TECHNICAL FIELD
[0001] The present invention relates to the field of antennas, and more particularly low
profile antennas.
BACKGROUND OF THE ART
[0002] A combination of a waveguide feed network and radiator element may be used to enable
an antenna to collect energy from a large area and guide the collected energy to a
single input/output waveguide, which may in turn be connected to a transmitter/receiver.
In order to economically transmit electromagnetic energy from an antenna aperture,
both an efficient radiating aperture and feed network are typically required.
[0003] For narrow-band, i.e. 5% bandwidth, applications, slot radiators are often used to
fill the antenna aperture. However, due to the periodicity of a wavelength of the
transmitted or received signal, the slots need to be spaced no more than one guide
wavelength apart in the vertical and horizontal direction. This architecture thus
requires N horizontal radiators and M vertical radiators, for a total of NxM radiators.
The resulting complexity in creating the feed network and fabricating the multitude
of slots is then costly and leads to poor performance. For example, limited bandwidth,
frequency scanning, and the like may result. This problem can also be found in other
conventional antenna designs using different radiators, such as patches, printed dipoles,
etc., as the latter usually still require NxM radiators.
[0004] There is therefore a need for an improved low profile antenna.
SUMMARY
[0005] In accordance with a first broad aspect, there is provided a low profile antenna
comprising a radiator array comprising a plurality of radiating elements arranged
linearly along a first direction, each one of the plurality of radiating elements
adapted to radiate along a second direction substantially perpendicular to the first
direction, and a corporate feed network integrated with the radiator array, the corporate
feed network comprising an input transmission line adapted to receive an input signal
and a plurality of output transmission lines each coupled to the input transmission
line and to a corresponding one of the plurality of radiating elements, the input
signal adapted to be routed among the plurality of output transmission lines for delivery
to the plurality of radiating elements.
[0006] In accordance with a second broad aspect, there is provided a method for manufacturing
a low profile antenna, the method comprising arranging a plurality of radiating elements
linearly along a first direction to form a radiator array, each one of the plurality
of radiating elements adapted to radiate along a second direction substantially perpendicular
to the first direction, and integrating a corporate feed network with the radiator
array, the corporate feed network comprising an input transmission line adapted to
receive an input signal and a plurality of output transmission lines each coupled
to the input transmission line and to a corresponding one of the plurality of radiating
elements, the input signal adapted to be routed among the plurality of output transmission
lines for delivery to the plurality of radiating elements.
BRIEF DESCRIPTION OF THE DRAWINGS
[0007] Preferred embodiments of the invention will now be described by way of example only
and with reference to the accompanying drawings, in which:
[0008] Figure 1 is a front perspective view of an antenna aperture in accordance with an
illustrative embodiment of the present invention;
[0009] Figure 2a is a cross-sectional view of the antenna aperture of Figure 1;
[0010] Figure 2b is a right side view of the corporate feed network of Figure 2a;
[0011] Figure 3a is a perspective view of a folded reflective line source for use in the
antenna of Figure 1;
[0012] Figure 3b is a perspective view of a discretized line source for use in the antenna
of Figure 1;
[0013] Figure 4 is a perspective view of the antenna aperture of Figure 1 mounted on an
elevation over azimuth computer controlled positioner;
[0014] Figure 5a is a plot of a simulated azimuth gain pattern for the antenna of Figure
1; and
[0015] Figure 5b is a plot of a simulated elevation gain pattern for the antenna of Figure
1.
[0016] It will be noted that throughout the appended drawings, like features are identified
by like reference numerals.
DETAILED DESCRIPTION
[0017] Referring now to Figure 1, an antenna aperture 100 having a low profile will now
be described. The antenna aperture 100 illustratively comprises a line source 102
and a linear radiator array 104 comprising a number N of horizontal radiators 106
1, ..., 106
N each extending along the X axis and a number M of vertical radiators (not shown)
each extending along the Y axis. It should be understood that the number of radiators
as in 106
1, ..., 106
N in the array 104 may vary according to system requirements. Each radiator as in 106
1, ..., or 106
N may be a tapered slot antenna that is adapted to radiate at a given directionality
the energy of an electromagnetic wave received thereat. It should be understood that
other configurations of the radiator may apply.
