U.S. patent number 3,754,270 [Application Number 05/237,670] was granted by the patent office on 1973-08-21 for omnidirectional multibeam array antenna.
This patent grant is currently assigned to Raythean Company. Invention is credited to Wilbur H. Thies, Jr..
United States Patent |
3,754,270 |
Thies, Jr. |
August 21, 1973 |
**Please see images for:
( Certificate of Correction ) ** |
OMNIDIRECTIONAL MULTIBEAM ARRAY ANTENNA
Abstract
An omnidirectional multibeam array antenna assembly, for use
particularly at radio frequencies, is shown. The preferred
embodiment includes a circular dielectrically loaded parallel-plate
lens joined by radially disposed transmission lines of equal length
to antenna elements disposed on a circle concentric with such lens
and radio frequency switching means to permit use of the assembly
in either a "transmit" or "receive" mode. The dielectric constant
of the material loading the parallel plate lens and the physical
diameter of the circular lens are so selected as to produce equal
RF path lengths to three (or four) points on a straight line
tangent to the arc of elements relative to each one of a plurality
of feed ports.
Inventors: |
Thies, Jr.; Wilbur H. (Santa
Barbara, CA) |
Assignee: |
Raythean Company (Lexington,
MA)
|
Family
ID: |
22894685 |
Appl.
No.: |
05/237,670 |
Filed: |
March 24, 1972 |
Current U.S.
Class: |
343/754; 342/372;
343/755; 343/773 |
Current CPC
Class: |
H01Q
21/0031 (20130101); H01Q 25/008 (20130101) |
Current International
Class: |
H01Q
21/00 (20060101); H01Q 25/00 (20060101); H01q
019/06 () |
Field of
Search: |
;343/754,755,854,773 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Lieberman; Eli
Claims
What is claimed is:
1. An omnidirectional antenna assembly for radio frequency energy,
such assembly comprising:
a. a plurality of antenna elements disposed at equal intervals
along the circumference of a circle;
b. a circular parallel-plate lens concentric with the circle and
having a radius less than the radius of the circle, such lens
including a dielectric material, the index of refraction, k, of the
dielectric material, the radius (r+d) of the circle on which the
antenna elements are disposed and the radius, r, of the circular
parallel-plate lens are related in accordance with the formula:
k = (r+d) (sin.sup.2 a/2)/(r) (1-cos a/2) where a is an angle less
than 90.degree.;
c. radio frequency energy conducting means for connecting each one
of the plurality of antenna elements to a different point on the
periphery of the circular parallel-plate lens, the electrical
length of each such conducting means being the same; and,
d. circulator means, in circuit with each one of the radio
frequency conducting means, for directing radio frequency energy to
and from each one of the antenna elements through the
parallel-plate lens.
2. An omnidirectional antenna as in claim 1 wherein the radio
frequency conducting means are radio frequency transmission
lines.
3. An omnidirectional antenna assembly as in claim 1 wherein the
circular parallel-plate lens, the radio frequency conducting means
and the circulator means are printed circuits on a first surface of
a dielectric substrate.
4. An omnidirectional antenna assembly as in claim 3 having,
additionally, an electrically conductive ground plane overlying a
second surface of the dielectric substrate.
Description
BACKGROUND OF THE INVENTION
This invention pertains generally to antenna assemblies for radio
frequency energy and particularly to antenna assemblies for
producing a plurality of simultaneously existing beams of radio
frequency energy.
It is known in the art that a plurality of simultaneously existing
beams of radio frequency energy may be formed in space in several
different ways. One approach, if it is desired that each beam
utilize the entire aperture of an antenna array, is to use a
so-called "multi-beam" array antenna assembly. In a typical
assembly of such a type, each antenna element in an array is
connected, through constrained paths of predetermined length, to
each one of a number of feed ports. With the electrical length of
each one of the constrained paths properly adjusted (through
variation of the lengths of the transmission lines and the
dimensions of a parallel-plate lens making up the required
constrained paths between the antenna elements and the feed ports)
it is possible, then, to create any desired number of beams. It is,
however, difficult, if not impossible, to arrange the components of
any known multibeam array antenna assembly so that the beams
produced will cover a field exceeding a semicircle (for a linear
array) or a hemisphere (for a planar array).
