands, or in the same frequency band. The antenna radiation characteristics with respect to pattern coverage and polarization are not necessarily identical. The advent of communications and navigation systems which utilize satellites have greatly complicated the design of common multipurpose antennas because of requirements for pattern coverage and polarization which differs from those for line-of-sight (LOS) ground-toground and ground-to-air links. The satellite systems require circular polarization and overhead coverage from ground base antennas, necessitating different modes of excitation in the antenna from those used for conventional systems.
SUMMARY OF THE INVENTION An object of the present invention is to provide a multimode antenna suitable for utilization in satellite systems.
Another object of the present invention is to provide a multimode discone antenna capable of having simultaneously a vertically polarized omnidirectional pattern, a right-hand circularly polarized omnidirectional pattern and a left-hand circularly polarized omnidirectional pattern.
Still another object of the present invention is to provide a multimode discone antenna capable of utilization with satellite systems, LOS communication systems and/or navigation systems.
A feature of the present invention is the provision of a multimode discone antenna capable of having simultaneously a vertically polarized omnidirectional pattern, a right-hand circularly polarized omnidirectional pattern and a left-hand circularly polarized omnidirectional pattern comprising four coaxial transmission lines disposed in a parallel relationship, each of the coaxial lines including an inner conductor and an outer conductor; first means to electrically and physically interconnect the outer conductors of all the coaxial lines; and four first members each coupled to the center conductor of a different one of a coaxial line and extending downwardly from an end of, and at a given angle less than 90 to, the associated one ofthe coaxial lines.
Another feature of the present invention is the provision of four second members each coupled to the free end of a different one of the above-mentioned first members and extending downwardly and toward the associated one of the coaxial lines at an angle less than 180 and greater than 90".
A further feature of the present invention is the provision of a disc and a second means to electrically connect the disc to the above-mentioned first means and to physically support the disc spaced from the end of, and orthogonal to, the abovementioned coaxial lines.
Still a further feature of this invention is the provision of a multimode discone antenna as described above wherein each of the four coaxial lines are excited by in-phase energy and simultaneously each of the coaxial lines are excited by different orthogonally related energy.
BRIEF DESCRIPTION OF THE DRAWING The above-mentioned and other features and objects of this invention will become more apparent by reference to the following description taken in conjunction with the accompanying drawings, in which:
FIG. I is a perspective view of a multimode discone antenna and its feed arrangement in accordance with the principles of the present invention;
FIG. 2 is atop view of FIG. I;
FIG. 3 is a schematic illustration of the electric field and current configuration for in-phase excitation of the coaxial lines of FIGS. 1 and 2;
FIG. 4 is the elevational pattern resulting from the electric field and current configuration as illustrated in FIG. 3;
FIG. 5 is a schematic illustration of the electric field and current configuration when the four coaxial lines of FIGS. 1
and 2 are subjected to a balanced excitation; and
FIG. 6 illustrates the elevational pattern resulting from the electric field and current configuration illustrated in FIG. 5.
DESCRIPTION OF THE PREFERRED EMBODIMENT For purposes of explanation, let us consider a UHF (ultrahigh frequency) line-of-sight (LOS) ground-to-ground communication, UHF satellite communications and L-band DME (distance-measuring equipment)fl"acan or RSB (Radar Safety Beacon)/IFF (Identification Friend or Foe) applications wherein the following requirements would exist for an antenna at a user terminal.
The term dual circular" as presented in the above table refers to right and left hand circularly polarized radiation. The term hemisphericaF present in the above table has reference to a rightand left-hand circularly polarized omnidirectional pattern.
Referring to FIGS. 1 and 2, there is illustrated therein a multimode discone antenna in accordance with the'principles of the present invention including four coaxial transmission lines 1-4, each of which includes an outer conductor 5 and an inner conductor 6.The outer conductors 5 of coaxial lines l-4 are interconnected electrically and physically by members7 and 8. To the center conductors 6 at the upper end thereof is connected a member 9 extending downward from the upper end of coaxial lines 14 and at a given angle less than to the associated one of coaxial lines l-4. 1
The structure just described provides a hemispherical antenna pattern when each of the pairs of coaxial lines 1 and 4 and coaxial lines 2 and 3 are excited in a balanced relationship and these pairs of coaxial lines are orthogonally excited by a given energy for transmission from the antenna structure, or
when hemispherically radiated energy is received by radiating elements 9. The radiating elements 9 in the form of wire or rods is equivalent to the cone of a discone antenna and due to its hemispherical antenna pattern provides the multifunction of providing both rightand left-hand circular polarization with an omnidirectional pattern. This arrangement as just described would be suitable for UHF satellite communication as indicated in the above table.
