U.S. patent number 3,906,508 [Application Number 05/488,770] was granted by the patent office on 1975-09-16 for multimode horn antenna.
This patent grant is currently assigned to RCA Corporation. Invention is credited to Peter Foldes.
United States Patent |
3,906,508 |
Foldes |
September 16, 1975 |
**Please see images for:
( Certificate of Correction ) ** |
Multimode horn antenna
Abstract
A horn antenna is described including a funnel-shaped coupler
with a port at the narrow end of the coupler adapted to excite a
symmetrical waveguide mode in the coupler and a plurality of side
wall input ports adapted to excite at least two difference
waveguide modes. The port at the narrow end of the coupler is
coupled by a first step to a smaller diameter cylindrical section
capable of propagating the dominant symmetrical mode. A larger
diameter cylindrical section is coupled to the larger end of the
coupler by a second step. A ring divides the larger diameter
cylindrical section into two parts. The first and second steps and
the dimensioning and placement of the ring are arranged so that the
two difference mode radiation patterns have essentially the same
combined beam width or pattern envelope as the symmetrical mode
radiation pattern.
Inventors: |
Foldes; Peter (Montreal,
CA) |
Assignee: |
RCA Corporation (New York,
NY)
|
Family
ID: |
23941054 |
Appl.
No.: |
05/488,770 |
Filed: |
July 15, 1974 |
Current U.S.
Class: |
343/786;
343/858 |
Current CPC
Class: |
H01Q
25/04 (20130101) |
Current International
Class: |
H01Q
25/04 (20060101); H01Q 25/00 (20060101); H01Q
013/00 () |
Field of
Search: |
;343/776,777,778,786,858 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Lieberman; Eli
Attorney, Agent or Firm: Norton; Edward J. Troike; Robert
L.
Claims
What is Claimed is:
1. A horn antenna comprising:
a funnel-shaped coupling member having two orthogonal symmetry
planes and having an aperture at the narrow end adapted to excite a
symmetrical mode wave therein and a larger diameter aperture at the
opposite end,
a first pair of side wall coupling apertures in the side wall of
said member at diametrically opposite surfaces of the member in one
symmetry plane,
a second pair of side wall coupling apertures in the side wall of
said member at diametrically opposite surfaces of said member in
the second of said orthogonal symmetry planes, said first and
second pair of side wall coupling apertures being adapted to excite
two orthogonal asymmetrical modes,
a waveguide section of a diameter large enough to support said
symmetrical mode and small enough to reflect said asymmetrical
modes and smaller than the diameter of the aperture at the narrow
end of said member coupled by a first step to said narrow end of
said member,
a cylindrical waveguide of a diameter larger than said larger
diameter aperture of said member coupled by a second step to said
opposite end of said member, said cylindrical waveguide section
having a ring-like member dividing said cylindrical waveguide into
two sections, said first and second steps and said ring-like member
being dimensioned and arranged so that the two main lobes in the
radiation patterns associated with the two asymmetrical modes have
substantially the same beamwidth pattern of the single main lobe
radiation pattern associated with the symmetrical mode.
2. The combination in claim 1 including a choke in the outer
surface wall of said cylindrical waveguide.
3. A variable beam position antenna comprising,
in combination:
a hollow member having a first opening at one end and an opening at
the opposite end;
a plurality of side wall coupling apertures in the side wall of
said member;
a first power divider means coupled between said plurality of side
wall coupling apertures and a terminal thereof for in response to
signal waves coupled to said terminal power dividing said waves and
coupling the power divided waves in a given phase relationship to
said side wall apertures to excite within said member a first
asymmetrical difference mode that provides a radiated pattern with
two main out of phase lobes;
means adapted at said one end of the hollow member to couple a
symmetrical mode wave and reflect said asymmetrical difference mode
waves, and means at said opposite end to couple said symmetrical
and asymmetrical modes, and
a controllable power divider means adapted to be coupled to a
source of signal waves for coupling signal waves of a selected
percentage of the power from said source to said one end, whereby a
symmetrical mode radiated pattern with one main lobe is produced,
and for coupling signal waves at the remaining power from said
source to said terminal of said first power divider means.
4. The combination claimed in claim 3, wherein said member is a
funnel-shaped member.
5. The combination claimed in claim 3, wherein said member has two
orthogonal symmetry planes.
6. The combination claimed in claim 5, wherein a first pair of said
plurality of side wall apertures is in a first of said planes and a
second pair of said plurality of side wall apertures is in a second
of said planes orthogonal to said first plane.
