U.S. patent number 3,681,772 [Application Number 05/103,116] was granted by the patent office on 1972-08-01 for modulated arm width spiral antenna.
This patent grant is currently assigned to TRW Inc.. Invention is credited to Paul G. Ingerson.
United States Patent |
3,681,772 |
Ingerson |
August 1, 1972 |
MODULATED ARM WIDTH SPIRAL ANTENNA
Abstract
A multi-arm spiral antenna which allows unlimited broadband
operation with dual senses of circular polarization. The antenna
comprises spiral arms having width variations which are
log-periodically scaled to produce local reflection (stopband)
regions along the arms. The position of the stop-band regions is a
function of the period and amplitude of width variations. Arm
currents are produced by excitation of the antenna. These currents
are reflected by the stopband regions. The relative phase of the
reflected currents is a function of the relative scaling of the
arms.
Inventors: |
Ingerson; Paul G. (Los Angeles,
CA) |
Assignee: |
TRW Inc. (Redondo Beach,
CA)
|
Family
ID: |
22293489 |
Appl.
No.: |
05/103,116 |
Filed: |
December 31, 1970 |
Current U.S.
Class: |
343/895 |
Current CPC
Class: |
H01Q
11/083 (20130101); H01Q 1/38 (20130101) |
Current International
Class: |
H01Q
11/08 (20060101); H01Q 11/00 (20060101); H01Q
1/38 (20060101); H01q 001/36 () |
Field of
Search: |
;343/802,895 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Lieberman; Eli
Claims
1. A multi-arm spiral antenna capable of radiating circularly
polarized electromagnetic energy with opposite senses of
polarization, said antenna comprising:
a. at least two spiral arms, each arm consisting of a plurality of
interconnected cells, each cell consisting of a wide and a narrow
section along the length of its arm, the transition between
adjacent wide and narrow sections being relatively abrupt, whereby
to reflect electromagnetic energy, the sections of each cell
increasing in length as the distance from the center increases,
and
b. means for feeding said arms at the center of the spiral with
2. The antenna of claim 1 wherein:
3. The antenna of claim 2 wherein:
the ratio of the widths of the wide section of adjacent arm-cells
is
4. The antenna of claim 3 wherein:
the ratios of the widths of the wide sections of adjacent cells and
the
5. The antenna of claim 3 wherein:
the ratio of the width of the narrow section of adjacent arm cells
is
6. The antenna of claim 4 wherein:
the ratios of the narrow sections of each cell are equal to the
ratios of
7. The antenna of claim 1 wherein:
8. The antenna of claim 7 wherein:
9. The antenna of claim 8 wherein:
10. An antenna as defined in claim 1 wherein the spacing between
adjacent ones of said arms is nonuniform, thereby to provide a
change of impedance
11. An antenna as defined in claim 1 wherein said arms are disposed
on the surface of a cone.
Description
BACKGROUND OF THE INVENTION
1. Field of the Invention
This invention relates to spiral antennas and specifically to
multi-arm spiral antenna having both left-hand and right-hand
circular polarization simultaneously produced over wide
bandwidths.
2. Description of the Prior Art
The customary method of feeding broadband spiral antennas at the
center terminals yields a radiation field which is elliptically
polarized. If the parameters of the antenna are chosen properly,
the radiation polarization can be made almost circular.
The sense of circular polarization (CP) is said to be right-handed
circular polarization (RHCP) if the electric field vector rotates
in the direction of the fingers of the right hand when the thumb
points in the direction of propagation. Correspondingly,
left-handed circular polarization (LHCP) is defined by an electric
field vector rotating in the direction of the fingers of the left
hand when the thumb points in the direction of propagation.
Spiral antennas are said to have a sense of wrap. The spiral sense
of wrap is, in accordance with general practice, determined by the
hand used when pointing the fingers in the direction of the arm
current and the thumb in the direction of propagation of the
radiated fields. Broadband operation of a spiral antenna yields the
sense of polarization of the radiated field determined by the sense
of wrap of the spiral.
Many applications of extremely broadband antennas require the
ability to receive both RHCP and LHCP signals simultaneously over
the entire bandwidth in a single antenna. One example where such a
single antenna would be required is for the feed of a parabolic
reflector. If the system is to be capable of receiving or
transmitting both RHCP and LHCP, as well as any linear polarized
signal without a loss in gain due to polarization, then the single
feed of the parabolic reflector must be capable of RHCP and LHCP
operation. Presently, such receiving or transmitting capability,
has not been possible with the whole class of frequency independent
spiral antennas. Some narrow band techniques are used whereby
spiral antennas can be fed from the outside of the spiral in
addition to feeding from the center. Since the direction of the
current relative to the direction of propagation when fed from the
outside is opposite to the direction of current, for the same
direction of propagation when fed from the center, both senses of
circular polarization can be obtained from a single spiral. This
dual sense of polarization operation is bandwidth limited. If the
ratio of the upper to lower frequencies of operation is used as a
measure of bandwidth, this ratio will be less than 2 to 1 for the
method of obtaining dual senses of CP from a single spiral antenna,
where the antenna is fed from both the outside and center.