To aid in the producing of the desired shape of the antenna pattern and also to adjust the impedance of the antenna structure, second members 10 are coupled to the free end of each of the members 9 and arranged to extend downwardly and toward the associated one of coaxial lines 14 at an angle between members 9 and 10 less than and greater than 90. The angle between each of the members 9 and 10 enables variation of space consideration and also impedance considerations in the antenna structure as well as the shape of the antenna pattern.
To provide vertical polarization for UHF LOS communications or DME/Tacan, RSB/IFF applications, a disc 11 is disposed orthogonal to the parallel coaxial lines l-4. Disc 11 is electrically connected to the outer conductors 5 of coaxial lines 1-4 by physical connection to members 7 and 8 via feed member 12 which is physically coupled to the center of disc 11. Feeder 12 also provides an electrical connection between the outer conductors of coaxial lines 1-4 and disc 11. Current-flows on outer conductor 5 of coaxial lines 14 due to inphase excitation thereof which could cause the coaxial lines to radiate and disturb the desired patterns. In accordance with this invention, a high impedance to this current flow and, hence, elimination of the unwanted radiation is provided by the one-quarter wavelength choke 19 having the end 20 thereof in electrical contact with outer conductor 5 of coaxial lines,l-4.
Disc 11 has a diameter approximately equal to 0.7 D, where the dimension D is illustrated in FIG. 2, at the operating frequency while wires 9 and 10 each have a length greater than a quarter wavelength. The lengths of wires 9 and 10, as well as the distance D, controls the radiation patterns generated by the antenna of this invention.
Another important dimension is the space between the ends of coaxial lines 1-4 and disc 11 as provided by the length of member 12 and also the diameter of member 12. The spacing, as provided by the length of member 12, and the diameter of member 12 may be adjusted to control the impedance levels of the antenna structure of this invention.
To provide transmission of vertically polarized omnidirectional energy, coaxial lines 1-4 must each be energized by the desired energy in-phase and upon reception of vertically polarized omnidirectional energy coaxial transmission lines again will be excited in-phase by the received energy.
FIG. 3 illustrates by virtue of the solid arrows the electrical field configuration when the antenna structure and, particularly, the coaxial lines 1-4 are excited in-phase. The dotted arrows illustrated the current flow present in the diagonally related members 9 and 10.
FIG. 4 illustrates the elevational antenna pattern resulting from the electric field and current configuration as illustrated in FIG. 3.
FIG. 5 illustrates by the solid arrows the electric field configuration when the antenna structure and, particularly, coaxial lines 1 and 4 and coaxial lines 2 and 3 are excited in a balanced relationship and these pairs are orthogonally excited through means of quadrature hybrid by the desired energy. The dotted arrows illustrate the current flow present in diagonallyrelated members 9 and 10 of FIG. 1.
FIG. 6 illustrates the elevational antenna pattern for the circularly polarized portion of the antenna structure shown in FIGS. 1 and 2.
The feed arrangement for the antenna structure of this invention as shown in FIG. 1 used for both transmission and reception includes two balanced hybrids 13 and 14 and a quadrature hybrid 15.
For transmission the feed arrangement operates as follows. The energy to be transmitted with vertical polarization is applied to port 16 and fed in common to the in-phase port of balanced hybrids l3 and 14. This results in an in-phase excitation of coaxial lines 1-4 asindicated by the symbol applied to the ports of hybrids l3 and 14 connected to the center conductors of coaxial lines l-4. This inphase excitation of the coaxial lines 14 will result in the figure-eight elevational antenna pattern provided by members 9 and 10disc l l.
