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US3633210A - Unbalanced conical spiral antenna - Google Patents

Unbalanced conical spiral antenna Download PDF

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US3633210A
US3633210A US641841A US3633210DA US3633210A US 3633210 A US3633210 A US 3633210A US 641841 A US641841 A US 641841A US 3633210D A US3633210D A US 3633210DA US 3633210 A US3633210 A US 3633210A
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conductors
antenna
cone
support
conical
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US641841A
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Charles Webster Westerman
William G Scott
William S Wales
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Maxar Space LLC
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Philco Ford Corp
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    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00—Details of, or arrangements associated with, antennas
    • H01Q1/36—Structural form of radiating elements, e.g. cone, spiral, umbrella; Particular materials used therewith
    • H01Q1/38—Structural form of radiating elements, e.g. cone, spiral, umbrella; Particular materials used therewith formed by a conductive layer on an insulating support
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q11/00—Electrically-long antennas having dimensions more than twice the shortest operating wavelength and consisting of conductive active radiating elements
    • H01Q11/02—Non-resonant antennas, e.g. travelling-wave antenna
    • H01Q11/08—Helical antennas
    • H01Q11/083—Tapered helical aerials, e.g. conical spiral aerials

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  • This invention relates generally to antennas and particularly to a broadband directionally radiating antenna of very small volume in relation to comparable counterparts thereof.
  • the prior art conical spiral antenna typified in U.S. Pat. No. 2,958,081 to Dyson, granted Oct. 25, 1960, is capable of broadband directional-radiating characteristics.
  • this type of antenna must have a relatively large size in order to radiate efficiently.
  • the prior art conical spiral antenna normally occupies about 0.04 cubic wavelength of volume at the longest wavelength of its operating band. As will be recognized by those skilled in the art, this size is un desirably large and creates various difficulties in practical installations of the antenna. It would therefore be highly desirable to provide a wideband, directionally radiating antenna of greatly reduced size.
  • a directional broadband antenna of greatly reduced size is provided in the form of a two-arm conical spiral antenna in which the electrical characteristics of the arms are dissimilar so as to create different standing wave patterns on the respective arms. Thereby identical fields will exist over a corresponding portion of each arm so that the antenna will be able to radiate efficiently even though the spacing between the arms is reduced by reducing the size of the antenna.
  • radio equipment may optionally be housed within a shielded enclosure positioned within a conical support for the antenna.
  • FIG. 1 is a diagram of charge distributions on balanced and unbalanced lines which aids in understanding the present invention
  • FIG. 2 is a side elevational view of one form of the antenna of the invention
  • FIG. 3 is an end view of the antenna of FIG. 2,
  • FIGS. 4 and 5 are flat developments of the respective radiating element of one form of the antenna of the invention.
  • FIG. 6 is a skeleton view of one practical installation of the antenna of the invention showing the placement of radio equipment within the antenna.
  • FIG. 1 A first figure.
  • a typical prior art conical spiral antenna (not shown) comprised a pair of identical (balanced) conductors formed on a dielectrical conical surface with one conductor displaced from the other by 180.
  • a l80of the two conductors on a planar surface perpendicular to the axis of the cone was a pair of interleaved spirals.
  • this antenna had to be relatively large in order to radiate efficiently.
  • the necessity for its relatively large size is due to the need for preventing the fields produced by each conductor, which are at all times equal and opposite at all corresponding portions of both conductors, from canceling each other.
  • FIG. 1A shows a diagram of the theoretical charge distribution on the unwrapped arms of a typical prior art balanced spiral antenna. It can be seen that the current nodes on each conductor are at corresponding points on each conductor and, as represented by the and signs, the instantaneous field produced by one conductor is opposite to that produced by the other conductor at all corresponding points. Since the fields produced by the separate conductors are equal and opposite, a large amount of mutual cancellation will occur unless the conductors are spaced apart by a substantial fraction of a wavelength. Thus in order to be able to radiate efiiciently, the balanced conical spiral antenna had to be relatively large.
  • a conical spiral antenna in which the respective arms thereof are electrically dissimilar so as to provide an unbalanced arrangement.
  • the stand-wave patterns on the respective arms, and the fields created on the two anns will not be equal and opposite over corresponding portions of both arms but will actually be in phase over a large corresponding portion of both arms. No cancellation will occur over these in-phase portions so that efficient radiation will be provided even though the arms are closely spaced by a very small fraction of a wavelength.
  • FIG. 1B shows a diagram of the instantaneous charge dis-' tribution on the unwrapped arms of an unbalanced spiral antenna according to the invention.
  • the lower arm B is made electrically dissimilar to the upper arm A by providing, in one preferred embodiment, a slow wave portion on arm B by shaping the right end thereof in the form of a zigzag.
