U.S. patent number 3,688,311 [Application Number 04/391,076] was granted by the patent office on 1972-08-29 for parabolic antennas.
This patent grant is currently assigned to CSF-Compagnie Generale De Telegraphie San Fil. Invention is credited to Jacques Salmon.
United States Patent |
3,688,311 |
Salmon |
August 29, 1972 |
**Please see images for:
( Certificate of Correction ) ** |
PARABOLIC ANTENNAS
Abstract
An ultra high frequency antenna comprising a reflector having a
focus and a focal plane, one radiating source at said focus and at
least one radiating source in said focal plane, offset with respect
to said focus, for illuminating said reflector, said sources
producing at least two wave fronts of different directions and
phase correcting means in the path of the wave front(s) originating
from said offset source(s), said correcting means lying outside the
path of said wave front originating from said source located at
said focus.
Inventors: |
Salmon; Jacques (Paris,
FR) |
Assignee: |
CSF-Compagnie Generale De
Telegraphie San Fil (N/A)
|
Family
ID: |
8811967 |
Appl.
No.: |
04/391,076 |
Filed: |
August 19, 1964 |
Foreign Application Priority Data
|
|
|
|
|
Sep 9, 1963 [FR] |
|
|
69946916 |
|
Current U.S.
Class: |
343/755; 343/756;
343/840; 343/781R |
Current CPC
Class: |
H01Q
19/195 (20130101); H01Q 15/12 (20130101); H01Q
15/22 (20130101); H01Q 1/421 (20130101) |
Current International
Class: |
H01Q
19/10 (20060101); H01Q 15/00 (20060101); H01Q
19/195 (20060101); H01Q 1/42 (20060101); H01Q
15/22 (20060101); H01Q 15/14 (20060101); H01Q
15/12 (20060101); H01q 019/12 () |
Field of
Search: |
;343/755,756,834,835,836,837,838,909,911,914 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Tubbesing; T. H.
Claims
1. An ultra high frequency antenna comprising a reflector having a
focus and a focal plane, one radiating source at said focus and at
least one radiating source in said focal plane, offset with respect
to said focus, for illuminating said reflector, said sources
producing at least two wave fronts of different directions and
phase correcting means in the path of the wave front(s) originating
from said offset source(s), said correcting means lying outside the
path of said wave front originating from said
2. An antenna as claimed in claim 1, wherein said phase correcting
means comprise a lens located in the path of the waves radiated by
said offset
3. An antenna as claimed in claim 1, wherein said phase correcting
means comprise a second reflector having a planar portion for
reflecting wave front originating from said source located at said
focus upon reflection thereof on said first mentioned reflector and
at least a curved end portion for reflecting wave front(s)
originating from said offset
4. An antenna as claimed in claim 1, comprising a plurality of
offset sources in said focal plane, said correcting means lying in
the path of
5. An antenna as claimed in claim 4, wherein said sources radiate
waves polarized in a first direction, said phase correcting means
comprise a second reflector having a planar portion for reflecting
the wave front originating from said source located at said focus,
upon reflection thereof on said first mentioned reflector, and
curved end portions for reflecting the wave fronts originating from
said plurality of offset sources upon reflection thereof on said
first mentioned reflector, said first reflector comprises wires
parallel to said first direction, said second reflector comprises
parallel wires inclined at 45.degree. to said first direction, a
screen being disposed behind said second reflector, parallel
thereto, at a distance equal to .lambda./4, .lambda. being the
operating wavelength.
Description
The present invention relates to antennas with radiating beams
stepped in elevation.
Antennas of this kind generally comprise several horns situated in
the focal plane of a reflector, which is generally parabolic.
Waves radiated by each horn are transformed, after reflection on
the reflector, into waves which are plane, as a first
approximation. This is strictly true in the case of a horn placed
at the focus of the paraboloid. But the farther the horn is placed
from the focus, the less plane are the wave surfaces.
It is an object of the invention to provide an antenna of this type
in which this drawback is avoided.
According to the invention there is provided an antenna comprising
a correcting arrangement for rendering plane the equiphase surfaces
of the waves issued from the horns which are not positioned at the
reflector focus, this arrangement being placed on the path of these
waves and away from the waves issuing from the horn positioned at
the reflector focus.