' The circular polarization pattern for transmission is simultaneously provided by exciting port 17 of quadrature hybrid 15 with left-hand circularly polarized signal and port 18 of quadrature hybrid 15 with right-hand circularly polarized signal. This results in a 0 phase shift for left-hand circularly polarized signal (a 90 phase shift for right-hand circularly polarized signal) at port 21 of hybrid 15 which is coupled to the balanced port of hybrid 13 and produces a 0 phase shift for left-hand circularly polarized signal (a +90 phase shift for right-hand circularly polarized signal) for excitation of transmission line 4 and a 180 phase shift for left-hand circularly polarized signal (a 90 phase shift for right-hand circularly polarized signal) for excitation of transmission line 1. Simultaneously, the energy applied to ports 17 and 18 is coupled from port 22 of hybrid 15 to the balanced port of hybrid 14 resulting in a +90 phase shift for left-hand circularly polarized signal (a 0 phase shift for right-hand circularly polarized signal) for excitation of transmission line 3 and a 90 phase shift for left-hand circularly polarized signal (a 180 phase shift for right-hand circularly polarized signal) for excitation of transmission line 2. The resultant excitation of coaxial lines 1-4 with different balanced and orthogonal energy results in a circularly polarized signal radiated from the antenna structure including members 9 and 10.
When the antenna structure of FIG. 1 is employed for receiving leftand right-hand circularly polarized energy members 9 and 10 cause coaxial transmission lines 1-4 to-be excited balanced and in-phase quadrature and excite the ports of hybrids 13 and 14 identified as the 0(+90), l(--90), +(O) and -90( l80) ports. There then will result at the output of ports 17 and 18, an output signal transmitted by the circularly polarized signal. When the antenna structure including members 9 and 10 and disc 11 receive vertically polarized omnidirectional radiation, coaxial transmission lines 1-4 are excited by in-phase received signals as indicated by the ports of hybrids 13 and 14. The output from the inphase ports of hybrids l3 and 14 are coupled to port 16.
While we have described above the principles of our inven-. tion in connection with specific apparatus, it is to be more clearly understood that this description is made only by way of example and not as a limitation to the scope of our invention as set forth in the objects thereof and in the accompanying claims.
We claim:
1. A multimode vertically polarized omnidirectional pattern, a right-hand circularly polarized omnidirectional pattern and a left-hand circularly polarized omnidirectional pattern comprising:
four coaxial transmission lines disposed in a parallel relationship, each of said coaxial lines including an inner conductor and an outer conductor: first means to electrically and physically interconnect said outer conductors of all said coaxial lines: fourth first members each coupled to said center conductor of a different one of said coaxial lines and extending downward from an end of and at a given angle less than 90 to the associated one of said coaxial lines: four second members each coupled to the free end of a different one of said first members and extending downwardly and toward the associated one of said coaxial lines at an angle less than and greater than 90: a disc; and second means to electrically connect said disc to said first means and to physically support said disc spaced from said end of and orthogonal to said coaxial lines. 2. An antenna according to claim 1, wherein: each of said coaxial lines are excited by in-phase energy;
and simultaneously each of said coaxial lines are excited by different orthogonally related energy. 3. An antenna according to claim 1, wherein: said disc has a diameter approximately equal to 0.7 D at the operating frequency of said antenna, where D is the distance between the free ends of diagonally related ones of said first members; and each of said first and second members have a length greater than one-quarter wavelength at said operating frequency. 4. An antenna according to claim 1, further including; a first balanced hybrid having a first balanced port, a first inphase port, a first port coupled to said center conductor of a first of said coaxial lines and a second port coupled to said center conductor of a second of said coaxial lines diagonally disposed with respect to said first of said coaxial lines, said first port being responsive to first energy, said second port being responsive to said first energy having a 180 phase relationship with said first energy at said a second balanced hybrid having a second balanced port, a
second iii-phase port, a third port coupled to said center conductor of a third of said coaxial lines and a fourth port coupled to said center conductor of a fourth of said coaxial lines diagonally disposed with respect to said third of said coaxial lines, said third port being responsive to said first energy having a -90 phase relationship with said first energy at said first port, said fourth port being responsive to said first energy having a +90 phase relationship with said first energy at said first port and said third and fourth ports simultaneously being responsive to said in-phase second energy;
third means interconnecting said first and second in-phase ports; and
a quadrature hybrid having a fifth port, a sixth port, a 0 phase port coupled to said first balanced port and a 90 port coupled to said second balanced port.
5. A multimode discone antenna capable of having simultaneously a vertically polarized omnidirectional pattern, a right-hand circularly polarized omnidirectional pattern and a left-hand circularly polarized omnidirectional pattern comprising:
four coaxial transmission lines disposed in a parallel relationship, each of said coaxial lines including an inner conductor and an outer conductor;
first means to electrically and physically interconnect said outer conductors of all said coaxial lines;
four first members each coupled to said center conductor of each of said coaxial lines are excited by in-phase energy and simultaneously each of said coaxial lines are excited by different orthogonally related energy. I
7. An antenna according to claim 5, wherein;
said disc has a diameter approximately equal to 0.7 D at the operating frequency of said antenna, where D is the distance between the free ends of diagonally related ones of said first members; and
each of said first members have a length greater than onequarter wavelength at said operating frequency.