If it be desired that the field covered by beams from a multibeam
array antenna assembly exceed either a semicircle or a hemisphere,
it is now felt to be necessary to use a lens antenna, for example
an antenna incorporating a so-called "Luneberg" lens to form the
required beams. Such a lens, as is well known, is a dielectric lens
in which the dielectric constant of the lens material varies with
distance from the center of the lens. While, in theory, the
dielectric constant of the lens material in a Luneberg lens should
vary smoothy, it is difficult to make a lens in such a way. It is,
therefore, common practice to approximate an ideal variation by
"zoning," i.e., by laminating materials having dielectric constants
which differ in a desired way. Obviously, however, even such an
expedient is both costly and difficult to implement.
SUMMARY OF THE INVENTION
Therefore, it is a primary object of this invention to provide an
improved multi-beam array antenna assembly which is adapted to
provide a field of coverage exceeding, for a linear array, a
semicircle and, for a planar array, a hemisphere.
Another object of this invention is to provide an improved
multibeam array antenna assembly which meets the primary object of
this invention without requiring the use of a dielectric lens in
which the dielectric constant of the lens material is varied.
These and other objects of this invention are attained generally by
providing an array configuration which is, in terms of its
electrical dimensions, perfectly symmetrical. Thus, in the case of
a linear array, individual antenna elements are disposed along the
circumference of a circle, each one of such elements being
connected, through a radial transmission line and a concentric
circular parallel-plate lens, to appropriately disposed feed ports.
By properly selecting the radii of the cicles and the dielectric
material in the parallel-plate lens, radio frequency energy passing
between each one of the feed ports and the antenna elements is
delayed so that the field of the directive beams associated with
the antenna elements covers 360.degree.. Similarly, if the antenna
elements disposed on the surface of a sphere are connected through
radial transmission lines and a concentric spherical lens, to
appropriately positioned feed ports, the field covered by the beams
from such elements may be spherical.
BRIEF DESCRIPTION OF THE DRAWINGS
For a more complete understanding of this invention, reference is
now made to the following description of a preferred embodiment of
this invention, as illustrated in the accompanying drawings, in
which:
FIG. 1 is an isometric view, somewhat simplified, of a multi-beam
array antenna assembly according to my invention, such assembly
being shown, in combination with a block diagram of other major
components, as a part of an omnidirectional transponder system;
FIG. 2 is a cross-sectional view of the multibeam array antenna
assembly shown in FIG. 1;
FIG. 3 is a sketch illustrating the principle of operation of the
contemplated multibeam array antenna assembly; and
FIG. 4 is a plan view, somewhat simplified, of a multibeam array
antenna according to my invention, such assembly being made by
using printed circuit techniques.
Referring now to FIG. 1, it may be seen that a transponder system
according to this invention comprises a multibeam array antenna
assembly 10 (to be described hereinafter) 12R, 12L and transmitters
14R, 14L, one of each of the latter cooperating, through
appropriate circulators 16L, 16R, 18L, 18R, with such assembly (in
response to signals from an associated one of a plurality of
controllers 20L, 20R and buffer amplifiers 22) to receive and
transmit radio frequency energy. The just-mentioned components of
the system, except for the multibeam array antenna assembly 10, are
conventional in construction. Thus, the circulators 16L - 18R may
each be a known three-port "Faraday rotation" circulator wherein
radio frequency energy entering one port may be directed to another
selected port by controlling the direction of magnetization of the
field of an electromagnet (not shown). Assuming a "normal"
direction of the magnetic field controlling each one of the
circulators 16L - 18R to be the direction which permits radio
frequency energy to pass only from port a to port b or from port b
to port c and a "reverse" direction to permit such energy to pass
only from port b to port a or from port c to port b, it may be seen
that the circulators 16R, 16L, 18R, 18L may be so actuated as to
direct radio frequency energy as follows. Radio frequency energy
entering port a of circulator 18R exits therefrom through port b,
passed to port c of circulator 18L and then, from port c to port b
of circulator 16L. Upon exiting from port c of circulator 16L, such
energy passes to receiver 12L. None of the radio frequency energy
may, however, pass to receiver 12R because circulator 18R prevents
passage of such energy from port a to port c. Upon actuation of the
controller 20L and a "reverse" direction signal being applied to
the circulators 18L, 18R, radio frequency energy from transmitter
14L is, therefore, caused to pass through circulator 16L,
circulator 18L (via ports c and b) and circulator 18R (via ports b
and a). Similarly, if radio frequency energy is received at port a
of circulator 18L (such circulator being in its "normal" condition)
such energy is passed through circulator 18L to circulator 18R and
circulator 16R to actuate receiver 12R. The signal out of the
latter, then, causes controller 20R to produce a "reverse"
direction signal (for circulators 18R, 18L) and a trigger signal
for transmitter 14R. The radio frequency signal out of the latter
is, therefore, conducted, through circulators 16R, 18R and 18L, to
port a of the latter. Each one of the controllers 20L, 20R may
consist, for example, of appropriate delay and signal forming
circuits to produce, in response to a signal out of its
corresponding receiver 12L, 12R, a reversing signal for the
electromagnets of circulators 18L, 18R and a trigger signal for its
associated transmitted 14L, 14R.
