[go: up one dir, main page]

US3717878A - Spiral antenna - Google Patents

Spiral antenna Download PDF

Info

Publication number
US3717878A
US3717878A US00707352*A US3717878DA US3717878A US 3717878 A US3717878 A US 3717878A US 3717878D A US3717878D A US 3717878DA US 3717878 A US3717878 A US 3717878A
Authority
US
United States
Prior art keywords
portions
conductor
spiral
length
convolution
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US00707352*A
Inventor
J Mosko
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
US Department of Navy
Original Assignee
US Department of Navy
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by US Department of Navy filed Critical US Department of Navy
Application granted granted Critical
Publication of US3717878A publication Critical patent/US3717878A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q9/00Electrically-short antennas having dimensions not more than twice the operating wavelength and consisting of conductive active radiating elements
    • H01Q9/04Resonant antennas
    • H01Q9/16Resonant antennas with feed intermediate between the extremities of the antenna, e.g. centre-fed dipole
    • H01Q9/26Resonant antennas with feed intermediate between the extremities of the antenna, e.g. centre-fed dipole with folded element or elements, the folded parts being spaced apart a small fraction of operating wavelength
    • H01Q9/27Spiral antennas

Definitions

  • ABSTRACT Spiral antenna in which adjacent conductors are three dimensional and composed of spaced segments of a spiral disposed in one plane, the ends of which are joined by conductors disposed in another plane which have lengths greater than the spacing between the ends of the segments, thereby increasing the wire length of the convolutions over that of conductors having convolutions which lie only in one plane.
  • each conductor forms a spiral, similar to. the patents referred to but the circumferential length at a given convolution is not a function of pi since the spiral is formed by winding the conductor in a direction other than planar which increases the length of a convolution beyond the relationship of pi times its diameter.
  • a wave length of conductor may thus be disposed in a considerably smaller diameter, thus reducing the size of the antenna in some proportion to the added length of conductor over'that of a single planar wound conductor as disclosed in the prior art referred to.
  • FIG. P.A. illustrates prior art
  • FIG. 1 is an isometric view of a portion of a conductor convolution, illustrating the general principle of the invention in one of its various forms;
  • FIG. 2 is an elevation of a preferred embodiment of the invention, illustrating the conductors, as viewed from the front of the antenna;
  • FIG. 3 is a section taken on line 3-3, FIG. 2;
  • FIG. 4 is a three-dimensional phantom view of a portion of FIGS. 2 and 3.
  • the circumferential length of a particular convolution of an Archimedian spiral, as disclosed by Turner is expressed by 1rD which may be considered as one wave length and the diameter at which response occurs.
  • a conductor may be formed so that portions are in one plane, portions 12 are in another spaced plane and portions 14 join portions 10 and 12. It will be apparent that the wave length of a convolution, formerly expressed as rrD, is now increased by the summation of the lengths of portions 14 contained in one convolution.
  • a convolution of one wave length will have a diameter less than D in FIG. P.A. and the overall diameter of the antenna may be reduced in some proportion to the added lengths 14, 14 in one convolution.
  • a diameter D, FIG. 1 for a convolution analogous to a convolution of FIG. P.A., is less than D of FIG. P.A. in some proportion to the added lengths of wire 14.
  • the spiral chosen for illustration of the preferred embodiment has conductor segments which have a constant angle with respect to their radius vectors.
  • the radial spacing between adjacent conductors (say a pair 180 out of phase) thus increases with increase of the radius vectors in distinction to remaining constant, as described in connection with the prior art.
  • a spiral which cuts the radius vectors at constant angle is generally known as a logarithmic spiral. This is illustrated in FIG. 2 wherein spiral conductors a and b have origins 180 apart and the angle between segment s at radius r, equals the angle between segment s at radius r etc.
  • each conductor a, b must be continuous between its origin near the center of the figure and its termination at the periphery of the figure, adjacent segments of each conductor must be joined together. This is attained in a manner similar to that illustrated in FIG. 1 and wherein two legs 14a, 14a extend rearwardly perpendicular to the page, one being connected to the outer end of a segment and the other to the inner end of the adjacent segment, the two legs being connected by a bight 12a spaced rearwardly from the plane of the segments.
  • the various segments s of two conductors a and b are illustrated as they appear as viewed toward the front face of "the antenna. As illustrated, only two conductors are shown having origins and terminations 180 apart. In an actual embodiment, however, four conductors are employed, these being disposed apart.
  • the visible segments s lie on a flat dielectric plate 20 which is drilled for receiving the rearwardly extending legs.
  • the legs 14a, 14a pass through similar holes in a rearwardly spaced conical dielectric plate 22, the bights 1201 being disposed at the rear surface of plate 22.
  • the outer ends of all conductors are connected to a ground ring 26 and their inner ends are connected to terminals 28, these being connected in any well known manner to a source for driving the antenna, or to a receiver, if used in such manner.
  • the distance d between the plates constantly increases in a radial outward direction, thus increasing the lengths of the conductors between adjacent seg ments s, the distance being a constant times a wave length. If desired, and weight is not critical, the space between the plates may be filled with a ferro-dielectric material.
  • the plates are secured to a suitable metallic cavity ring 30, closed at its rear end by a plate 32 which renders the operation of the antenna unidirectional. If
  • the space between plates 22,32 may be filled with foam material to render the space electrically absorbent.
  • Any suitable mounting device, such as ring 34, may be employed to secure the antenna to its supporting structure.
  • the surface of plate is generated by a straight line rotated perpendicular to the antenna axis (planar) and the surface of plate 22 is generated by a straight line rotated nonperpendicular to such axis (cone).
  • These surfaces may be of other shapes but normally will be formed as surfaces of revolution of either straight lines or curves.
  • a reduced size antenna comprising:
  • each conductor having segmental portions lying adjacent said surface, the segmental portions forming a spiral
  • segmental portions being series connected by other portions of the conductor
  • each of said other portions having a length in excess of the distance between ends of adjacent segments
  • An antenna in accordance with claim 1 including a second dielectric surface disposed in spaced relation to said mounting surface, each of said other portions extending between said mounting surface and the second dielectric surface and each having a portion disposed adjacent and supported by the second dielectric surface.
  • each of said segments is disposed at a constant angle to its radius vector.