7. The combination claimed in claim 6, including means coupled to
said one end for controlling said symmetrical mode and means
coupled to said opposite end for controlling said asymmetrical mode
whereby the two out of phase difference lobes in the pattern
associated within the asymmetrical mode fall within the main
pattern lobe associated with the symmetrical mode.
8. The combination claimed in claim 6 wherein said two asymmetrical
difference modes are the TE.sub.12 mode and a hybrid TM.sub.01 +
TE.sub.21 mode.
9. The combination claimed in claim 6 wherein said first power
divider means includes a second terminal which in response to
signal waves coupled thereto power divides said waves and couples
these power divided waves in a phase relationship to excite within
said member a second asymmetrical difference mode orthogonal to
said first asymmetrical difference mode.
10. A variable beam position antenna comprising, in
combination:
a funnel-shaped hollow member having two orthogonal symmetry planes
and a first opening at one end and a larger opening at the opposite
end adapted to be coupled to free space;
a first terminal means coupled to said one end;
first and second apertures in the side wall of said member at
diametrically opposite surfaces of the member in one of said
symmetry planes;
third and fourth apertures in the side wall of said member at
diametrically opposite surfaces of said member in the second of
said planes;
second and third terminal means;
means coupled between the first, second, third and fourth apertures
and said second and third terminal means for, in response to signal
waves at said second terminal means, equally distributing the
energy of said signal waves applied thereto to each of said side
wall apertures with signal waves at the first and third side wall
apertures being advanced 90.degree. relative to signal waves at the
remaining second and fourth side wall apertures and for, in
response to signal waves at said third terminal means, equally
distributing the energy of said signal waves applied thereto to
each of said sidewall apertures with the signal waves at the second
and fourth apertures being advanced 90.degree. relative to the
signal waves at the first and third sidewall apertures;
a controllable power divider means adapted to be coupled to a
source of radio frequency signals for power dividing said signals
in a selective manner to provide at least one half of the signal
energy of said signals at said source to said first terminal means,
whereby a symmetrical mode pattern is exited in the member, and the
remaining percentage of signal energy of said signals at said
source to a selected one of said second and third terminals in
either a selective in phase at 180.degree. out of phase
relationship with said signals applied to said first terminal.
Description
BACKGROUND OF THE INVENTION
This invention relates to horn antennas and horn antenna feed
systems and more particularly to a horn antenna feed system that
when properly excited generates at least one symmetrical mode and
two asymmetrical modes where the radiated pattern associated with
the asymmetrical modes has two main lobes which essentially have
the same pattern envelope as the radiated pattern associated with
the symmetrical mode having one main lobe.
It is desirable in many applications, such as steerable radar
antennas, aircraft collision prevention equipments, tracking
antennas, and radiating elements for steerable arrays that a
multiple beam position radiating element be provided. It is of
particular interest to construct a multiple beam position radiating
element in which the beam can be switched several positions, for
example, four or five, electronically with a medium gain (in the
range of 8 to 20 db) in the peak direction while the sidelobes of
the switched beam in the rear hemisphere remain below -25 db
relative to the peak of the beam.
SUMMARY OF THE INVENTION
A horn antenna is provided by a structure including a funnel-shaped
coupler with an aperture at the narrow end of the coupler adapted
to excite a symmetrical mode therein, a larger diameter aperture at
the opposite end, and a plurality of side wall coupling apertures
adapted to excite two orthogonal asymmetrical difference modes. The
narrow end of the coupler is coupled by a first step to a smaller
dimensional waveguide section capable of propagating the dominant
symmetrical mode. The larger diameter end of the coupler is coupled
by a second step to a larger diameter cylindrical waveguide
section. The larger diameter cylindrical waveguide section is
divided by a ring into two subwaveguide sections. The first and
second steps and the ring are dimensioned and arranged so that the
radiation patterns associated with the two asymmetrical modes have
substantially the same pattern envelope as the radiation pattern
associated with the symmetrical mode.
DETAILED DESCRIPTION OF THE INVENTION
A detailed description follows in conjunction with the attached
drawing wherein:
FIG. 1 is a side elevation view of the horn antenna according to a
preferred embodiment of the present invention.
FIG. 2 is an end view of the antenna of FIG. 1.
FIG. 3 is a front view of the antenna of FIG. 1.
FIG. 4 is a cross-sectional view of the horn antenna in FIG. 2
taken along lines 4--4.