  • This slow wave portion will shift the current node 10 on arm B to the right, toward the slow wave portion. This will shift the entire field produced by arm B to the right so as to create a region 12 on both arms in which the charges produced by the respective arms are similar. It will be evident that the arms now will be able to radiate efficiently no matter how closely the arms are spaced since no opposite polarity, mutually cancelling fields will exist in region 12.
  • FIGS. 2 and3 FIGS. 2 and 3 show side elevational and end views of an unbalanced conical spiral antenna according to the preferred embodiment of the invention in which unbalanced arms such as shown in FIG. 1B are formed on a conical dielectric support 14.
  • the arms As indicated by the end view of FIG. 3, which shows a projection of the arms on a planar surface perpendicular to the axis of the cone, the arms form a pair of interleaved equiangular spirals, with the envelope of the zigzag portion 16 forming part of the spiral shape of arm B.
  • the dielectric support 14 has no significant electrical function and may be omitted if the arms are made rigid enough to be self-supporting or are otherwise supported.
  • the arms are normally excited at the ends thereof closest to the narrower end of the conical support 14. As indicated by arrows 18, the antenna will radiate in the direction in which the cone points over the higher frequency portion of the operating band. Over the lower frequency portion of the operating band, the antenna will radiate with less intensity in the direction in which the cone points, but with increasing intensity in the directions normal to the cone 5 axis.
  • the length of the unbalancing zigzag portion 16 of arm B is not critical and desirably extends up from the end of the arm from one-eighth to one-fourth wavelength at the lowest wavelength of the radiated band as measured along the centerline of the arm.
  • the U-shaped portion 19 at the end of the zigzag is an end loading element for fine tuning; this element has been found to increase the operating bandwidth by reducing the lowest operating frequency by 20 percent.
  • the use of a zigzag portion 16 is only one way of unbalancing the arms so that the standing-wave patterns thereof are not opposite in the two arms.
  • the arms can be unbalanced in other ways such as: 1) terminating one arm in a capacitor and the other arm in an inductor, (2) adding a fast wave structure such as a series of ungrounded capacitor elements in series to one arm, (3) replacing the zigzag structure with any slow wave structure such as (a) a group of ungrounded inductive elements in series, (b) a toothed structure, and (c) different dielectric loading than the other arm, or (4) lengthening one arm (the additional arm length may be coiled or spiraled inside the antenna cone).
  • volume ofthe antenna cone was0.003 cubic wavelength atthe longest wavelength of the band, a reduction to less than 8 percent of the volume of a corresponding balanced arm conical spiral antenna. This dramatic reduction in size is possible because of the unbalancing slow wave zigzag portion 16.
  • FIGS. 4 and 5 show flat layout views of the individual radiating arms A and B and the tables below give dimensions in inches from the reference points X to the other lettered reference points A to T. On a flat pattern, the angle between adjacent reference lines in the group XA to XT in FIGS. 4 and 5 was 6 57.5.
  • the actual dimensions of the radiating elements and the details of the zigzag portion are not critical and the diagrams of FIGS. 4 and 5 and the tables below are given as an example of one optimized design of a preferred embodiment of the antenna.
  • FIG. 4 FIG. 5
  • radio equipment may be placed within the dielectric support 14 if a suitable isolating metal shield 15, smaller than the dielectric support 14, but corresponding in configuration thereto, is provided within support 14.
  • the metal shield 15 has no significant electrical function in the operation of the antenna; however it should not be spaced close to the radiating arms in order to minimize loading.
  • Within the metal shield 15 can be placed a transmitter which is excited by an input 22.
  • Balun 26 can be formed from a coaxial cable in which a slot in the outer conductor thereof widens gradually until the inner and outer conductors form a balanced two-wire line such as shown at 28.
  • the dielectric cone 14 may be made of any material which has a low dielectric loss, such as fiber glass.
  • a streamlining apex portion 30 for the dielectric support 14 is shown in FIG. 6.
  • Portion 30 has no electrical function and can be formed of the same material as support 14 or can be metallic, if desired.
  • the antenna of the invention can be formed as part of the nose of any airborne, surface, or undersea vehicle.
  • a directional broadband antenna comprising two elongated electrical conductors shaped in a three-dimensional configuration such that (l) the projection thereof on a planar surface is a pair of separated interleaved spirals and (2) no two separate points on the axis of either of said conductors lie in any one plane parallel to said planar surface, said conductors being electrically dissimilar such that if two respective points on said conductors which lie in a plane parallel to said planar surface are excited by a radiofrequency voltage source, the resultant standing-wave current pattern in said conductors, and hence the resultant fields produced thereby, will be in phase over a corresponding portion of each of said conductors with respect to said coplanar points, whereby said antenna will be able to radiate efficiently even though said conductors are closely spaced.