The present invention provides a new design of spiral antenna
requiring only a center feed and which is capable of simultaneous
dual circular polarization operation over any chosen bandwidth
limited only by practical construction considerations in the feed
region.
BRIEF SUMMARY OF INVENTION
This invention relates to a multi-arm spiral antenna which is fed
at the center of the spiral. Each of the spiral arms of the antenna
have a cascade of cells, with each cell having a wide and narrow
section along the lengths of the arms. The lengths of the sections
increase for increasing distance from the center.
BRIEF DESCRIPTION OF DRAWINGS
FIG. 1a shows an elevation view of a conventional 2 arm equiangular
spiral;
FIG. 1b shows an enlarged plan view of the top portion of the
conventional 2 arm equiangular spiral;
FIG. 2 shows an elevation view of a 2 arm equiangular modulated
arm-width spiral embodying the invention;
FIG. 3 is an enlarged plan view of the top portion of the 2 arm
spiral width self-complementary modulated arm width as shown in
FIG. 2;
FIG. 4 is a plan view of a 4 arm equiangular modulated arm width
spiral;
FIG. 5 illustrates the coordinate system;
FIG. 6a and 6b show typical radiation patterns of the electric
field for two modes (M.sub.1 and M.sub.3) of feeding a four arm
spiral using conventional antennas;
FIGS. 7a and 7b show the radiation patterns in the same modes of
feeding (M.sub.1 and M.sub.3) as represented in FIG. 6 using the
antenna of this invention.
DESCRIPTION OF THE PREFERRED EMBODIMENTS
FIGS. 1a and 1b show a conventional two arm conical spiral antenna
19 comprising two spiral arms 20 and 21 which are wound on the
surface of an electrically nonconductive cone 22. A balanced feed
line 23 is located at the cone axis of symmetry. The balanced feed
line 23 comprises two coaxial transmission lines, 24 and 25. The
outer shields of the coaxial lines 24 and 25 are electrically
connected together in FIG. 1b, along their lengths. The center
conductors 26 and 27 of the lines 24 and 25 are electrically
connected to the feed terminals 28 and 29, respectively, as shown
in FIG. 1b.
The parameters which define the equiangular conical spiral are also
shown on FIG. 1a. These are: (1) .theta./2, the half-angle of the
cone (2) .alpha., the angle of spiral wrap, which is the angle
between a tangent to the edge of an arm and a line joining the
tangent point and apex of the cone, and (3) .delta., the angular
width of the spiral arms, found by the angular rotation needed to
rotate the spiral defined by one edge a of the arm into congruence
with the opposite edge b.
The customary method of feeding a broadband two-arm spiral at the
center terminals yields two modes of operation whose sense of
polarization depends on the sense of wrap of the spiral. In
accordance with general practice, the polarization sense of the
spiral antenna is determined from the hand used when pointing the
fingers in the direction of the spiral arms current and the thumb
in the direction of propagation of the radiated fields. Since the
currents are assumed to travel away from the input terminal,
right-hand circular polarization (RHCP) corresponds to progressive
phase delay of the arm currents in the increasing .phi. direction;
left-hand circular polarization (LHCP) to progressive phase advance
of the arm currents in the decreasing .phi. direction; where .phi.
is the conventional polar coordinate and increases in the counter
clockwise direction as shown in FIG. 5.
The push-pull mode, referred to herein as Mode 1, is obtained when
the two spiral arms are fed 180.degree. out of phase. The radiation
patterns of Mode 1 are single beam patterns, which in the case of
conical spirals are undirectional and directed along the axis in
the direction of the apex of the cone.
The push-push mode, referred to herein as Mode 2, is obtained when
the arms are fed in phase, with a center post formed by the outer
shields of the two feed lines, fed 180.degree. out of phase.
The radiation pattern of Mode 2 is a toroid about the axis of the
cone. The characteristic of this mode is a null in the radiation
pattern along the axis of the spiral.
