|Publication number||US3820117 A|
|Publication date||Jun 25, 1974|
|Filing date||Dec 26, 1972|
|Priority date||Dec 26, 1972|
|Also published as||DE2362913A1, DE2362913B2, DE2362913C3|
|Publication number||US 3820117 A, US 3820117A, US-A-3820117, US3820117 A, US3820117A|
|Inventors||Hall R, Johnson R|
|Original Assignee||Bendix Corp|
|Export Citation||BiBTeX, EndNote, RefMan|
|Referenced by (26), Classifications (21)|
|External Links: USPTO, USPTO Assignment, Espacenet|
United States Patent [191 Hall et al,
[ June 25, 1974 FREQUENCY EXTENSION OF CIRCULARLY POLARIZED ANTENNA  Inventors: Roger D. Hall, Encino; Robert P.
Johnson, Granda Hills, both of Calif.
 Assignee: The Bendix Corporation, North Hollywood, Calif.
 Filed: Dec. 26, 1972  Appl. No.: 318,137
 US. Cl 343/802, 343/806, 343/895  Int. Cl H0lq 9/26, l-lOlq 1/38  Field of Search 343/802, 806, 789, 895
 References Cited UNITED STATES PATENTS 2,495,399 l/l950 Wheeler 343/895 FOREIGN PATENTS OR APPLICATIONS 411,888 7/1945 Italy 343/895 Primary ExaminerEli Lieberman Assistant ExaminerWm. H. Punter Attorney, Agent, or Firm-Robert C. Smith ABSTRACT The frequency response of a cavity-backed planar microwave antenna having an element including a pair of spiral antenna tracks fixed to a substrate of insulating material is substantially extended by connecting a pair of cavity-backed outwardly extending dipole elements to the outer ends of each of said spiral tracks. The lower range of useful frequency response is thereby changed from a minimum operating frequency wherein the diameter of the spiral tracks constitutes approximately one-half wave length to a value wherein one-half wave length is approximately equal to the width of the antenna elements including the dipoles. This composite structure may be curved to some degree to enable it to conform to the inside surface of a curved radome.
6 Claims, 3 Drawing Figures This invention relates to circularly polarized, cavitybacked microwave spiral antennas and more particularly to a method and structure for providing a linearly polarized low-frequency extension of the antennas operation. I
For radar warning direction-finding systems installed on aircraft and using remotely located antennas, particularly those installed adjacent to radome structures, it occasionally becomes necessary to extend operating frequencies into lower frequencies without major modifications of the existing antenna locations and radome configurations. In addition to extending the low frequency response of the existing circularly polarized spiral antennas, there may also be a requirement for response to left and right circular polarization, linear polarization and dominantly horizontally polarized lower frequencies.
In most applications, radar warning direction finding systems use circularly polarized, cavity-backed spiral antenna elements operating in the axial mode and producing a cosine pattern. In this mode of operation, maximum radiation will occur along a line normal to the plane of the spiral element. If a reflecting cavity is placed behind the spiral element, a single lobed radiation pattern perpendicular to the plane of the spiral exists. The present invention is concerned with an extension of this mode of operation into lower frequency bands and with response to left and right-hand circular polarization, as well as linear polarizations and dominantly horizontal polarizations at lower frequency bands.
For the axial mode, the generally accepted theoretical basis for operation of the spiral antenna is the current band theory. If a spiral antenna is fed so that energy entering the two spiral tracks at the origin is 180 out of phase, the first current band will occur where current in one arm returns to an in-phase condition with the other arm. This condition will occur because of the geometry of the spiral element; that is, each successive turn of the spiral progressively is longer. Analysis indicates that current in adjacent conductors will reach an in-phase condition where the circumference of the ring is equal to one wave length.
To extend the lower frequency capability of the cavity-backed spiral antenna, the generally accepted approach is to increase the diameter of the antenna until the circumference equals one wave length at the lowest frequency required. This approach is incompatible with the need to extend operating frequencies without major modifications of the existing antenna sites.
The applicants approach herein depends upon using a spiral antenna whose feed systems provide the 180 phase difference for a suitable band width to satisfy both the initial frequency and the extended (lower) frequencies.
The outside ends of the cavity-backed spiral elements are extended by the integration of a cavity-backed dipole element whose effective aperture approximates one half wave length at the lowest required operating frequency. The selected sense of a dominant linear polarization is optional and is determined by the orientation of the dipole elements with respect to the radius vector from the origin of the spiral elements.
In the drawings:
FIG. 1 is a perspective view of an extended frequency range antenna according to our invention.
FIG. 2 is a schematic diagram of the antenna of FIG. 1.
FIG. 3 is a view of a typical radome, shown partly in section, with our antenna installed.