FIG. 5 illustrates the dominant symmetrical TE.sub.11 mode, the
asymmetrical TE.sub.12 mode and the orthogonal asymmetrical hybrid
TE.sub.21 + TM.sub.01 mode.
FIG. 6 illustrates the patterns associated with the symmetrical and
asymmetrical modes from the antenna of FIG. 1.
FIG. 7 is a schematic diagram of a switched beam position antenna
using the horn in FIG. 1.
FIG. 8 illustrates a coverage area of the switched beam antenna of
FIG. 7.
FIG. 9 illustrates a combined radiation pattern observed by adding
the sum and one set of difference modes.
Referring to FIGS. 1 through 4, there is illustrated a horn antenna
10. A horn antenna 10 includes a funnel-shaped coupler 11, a
cylindrical waveguide section 13 coupled to one end 11a of coupler
11, a smaller cylindrical waveguide section 15 coupled to the
smaller opposite end 11b, a rectangular waveguide section 17
coupled to smaller cylindrical waveguide section 15 at end 17a, and
a choke section 19 coupled to the end 13a of cylindrical waveguide
13. The coupler 11 is a hollow, conically shaped member of a
diameter at end 11b sufficient at least to excite the dominant
TE.sub.11 mode and to reflect those of the TE.sub.12, TE.sub.21 and
TM.sub.01 modes that may be coupled thereto. FIG. 5 illustrates
these modes. The large aperture at the opposite end 11a is made
large enough to couple the TE.sub.11, TE.sub.12, TE.sub.21 and
TM.sub.01 modes.
Four side wall slot apertures 21, 23, 25 and 27 are located in the
side wall of the coupler. See FIGS. 2 thru 4. The center of
apertures 21 and 25 lie in plane 26 and the center of apertures 23
and 27 lie in plane 29. The planes 26 and 29 are at an angle of
45.degree. with respect to the vertical axis 28. The orientation of
these slots in the side wall of the coupler determines the
polarization of the asymmetrical mode. For vertical polarization
shown in FIGS. 2 and 3, the slots are rotated 45.degree. around
their centers and relative to the plane containing the centers of
the four slots. A rectangular coupling cavity is mounted above each
of the side wall apertures. A rectangular cavity 31 is mounted
above coupling aperture 21, a rectangular coupling cavity 33 is
mounted above coupling aperture 23; a rectangular coupling cavity
35 is mounted above coupling aperture 25; and a rectangular
coupling cavity 37 is mounted above coupling aperture 27. The width
w and length l.sub.3, as shown in FIGS. 2 and 4, of each of the
cavities 31, 33, 35 and 37 is made sufficient to support the
TE.sub.10 and the TE.sub.01 rectangular waveguide modes. Coupling
probes 41, 43, 45 and 47 act to excite the TE.sub.10 mode in the
cavities from some external source to be discussed later. The
diameter D.sub.s of the coupler 11 taken as shown in FIG. 4 at the
center of the slot apertures 21, 23, 25 and 27 is made so as to
support at least the TE.sub.12, TE.sub.21 and TM.sub.01 modes in
the coupler. From the above set of modes the TE.sub.12 mode has the
lowest ratio of .lambda..sub.c /D.sub.s = 0.5892, and thus D.sub.s
.gtoreq..lambda./0.5892, where .lambda. is the operational
wavelength. As discussed later, a hybrid mode made up of the
TE.sub.21 + TM.sub.01 modes is also excited at the apertures 21,
23, 25 and 27. The dimension of the coupler at the end 11b and the
axial distance from the center of apertures 21, 23, 25 and 27 to
the end 11b are determined so that the hybrid difference mode
(TE.sub.21 + TM.sub.01) is reflected back toward the larger
aperture 11a of the coupler and combines in phase with the waves
directly travelling from the slot apertures toward the wider end
11a of the coupler.
The symmetrical TE.sub.11 circular waveguide mode and the other
symmetrical modes are excited at the end 11b by means of the
rectangular waveguide section 17, the circular waveguide section 15
and the step 20 between the waveguide section 15 and the end 11b of
the coupler 11. The TE.sub.10 rectangular waveguide mode is excited
in rectangular waveguide 17 by means of coupling probe 51. Each of
the coupling probes as used herein are coaxial probes having the
outer conductor connected to the waveguiding section and the
insulated inner conductor extending into the waveguiding section
through an aperture therein. This TE.sub.10 mode is coupled through
an aperture in the top wall 17a of waveguide 17 into the larger
diameter circular waveguide section 15 wherein the TE.sub.11
circular waveguide mode is excited in cylindrical waveguide section
15. The cylindrical waveguide section 15 terminates in the step 20
at the narrow end 11b of the coupler 11 as mentioned previously.