Landscapes

  • Details Of Aerials (AREA)

Abstract

Spiral antenna in which adjacent conductors are three dimensional and composed of spaced segments of a spiral disposed in one plane, the ends of which are joined by conductors disposed in another plane which have lengths greater than the spacing between the ends of the segments, thereby increasing the wire length of the convolutions over that of conductors having convolutions which lie only in one plane.

Description

United States Patent [191 Mosko i 1 SPIRAL ANTENNA [75] Inventor: Joseph A. Mosko, China Lake,
Calif.
[73] Assignee: The United States of America as represented by the Secretary of the Navy 221 Filed: Jan. 31, 1968 211 Appl.No.:707,352
n11 3,717,878 [451 Feb. 20, 1973 3,106,714 10/1963 Minerva ..343/792.5
Primary Examiner-Samuel Feinberg Assistant Examiner-Richard E. Berger Attorney-G. J. Rubens, R. Miller and V. C. Muller 57 ABSTRACT Spiral antenna in which adjacent conductors are three dimensional and composed of spaced segments of a spiral disposed in one plane, the ends of which are joined by conductors disposed in another plane which have lengths greater than the spacing between the ends of the segments, thereby increasing the wire length of the convolutions over that of conductors having convolutions which lie only in one plane.
4 Claims, 5 Drawing Figures IIIIIIIIIIIII: 711: VA!
- suinm? 2 1 I (FRI OR ART) FIG. PA.
E L IO 1 FIG; L
FIG. 3.
v'qc,v MULLER ROY MILLER ATTORNEYS.
SPIRAL ANTENNA The invention described herein may be manufactured and used by or for the Government of the United States of America for governmental purposes without the payment of any royalties thereon or therefor.
BACKGROUND OF THE INVENTION As exemplified by US. Pats. No. 2,863,145 and No. 2,947,000 to Turner and Marston, respectively, spiral dipole antennas which respond to wide frequency ratios are now well known and have the advantage over former rod-type antennas in that they occupy less space. In each of these patents the two conductors are wound in the form of equi-distant spaced spirals having portions which radiate at certain frequencies. As dis- 'closed by Turner, the circumference of a circle at which response occurs equals one wave length of the particular frequency, the diameter of the circle thus having the wave length divided by pi. Turner also disclosed that this relationship determines the minimum size of a many turn spiral antenna. As will subsequently appear, this assumption is valid only if the conductors are simple convolutions in a single plane in which the length of a convolution is pi times its diameter.
SUMMARY OF THE INVENTION In the present invention, the total length of each conductor forms a spiral, similar to. the patents referred to but the circumferential length at a given convolution is not a function of pi since the spiral is formed by winding the conductor in a direction other than planar which increases the length of a convolution beyond the relationship of pi times its diameter. A wave length of conductor may thus be disposed in a considerably smaller diameter, thus reducing the size of the antenna in some proportion to the added length of conductor over'that of a single planar wound conductor as disclosed in the prior art referred to.
BRIEF DESCRIPTION OF THE DRAWING FIG. P.A. illustrates prior art;
FIG. 1 is an isometric view of a portion of a conductor convolution, illustrating the general principle of the invention in one of its various forms;
FIG. 2 is an elevation of a preferred embodiment of the invention, illustrating the conductors, as viewed from the front of the antenna;
FIG. 3 is a section taken on line 3-3, FIG. 2; and
FIG. 4 is a three-dimensional phantom view of a portion of FIGS. 2 and 3.
DESCRIPTION OF GENERAL CONCEPT The detailed description of a preferred embodiment, to follow, may be better understood by first comparing the inventive concept with a spiral antenna having conductors which lie in a single plane, such as those disclosed in the prior art referred to.
Referring first to FIG. P.A., the circumferential length of a particular convolution of an Archimedian spiral, as disclosed by Turner, is expressed by 1rD which may be considered as one wave length and the diameter at which response occurs. Referring now to FIG. 1, which represents a portion of a like convolution, a conductor may be formed so that portions are in one plane, portions 12 are in another spaced plane and portions 14 join portions 10 and 12. It will be apparent that the wave length of a convolution, formerly expressed as rrD, is now increased by the summation of the lengths of portions 14 contained in one convolution. (It being assumed that portions 12 are of a length equal to the gaps between portions 10, 10.) It follows, then, that a convolution of one wave length will have a diameter less than D in FIG. P.A. and the overall diameter of the antenna may be reduced in some proportion to the added lengths 14, 14 in one convolution. Thus a diameter D, FIG. 1, for a convolution analogous to a convolution of FIG. P.A., is less than D of FIG. P.A. in some proportion to the added lengths of wire 14.
