U.S. patent number 3,828,351 [Application Number 05/381,707] was granted by the patent office on 1974-08-06 for broadband spiral antenna.
This patent grant is currently assigned to Textron Inc.. Invention is credited to George N. Voronoff.
United States Patent |
3,828,351 |
Voronoff |
August 6, 1974 |
BROADBAND SPIRAL ANTENNA
Abstract
A frequency independent spiral antenna having a plurality of
pairs of arms energized with currents equal to the sine of the
respective terminal position angles of the arms for substantially
removing bandwidth limitations.
Inventors: |
Voronoff; George N. (San
Francisco, CA) |
Assignee: |
Textron Inc. (Belmont,
CA)
|
Family
ID: |
23506073 |
Appl.
No.: |
05/381,707 |
Filed: |
July 23, 1973 |
Current U.S.
Class: |
343/740; 343/853;
343/895 |
Current CPC
Class: |
H01Q
9/27 (20130101); H01Q 21/20 (20130101) |
Current International
Class: |
H01Q
21/20 (20060101); H01Q 9/27 (20060101); H01Q
9/04 (20060101); H01q 001/36 () |
Field of
Search: |
;343/740,853,895 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Lieberman; Eli
Attorney, Agent or Firm: Gregg, Hendricson & Caplan
Claims
What is claimed is:
1. A broadband frequency-independent spiral antenna comprising
an even number of spiral arms equally spaced circumferentially
about a center and having a center line extending through the inner
terminals of two opposite arms, and
means energizing said arms in accordance with the relationship
I.sub.n = Sin.phi..sub.n where I.sub.n is the excitation current of
the nth arm of the antenna and .phi. is the angle between the
center line and the inner terminal of the nth arm of the
antenna.
2. The antenna of claim 1 further defined by said means energizing
said antenna arms comprising a circuit element adapted to receive
electrical current and pass current onto two output lines in
opposite phase, and a pair of power dividers connected one in each
of said output lines and to separate antenna arms.
3. The antenna of claim 1 further defined by means resistively
loading each of said antenna arms adjacent the outer ends thereof
for suppressing mode 7 radiation therefrom.
Description
BACKGROUND OF INVENTION
Spiral antennas commonly denominated as frequency independent
antennas are actually only relatively insensitive to frequency
variations above some minimum frequency. In actual practice it is
found that mounting of such antennas relatively close to a ground
plane or the like increases frequency dependency which is highly
undesirable for many applications. This problem is particularly
noted in aircraft installations of antennas directly over the
aircraft skin which are often employed with communications or
direction-finding equipment.
There has been developed an antenna described and claimed in U.S.
Pat. No. 3,624,658 which provides a major improvement in the field
of frequency independent antennas capable of producing a stable
radiation pattern over an appreciable bandwidth such as a bandwidth
of 4:1 or greater.
The present invention provides a further improvement in spiral
antennas to substantially eliminate bandwidth limitations.
SUMMARY OF INVENTION
The antenna of the present invention is comprised as a plurality of
pairs of spiral arms particularly energized to maximize frequency
independence of the antenna. The curvature of the arms of the
antenna hereof may be properly delineated as either an Archimedean
spiral or as a logarithmic spiral; however, in the following
description of the present invention the term "spiral" is taken to
denominate an antenna having curved arms of these general
types.
The antenna of this invention has a generally flat configuration
which may be closely spaced from a ground plane or the like with
the outer ends of the spiral arms being terminated as by resistive
coupling to the ground plane or the like. The individual arms of
the antenna hereof have the inner terminations thereof spaced
equally about a circle surrounding the center of the antenna.
Considering a center line through two oppositely spaced points on
such circle the terminal position angle of each antenna arm is
taken as the angle between such center line and the inner terminus
of the arm. In accordance with the present invention, the spiral
arms of the antenna are energized by excitation currents, I.sub.n,
of an N arm spiral equal to the sine of the terminal position
angle. With the terminal position angle being identified as
.phi..sub.n, excitation is then I.sub.n = Sin .phi..sub.n, where n
= 1, 2, 3, . . . N. With this energization the only possible modal
regions on the spiral will be 1 and N-1 to thus achieve an
approximate bandwidth of (N-2): 1.
It will be seen from the foregoing that the frequency independent
bandwidth of the present invention increases with increasing
numbers of spiral arms and it is further noted that energization or
excitation of the antenna arms may be provided by a simple power
divider so as to minimize complexity of antenna energization.