This step 20 acts as a controlling device for generating a set of
symmetrical modes to produce a Gaussian shape resultant amplitude
distribution in the large aperture at end 12 of the device 10 with
the Gaussian shaped pattern in both the E and H planes. The
TE.sub.11 mode signals together with the other higher order
symmetrical modes (for example TE.sub.30 mode) generated by the
step 20 are radiated out of end 11a of the coupler 11.
Also radiated out of the aperture at end 11a of coupler 11 are
waves in the TE.sub.12 circular waveguide mode and in the hybrid
mode made up of the TE.sub.21 + TM.sub.01 circular waveguide modes.
The signals at the coupler end 11a are coupled to the cylindrical
waveguide section 13 which has a larger diameter than that of end
11a of coupler 11 and thus forms a step 30. The second step 30
provides refinement in the control of the symmetrical modes and
provides proper phasing of the asymmetrical difference modes
TE.sub.12 and hybrid TE.sub.21 + TM.sub.01 modes to maintain their
orthogonal relationships. Essentially, the TE.sub.13 mode is
compensated for the difference in phase velocity relative to the
signals in the hybrid TE.sub.13 + TM.sub.01 modes. Additional
compensation for the phasing between the TE.sub.12 modes and the
hybrid TE.sub.21 + TM.sub.01 modes is achieved by the ring 13b in
the cylindrical waveguide section 13 and by the distance l.sub.7,
FIG. 4, the ring 13b is from the step 30. Further, the ring 13b
contributes to matching of the different modes to free space. A
choke member 19 is located between the output aperture at end 12
and is a continuation of the section 13 from the end 13a of the
cylindrical section 13. The choke 19 includes a section in which
the inside diameter is reduced and the outside surface diameter of
the horn antenna is reduced approximately a quarter wavelength for
an axial length of approximately a quarter wavelength, where a
wavelength is taken at an operating frequency of the antenna. This
quarter wave choke 19 helps to eliminate the flow of surface
currents on the outside of the horn antenna.
In an embodiment designed to operate at a frequency of
approximately 1825 MHz, the horn antenna described above and shown
in FIGS. 1 thru 4 has the following dimensions:
Overall length l.sub.1 of coupler 11 = 7.37 inches
Length l.sub.2 between end 11b and center line of slots 21-25,
23-27 = 5 inches
Length l.sub.3 of cavities 33 and 37 = 6.25 inches
Diameter (D.sub.1) of coupler 11 at end 11b = 7.30 inches
Diameter (D.sub.2) of coupler 11 at end 11a = 10.20 in.
Diameter (D.sub.3) of circular waveguide section 13 between 13a and
11a = 13.23 inches
Diameter of aperture (D.sub.4) in ring 13b, diameter of aperture
(D.sub.5) at end 13a of section 13, and diameter (D.sub.7) of
aperture at end 12 are each = 10.12 inches
Diameter of coupler 11 at center of slots D.sub.s = 9.25 inches
Diameter (D.sub.6) of circular waveguide section 15 = 5.36
inches
Height H.sub.1 of rectangular waveguide section 17 = 2.880
inches
Axial length (l.sub.5) and depth (D.sub.8) of choke 19 = at 1.5
inches
Length (l.sub.6) of circular waveguide section 13 = 5 inches
The distance (l.sub.7) ring 13b is from step 30 = 3.39 inches
Width (w) of coupling cavity 31, 33, 35 and 37 = 4.4 inches.
By the arrangement described above, the symmetrical mode generated
at the step 20 and processed through the antenna has an aperture
distribution as shown by curve 54 in FIG. 6. This response
approximates a Gaussian type response. By the arrangement of the
step 30, the placement of the ring and the dimension of the ring
13b, the asymmetrical difference modes generated in (both the
azimuth and elevation plane or in the TE.sub.12 mode and the hybrid
TE.sub.21 + TM.sub.01 modes) has an aperture distribution similar
to that shown by the dashed line 56 in FIG. 6. As shown in FIG. 6,
at about the -3 db point from the center of the main beam (symmetry
axis) the symmetrical mode beam width is about .+-.18.degree.. The
difference modes fall within the envelope of the pattern defined by
the sum mode with the null of the difference mode pattern in the
center (at the symmetry axis) and the two peaks of the difference
mode at the -3 db point at the .+-.18.degree. points on either side
of the null. This difference mode characteristic is achieved by the
step 30 and the ring 13b.