8. An antenna according to claim 5, further including:
a first balanced hybrid having a first balanced port. a first inphase port, a first port coupled to said center conductor of a first of said coaxial lines and a second port coupled to said center conductor of a second of said coaxial lines diagonally disposed with respect to said first of said coaxial lines, said first port being responsive to first energy, said second port being responsive to said first energy having a 180 phase relationship with said first energy at said first port and said first and second ports simultaneously being responsive to in-phase second energy;
a second balanced hybrid having a second balanced port, a
second in-phase port, a third port coupled to said center conductor of a third of said coaxial lines and a fourth port coupled to said center conductor of a fourth of said coaxial lines diagonally disposed with respect to said third of said coaxial lines, said third port being responsive to said first energy having a phase relationship with said first energy at said first port, said fourth port being responsive to said first energy having a +90 phase relationship with said first energy at said first port and said third and fourth ports simultaneously being responsive to said in-phase second energy;
third means interconnecting said first and second in-phas ports; and
a quadrant hybrid having a fifth port, a sixth port, a 0 phase port coupled to said first balanced port and a 90 port coupled to said second balanced port.

Claims (8)

1. A multimode vertically polarized omnidirectional pattern, a right-hand circularly polarized omnidirectional pattern and a left-hand circularly polarized omnidirectional pattern comprising: four coaxial transmission lines disposed in a parallel relationship, each of said coaxial lines including an inner conductor and an outer conductor; first means to electrically and physically interconnect said outer conductors of all said coaxial lines; fourth first members each coupled to said center conductor of a different one of said coaxial lines and extending downward from an end of and at a given angle less than 90* to the associated one of said coaxial lines; four second members each coupled to the free end of a different one of said first members and extending downwardly and toward the associated one of said coaxial lines at an angle less than 180* and greater than 90*; a disc; and second means to electrically connect said disc to said first means and to physically support said disc spaced from said end of and orthogonal to said coaxial lines.
2. An antenna according to claim 1, wherein: each of said coaxial lines are excited by in-phase energy; and simultaneously each of said coaxial lines are excited by different orthogonally related energy.
3. An antenna according to claim 1, wherein: said disc has a diameter approximately equal to 0.7 D at the operating frequency of said antenna, where D is the distance between the free ends of diagonally related ones of said first members; and each of said first and second members have a length greater than one-quarter wavelength at said operating frequency.
4. An antenna according to claim 1, further including; a first balanced hybrid having a first balanced port, a first in-phase port, a first port coupled to said center conductor of a first of said coaxial lines and a second port coupled to said center conductor of a second of said coaxial lines diagonally disposed with respect to said first of said coaxial lines, said first port being responsive to first energy, said second port being responsive to said first energy having a 180* phase relationship with said first energy at said first port and said first and second ports simultaneously being responsive to in-phase second energy; a second balanced hybrid having a second balanced port, a second in-phase port, a third port coupled to said center conductor of a third of said coaxial lines and a fourth port coupled to said center conductor of a fourth of said coaxial lines diagonally disposed with respect to said third of said coaxial lines, said third port being responsive to said first energy having a -90* phase relationship with said first energy at said first port, said fourth port being responsive to said first energy having a +90* phase relationship with said first energy at said first port and said third and fourth ports simultaneously being responsive to said in-phase second energy; third means interconnecting said first and second in-phase ports; and a quadrature hybrid having a fifth port, a sixth port, a 0* phase port coupled to said first balanced port and a 90* port coupled to said second balanced port.
5. A multimode discone antenna capable of having simultaneously a vertically polarized omnidirectional pattern, a right-hand circularly polarized omnidirectional pattern and a left-hand circularly polarized omnidirectional pattern comprising: four coaxial transmission lineS disposed in a parallel relationship, each of said coaxial lines including an inner conductor and an outer conductor; first means to electrically and physically interconnect said outer conductors of all said coaxial lines; four first members each coupled to said center conductor of a different one of said coaxial lines and extending downward from and end of and at a given angle less than 90* to the associated one of said coaxial lines; a disc; and second means to electrically connect said disc to said first means and to physically support said disc spaced from said end of and orthogonal to said coaxial lines.
