U.S. patent number 3,643,262 [Application Number 03/855,234] was granted by the patent office on 1972-02-15 for microstrip aerials.
This patent grant is currently assigned to Compagnie Generale de Telegraphie Sans Fil. Invention is credited to Roger Dumanchin.
United States Patent |
3,643,262 |
Dumanchin |
February 15, 1972 |
MICROSTRIP AERIALS
Abstract
A microstrip aerial having a plurality of equally spaced
radiating discontinuities obtained by laterally shifting the edges
of the strip.
Inventors: |
Dumanchin; Roger (Paris,
FR) |
Assignee: |
Compagnie Generale de Telegraphie
Sans Fil (FR)
|
Family
ID: |
8708979 |
Appl.
No.: |
03/855,234 |
Filed: |
November 24, 1959 |
Foreign Application Priority Data
Current U.S.
Class: |
343/846; 343/708;
343/908 |
Current CPC
Class: |
H01Q
13/26 (20130101); H01Q 13/206 (20130101); H01Q
13/28 (20130101) |
Current International
Class: |
H01Q
13/26 (20060101); H01Q 13/20 (20060101); H01Q
13/28 (20060101); Ho1q 001/48 () |
Field of
Search: |
;343/772,776,705,708,828 |
References Cited
[Referenced By]
U.S. Patent Documents
Foreign Patent Documents
Primary Examiner: Bennett, Jr.; Rodney D.
Assistant Examiner: Berger; Richard E.
Claims
What is claimed is:
1. A microwave directional aerial comprising at least one
microstrip line having a ground plate, an insulating plate and a
conductive strip superimposed upon each other, said strip having
edges; means for feeding to said line ultrahigh frequency energy;
both edges being laterally set off in the same direction at
uniformly spaced points, thus forming radiating
discontinuities.
2. A microwave directional aerial comprising a plurality of
parallel, equally spaced lines having a common ground plate and a
common insulating plate, each line having a conductive strip, said
strips having edges; means for feeding to said lines ultrahigh
frequency energy; both edges of each line being laterally set off
in the same direction at uniformly spaced points, thus forming
radiating discontinuities.
3. A microwave directional aerial comprising a plurality of
parallel equally spaced lines, having a common ground plate and a
common insulating plate, each line having a conductive strip, said
strips having edges; means for feeding to said lines ultrahigh
frequency energy; both said edges being laterally set off in the
same direction, thus forming along a predetermined length of said
strips radiating discontinuities, said discontinuities being spaced
apart by the length in said microstrip of the operating wave and
said predetermined length being the same for all the strips.
4. A microwave directional aerial comprising a plurality of
parallel equally spaced strip lines, having a common ground plate
and a common insulating plate, each line having a conductive strip,
said strips having edges; both said edges being laterally set off
in the same direction thus forming along a predetermined length of
said strips radiating discontinuities, said discontinuities being
spaced apart by the length in said microstrip of the operating wave
and said predetermined length being the same for all the strips; a
wave guide extending normally to said strip lines, said guide
having a pair of large walls, one of said walls supporting said
ground plate; and probes respectively coupling said strips to said
guide.
Description
The present invention relates to directional aerials and more
particularly to directional aerials for use in moving bodies whose
aerodynamical characteristics should be affected as little as
possible by the presence of the aerial.
An aerial according to the invention comprises, at least, one
microstrip having a plurality of equally spaced radiating
discontinuities obtained by laterally sifting the edges of the
strip, thus forming laterally set off rectangular strip
portions.
The invention will be best understood from the following
description and appended drawing wherein:
FIG. 1 is a diagrammatic top view of the microstrip aerial
according to the invention;
FIG. 2 is a detail of the aerial of FIG. 1;
FIGS. 3 to 8 are explanatory curves;
FIG. 9 is an embodiment of a directive aerial according to the
invention;
FIG. 10 illustrates a cross section of the aerial of FIG. 9;
FIG. 11 is an explanatory perspective view; and
FIG. 12 is a radiating pattern of an aerial according to the
invention.
In FIG. 1, a microstrip line 1 is illustrated as viewed from above,
the ground plate being disposed in the plane of the figure.
According to the invention this line comprises a plurality of
discontinuities 2, spaced from each other by .lambda..sub.s,
.lambda..sub.s designating the wavelength in the line of the energy
propagating along the same.