A switched beam position antenna or scanning antenna system is
provided by coupling the horn antenna 10 shown in FIGS. 1 thru 4 to
a circuitry including a monopulse comparator 55 and a switchable
power divider network 85 as shown in FIG. 7. The TE.sub.11 mode
coupling port 51, FIGS. 1 and 4, is represented by terminal 51a in
FIG. 7, and the sidewall apertures 21, 23, 25 and 27 are
represented by probes 21a, 23a, and 27a. The coupling cavities 31,
33, 35 and 37 are represented by boxes 31a, 33a, 35a and 37a in
FIG. 7. The sidewall coupling members 21a, 23a, 25a and 27a are
coupled to a monopulse comparator network 55 via the coupling
cavities 31a, 33a and 37a.
This comparator 55 network is like that of comparator network 15 in
applicant's copending application, Ser. No. 470,574, filed May 16,
1974. The comparator 55 consists of two magic-tee (0.degree.
hybrids) hybrids 65 and 67 and two short-slot hybrids (90.degree.
hybrids) 69 and 71 and connections therebetween. One terminal of
each of the magictee hybrids is coupled to a load (indicated by
resistor). One of the magic-tee hybrids 65 is coupled at one end to
terminal 75 of the comparator 55 and at the opposite end to
terminal 69b of short-slot hybrid 69 and terminal 71a of short-slot
hybrid 71. The other magic-tee hybrid 67 is coupled at one end to
the terminal 77 of the comparator 55 and at the opposite end to
terminal 69a of short-slot hybrid 69 and terminal 71b of short-slot
hybrid 71. The terminals 69c, 69d, 71c and 71d of short-slot
hybrids 69 and 71 form the terminals of the monopulse comparator
55. The terminals 69c, 69d, 71d of the comparator 55 are coupled
via suitable transmission lines 79, 80, 81 and 82 and the
respective coupling cavities 33a, 31a, 37a and 35a to the coupling
members 23a, 21a, 27a and 25a. The signal waves at terminal 75 are
power divided at hybrid 65 and are coupled with equal phase to
terminal 69b of hybrid 69 and terminal 71a of hybrid 71. The wave
at terminal 69b is power divided with the output waves coupled to
coupling member 23a via terminal 69c undergoing 90.degree. more
phase shift than the wave coupled to coupling member 21 a. This
additional phase shift is due to the coupling of the waves through
the short slot 69e of hybrid 69. The signal waves at terminal 71a
are power divided with the output power divided waves coupled
through slot 71e to coupling member 25a undergoing 90.degree. more
phase shift than the power divided waves coupled to coupling member
27a. With this phase distribution the signals at coupling members
23a and 25a undergo 90.degree. more phase shift than the signals at
the coupling members 21a and 27a. If the coupling members 21a, 23a,
25a and 27a are oriented as shown in FIG. 7 and the above phase
relationships exist, the linearly polarized TE.sub.12 mode circular
waveguide as shown in FIG. 5 is excited with the null in the plane
of coupling members 23a and 27a. The waves at terminal 77 are power
divided by hybrids 67, 69 and 71. This results in 90.degree. more
phase shift to the waves at coupling members 21a and 27a than at
coupling members 23a and 25a. When the coupling slots are oriented
in the same direction as stated previously (shown in FIG. 2), the
signals in the coupler 11 of antenna 10 are excited in the
TE.sub.21 + TM.sub.01 so called circular waveguide hybrid mode as
shown in FIG. 5. The null plane is in the plane of the coupler
determined by coupling members 21a and 25a. The radiation pattern
from these two sets of modes will have two out of phase main lobes
and their null planes will be orthogonal to each other and will
coincide with the plane of the coupling members. The difference
mode pattern is illustrated by dashed line 56 in FIG. 6.