  • the antenna of claim 1 further including a dielectric cone, said conductors being formed on the tapered surface of said dielectric cone.
  • the antenna of claim 1 further including a dielectric cone, said conductors being formed on the tapered surface of said dielectric cone, and further including a conductive enclosure positioned within said cone, said enclosure containing electronic means for supplying radiofrequency energy to said antenna, and means for coupling radiofrequency energy from said electronic means to a pair of coplanar points on said respective conductors.
  • a broadband directional antenna comprising a conical dielectric support, a pair of conductors positioned on said support, said conductors having a configuration such that the projection thereof on a plane perpendicular to the axis of said cone is a pair ofinterleaved spirals, the end of one ofsaid conductors being coplanar with and displaced from the end of the other by an angle of about said conductors being electrically dissimilar such that if said ends thereof are excited by a radiofrequency voltage source, the standing-wave current patterns in said conductors, and hence the resultant fields produced thereby, will be in phase over a corresponding portion of each of said conductors.
  • one only of said conductors has a zigzag configuration over a portion of its length, the projection of the envelope of said zigzag forming part of one of said spirals.
  • the antenna of claim 6 further including a conductive enclosure positioned within said conical support, and also including a source of radiofrequency energy within said enclosure.
  • said conductors are flat strips formed on said conical support, the width of said strips increasing toward the wider part of said support, one of said strips having a zigzag portion near the end thereof at the base of said support, the envelope of said zigzag portion forming part of one of said spirals, the end of said one strip having a U- shaped loading element connected thereto, a conical conductive enclosure having substantially the same taper angle as said conical support positioned within said support, said enclosure including a source of radiofrequency energy for exciting said antenna, and means coupling said source to the ends of said strips at the narrower end of said conical support.

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Abstract

A directional broadband antenna utilizing two dissimilar interleaved spiral radiators of conical configuration with radio equipment optionally housed in shield within dielectric conical support for radiators.

Description

Unite States Pate [56] References Cited UNITED STATES PATENTS 2,958,081 10/1960 Dyson [72] Inventors Charles Webster Westerman Anaheim;
William G. Scott, Orange; William S. Wales, Long Beach, all of Calif. 641,841
3,241,148 3/1966 Lechtreck........
Primary Examiner-Rodney D. Bennett, Jr. Assistant Examiner-Richard E. Berger Attorney-Robert D. Sanborn [54] UNBALANCED CONICAL SPIRAL ANTENNA 10 Claimsmnmwing Figs ABSTRACT: A directional broadband antenna utilizing two dissimilar interleaved spiral radiators of conical configuration with radio equipment optionally housed in shield within dielectric conical support for radiators.
343/895 l-l0lq1/36 so FieldofSearch........................................... 343/895 [51] Int.Cl...............;
6952770 9/ A li/4 7704 UNBALANCED CONICAL SPIRAL ANTENNA This invention relates generally to antennas and particularly to a broadband directionally radiating antenna of very small volume in relation to comparable counterparts thereof.
The prior art conical spiral antenna, typified in U.S. Pat. No. 2,958,081 to Dyson, granted Oct. 25, 1960, is capable of broadband directional-radiating characteristics. However this type of antenna must have a relatively large size in order to radiate efficiently. For example, the prior art conical spiral antenna normally occupies about 0.04 cubic wavelength of volume at the longest wavelength of its operating band. As will be recognized by those skilled in the art, this size is un desirably large and creates various difficulties in practical installations of the antenna. It would therefore be highly desirable to provide a wideband, directionally radiating antenna of greatly reduced size.
Accordingly, several objects of the present invention are: (1) to provide a directional broadband antenna of greatly reduced size, and (2) to provide an improved conical spiral antenna. Another object is to provide an antenna in which transmitting or other equipment can be housed conveniently within the antenna so as not to require additional space. Further objects and advantages of the present invention will become apparent from the ensuing description thereof.
SUMMARY A directional broadband antenna of greatly reduced size is provided in the form of a two-arm conical spiral antenna in which the electrical characteristics of the arms are dissimilar so as to create different standing wave patterns on the respective arms. Thereby identical fields will exist over a corresponding portion of each arm so that the antenna will be able to radiate efficiently even though the spacing between the arms is reduced by reducing the size of the antenna. Also radio equipment may optionally be housed within a shielded enclosure positioned within a conical support for the antenna.