DESCRIPTION OF FIGURES
The present invention is illustrated as to a single preferred
embodiment thereof in the accompanying drawings wherein:
FIG. 1 is an illustration of a prior art broadband spiral
antenna;
FIG. 2 is an illustration of radiation patterns of various
harmonics of a spiral antenna;
FIG. 3 is a schematic illustration of a spiral antenna in
accordance with the present invention;
FIG. 4 is a schematic representation of the inner ends of spiral
arms of an antenna in accordance with the present invention and
identifying terminal position angle .phi.;
FIG. 5 is a schematic representation of an antenna feed network for
the antenna of FIG. 3; and
FIG. 6 is a schematic representation of the antenna of FIG. 3 in
side elevation.
DESCRIPTION OF PREFERRED EMBODIMENT
The antenna of the present invention comprises a multiarm spiral
antenna having an even number of arms from 4 to 20 or more. In FIG.
1 of the drawings there is is illustrated the prior art antenna of
U.S. Pat. No. 3,624,658 having 6 spiral arms. The first and second
arms are connected together and energization is applied between
such connection and a connection between the fourth and fifth arms
as shown. The opposite third and sixth arms of the antenna are
parasitically excited. This prior art antenna produces only Mode 1
and Mode 5 radiation and in accordance with the teaching of the
above-noted patent, Mode 5 radiation is suppressed by the
utilization of an absorber or resistive terminations at particular
antenna arm radius. This antenna has a frequency independent
bandwidth of the order of 4:1. The antenna of the present invention
may be physically configured in much the same manner as the antenna
of FIG. 1; however, the present invention is not limited to a 6 arm
spiral and, furthermore, is energized in a different manner.
There is illustrated in FIG. 2 the radiation patterns for different
modes or harmonics of energy radiated from a spiral antenna as
originally presented in the publication "Frequency-Independent
Antennas" by Victor H. Rumsey, Academic Press, 1966, page 122. It
will be seen that Mode 1 radiation comprises a single lobe
extending in one direction from the source or antenna and for many
purposes this type of radiation is highly desirable.
In order to preserve these desirable features of Mode 1 in a truly
frequency independent manner, all other modes must be eliminated or
at least suppressed to such an extent that their effect on the
radiation becomes minimal.
There is illustrated in FIG. 3 an eight arm spiral antenna in
accordance with the present invention and it will be seen that the
arms A through H are equiangular, for example, and equally spaced
apart with inner terminal points A1, B1, etc., which may lie on a
circle about the center of the antenna. In FIG. 4 there are
illustrated these inner terminal points in connection with an XY
coordinate system having a center at the center of the antenna. A
center line along the X axis of the coordinate system is taken as a
reference line for measurement of terminal position angles .phi..
With an eight arm spiral antenna, as illustrated in FIG. 3, and the
arms being equally spaced apart, .phi. = 0.degree. for A1, .phi. =
45.degree. for B1, etc. Obviously with a different number of arms
the increase in terminal position angle between successive arms
will be different. It is particularly noted that the present
invention is limited to a spiral antenna having an even number of
arms and this even number may be any number from 4 to 20 or more,
with the example of eight illustrated herein being chosen solely
for convenience.
The present invention provides an unobvious and highly advantageous
energization of the spiral antenna hereof in accordance with the
limitation
I.sub.n = Sin .phi..sub.n
wherein I.sub.n is the excitation current of the Nth arm and
.phi..sub.n is the terminal position angle of the Nth arm.
It will be appreciated that the relative excitation currents of
different arms of the antenna of the present invention are
proportioned in accordance with the sines of the terminal position
angles of the arms; however, the absolute value of any excitation
current is, in fact, the product of the sine of the terminal
position angle of the arm multiplied by a fixed arbitrary current
value I. Thus the excitation current of the Nth arm of an N arm
spiral antenna in accordance with the present invention is
I.sub.n = I .sup.. Sin .phi..sub.n
In the illustrated example of the present invention there are
provided eight arms in the spiral with the first arm A having a
terminal position angle .phi. = 0. Sin 0.degree. = 0 and thus the
excitation I.sub.A = 0. With the arms of the antenna equally spaced
apart, it will be seen that sin .phi..sub.B = 45.degree., sin
.phi..sub.C = 90.degree., sin .phi..sub.D = 135.degree., sin
.phi..sub.E = 180.degree., etc. In other words, the terminal
positions of the antenna arms are separated 45.degree. apart about
a circle and thus excitation of the arms will be as follows:
I.sub.A = 0
I.sub.B = 0.707
I.sub.C = 1.00
I.sub.D = 0.707
I.sub.E = 0
I.sub.F = -0.707
I.sub.G = -1.00
I.sub.H = -0.707
In this illustrated example the figures set forth above are
intended to be relative, i.e., each of the numbers in the foregoing
table are multiplied by I which is some predetermined basic
excitation current value determining the overall power to be
transmitted from the antenna. It is furthermore to be noted that in
the foregoing table the negative values represent currents of
opposite phase and thus, for example, the excitation currents
I.sub.B and I.sub.F are 180.degree. out of phase.