In passing, it will be noted that, for clarity in the drawing and
simplicity of explanation, only two sets of receivers, transmitters
and controllers and circulators have been shown and described. It
will be evident to one of skill in the art, however, that a similar
set of elements would be provided in a working embodiment of this
invention for each antenna element in the multibeam array antenna
assembly 10.
Referring now to FIG. 2 along with FIG. 1, it may be seen that the
multibeam array antenna assembly 10 here is made up of a plurality
of antenna elements, as antenna elements 25L, 25R, equally spaced
and positioned in any convenient manner, in an annular horn (not
numbered) but formed from conducting flared sections 27u, 27d and
backwall 29. The dimensions and shape of the annular horn are not
essential to the invention and may be changed to shape the beams as
desired in the plane orthogonal to the circle on which the antenna
elements are mounted. Each antenna element is connected through a
constrained path, here consisting of lengths of transmission line
31 and connectors (not numbered) circulator 18r or 18L (each of
which here is considered to be initially in its "normal"
condition), to a different one of printed lines 33 and a ground
plane 35 of microstrip circuitry (not numbered) which may be
supported centrally of the annular horn. Each one of the printed
lines 33, in turn, is terminated (through matching sections, not
numbered) in a printed circle 37 which is concentric with the
circle on which the antenna elements 25 are mounted. It is here
noted that the electrical length of all the radial paths from the
center of the printed circle 37 through any printed line 33,
transmission line 31 and circulator is the same.
To complete the description of the microstrip circuitry it may be
seen (FIG. 2) that the ground plane 35 is formed by applying, using
printed circuit techniques, a conductive coating to one side of a
dielectric substrate 39 and applying, again as by using printed
circuit techniques, to the opposite surface of such substrate. The
microstrip circuitry is then mounted in a clamping ring assembly 40
which is adapted, as shown, to receive connectors (not numbered)
for each one of the transmission lines 31. The microstrip
circuitry, then, is held in position relative to the antenna
elements 25 by an annulus 41 secured in any convenient manner to
the clamping ring assembly 40 and the annular horn.
Referring now to FIG. 3, the manner in which the just described
multibeam array antenna assembly 10 operates may be seen. A
moment's thought before proceeding will make it clear that, because
the circulators 18L, 18R, 16L, 16R are simply radio frequency
switches and because the length of line between any one of the
transmitters 14L, 14R and the junction of the printed lines 33 with
the transmission lines 31 is common to radio frequency energy from
all antenna elements 25, the point marked P may be deemed to be the
origin of such radio frequency energy, i.e., point P is the phase
center of a feed port. Thus, the electrical length of the path of
radio frequency energy from point "P" to the diametrically opposite
antenna element 25, i.e., to the point marked Q may be written as:
PQ.sub.e = 2k.sub.1 r + k.sub.2 d (1)
where r equals the radius of the printed circle 37 measured to the
phase center of the matching section or printed "horn" (in
wavelengths in free space at a design frequency); d equals the
length of any one of the transmission lines 31, all of which are
equal, (in wavelengths in free space at a design frequency); and
k.sub.1 and k.sub.2 are, respectively, the index of refraction
(meaning the square root of the effective dielectric constant) of
the dielectric substrate 39 and the dielectric material in the
transmission line 31.