DESCRIPTION OF THE PREFERRED EMBODIMENT While the invention may be practiced with equispaced conductors, as just referred to, the spiral chosen for illustration of the preferred embodiment has conductor segments which have a constant angle with respect to their radius vectors. The radial spacing between adjacent conductors (say a pair 180 out of phase) thus increases with increase of the radius vectors in distinction to remaining constant, as described in connection with the prior art. A spiral which cuts the radius vectors at constant angle is generally known as a logarithmic spiral. This is illustrated in FIG. 2 wherein spiral conductors a and b have origins 180 apart and the angle between segment s at radius r, equals the angle between segment s at radius r etc. Since each conductor a, b, must be continuous between its origin near the center of the figure and its termination at the periphery of the figure, adjacent segments of each conductor must be joined together. This is attained in a manner similar to that illustrated in FIG. 1 and wherein two legs 14a, 14a extend rearwardly perpendicular to the page, one being connected to the outer end of a segment and the other to the inner end of the adjacent segment, the two legs being connected by a bight 12a spaced rearwardly from the plane of the segments.
Referring now to FIG. 2, the various segments s of two conductors a and b are illustrated as they appear as viewed toward the front face of "the antenna. As illustrated, only two conductors are shown having origins and terminations 180 apart. In an actual embodiment, however, four conductors are employed, these being disposed apart. The visible segments s lie on a flat dielectric plate 20 which is drilled for receiving the rearwardly extending legs. The legs 14a, 14a pass through similar holes in a rearwardly spaced conical dielectric plate 22, the bights 1201 being disposed at the rear surface of plate 22. The outer ends of all conductors are connected to a ground ring 26 and their inner ends are connected to terminals 28, these being connected in any well known manner to a source for driving the antenna, or to a receiver, if used in such manner. The distance d between the plates constantly increases in a radial outward direction, thus increasing the lengths of the conductors between adjacent seg ments s, the distance being a constant times a wave length. If desired, and weight is not critical, the space between the plates may be filled with a ferro-dielectric material. The plates are secured to a suitable metallic cavity ring 30, closed at its rear end by a plate 32 which renders the operation of the antenna unidirectional. If
desired, the space between plates 22,32 may be filled with foam material to render the space electrically absorbent. Any suitable mounting device, such as ring 34, may be employed to secure the antenna to its supporting structure.
As will be apparent, the surface of plate is generated by a straight line rotated perpendicular to the antenna axis (planar) and the surface of plate 22 is generated by a straight line rotated nonperpendicular to such axis (cone). These surfaces may be of other shapes but normally will be formed as surfaces of revolution of either straight lines or curves.
What is claimed is:
l. A reduced size antenna comprising:
a dielectric planar mounting surface;
at least two substantially identical equiangularly spaced conductors;
each conductor having segmental portions lying adjacent said surface, the segmental portions forming a spiral;
said segmental portions being series connected by other portions of the conductor;
each of said other portions having a length in excess of the distance between ends of adjacent segments;
said other portions being disposed away from the plane of said mounting surface;
whereby the conductor length of a convolution of the spiral is greater than the length around the convolution.
2. An antenna in accordance with claim 1 including a second dielectric surface disposed in spaced relation to said mounting surface, each of said other portions extending between said mounting surface and the second dielectric surface and each having a portion disposed adjacent and supported by the second dielectric surface.
3. An antenna in accordance with claim 2 wherein the second dielectric surface is conical and the distance between it and the mounting surface constantly increases in a radially outward direction.
4. An antenna in accordance with claim 3 wherein each of said segments is disposed at a constant angle to its radius vector.