For analysis, the antenna is divided into three regions, "the
transmission region," the "active region" and the "unexcited
region." In the transmission region the arm currents travel along
each arm with essentially free-space phase velocity and negligible
radiation. The active region corresponds approximately to the
region where the phase difference in the currents in the arm allows
substantial radiation. If the active region is sufficiently wide to
allow substantially total radiation of energy carried by the arm
currents, the portion of the arms following the active region are
essentially unexcited and hence constitute the unexcited region in
a properly operating frequency independent antenna.
In Mode 1 (M.sub.1) the active region is approximately located at a
diameter of the cone (D) of .gamma./.pi. (where .gamma. is the
wavelength at the given frequency) so that the currents in the arms
are phased approximately an extra 180.degree. each half turn and,
hence, are in phase.
In Mode 2 (M.sub.2), the active region does not occur until D =
2.gamma./.pi.. Hence, when the spiral's diameter is smaller than
2.gamma./.pi., the incident energy into Mode 2 is not efficiently
radiated.
FIG. 2 shows an embodiment of the invention which is a multi-arm
conical spiral antenna having two arms. The arms 30 and 31 are
wound on an electrically non-conductive cone 32. The arms, however,
have periodic variations in the conductor arm width, called
modulation. The arms of the antenna with such periodic variations
can be thought of as being constructed from a cascade of cells,
with a cell, for example 33, having a wide section, 34, and narrow
section 35. Amplitude is defined as the ratio of the width of the
wide section 34 to the width of the narrow section 35. The period
is defined as the ratio of the lengths of adjacent cells. The
lengths of the sections increase for increasing distance from the
feed terminals 40 and 41 at the apex of the cone shown in FIG. 3.
The antenna is fed by two coaxial lines 36 and 37, located on the
axis of symmetry, whose outer shields are electrically shorted
together along their lengths, as shown in FIG. 3. The center
conductors 38 and 39 of the two lines 36 and 37, are connected at
the top of the cone to the arms 30 and 31 at the terminals 40 and
41, respectively. When the arms 30 and 31 are fed 180.degree. out
of phase (Mode 1), the currents along the center post cancel each
other. The Mode 1 method of feeding yields single beam patterns,
which are essentially unidirectional and directed along the axis in
the direction of the apex of the cone, as with the conventional
unmodulated arm width spiral, as illustrated in FIG. 1. In Mode 2
the arms are fed in phase with the center post 42 formed by the
outer shields of the coaxial lines 36 and 37 fed 180.degree. out of
phase.
The energy in Mode 2 (M.sub.2) generally will not radiate
efficiently until the circumference of the spiral is approximately
2 wavelengths. By making the variations in the arm width
sufficiently large, it is possible to form reflection regions along
the arms such that essentially all the incident energy along the
arms is reflected by the arm impedance mismatch caused by these
variations.
The maximum reflection along the arms is found to occur in that
region where the length of the cells becomes approximately
1/2.gamma.. Further, the reflection from cells which are shorter
than 1/2.gamma. is small. Hence, the reflection of the incident
energy along the arms is confined to a region of the arms where the
cells are approximately 1/2.gamma. long. This region is called a
stopband region. By choosing the proper parameters of amplitude of
the variations and the period of the variations, the stopband
region can be placed at any desired diameter.
In the two-arm spiral case the stopband would be placed between the
active regions of the M.sub.1 and M.sub.2 modes. Hence, the normal
M.sub.1 mode would be unaffected if the M.sub.1 active region is
efficient. The placing of the stopband ahead of the active region
for the M.sub.2 mode assures that the structure when fed from the
center in the M.sub.2 mode will not radiate efficiently, since the
energy is reflected before reaching the required active region for
substantial radiation.
If, further, the modulation of the arms is complementary, in the
sense that the regions of modulation are opposite in the two arms
at corresponding points, then the reflected energy will be
180.degree. out of phase between the two arms. This is then the
condition for substantial radiation of the reflected energy in the
opposite sense of polarization to Mode 1 as discussed. If the
spiral is an equiangular (logarithmic spiral), then
log-periodically scaling the lengths of the cells, allows this
region to move along the structure retaining its relative position
between the active regions of the M.sub.1 and M.sub.2 modes. The
self complementary geometry makes the relative phase of the
reflected arm currents 180.degree. out of phase, independent of
frequencies. Hence, the antenna will now have broadband operation
with both senses of circular polarization in a simple single beam,
the M.sub.1 mode giving one sense of CP and the M.sub.2 mode the
opposite.
In the general case of an N arm antenna, the phase change between
successive arms would be
M 360.degree./N
where M = 1 . . . N.
In general, only those choices which suppress radiation from the
center feed post are used. Hence, M = N is in general not used
since the arms would be fed against the feed post for this
mode.