6. An antenna according to claim 5, wherein: each of said coaxial lines are excited by in-phase energy and simultaneously each of said coaxial lines are excited by different orthogonally related energy.
7. An antenna according to claim 5, wherein; said disc has a diameter approximately equal to 0.7 D at the operating frequency of said antenna, where D is the distance between the free ends of diagonally related ones of said first members; and each of said first members have a length greater than one-quarter wavelength at said operating frequency.
8. An antenna according to claim 5, further including: a first balanced hybrid having a first balanced port, a first in-phase port, a first port coupled to said center conductor of a first of said coaxial lines and a second port coupled to said center conductor of a second of said coaxial lines diagonally disposed with respect to said first of said coaxial lines, said first port being responsive to first energy, said second port being responsive to said first energy having a 180* phase relationship with said first energy at said first port and said first and second ports simultaneously being responsive to in-phase second energy; a second balanced hybrid having a second balanced port, a second in-phase port, a third port coupled to said center conductor of a third of said coaxial lines and a fourth port coupled to said center conductor of a fourth of said coaxial lines diagonally disposed with respect to said third of said coaxial lines, said third port being responsive to said first energy having a -90* phase relationship with said first energy at said first port, said fourth port being responsive to said first energy having a +90* phase relationship with said first energy at said first port and said third and fourth ports simultaneously being responsive to said in-phase second energy; third means interconnecting said first and second in-phase ports; and a quadrant hybrid having a fifth port, a sixth port, a 0* phase port coupled to said first balanced port and a 90* port coupled to said second balanced port.
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Cited By (24)

* Cited by examiner, † Cited by third party
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US3725929A (en) * 1971-06-28 1973-04-03 Itt Steerable null antenna arrangement
US3765023A (en) * 1972-09-21 1973-10-09 Rca Corp Circularly polarized antenna
US3771162A (en) * 1971-05-14 1973-11-06 Andrew California Corp Omnidirectional antenna
US3789416A (en) * 1972-04-20 1974-01-29 Itt Shortened turnstile antenna
US3811127A (en) * 1972-08-10 1974-05-14 Collins Radio Co Antenna for airborne satellite communications
DE2315241A1 (en) * 1973-03-27 1974-10-10 Siemens Ag POLARIZATION ISOLATION FOR OPPOSITE CIRCULAR-POLARIZED MICROWAVES
US3925784A (en) * 1971-10-27 1975-12-09 Radiation Inc Antenna arrays of internally phased elements
US4031539A (en) * 1975-12-11 1977-06-21 Rca Corporation Broadband turnstile antenna
FR2336810A1 (en) * 1975-12-22 1977-07-22 Motorola Inc MULTIPLE INPUT ANTENNA KIT
US4072913A (en) * 1976-02-03 1978-02-07 Harvard Industries, Inc. Feed forward passive coupling system and method
FR2363936A1 (en) * 1976-09-01 1978-03-31 Tekade Felten & Guilleaume MOUNTING FOR THE CONNECTION OF SEVERAL TRANSMITTERS MUTUALLY DECOUPLED
US4258341A (en) * 1976-02-03 1981-03-24 Fel Corporation Feed forward passive coupling system and method
US4446463A (en) * 1982-02-24 1984-05-01 The United States Of America As Represented By The Secretary Of The Navy Coaxial waveguide commutation feed network for use with a scanning circular phased array antenna
US4608572A (en) * 1982-12-10 1986-08-26 The Boeing Company Broad-band antenna structure having frequency-independent, low-loss ground plane
US4737793A (en) * 1983-10-28 1988-04-12 Ball Corporation Radio frequency antenna with controllably variable dual orthogonal polarization
US4851859A (en) * 1988-05-06 1989-07-25 Purdue Research Foundation Tunable discone antenna
US5189434A (en) * 1989-03-21 1993-02-23 Antenna Products Corp. Multi-mode antenna system having plural radiators coupled via hybrid circuit modules