DRAWINGS FIG. 1 is a diagram of charge distributions on balanced and unbalanced lines which aids in understanding the present invention,
FIG. 2 is a side elevational view of one form of the antenna of the invention,
FIG. 3 is an end view of the antenna of FIG. 2,
FIGS. 4 and 5 are flat developments of the respective radiating element of one form of the antenna of the invention,
FIG. 6 is a skeleton view of one practical installation of the antenna of the invention showing the placement of radio equipment within the antenna.
FIG. 1
A typical prior art conical spiral antenna (not shown) comprised a pair of identical (balanced) conductors formed on a dielectrical conical surface with one conductor displaced from the other by 180. Thus a l80of the two conductors on a planar surface perpendicular to the axis of the cone was a pair of interleaved spirals. As stated, this antenna had to be relatively large in order to radiate efficiently. The necessity for its relatively large size is due to the need for preventing the fields produced by each conductor, which are at all times equal and opposite at all corresponding portions of both conductors, from canceling each other.
FIG. 1A shows a diagram of the theoretical charge distribution on the unwrapped arms of a typical prior art balanced spiral antenna. It can be seen that the current nodes on each conductor are at corresponding points on each conductor and, as represented by the and signs, the instantaneous field produced by one conductor is opposite to that produced by the other conductor at all corresponding points. Since the fields produced by the separate conductors are equal and opposite, a large amount of mutual cancellation will occur unless the conductors are spaced apart by a substantial fraction of a wavelength. Thus in order to be able to radiate efiiciently, the balanced conical spiral antenna had to be relatively large.
According to the invention, a conical spiral antenna is provided in which the respective arms thereof are electrically dissimilar so as to provide an unbalanced arrangement. Thereby the stand-wave patterns on the respective arms, and the fields created on the two anns will not be equal and opposite over corresponding portions of both arms but will actually be in phase over a large corresponding portion of both arms. No cancellation will occur over these in-phase portions so that efficient radiation will be provided even though the arms are closely spaced by a very small fraction of a wavelength.
FIG. 1B shows a diagram of the instantaneous charge dis-' tribution on the unwrapped arms of an unbalanced spiral antenna according to the invention. The lower arm B is made electrically dissimilar to the upper arm A by providing, in one preferred embodiment, a slow wave portion on arm B by shaping the right end thereof in the form of a zigzag. This slow wave portion will shift the current node 10 on arm B to the right, toward the slow wave portion. This will shift the entire field produced by arm B to the right so as to create a region 12 on both arms in which the charges produced by the respective arms are similar. It will be evident that the arms now will be able to radiate efficiently no matter how closely the arms are spaced since no opposite polarity, mutually cancelling fields will exist in region 12.
FIGS. 2 and3 FIGS. 2 and 3 show side elevational and end views of an unbalanced conical spiral antenna according to the preferred embodiment of the invention in which unbalanced arms such as shown in FIG. 1B are formed on a conical dielectric support 14. As indicated by the end view of FIG. 3, which shows a projection of the arms on a planar surface perpendicular to the axis of the cone, the arms form a pair of interleaved equiangular spirals, with the envelope of the zigzag portion 16 forming part of the spiral shape of arm B.
The dielectric support 14 has no significant electrical function and may be omitted if the arms are made rigid enough to be self-supporting or are otherwise supported.
The arms are normally excited at the ends thereof closest to the narrower end of the conical support 14. As indicated by arrows 18, the antenna will radiate in the direction in which the cone points over the higher frequency portion of the operating band. Over the lower frequency portion of the operating band, the antenna will radiate with less intensity in the direction in which the cone points, but with increasing intensity in the directions normal to the cone 5 axis.
The length of the unbalancing zigzag portion 16 of arm B is not critical and desirably extends up from the end of the arm from one-eighth to one-fourth wavelength at the lowest wavelength of the radiated band as measured along the centerline of the arm. The U-shaped portion 19 at the end of the zigzag is an end loading element for fine tuning; this element has been found to increase the operating bandwidth by reducing the lowest operating frequency by 20 percent.
The use of a zigzag portion 16 is only one way of unbalancing the arms so that the standing-wave patterns thereof are not opposite in the two arms. The arms can be unbalanced in other ways such as: 1) terminating one arm in a capacitor and the other arm in an inductor, (2) adding a fast wave structure such as a series of ungrounded capacitor elements in series to one arm, (3) replacing the zigzag structure with any slow wave structure such as (a) a group of ungrounded inductive elements in series, (b) a toothed structure, and (c) different dielectric loading than the other arm, or (4) lengthening one arm (the additional arm length may be coiled or spiraled inside the antenna cone). It has been found that unbalancing by lengthening one arm produces matched input impedances at frequencies lower than those obtainable with the use of the zigzag portion. Other suitable ways of unbalancing the two arms of the antenna will be visualized by those skilled in the art and accordingly the invention is not limited to the specific embodiment shown or the other examples given but contemplates all unbalanced structures within the scope of the appended claims.
radar:
than i2jto 1 relative to 50 ohm over the entire band. The
volume ofthe antenna cone was0.003 cubic wavelength atthe longest wavelength of the band, a reduction to less than 8 percent of the volume of a corresponding balanced arm conical spiral antenna. This dramatic reduction in size is possible because of the unbalancing slow wave zigzag portion 16.