[0018] Referring to Figure 2a and Figure 2b in addition to Figure 1, the antenna aperture
100 further comprises a corporate feed network 108 supplying electromagnetic energy
to the radiators 106
1, ..., 106
N. In one embodiment, the radiators 106
1, ..., 106
N are integrated with the feed network 108 as a single component. For this purpose,
both the radiators 106
1, ..., 106
N and the feed network 108 may be manufactured from the same waveguide piece 110 having
an air-filled or other appropriate structure, such as a dielectric-filled or partially-filled
waveguide structure. For example, each radiator as in 106
1, ..., or 106
N may be etched on the waveguide piece 110 and excited using the corporate feed network
108 also etched on the waveguide piece 110. High speed machining, extrusion, casting,
molding, e.g. injection molding, or any other suitable manufacturing process known
to those skilled in the art may also be used. The radiator array 104 may for instance
be manufactured using solid metal extrusions, hollow extrusions, plastic extrusions,
or composite extrusions with application of a metal coating or foil. The line source
102 may then be provided separately from the integrated radiators 106
1, ..., 106
N and feed network 108. In particular, when in use, the line source 102 may be coupled
to feed network 108 to become part thereof. In this manner, a low weight and compact
size antenna aperture 100 may be provided.
[0019] The line source 102 may further be coupled to a source of electromagnetic signals
(not shown), from which an input signal may be received. The line source 102 may then
transform the input into an output having an expanded dimension, e.g. width, along
the X axis. In one embodiment discussed further below, a single mode input is provided
by the source to the line source 102 and the latter outputs a single linear beam that
is continuous along the X axis. The signal output by the line source 102 may then
be transmitted to the feed network 108 and replicated thereby to feed each one of
the N horizontal radiators 106
1, ..., 106
N for transmittal. Although the antenna aperture 100 is described herein in the context
where it is used as a transmitter, it should be understood that the antenna aperture
100 may, by reciprocity, be used as a receiver and route receive signals to single
outputs.
[0020] The feed network 108 may comprise a plurality of transmission or feed lines as in
112
1, ..., 112
n and power dividers (not shown) provided over a number n of successive feed levels.
The first feed level, i.e. level 1, is illustratively the level closest to the line
source 102 while the last feed level, i.e. level n, is the level closest to the radiator
array 104. Each one of the transmission lines provided at the last feed level n, e.g.
transmission line 112
n in Figure 2a and Figure 2b, may then be coupled to a corresponding radiator, e.g.
radiator 106
1, of the radiator array 104. In this manner, the output of each one of the transmission
lines found at the last feed level may be provided to the corresponding radiator as
in 106
1, ..., or 106
N for feeding thereof. In particular, the feed network 108 illustratively receives
at an input port 114 thereof the expanded signal output by the line source 102. The
feed network 108 may then split the energy of the received signal among the transmission
lines 112
1, ..., 112
n of the multiple feed levels. This may be achieved using power dividers that implement
binary power splits, i.e. power splits of 2
n-1, with n = 1, 2, 3, 4... being the number of feed levels of the corporate feed architecture.
As known to those skilled in the art, the power splits may be accomplished by using
tapered lines or impedance transformers. It should also be understood that, instead
of binary power splits, the feed network 108 may achieve triple or quadruple power
splits. Still, binary power splits may be preferable as they gave a simple design.
[0021] For this purpose, each one of the transmission lines 112
1, ..., 112
n-1 is split into two (2) transmission lines provided at the next feed level. For instance,
a transmission line at a level n, e.g. transmission line 112
2 at the second feed level, is illustratively terminated by a junction 116, which branches
out into a first and a second transmission line provided at the following level n+1,
e.g. transmission lines 112
3 at the third feed level. It should be understood that depending on the type of power
splits accomplished, each transmission line at a given level may be split into more
than two (2) transmission lines at the next level. The junction 116 may be a tee junction
where the first and second transmission lines, e.g. transmission lines 112
3, meet at an angle of substantially ninety (90) degrees and are collinear to one another.
It should be understood that, although other configurations, e.g. y-junction geometries,
may apply, the tee junction geometry may be preferable as it ensures a low profile
for the feed network 108. Also, the energy of the signal routed through the transmission
line of level n, e.g. transmission line 112
2, is illustratively divided at the junction 116 among the first and second transmission
lines of level n+1, e.g. transmission lines 112
3.
[0022] Although even power distribution may be desirable, the power split provided at each
junction 116 of the feed network 108 may be an equal or unequal power split. Thus,
the amplitudes of the signals provided at the first and the second transmission lines
of level n+1 may be equal or unequal. As will be discussed further below, non-uniform
power distribution may be used to lower sidelobe levels of the gain pattern of the
antenna aperture 100. The phases of the signals provided at the first and the second
transmission lines of level n+1 may also be uniform or non-uniform, e.g. equal or
unequal. For instance, non-uniform phases may be used when it is desired to squint
a beam or otherwise shape the far-field gain pattern of the antenna aperture 100.
In Figure 2a and Figure 2b, the feed network 108 feeds N = 16 radiators 106
1, ..., 106
N using equal binary power splits and uniform phase over n = 5 levels.