Claims (4)

1. A reduced size antenna comprising: a dielectric planar mounting surface; at least two substantially identical equiangularly spaced conductors; each conductor having segmental portions lying adjacent said surface, the segmental portions forming a spiral; said segmental portions being series connected by other portions of the conductor; each of said other portions having a length in excess of the distance between ends of adjacent segments; said other portions being disposed away from the plane of said mounting surface; whereby the conductor length of a convolution of the spiral is greater than the length around the convolution.
1. A reduced size antenna comprising: a dielectric planar mounting surface; at least two substantially identical equiangularly spaced conductors; each conductor having segmental portions lying adjacent said surface, the segmental portions forming a spiral; said segmental portions being series connected by other portions of the conductor; each of said other portions having a length in excess of the distance between ends of adjacent segments; said other portions being disposed away from the plane of said mounting surface; whereby the conductor length of a convolution of the spiral is greater than the length around the convolution.
2. An antenna in accordance with claim 1 including a second dielectric surface disposed in spaced relation to said mounting surface, each of said other portions extending between said mounting surface and the second dielectric surface and each having a portion disposed adjacent and supported by the second dielectric surface.
3. An antenna in accordance with claim 2 wherein the second dielectric surface is conical and the distance between it and the mounting surface constantly increases in a radially outward direction.
US00707352*A 1968-01-31 1968-01-31 Spiral antenna Expired - Lifetime US3717878A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US70735268A 1968-01-31 1968-01-31

Publications (1)

Publication Number Publication Date
US3717878A true US3717878A (en) 1973-02-20

Family

ID=24841358

Family Applications (1)

Application Number Title Priority Date Filing Date
US00707352*A Expired - Lifetime US3717878A (en) 1968-01-31 1968-01-31 Spiral antenna

Country Status (1)