FIGS. 4 and 5 FIGS. 4 and 5 show flat layout views of the individual radiating arms A and B and the tables below give dimensions in inches from the reference points X to the other lettered reference points A to T. On a flat pattern, the angle between adjacent reference lines in the group XA to XT in FIGS. 4 and 5 was 6 57.5. The actual dimensions of the radiating elements and the details of the zigzag portion are not critical and the diagrams of FIGS. 4 and 5 and the tables below are given as an example of one optimized design of a preferred embodiment of the antenna.
FIG. 4 FIG. 5
A1 10.75 A2 A1 10.75 A2 Bl 11.60 B2 10.42 B1 11.60 B2 10.42 C1 12.50 C2 11.32 Cl 12.50 C2 11.32 D1 13.50 D2 12.32 D1 13.50 D2 12.32 E1 14.58 E2 13.40 E1 14.58 E2 13.40 Fl 15.72 F2 14.54 F1 15.72 F2 14.54 G1 16.96 O2 1572 G1 16.96 G2 15.72 H1 18.30 H2 16.96 H1 18.30 H2 16.96 J1 19.75 J2 18.30 .11 19.75 .12 18.30 K1 21.30 K2 19.75 Kl 21.30 K2 19.75 L1 23.00 L2 2130 L1 23.00 L2 21.30 MI 24.85 M2 23.00 MI 24.85 M2 23.00 N1 26.80 N2 24.85 N1 26.80 N2 24.85 Pl 28.90 P2 2680 P1 28.90 P2 26.80 R1 31.10 R2 28.80 R1 30.08 R2 28.90 S1 33.50 S2 31.10 S1 32.28 S2 31.10 Tl 36.10 T2 33.50 T1 34.50 T2 33.50
Table ofdistances in inches from reference point X to reference points Al to T2 in FIGS. 4 and 5.
FIG. 6
According to the invention, radio equipment may be placed within the dielectric support 14 if a suitable isolating metal shield 15, smaller than the dielectric support 14, but corresponding in configuration thereto, is provided within support 14. The metal shield 15 has no significant electrical function in the operation of the antenna; however it should not be spaced close to the radiating arms in order to minimize loading. Within the metal shield 15 can be placed a transmitter which is excited by an input 22.
The unbalanced (coaxial) output 24 of transmitter 20 is converted to a balanced output by a balun 26. Balun 26 can be formed from a coaxial cable in which a slot in the outer conductor thereof widens gradually until the inner and outer conductors form a balanced two-wire line such as shown at 28.
The dielectric cone 14 may be made of any material which has a low dielectric loss, such as fiber glass. A streamlining apex portion 30 for the dielectric support 14 is shown in FIG. 6. Portion 30 has no electrical function and can be formed of the same material as support 14 or can be metallic, if desired.
Obviously the antenna of the invention can be formed as part of the nose of any airborne, surface, or undersea vehicle.
While there has been described what is at present considered to be the preferred embodiment of the invention it will be apparent that various modifications and other embodiments thereof will occur to those skilled in the art within the scope of the invention. Accordingly, it is desired that the scope of the invention be limited by the appended claims only.
We claim: 1. A directional broadband antenna comprising two elongated electrical conductors shaped in a three-dimensional configuration such that (l) the projection thereof on a planar surface is a pair of separated interleaved spirals and (2) no two separate points on the axis of either of said conductors lie in any one plane parallel to said planar surface, said conductors being electrically dissimilar such that if two respective points on said conductors which lie in a plane parallel to said planar surface are excited by a radiofrequency voltage source, the resultant standing-wave current pattern in said conductors, and hence the resultant fields produced thereby, will be in phase over a corresponding portion of each of said conductors with respect to said coplanar points, whereby said antenna will be able to radiate efficiently even though said conductors are closely spaced.
2. The antenna of claim 1 wherein a portion of only one of said conductors has a zigzag configuration, the projection of the envelope of said zigzag portion conforming to part of one of said spirals.
3. The antenna of claim 1 further including a dielectric cone, said conductors being formed on the tapered surface of said dielectric cone.