US5793338A (en) * 1995-08-09 1998-08-11 Qualcomm Incorporated Quadrifilar helix antenna and feed network
WO2000024085A1 (en) * 1998-10-16 2000-04-27 Ems Technologies Canada, Ltd. Crossed bent dipole antenna
US20100277389A1 (en) * 2009-05-01 2010-11-04 Applied Wireless Identification Group, Inc. Compact circular polarized antenna
US8217850B1 (en) * 2008-08-14 2012-07-10 Rockwell Collins, Inc. Adjustable beamwidth aviation antenna with directional and omni-directional radiation modes
US8618998B2 (en) 2009-07-21 2013-12-31 Applied Wireless Identifications Group, Inc. Compact circular polarized antenna with cavity for additional devices
US20140197901A1 (en) * 2013-01-15 2014-07-17 Tyco Electronics Corporation Feed Network
US8803749B2 (en) 2011-03-25 2014-08-12 Kwok Wa Leung Elliptically or circularly polarized dielectric block antenna

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Cited By (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3771162A (en) * 1971-05-14 1973-11-06 Andrew California Corp Omnidirectional antenna
US3725929A (en) * 1971-06-28 1973-04-03 Itt Steerable null antenna arrangement
US3925784A (en) * 1971-10-27 1975-12-09 Radiation Inc Antenna arrays of internally phased elements
US3789416A (en) * 1972-04-20 1974-01-29 Itt Shortened turnstile antenna
US3811127A (en) * 1972-08-10 1974-05-14 Collins Radio Co Antenna for airborne satellite communications
US3765023A (en) * 1972-09-21 1973-10-09 Rca Corp Circularly polarized antenna
DE2315241A1 (en) * 1973-03-27 1974-10-10 Siemens Ag POLARIZATION ISOLATION FOR OPPOSITE CIRCULAR-POLARIZED MICROWAVES
US4031539A (en) * 1975-12-11 1977-06-21 Rca Corporation Broadband turnstile antenna
FR2336810A1 (en) * 1975-12-22 1977-07-22 Motorola Inc MULTIPLE INPUT ANTENNA KIT
US4072913A (en) * 1976-02-03 1978-02-07 Harvard Industries, Inc. Feed forward passive coupling system and method
US4258341A (en) * 1976-02-03 1981-03-24 Fel Corporation Feed forward passive coupling system and method
FR2363936A1 (en) * 1976-09-01 1978-03-31 Tekade Felten & Guilleaume MOUNTING FOR THE CONNECTION OF SEVERAL TRANSMITTERS MUTUALLY DECOUPLED
US4446463A (en) * 1982-02-24 1984-05-01 The United States Of America As Represented By The Secretary Of The Navy Coaxial waveguide commutation feed network for use with a scanning circular phased array antenna
US4608572A (en) * 1982-12-10 1986-08-26 The Boeing Company Broad-band antenna structure having frequency-independent, low-loss ground plane
US4737793A (en) * 1983-10-28 1988-04-12 Ball Corporation Radio frequency antenna with controllably variable dual orthogonal polarization
US4851859A (en) * 1988-05-06 1989-07-25 Purdue Research Foundation Tunable discone antenna
US5189434A (en) * 1989-03-21 1993-02-23 Antenna Products Corp. Multi-mode antenna system having plural radiators coupled via hybrid circuit modules
US5793338A (en) * 1995-08-09 1998-08-11 Qualcomm Incorporated Quadrifilar helix antenna and feed network
US6211840B1 (en) 1998-10-16 2001-04-03 Ems Technologies Canada, Ltd. Crossed-drooping bent dipole antenna
WO2000024085A1 (en) * 1998-10-16 2000-04-27 Ems Technologies Canada, Ltd. Crossed bent dipole antenna
US8217850B1 (en) * 2008-08-14 2012-07-10 Rockwell Collins, Inc. Adjustable beamwidth aviation antenna with directional and omni-directional radiation modes
US20100277389A1 (en) * 2009-05-01 2010-11-04 Applied Wireless Identification Group, Inc. Compact circular polarized antenna
US8106846B2 (en) 2009-05-01 2012-01-31 Applied Wireless Identifications Group, Inc. Compact circular polarized antenna
US8618998B2 (en) 2009-07-21 2013-12-31 Applied Wireless Identifications Group, Inc. Compact circular polarized antenna with cavity for additional devices
US8803749B2 (en) 2011-03-25 2014-08-12 Kwok Wa Leung Elliptically or circularly polarized dielectric block antenna
US20140197901A1 (en) * 2013-01-15 2014-07-17 Tyco Electronics Corporation Feed Network
US9178262B2 (en) * 2013-01-15 2015-11-03 Tyce Electronics Corporation Feed network comprised of marchand baluns and coupled line quadrature hybrids

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