Country Link
US (1) US3717878A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4630064A (en) * 1983-09-30 1986-12-16 The Boeing Company Spiral antenna with selectable impedance
US4823145A (en) * 1986-09-12 1989-04-18 University Patents, Inc. Curved microstrip antennas
EP0762539A1 (en) * 1995-08-17 1997-03-12 Murata Manufacturing Co., Ltd. Chip antenna
US6791508B2 (en) 2002-06-06 2004-09-14 The Boeing Company Wideband conical spiral antenna
US8922452B1 (en) 2014-03-21 2014-12-30 University Of South Florida Periodic spiral antennas
US9437932B1 (en) 2011-09-09 2016-09-06 The United States Of America As Represented By The Secretary Of The Navy Two-arm delta mode spiral antenna
US20180083350A1 (en) * 2016-09-21 2018-03-22 Lockheed Martin Corporation Up-down zigzag additive spiral antenna

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2005805A (en) * 1930-04-02 1935-06-25 Rca Corp Aerial
US3039099A (en) * 1959-06-25 1962-06-12 Herman N Chait Linearly polarized spiral antenna system
US3106714A (en) * 1960-10-18 1963-10-08 Collins Radio Co Log periodic antenna with accordioned radiators to increase shunt capacitance

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2005805A (en) * 1930-04-02 1935-06-25 Rca Corp Aerial
US3039099A (en) * 1959-06-25 1962-06-12 Herman N Chait Linearly polarized spiral antenna system
US3106714A (en) * 1960-10-18 1963-10-08 Collins Radio Co Log periodic antenna with accordioned radiators to increase shunt capacitance

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4630064A (en) * 1983-09-30 1986-12-16 The Boeing Company Spiral antenna with selectable impedance
US4823145A (en) * 1986-09-12 1989-04-18 University Patents, Inc. Curved microstrip antennas
EP0762539A1 (en) * 1995-08-17 1997-03-12 Murata Manufacturing Co., Ltd. Chip antenna
US6791508B2 (en) 2002-06-06 2004-09-14 The Boeing Company Wideband conical spiral antenna
US9437932B1 (en) 2011-09-09 2016-09-06 The United States Of America As Represented By The Secretary Of The Navy Two-arm delta mode spiral antenna
US8922452B1 (en) 2014-03-21 2014-12-30 University Of South Florida Periodic spiral antennas
US20180083350A1 (en) * 2016-09-21 2018-03-22 Lockheed Martin Corporation Up-down zigzag additive spiral antenna
US10903556B2 (en) * 2016-09-21 2021-01-26 Lockheed Martin Corporation Up-down zigzag additive spiral antenna

Similar Documents

Publication Publication Date Title
US3942180A (en) Wide-band omnidirectional antenna
US4012744A (en) Helix-loaded spiral antenna
US4658262A (en) Dual polarized sinuous antennas
US3787871A (en) Terminator for spiral antenna
US4772891A (en) Broadband dual polarized radiator for surface wave transmission line
US3568204A (en) Multimode antenna feed system having a plurality of tracking elements mounted symmetrically about the inner walls and at the aperture end of a scalar horn
Bawer et al. The spiral antenna
US2275646A (en) Antenna
US2978702A (en) Antenna polarizer having two phase shifting medium
US3956752A (en) Polarization insensitive lens formed of spiral radiators
US2977594A (en) Spiral doublet antenna
US3017633A (en) Linearly polarized spiral antenna system and feed system therefor
US2677766A (en) Scalloped limacon pattern antenna
US2472106A (en) Broad band antenna
US3717878A (en) Spiral antenna
US4014028A (en) Backfire bifilar helical antenna
US4225869A (en) Multislot bicone antenna
US3039099A (en) Linearly polarized spiral antenna system
US3135960A (en) Spiral mode selector circuit for a twowire archimedean spiral antenna
US2462881A (en) Antenna
US8547291B1 (en) Direct fed bifilar helix antenna
US2482767A (en) Broad band antenna
Jordan et al. Developments in broadband antennas
US3192529A (en) Multi-helix antenna on inflatable satellite
US3137002A (en) Spiral antenna with arms of different lengths for polarization change