With an eight arm antenna, as illustrated, energization or
excitation of the arms may be very simply accomplished to attain
the excitation values of the present invention. This is illustrated
in FIG. 5 wherein an input power terminal 51 is shown to be
connected to a 180.degree. hybrid or balun 52 which then provides
currents on the two output lines 53 and 54 which are 180.degree.
out of phase. Across the top of FIG. 5 there are illustrated eight
terminals representing the arms A to H of the antenna and labeled
with these letters. It will be seen that terminal arm A is not
connected to the power supply inasmuch as the present invention, as
described above, provides for zero excitation current applied to
antenna arm A. The line 53 extends from the hybrid 52 to a power
splitter 56 which may be wholly conventional and which has three
output lines leading to antenna arm terminals B, C, and D. This
power splitter 56 applies current to the antenna arms B, C and D in
the proporations I.sub.B = 0.707, I.sub.C = 1.00 and I.sub.D =
0.707. The other lead 54 from the hybrid 52 extends to another
power splitter 57, also of conventional design, having three output
lines connected to antenna arms or terminals F, G and H. Current is
split to provide excitation currents to these arms in the
proportions I.sub.F = 0.707, I.sub.G = 1.00 and I.sub.H = 0.707. It
will, however, be appreciated that the hybrid or balun 52 provides
a 180.degree. phase difference between currents applied to the
output lines 53 and 54 thereof and thus the currents to the left of
the hybrid may be considered as being defined by a minus sign so
that in fact I.sub.F = -0.707, I.sub.G = -1.00 and I.sub.H =
-0.707. The antenna arm E is to receive no energization and thus it
will be noted that terminal E is not connected to the power
supply.
Power supply connections to the eight arms of the illustrated
antenna are clearly of a very simple nature employing only
conventional circuit elements to split the excitation currents as
required by the present invention. It has been determined that with
the recited excitation currents of the arms of the antenna hereof,
the only possible modal regions on the spiral antenna will be 1 and
N-1. For an eight arm spiral where N = 8 there then results only
the possibility of Mode 1 and Mode 7 excitation. It is believed
clear from FIG. 2 that Mode 7 excitation is the very minor one.
This mode, however, can be completly eliminated by resistively
loading the spiral at a predetermined radius. It has furthermore
been determined that the approximate achievable bandwidth is (N-2):
1 and thus, in the present example of this invention where N = 8,
the bandwidth is 6:1. This in itself will be appreciated to be a
major improvement in the art.
Although the present invention has been described with respect to
an eight arm antenna, it has been noted above that the invention is
applicable with any spiral antenna having an even number of arms
wherein such number lies in the range of 4 to 20 or more. A spiral
antenna, in accordance with the present invention, having sixteen
arms and energized as set forth above, would have a bandwidth of
14:1 and it will be appreciated that this is, in fact,
substantially no bandwidth limitation at all. For practical
applications it is generally considered that a bandwidth of 6:1 or
more is so broad as to comprise substantially no bandwidth
limitation.
It is preferable for the antenna arms of the present invention to
be resistively terminated to a ground plane such as illustrated in
FIG. 6 wherein resistive terminations 61 and 62 are schematically
shown to extend from antenna arms to a ground plane 63. It is not,
however, necessary with the present invention to employ absorbers
behind the antenna even though the antenna is formed as a low
profile unit, i.e., is closely spaced to a ground plane or cavity
wall. The invention is equally applicable to VHF and UHF
applications and will thus be seen to be highly advantageous for
air-borne applications.
Although the present invention has been described with respect to a
single preferred embodiment thereof, it will be appreciated that
variations and modifications may be made within the spirit of the
present invention. It is thus not intended to limit the present
invention to the precise details of description or
illustration.
* * * * *