4. The antenna of claim 1 further including a dielectric cone, said conductors being formed on the tapered surface of said dielectric cone, and further including a conductive enclosure positioned within said cone, said enclosure containing electronic means for supplying radiofrequency energy to said antenna, and means for coupling radiofrequency energy from said electronic means to a pair of coplanar points on said respective conductors.
5. The antenna of claim 4 in which said conductors are excited at the ends thereof at the narrower portion of said cone.
6. A broadband directional antenna comprising a conical dielectric support, a pair of conductors positioned on said support, said conductors having a configuration such that the projection thereof on a plane perpendicular to the axis of said cone is a pair ofinterleaved spirals, the end of one ofsaid conductors being coplanar with and displaced from the end of the other by an angle of about said conductors being electrically dissimilar such that if said ends thereof are excited by a radiofrequency voltage source, the standing-wave current patterns in said conductors, and hence the resultant fields produced thereby, will be in phase over a corresponding portion of each of said conductors.
7. The antenna of claim 6 wherein one only of said conductors has a zigzag configuration over a portion of its length, the projection of the envelope of said zigzag forming part of one of said spirals.
8. The antenna of claim 6 further including a conductive enclosure positioned within said conical support, and also including a source of radiofrequency energy within said enclosure.
9. The antenna of claim 8 wherein said enclosure is cone shaped.
10. The antenna of claim 8 wherein said conductors are flat strips formed on said conical support, the width of said strips increasing toward the wider part of said support, one of said strips having a zigzag portion near the end thereof at the base of said support, the envelope of said zigzag portion forming part of one of said spirals, the end of said one strip having a U- shaped loading element connected thereto, a conical conductive enclosure having substantially the same taper angle as said conical support positioned within said support, said enclosure including a source of radiofrequency energy for exciting said antenna, and means coupling said source to the ends of said strips at the narrower end of said conical support.
@3 33 3 11mm sures PATENT OFFICE CERTIFICATE OF CORRECTION Patent No. 3,633,210 Dated January L, 1972 nt fll) Charles W. Westerman. William G. Scott, William S. Wales It in certified the: error appears in the above-identified patent and that said Letters Patent are hereby corrected as shown below:
Column 1, in paragraph beginning "FIGS. L and 5", second line (line A l) "element" shouldbe -elements--.
Column 1, in penultimate paragraph, fourth line (line 52) 2 "180 should be -projection--.
Column 2, line": "stand-" should be --standing--.
Column 3, line 2: "designated" should be --designed--.
Column 3', line 5: after "8-3/8", --inches-- should be inserted.
Signed and sealed this 6th day of Jun 19 2,
(SEAL) Attest:
EDWARD M .FLETCHER,J'R. ROBERT GOTTSCHALK Attesting Officer Commissioner of Patents

Claims (10)

1. A directional broadband antenna comprising two elongated electrical conductors shaped in a three-dimensional configuration such that (1) the projection thereof on a planar surface is a pair of separated interleaved spirals and (2) no two separate points on the axis of either of said conductors lie in any one plane parallel to said planar surface, said conductors being electrically dissimilar such that if two respective points on said conductors which lie in a plane parallel to said planar surface are excited by a radiofrequency voltage source, the resultant standing-wave current pattern in said conductors, and hence the resultant fields produced thereby, will be in phase over a corresponding portion of each of said conductors with respect to said coplanar points, whereby said antenna will be able to radiate efficiently even though said conductors are closely spaced.
2. The antenna of claim 1 wherein a portion of only one of said conductors has a zigzag configuration, the projection of the envelope of said zigzag portion conforming to part of one of said spirals.
3. The antenna of claim 1 further including a dielectric cone, said conductors being formed on the tapered surface of said dielectric cone.
4. The antenna of claim 1 further including a dielectric cone, said conductors bEing formed on the tapered surface of said dielectric cone, and further including a conductive enclosure positioned within said cone, said enclosure containing electronic means for supplying radiofrequency energy to said antenna, and means for coupling radiofrequency energy from said electronic means to a pair of coplanar points on said respective conductors.
5. The antenna of claim 4 in which said conductors are excited at the ends thereof at the narrower portion of said cone.
6. A broadband directional antenna comprising a conical dielectric support, a pair of conductors positioned on said support, said conductors having a configuration such that the projection thereof on a plane perpendicular to the axis of said cone is a pair of interleaved spirals, the end of one of said conductors being coplanar with and displaced from the end of the other by an angle of about 180*, said conductors being electrically dissimilar such that if said ends thereof are excited by a radiofrequency voltage source, the standing-wave current patterns in said conductors, and hence the resultant fields produced thereby, will be in phase over a corresponding portion of each of said conductors.