As shown in FIG. 2, each discontinuity 2 is formed by laterally
shifting the edges of a portion of the strip in a direction
perpendicular to the longitudinal axis thereof. In FIG. 2, edge 3
is shifted by a distance c and edge 4 by a distance d.
The length l of each discontinuity is, in the embodiment shown,
substantially equal to .lambda..sub.s/ 4. The radiation factor
.rho., i.e., the ratio of the radiated energy to the incident
energy, varies as a function of d.
To each length d corresponds a length c for which the discontinuity
is matched to the line. All discontinuities being matched to the
line, the energy fed to the line propagates as a progressive
wave.
The projecting strip portions radiate energy and the reentrant
portions insure the matching.
FIGS. 3, 4 and 5 show curves indicating how different parameters
vary as a function of d, namely: the standing wave ratio with c=0
(FIG. 3); the radiation factor .rho. (FIG. 4), distance c with the
standing wave ratio equal to 1.
FIG. 6 shows the phase shift .PHI. due to energy radiation as a
function of d.
All these diagrams have been established for a line operating in
the 10,000 Mc.-band. The line is constituted by a "rexolite" plate
1.6-mm.-thick and metallized on both faces. The strips are
established according to the printed circuit techniques. The strip
is 34.mu. thick and 4.5 mm. wide. The wavelength in such a
microstrip is 19.8 mm. at 10,000 mc., and l= .lambda.s/4=5 mm.
It appears from the diagrams of FIGS. 3 and 5 that, for c=0 and
d=2, the standing wave ratio is 1.6, the radiation ratio .rho.
being equal to 0.2.
It will be apparent from FIG. 5 that, for each value of d less than
d=2 mm., there is a value of c such that the standing wave ratio is
made equal to 1. For d greater than 2, this correction is no longer
possible. This may be clearly seen from FIGS. 7 and 8. FIG. 7
illustrates the standing wave ratio as a function of c for d=2 mm.
It is seen that this ratio is about 1.7 for c=0 and equal to 1 for
c=3.
In FIG. 8, for d=2.5 mm., the standing wave ratio has a minimum
equal to 1.5, for c=2.5.
FIG. 9 illustrates a guide, which feeds a plurality of lines 11,
12, 13 and 14, each line being fed at its center. The distance
between two adjacent lines is .lambda./2, .lambda. being the
operating wavelength. FIG. 10 shows in section how each line is
coupled to guide 10. A metal plate 5 which is common to microstrips
10 and 14, is supported on a metal block 9 which rests on guide 10.
A passage 15 is formed in block 9, symmetrically with respect to
guide 10, for coupling strips 11 to 14 to the guide. A dielectric
layer 17 rests on plate 5, the same dielectric lining passages 15.
A probe 16 couples the conductive strips 1 to guide 10, probe 16
and lining 15 thus forming a coaxial cable.
The discontinuities 20 are all fed in phase; they are separated by
an electrical distance l substantially equal to .lambda..sub.s and
given more precisely by the formula:
l=.lambda..sub.s (1-.DELTA..PHI./2.pi.).
An aerial according to the invention is directional. The radiation
direction is along a straight line defined by the intersection
of:
a. The symmetry plane of the large side of guide 10 in which all
the discontinuities are radiating in phase. This plane corresponds
to plane x0z in FIG. 11, 0x being the axis of guide 10 and 0y
parallel to the longitudinal axis of the strips.
b. A plane including axis 0y and making an angle .theta. with the
axis 0x, with cos .theta.=c./Vg., c being the velocity of light and
Vg. the phase velocity of the wave in guide 10.
FIG. 12 shows the directive pattern obtained with an aerial
according to the invention, operating at 10,000 mc., in the above
defined planes. The width M of the beam at a level 3 db. below the
maximum is given by the formula;
M=.lambda./a
where a is the transversal dimension of the aerial. The highest
secondary lobes are 25 db. lower than the main lobe. The gain is 27
db., i.e., 2 db. above the gain given by formula:
G=4.pi..sub.s .lambda..sup.2
where s is the surface of the aerial.
The invention, is of course, not limited to the embodiment shown,
which is given by way of example. In particular, the distance
between the discontinuities could be different from .lambda..sub.s.
In this case the two planes respectively comprising the radiation
directions would be inclined over the horizontal. The distance
between the points where the strips are coupled to the guide could
be separated by distance different from .lambda./2.
* * * * *