U.S. patent number 3,820,117 [Application Number 05/318,137] was granted by the patent office on 1974-06-25 for frequency extension of circularly polarized antenna.
This patent grant is currently assigned to The Bendix Corporation. Invention is credited to Roger D. Hall, Robert P. Johnson.
United States Patent |
3,820,117 |
Hall , et al. |
June 25, 1974 |
FREQUENCY EXTENSION OF CIRCULARLY POLARIZED ANTENNA
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.
Inventors: |
Hall; Roger D. (Encino, CA),
Johnson; Robert P. (Granda Hills, CA) |
Assignee: |
The Bendix Corporation (North
Hollywood, CA)
|
Family
ID: |
23236818 |
Appl.
No.: |
05/318,137 |
Filed: |
December 26, 1972 |
Current U.S.
Class: |
343/802; 343/806;
343/895 |
Current CPC
Class: |
H01Q
9/27 (20130101); H01Q 1/405 (20130101); H01Q
21/29 (20130101) |
Current International
Class: |
H01Q
1/40 (20060101); H01Q 9/27 (20060101); H01Q
1/00 (20060101); H01Q 21/29 (20060101); H01Q
9/04 (20060101); H01Q 21/00 (20060101); H01q
009/26 (); H01q 001/38 () |
Field of
Search: |
;343/802,806,789,895 |
References Cited
[Referenced By]
U.S. Patent Documents
Foreign Patent Documents
Primary Examiner: Lieberman; Eli
Assistant Examiner: Punter; Wm. H.
Attorney, Agent or Firm: Smith; Robert C.
Claims
We claim:
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 comprising:
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.
5. A wide band antenna assembly as set forth in claim 2 wherein
said substrate is dome-shaped and said dipole elements are
curved.
6. A wide band antenna assembly as set forth in claim 2 wherein the
height of said antenna tracks and dipole members from the back
walls of their respective cavities is less than one-quarter wave
length over the frequencies received.
Description
This invention relates to circularly polarized, cavity-backed
microwave spiral antennas and more particularly to a method and
structure for providing a linearly polarized low-frequency
extension of the antenna's operation.
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.degree. 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.degree. 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. 1, 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 cavity-backed 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 10b 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 14a and 14b are connected
to the spiral elements 10a 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 14b. 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 described 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
effect. From the foregoing, it will be appreciated that applicants
have provided an antenna structure which conforms to the internal
dimensions of the radome 25 to much better advantage than would the
cavity-backed spiral antenna of substantially larger diameter, yet
its performance is quite similar.
* * * * *