7. The antenna of claim 6 wherein one only of said conductors has a zigzag configuration over a portion of its length, the projection of the envelope of said zigzag forming part of one of said spirals.
8. The antenna of claim 6 further including a conductive enclosure positioned within said conical support, and also including a source of radiofrequency energy within said enclosure.
9. The antenna of claim 8 wherein said enclosure is cone shaped.
10. The antenna of claim 8 wherein said conductors are flat strips formed on said conical support, the width of said strips increasing toward the wider part of said support, one of said strips having a zigzag portion near the end thereof at the base of said support, the envelope of said zigzag portion forming part of one of said spirals, the end of said one strip having a U-shaped loading element connected thereto, a conical conductive enclosure having substantially the same taper angle as said conical support positioned within said support, said enclosure including a source of radiofrequency energy for exciting said antenna, and means coupling said source to the ends of said strips at the narrower end of said conical support.
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Cited By (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3900849A (en) * 1973-10-17 1975-08-19 Us Air Force Conical unbalanced spiral radar modulator
FR2315179A1 (en) * 1975-06-20 1977-01-14 Aerospatiale Half wave aerial for circularly polarised signals - has two plane parallel loops of opposite sense connected by straight conductor
US4243993A (en) * 1979-11-13 1981-01-06 The Boeing Company Broadband center-fed spiral antenna
US4489276A (en) * 1982-01-20 1984-12-18 The United States Of America As Represented By The United States Department Of Energy Dual-cone double-helical downhole logging device
US4605934A (en) * 1984-08-02 1986-08-12 The Boeing Company Broad band spiral antenna with tapered arm width modulation
JPS621409U (en) * 1986-06-12 1987-01-07
US4847627A (en) * 1987-09-08 1989-07-11 Lockheed Corporation Compact wave antenna system
US5479180A (en) * 1994-03-23 1995-12-26 The United States Of America As Represented By The Secretary Of The Army High power ultra broadband antenna
US5677699A (en) * 1994-11-29 1997-10-14 Cal Corporation Helical microstrip antenna with impedance taper
US5815122A (en) * 1996-01-11 1998-09-29 The Regents Of The University Of Michigan Slot spiral antenna with integrated balun and feed
US5854608A (en) * 1994-08-25 1998-12-29 Symetri Com, Inc. Helical antenna having a solid dielectric core
US5859621A (en) * 1996-02-23 1999-01-12 Symmetricom, Inc. Antenna
US5929824A (en) * 1995-06-20 1999-07-27 Saab Ericsson Space Ab Antenna element, conically helical, for polarization purity within a broad frequency range
US5945963A (en) * 1996-01-23 1999-08-31 Symmetricom, Inc. Dielectrically loaded antenna and a handheld radio communication unit including such an antenna
US5963180A (en) * 1996-03-29 1999-10-05 Symmetricom, Inc. Antenna system for radio signals in at least two spaced-apart frequency bands
US6300917B1 (en) 1999-05-27 2001-10-09 Sarantel Limited Antenna
US20020030168A1 (en) * 2000-06-27 2002-03-14 Gabriel Martinez Martin Energy regenerating device
US6369776B1 (en) 1999-02-08 2002-04-09 Sarantel Limited Antenna
US6552693B1 (en) 1998-12-29 2003-04-22 Sarantel Limited Antenna
US6661391B2 (en) * 2000-06-09 2003-12-09 Matsushita Electric Industrial Co., Ltd. Antenna and radio device comprising the same
US6690336B1 (en) 1998-06-16 2004-02-10 Symmetricom, Inc. Antenna
US20040257298A1 (en) * 2003-06-18 2004-12-23 Steve Larouche Helical antenna
US7586462B1 (en) 2007-01-29 2009-09-08 Stephen G. Tetorka Physically small spiral antenna
US20120075820A1 (en) * 2008-04-04 2012-03-29 American Technical Ceramics, Corp. Ultra-Wideband Assembly System and Method
US8922452B1 (en) * 2014-03-21 2014-12-30 University Of South Florida Periodic spiral antennas
US9337533B2 (en) 2014-08-08 2016-05-10 The Charles Stark Draper Laboratory, Inc. Ground plane meandering in Z direction for spiral antenna
WO2021034662A1 (en) * 2019-08-20 2021-02-25 Bae Systems Information And Electronic Systems Integration Inc. Cavity backed notch antenna with additively manufactured radome

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2958081A (en) * 1959-06-30 1960-10-25 Univ Illinois Unidirectional broadband antenna comprising modified balanced equiangular spiral