Referring now to FIG. I, a planar spiral microwave antenna element 10 having two separate interlaced spiral tracks 10a and 10b is normally formed as a printed circuit on a substrate of insulating material. Antenna element 10 is positioned overlying a microwave cavity consisting of a cylindrical container 12 which is normally lined internally with microwave absorber material which may be held in place by plastic foam material. Details of the construction of a similar cavitybacked microwave antenna appear in U.S. Pat. No. 3,441,937 (common assignee). Wired to the outside ends of each of conductor tracks 10a and 1012 are dipole elements 14a and 14b. Each of dipole elements 14a and 14b is physically positioned on an insulating substrate 16a and 16b, respectively, supported on housings 18a and 18b which constitute extensions of the microwave cavity housing 12. These housings are also lined with microwave absorber material.
FIG. 2 is a schematic drawing showing some of the electrical properties of the device'of FIG. 1. A pair of conductors 20 and 22 are connected to the antenna element with conductor 20 connected to spiral track 10a and conductor 22 connected to spiral track 10b. These conductors are normally supplied through a coaxial connector having a shield 24. The dipole elements 140 and 14b are connected to the spiral elements and 10b, respectively, as described above, and these are held physically displaced from the back side of the cavity element 12. In the space between cavity 12 and elements 10a, 10b, 14a and 14b is placed a layer of microwave absorber material.
In FIG. 3 is shown a radome 25 which is partially broken away to show the antenna installation against its inside wall. In this installation the insulating substrate for the antenna element 10 is formed in a dome-shaped configuration to minimize the air space between the antenna surface and the interior surface of the radome 25. The dipole extensions 14a and 14b are positioned against the inside surface of the radome and therefore curved to follow its configuration. Attached to the lower part of housing 12 are metal plates 26a and 26b which constitute ground plane elements for the dipole antenna elements 14a and 14b, respectively. Located between ground plane element 28a and antenna element 14a is a layer of material which may be all microwave absorber material or partially microwave absorber material and partially a plastic foam material which is used as a spacer. Similar material is shown at 28b between ground plane 26b and antenna element 1412. To take up any possible remaining air space between the surface of antenna element 10 and the interior surface of the radome 25, a spacer 30 of flexible compressible material may be used between these members. Such a spacer may be made of silicon rubber or other suitable material having dielectric characteristics very similar to that of the radome material.
While only a single embodiment is shown and de scribed herein, modifications may be made to suit certain particular installations. The curved arrangement shown in FIG. 3 causes a flattening or broadening of the antenna characteristic but otherwise has little effeet. From the foregoing, it will be appreciated that applicants have provided an antenna structure which con- I 1. A wide band microwave antenna assembly comprising:
a planar spiral antenna mounted on a substrate of insulating material, said antenna including a pair of interlaced spiral elements having terminals near the axis of said assembly,
a cavity structure of generally cylindrical configuration supporting said antenna element and positioned at the back of said planar spiral antenna,
and a lower frequency linearly polarized antenna extension comprising a cavity-backed dipole element electrically connected to the outside ends of each of said spiral elements.
2. A wide band microwave antenna assembly com prising:
a cylindrical cavity,
an antenna element overlying said cavity including a substrate of insulating material and a pair of interlaced spiral antenna tracks fixed to said substrate,
and a lower frequency extension comprising a cavity backed dipole element connected to the outside end of each of said tracks such that the overall width of the assembly is approximately one-half wave length at the lowest frequency for which the antenna is expected to provide significant gain.
3. A wide band antenna assembly as set forth in claim 2 wherein said cavity and the cavities backing said dipole elements are lined with microwave absorber material.
4. A wide band antenna assembly as set forth in claim 2 wherein said spiral track and said dipole elements are conformed to fit against a rounded radome structure.
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|US4012744 *||Oct 20, 1975||Mar 15, 1977||Itek Corporation||Helix-loaded spiral antenna|
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|US4042935 *||Oct 8, 1975||Aug 16, 1977||Hughes Aircraft Company||Wideband multiplexing antenna feed employing cavity backed wing dipoles|
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|WO1992013372A1 *||Jan 21, 1992||Aug 6, 1992||Rdi Electronics, Inc.||Broadband antenna|
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|WO2015007726A1 *||Jul 15, 2014||Jan 22, 2015||Plath Gmbh||Assembly and method for installing a direction-finding antenna in a radome, preferably for retrofitting a direction-finding antenna in a radome|
|U.S. Classification||343/802, 343/806, 343/895|
|International Classification||H01Q9/04, H01Q9/16, H01Q11/04, H01Q5/00, H01Q21/29, G01S3/04, H01Q9/27, H01Q21/00, H01Q1/00, H01Q11/00, H01Q1/40, G01S3/02|
|Cooperative Classification||H01Q1/405, H01Q9/27, H01Q21/29|
|European Classification||H01Q9/27, H01Q21/29, H01Q1/40B|