The invention will be better understood from the following
description and the appended drawing, in which:
FIGS. 1 and 2 show, very diagrammatically, two embodiments of the
antenna according to the invention; and
FIGS. 3 and 4 show in plane view two details of FIG. 1.
The antenna shown in FIG. 1 comprises two horns: a horn S.sub.1 is
placed at the focus of a parabolic reflector A and a further horn
S.sub.2 is placed at a distance from horn S.sub.1 in the focal
plane of reflector A. Both horns transmit vertically polarized
waves. Reflector A is built up, as known in the art, by vertical
wires, as shown in FIG. 3, which are spaced apart by a distance of
the order .lambda./10, .lambda.being the operating wavelength. The
arrow in FIG. 3, indicates the direction of the electric field of
the wave radiated by horns S.sub.1 and S.sub.2.
A further reflector M, formed by wires inclined by 45.degree. to
the horizontal, is positioned for receiving the waves reflected by
reflector A. It is followed by reflector E, having a full
reflecting surface and spaced by .lambda./4 from reflector M.
Reflectors M and E are positioned normally to the axis of reflector
A. Reflector M is shown in FIG. 4.
The waves transmitted by horn S.sub.1 are vertically polarized.
These waves are reflected as plane waves R by reflector A. The
vertically polarized wave R may be considered as the resultant of
two component plane waves respectively polarized normally and
parallel to the wires of reflector M. Vectors e and e.sub.2
represent respectively the electric fields of wave R and of said
two components.
Upon striking reflector M, the plane wave parallel to the wires is
reflected by the latter with phase inversion, as indicated by
vector e'.sub.2 in opposition to vector e.sub.2, while the wave
normal to the wires propagates through reflector M and is reflected
by reflector E with a phase inversion. Due to the fact that the
distance B between reflectors M and E is .lambda./4 the electric
field vector e'.sub.1, at the wires, of the wave reflected by
reflector E, is again parallel to e.sub.1. The two reflected
component waves combine to form a wave whose electric field is the
resultant of vectors e'.sub.1, i.e., e.sub.1 and e'.sub.2, i.e.
along the horizontal vector T. Thus, this wave is horizontally
polarized and propagates through reflector A.
The same is true for the waves radiated by horn S.sub.2, except for
the fact that they do not possess, after reflection upon mirror A,
plane equiphase surfaces, horn S.sub.2 being offset with respect to
the forms of reflector A.
The shape of this equiphase surface P.sub.1 is shown in FIG. 1. In
its upper part, assuming the antenna axis to be horizontal, it is
advanced in phase as compared to the plane surface wave shown in
dotted line. This alters the shape of the radiation diagram. In
order to avoid this defect, according to the invention, reflector M
is curved in its upper part C turning its concavity in the same
sense as surface P.sub.1 so compensating phase advances. After
reflection on this upper part, the shape of the equiphase surface
is as shown at P.sub.2.
It will be noted that the only equiphase surfaces to be corrected
are those of the waves from horns which are substantially offset
with respect to the focus of reflector A.
The advantages of the invention are the following:
a. Sources which are more offset than in conventional systems may
be used in combination with a source at the focus, which results in
respective plane waves having direction of propagation at large
angles with respect to each other; thus the average space angle
covered by the whole radiation system, or radiation aperture, may
be 10 times, for example, the space angle covered by the radiation
originating from a single source.
b. The curvature of mirror M is calculated for the horn which is
most offset with respect to the focus. The more offset the
intermediate sources, the more they are subject to correction.
c. The shape of the curved part can be easily improved by trail and
error.
FIG. 2 shows another embodiment of the invention.
The primary sources S are placed in the focal plane of a parabolic
reflector A. The whole assembly is placed in a radome Ra. The
correction device C is a lens placed at the top of the radome, and
through which propagate the waves radiated by the sources which are
offset with respect to the focus of reflector A.
Since the phase shift is a maximum of 360.degree., this lens may be
constituted by a zone, at the top of the radome, of a thickness
which is variable and greater than the normal thickness of the
radome, this thickness not exceeding one wavelength of the radiated
wave.
Of course the invention is not limited to the embodiments described
and shown which were given solely by way of example.
* * * * *