US3241148A (en) * 1960-04-04 1966-03-15 Mcdonnell Aircraft Corp End loaded planar spiral antenna

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2958081A (en) * 1959-06-30 1960-10-25 Univ Illinois Unidirectional broadband antenna comprising modified balanced equiangular spiral
US3241148A (en) * 1960-04-04 1966-03-15 Mcdonnell Aircraft Corp End loaded planar spiral antenna

Cited By (34)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3900849A (en) * 1973-10-17 1975-08-19 Us Air Force Conical unbalanced spiral radar modulator
FR2315179A1 (en) * 1975-06-20 1977-01-14 Aerospatiale Half wave aerial for circularly polarised signals - has two plane parallel loops of opposite sense connected by straight conductor
US4243993A (en) * 1979-11-13 1981-01-06 The Boeing Company Broadband center-fed spiral antenna
US4489276A (en) * 1982-01-20 1984-12-18 The United States Of America As Represented By The United States Department Of Energy Dual-cone double-helical downhole logging device
US4605934A (en) * 1984-08-02 1986-08-12 The Boeing Company Broad band spiral antenna with tapered arm width modulation
JPS621409U (en) * 1986-06-12 1987-01-07
US4847627A (en) * 1987-09-08 1989-07-11 Lockheed Corporation Compact wave antenna system
US5479180A (en) * 1994-03-23 1995-12-26 The United States Of America As Represented By The Secretary Of The Army High power ultra broadband antenna
US5854608A (en) * 1994-08-25 1998-12-29 Symetri Com, Inc. Helical antenna having a solid dielectric core
US6181297B1 (en) 1994-08-25 2001-01-30 Symmetricom, Inc. Antenna
US5677699A (en) * 1994-11-29 1997-10-14 Cal Corporation Helical microstrip antenna with impedance taper
US5929824A (en) * 1995-06-20 1999-07-27 Saab Ericsson Space Ab Antenna element, conically helical, for polarization purity within a broad frequency range
US5815122A (en) * 1996-01-11 1998-09-29 The Regents Of The University Of Michigan Slot spiral antenna with integrated balun and feed
US5945963A (en) * 1996-01-23 1999-08-31 Symmetricom, Inc. Dielectrically loaded antenna and a handheld radio communication unit including such an antenna
US5859621A (en) * 1996-02-23 1999-01-12 Symmetricom, Inc. Antenna
US5963180A (en) * 1996-03-29 1999-10-05 Symmetricom, Inc. Antenna system for radio signals in at least two spaced-apart frequency bands
US6690336B1 (en) 1998-06-16 2004-02-10 Symmetricom, Inc. Antenna
US6552693B1 (en) 1998-12-29 2003-04-22 Sarantel Limited Antenna
US6369776B1 (en) 1999-02-08 2002-04-09 Sarantel Limited Antenna
US6300917B1 (en) 1999-05-27 2001-10-09 Sarantel Limited Antenna
US6661391B2 (en) * 2000-06-09 2003-12-09 Matsushita Electric Industrial Co., Ltd. Antenna and radio device comprising the same
US20020030168A1 (en) * 2000-06-27 2002-03-14 Gabriel Martinez Martin Energy regenerating device
US20040257298A1 (en) * 2003-06-18 2004-12-23 Steve Larouche Helical antenna
US7038636B2 (en) * 2003-06-18 2006-05-02 Ems Technologies Cawada, Ltd. Helical antenna
US7586462B1 (en) 2007-01-29 2009-09-08 Stephen G. Tetorka Physically small spiral antenna
US8797761B2 (en) * 2008-04-04 2014-08-05 John Mruz Ultra-wideband assembly system and method
US20120075820A1 (en) * 2008-04-04 2012-03-29 American Technical Ceramics, Corp. Ultra-Wideband Assembly System and Method
US9854665B2 (en) 2008-04-04 2017-12-26 American Technical Ceramics Corp. Ultra-wideband assembly system and method
US10165675B2 (en) 2008-04-04 2018-12-25 American Technical Ceramics Corp. Ultra-wideband assembly system and method
US8922452B1 (en) * 2014-03-21 2014-12-30 University Of South Florida Periodic spiral antennas
US9337533B2 (en) 2014-08-08 2016-05-10 The Charles Stark Draper Laboratory, Inc. Ground plane meandering in Z direction for spiral antenna
WO2021034662A1 (en) * 2019-08-20 2021-02-25 Bae Systems Information And Electronic Systems Integration Inc. Cavity backed notch antenna with additively manufactured radome
US11088456B2 (en) 2019-08-20 2021-08-10 Bae Systems Information And Electronic Systems Integration Inc. Cavity backed notch antenna with additively manufactured radome
AU2020334887B2 (en) * 2019-08-20 2022-03-17 Bae Systems Information And Electronic Systems Integration Inc. Cavity backed notch antenna with additively manufactured radome

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