Similarly, the electrical length of the path of radio frequency
energy from point P to a selected antenna element 25 (other than
the one diametrically opposite point P) and thence to a point F on
a planar wavefront designated FQ may be written as:
PD.sub.e + DE.sub.e + EF.sub.e = 2k.sub.1 r cos a/2 + k.sub.2 d +
(r+d)k.sub.o (1-cos a) (2)
where a is the angle between the radial lines from the center of
the ring of elements to the antenna elements at point Q and E; and,
k.sub.o is the square root of the dielectric constant of free space
(taken to be 1).
Setting Eq. (1) equal to Eq. (2) and solving for k.sub.1, the
following is obtained.
k.sub.1 = (r+d) (sin.sup.2 a/2 )/(r) (1-cos a/2) (3)
Further, if the angle a is assumed to be 45.degree., then k.sub.1 =
1.924 (r+d )/(r) (4)
It will be observed that (r+d) equals the radius of the circle on
which the antenna elements 25 are mounted and r equals the radius
of the printed circle 37. Thus, it is evident that, so long as the
index of refraction of the material chosen for the dielectric
substrate 39 exceeds 1.924, the length d is greater than zero and
has a definite relationship (depending on the actual value of the
selected k.sub.1) to the length r. It follows, then, that by
selecting a material with a k.sub.1 somewhat greater than 1.926
(say a k of 4.0) for the dielectric substrate, a multi-beam array
antenna assembly may be designed for any desired number of antenna
elements with sufficient space being available between the
periphery of the printed circle 37 and the antenna elements 25 for
the printed lines 33, the transmission lines 31, the circulators
18L, 18R and any required connectors.
Further, by adding an identical length of line to each of the
circuit paths between each feed port and its corresponding element,
as with semi-rigid cable, the parallel plate lens and associated
switches may be positioned in any convenient location with respect
to the array elements rather than physically concentric with
them.
With the foregoing in mind, it may be seen that different
constrained paths for radio frequency energy exist between each
feed port and the antenna elements. That is, radio frequency energy
from any given feed port passes, via paths of different electrical
length, to the antenna elements. Obviously, however, only the
antenna elements in the semicircle opposite to any feed port co-act
to form a beam. Therefore, in the "transmit" mode, radio frequency
energy radiated from the antenna elements in the semicircle
opposite to a particular feed port is propagated along a planar
wavefront in a beam whose axis is an extension of the diameter
containing the feed port. The width of the beam is, of course,
dependent upon the number of antenna elements in the semicircle and
of illumination taper. Conversely, in the "recive" mode, radio
frequency energy in a planar wave is intercepted by each antenna
element in a semicircle and directed to the diametrically opposite
feed port, arriving there substantially "in phase
Referring now to FIG. 4 it may be seen that a multibeam array
antenna assembly according to this invention may be made using only
printed circuit techniques. Thus, in FIG. 4 one side of a circular
dielectric substrate 39' is partially covered with a ground plane
35' (the outside of such plane being indicated by dotted lines) and
the remainder of the microstrip circuitry is printed on the other
side of such substrate. That is, a printed circle 39' is located
centrally of the dielectric substrate 39' and printed lines 31',
33' are disposed, through unnumbered matching sections, radially of
such circle. A circulator 18' is formed in each one of such lines
and the outer end of each is terminated in a monopole antenna
element 25'. The radius of the printed circle 25, the overall
length of each printed line 31' and the index of refraction of the
dielectric substrate 39' are related one to another as described
hereinbefore.
It will evident to one of skill in the art that changes from the
illustrated embodiments of my invention may be made without
departing from my inventive concepts. Thus, in lieu of a
disc-shaped dielectric substrate, a spherical substrate could be
used to form a plurality of pencil beams covering a spherical
field. Or, alternatively, multiplicity of disc-shaped substrates
could be used to feed rings of elements on a cylindrical surface.
Further, it is obvious that the disclosed antenna assembly may be
used as the radiating and/or receiving element in apparatus other
than transponders or direction finders. It is felt, therefore, that
this invention should not be restricted to its disclosed
embodiments but rather should be limited only by the spirit and
scope of the appended claims.
* * * * *