It has been found that by controlling the amount of power to
terminal 51a of the antenna 10 relative to the power at terminals
75 and 77 of the comparator 55, a switched beam position antenna
system is provided. In other words with respect to the above
described arrangement, by controlling the power levels of the
excited symmetrical mode such as the dominant TE.sub.11 mode, and
the asymmetrical modes such as the TE.sub.12 and hybrid TE.sub.21 +
TE.sub.01 modes in the antenna coupler 11, a switched beam position
antenna system can be produced. This switchable power division is
provided by the switchable power divider network 85. The switchable
power dividing network 85 includes a power divider 95, three
switches 96, 97 and 99 and a 180.degree. phase shifter 101. The
terminal 91 of switchable power divider network 85 is coupled to a
source of signal waves. The power from that source is power divided
at power divider 95 wherein waves with a selected percentage of the
input power from the source are coupled via a trimming phase
shifter 104 to terminal 51a of antenna 10 and the remaining power
in the form of signal waves is coupled to switch 96. The switch 99
in a first position (contacting terminal 99a) couples the applied
remaining power via synchronized switches 96 and 97 to terminal 75
of comparator network 55. In a second position of switch 99
(contacting terminal 99b) the applied remaining power is coupled to
terminal 77. If switches 96 and 97 are in a first position
(contacting terminals 96a and 97a) the remaining power is coupled
over a transmission line path 105 therebetween to terminal 75 or
77. If switches 96 and 97 are in their second position (contacting
terminals 96b and 97b), the remaining power is coupled over a
transmission path 106 including 180.degree. phase shifter 101 to
terminal 75 or 77. Thus, the switchable power divider delivers the
remaining power to either terminal 75 or 77 in either 0.degree. or
180.degree. phase, providing a total of four conditions.
When the variable power divider 95 is adjusted so that all of the
power is coupled to terminal 51a, a beam is excited having its
maximum along the mechanical axis (symmetry axis in FIG. 6) of the
radiating antenna 10. If the variable power divider 95 couples one
half of the power to terminal 51a and the remaining power to switch
96, four additional beam positions are provided by the four
conditions of switchable power divider 85 which have their maximum
in the 45.degree., 135.degree., 225.degree. and 315.degree. azimuth
directions and at 1/2 .theta..sub.3 angle away from the original
mechanical (symmetry) axis of the system. Here .theta..sub.3 is the
3 db beamwidth of the symmetrical mode beam associated with signals
in the TE.sub.11 mode coupled to terminal 51a.
The square 120 outlined in FIG. 8 illustrates a given required
angular coverage, the dot 123 in the center represents the
mechanical axis of the antenna and the small circle 121 represents
the angular coverage when all the input power is delivered to the
sum port 51a. When one half of the power is coupled either in phase
or with 180.degree. phase reversal to either terminals 75 or 77 the
center of the radiated pattern is switched in the direction of the
arrows to provide the coverage areas A, B, C and D which are
quadrants of coverage area 120.
As mentioned previously, the two difference mode patterns have two
out of phase main lobes. By the arrangement discussed above a first
of these two main lobes associated with each difference mode is in
phase with the single main lobe associated with the TE.sub.11 mode.
These in phase lobes add and the out of phase lobe subtracts,
resulting in a combined beam with maximum signal in a direction
toward the peak of the in phase lobe of the difference mode. By
adding, the 180.degree. phase shift to the signals coupled to
terminals 75 or 77, the sum mode (symmetrical mode) wave associated
with terminal 51a is in phase with the second of the two main lobes
associated with each difference mode and is out of phase with the
first of these modes. Consequently, the maximum beam direction is
moved to the directly opposite quadrant (for example from A to D or
C to B).
To summarize the variable power divider switch 95 controls the
percentage of the power to excite the main symmetrical TE.sub.11
mode. The switch 99 switches the remaining percentage of power to
excite either the TE.sub.12 mode via terminal 75 (if 50 percent of
the power at that terminal 75 illuminate quadrants A or D in FIG.
8) or excite the hybrid mode of TE.sub.12 + TM.sub.01 modes via
terminal 77 (if 50 percent of the power at the terminal 77
illuminate quadrants B or C in FIG. 7). The synchronized switches
96 and 97 control which of the two quadrants A or D are illuminated
when the power goes via terminal 75. The synchronized switches 96
and 97 control which of the two quadrants B or C are illuminated
when the power goes via terminal 77.
FIG. 9 illustrates a combined beam 131 which is the result of 50
percent of the power being coupled to terminal 51a and 50 percent
of the power to either terminals 75 or 77. Because the sum and
difference mode component patterns have the same envelope, the
resultant scanned pattern is practically sidelobe free. This same
envelope characteristic as discussed previously is achieved by the
dimensioning of the steps at the junction of the conical coupler
section 11 and the cylindrical section, by the length of the
cylindrical section and the position of the ring 13b in the
cylindrical section.
* * * * *