For a multi-arm spiral we can identify the modes by the excitation
of the arms, and hence for M = 1, 2, 3 we will refer to these as
M.sub.1, M.sub.2, and M.sub.3 modes of excitation,
respectively.
The principles may be applied to a multi-arm spiral having 4 spiral
arms as follows. Assume the four arm spiral is initially a LH wound
spiral as shown in FIG. 4. The normal feed for LHCP sum pattern
(Mode 1) is
A.sub.1 = (0, - 90, 180, + 90)
where
A.sub.m 32 (I.sub.51, I.sub.52, I.sub.53, I.sub.54) is the current
vector notation for the phase of the excitation at the four input
terminals 51, 52, 53, 54.
For the M = 1 Mode (M.sub.1), the four arm spiral gives a typical
pattern shown in FIG. 6A. For the M = 1 mode (M.sub.1) of the four
arm spiral, the active region still occurs at a diameter (D) of
about 1 wavelength. The M = 3 Mode (M.sub.3) has the
excitation:
A.sub.3 = (0, + 90, + 180, - 90)
The active region for this mode will occur approximately at a
diameter of 3 wavelengths. When the antenna is large enough (D >
3.gamma.) to support substantial radiation from this mode, the
antenna gives a typical pattern shown in FIG. 6B.
If, however, the structure is not large enough to suPport
substantial radiation of the M.sub.3 mode, simple reflection of the
current at the ends of the structure 55, 56, 57, 58 produce a
return excitation which efficiently radiates like the M.sub.1 mode,
i.e. a smooth lobe pattern, but with the opposite sense of
polarization.
Hence, introducing a modulation in the arms to effect a stopband
region with the proper relative phasing between the arms after the
M = 1 active region (i.e. at a diameter larger than 1.gamma.), but
before the normal M = 3 active region, is sufficient to give the
required dual-polarization operation. With the relative phase of
the reflected arm currents the same (all the reflection
coefficients the same) it is possible to obtain the opposite
polarization for the M.sub.1 mode; since, however, the excitation
vector, A.sub.4 = (0, 0, 0, 0) or (180, 180, 180, 180) is not
useful if the modulation is scaled the same in each arm so that the
arms are identical, a six arm spiral must be used to obtain
multi-mode operation with dual polarization.
While the theory of log-periodically modulating the arm width of
spiral antennas to effect stopband regions does not depend upon the
proximity of the modulated sections between each arm, the actual
construction for planar and conical spirals appears to be optimized
by using a self-complementary arrangement i.e., a structure in
which the metal area is identical in size and shape to the open
area. This leads to dividing each turn of the spiral into 2N
equiangular segments. In the alternate sections the arm widths are
made wide or narrow. A cell is, as defined before, composed of two
sections of line--one section of wider width and one narrower.
Since the maximum reflection along each arm occurs when the total
length of a cell is approximately 1/2.gamma. long, the number of
cells in circumference of the spiral in the region of maximum
reflection will be N = 1,2,3, etc. By selecting N to be an integer,
all the wide or narrow segments will lie in pie shaped wedges,
shown as 70 - 77 in FIG. 4, allowing the most interaction of the
wide portions of each arm, since they are then closest to each
adjacent arm's wide segments over the longest distance.
Correspondingly, the narrow portions have the least interaction
over the longest distance. This then should allow the smallest
modulation for a given size stopband region since the size of the
stopband region in the periodically modulated transmission line
structure appears to be maximized when the change between the two
impedance levels is a step function.
Thus, for the two arm spiral where the modulation of the arms
themselves is to be opposite to give the reflected energy a
relative 180.degree. phase shift, the number of cells in
circumference must be odd. This guarantees that the two arms will
be physically complementary to each other. For a four arm spiral,
using the M = 1 and M = 3 modes to obtain dual polarization, the
arms will all be the same and, hence, an even number of cells will
be used.
Since the location of the maximum reflection region occurs when the
cell length is approximately 1/2.gamma. and the size of the
stopband region is controlled by the amplitude of the modulation,
it is apparent that the location and size of the stopband region
can be selected by parameter choice.
The value of N is to be chosen so that the reflection region occurs
between the active region of the selected modes on unmodulated
armwidth spirals. Hence, in the two arm case, N = 3 seems
appropriate while in the four arm case N = 4 for the M = 1 and 3
modes. This physical arrangement was used in FIGS. 2, 3 and 4 it is
believed to be the optimum. The ratio of the angular width of the
wide section of a cell to a narrow section is defined as the
modulation ratio. It has been found that ratios of four are
sufficient to form the necessarY stopband regions when the other
parameters of the spiral, i.e. .theta. and .alpha., are selected to
give good performance of the regular unmodulated spiral.
* * * * *