[0023] In one embodiment, the combination of the line source 102 and the feed network 108
may be used to feed N horizontal radiators 106
1, ..., 106
N and M = 1 vertical radiators (not shown), i.e. a single vertical radiator as in 118
1. As such, the linear radiator array 104 illustratively comprises N horizontal radiators
106
1, ..., 106
N arranged in a single column along the Y axis so that the radiator array 104 comprises
a radiator arrangement, which is discrete along the vertical Y axis and continuous
along the horizontal X axis. The line source 102 may then provide the horizontal excitation
to the radiator array 104 while the corporate feed network 108 provides the vertical
excitation.
[0024] Referring to Figure 3a and Figure 3b in addition to Figure 1, although the embodiment
of Figure 1 illustrates a radiator array 104 where each horizontal radiator as in
106
1, ..., 106
N is continuous along the X axis, it should be understood that each horizontal radiator
as in 106
1, ..., 106
N may also be discretized along the X axis. In particular, to arrive at the embodiment
of Figure 1, the line source 102 may comprise a folded reflective line source architecture
200, as shown in Figure 3a. Still, it should be understood that other configurations
may apply. The folded reflective line source 200 may be used to transform a single
mode input 202 into a single line source 204 that is continuous along the X axis,
i.e. the horizontal direction. The line source 204 illustratively has a dimension
along the X axis, e.g. a width, that is expanded compared to the dimension of the
single mode input 202 along the same X axis.
[0025] For this purpose, the folded reflective line source 200 may comprise a plurality
of taper regions as in 206 adapted to expand a beam propagating therethrough. The
taper regions 206 may be provided in a stacked relationship and connected by 180 degree
reflectors as in 208. Each reflector 208 may be used to fold the direction of propagation
of a beam traveling down each one of the taper regions 206, thereby ensuring compactness
of the structure. The folded reflective line source 200 may also comprise a reflective
phase compensator 210 for compensating for the phase error introduced during travel
of the beam down the successive taper regions 206. Using such a folded reflective
line source 200 to build the antenna aperture 100 may result in a circuit largely
comprised of slab waveguides. Such a slab waveguide geometry illustratively has low
loss and allows most of the antenna design to be constructed from low cost extrusions.
For example, aluminum metal extrusions or metal coated plastic extrusions or molded
parts may be used.
[0026] Alternatively and as shown in Figure 3b, the line source 102 may comprise a corporate
feed line source architecture 300, which produces an output that is discretized along
the X axis. The energy radiated by each one of the horizontal radiators as in 106
1, ..., 106
N may in turn be discretized. In particular, the corporate feed line source 300 may
be used to transform a single mode input 302 into a plurality of discrete outputs
304 distributed along the direction of the X axis. The discrete outputs 304 may together
form a discretized output 306 having an overall dimension along the X axis, e.g. a
width, that is expanded compared to the dimension of the single mode input 302 along
the same X axis. For this purpose, the corporate feed line source 300 may comprise
multiple feed lines as in 308 providing binary power splits over a plurality of levels
(not shown). In the embodiment of Figure 3b, the corporate feed line source 300 transforms
the single mode input 302 into sixty-four (64) discretized outputs 304 over seven
(7) levels.
[0027] Referring now to Figure 4 in addition to Figure 1, the antenna aperture 100 may be
incorporated into a computer-controlled elevation over azimuth rotary antenna positioner
400. As known to those skilled in the art, such an antenna positioner 400 may be used
to position the antenna 100 for tracking a moving object (not shown). In the embodiment
of Figure 4, an antenna aperture having a dimension along the X axis, i.e. a length,
of 594.06mm, a dimension along the Y axis, i.e. a height of 152.50mm, and a dimension
along the Z axis, i.e. a width of 56.31 mm is used. Elevation and azimuth gain patterns
may then be measured, as shown in Figure 5a and Figure 5b.
[0028] Figure 5a shows a simulated azimuth gain pattern 500 at a frequency of 30GHz for
the antenna aperture 100 of Figure 4. It can be seen that the first sidelobe 502 in
the azimuth gain pattern 500 is approximately 23dB below the peak 504, as desired
in aeronautical applications and the like. Indeed, it is desirable, when communicating
with a geostationary satellite, for the azimuth pattern as in 500 to provide low side
lobe levels in order to comply with regulatory requirements to limit interference
with adjacent satellites.
[0029] Figure 5b shows a simulated elevation gain pattern 600 at a frequency of 30GHz for
the antenna aperture 100 of Figure 4. As discussed above, since the elevation feed
shown in Figure 5b illustratively uses equal output binary power splitters (not shown)
for splitting the power of the signal received from the line source 102, a uniform
excitation may be achieved along the Y axis, i.e. the vertical direction, of the radiator
array 104. This results in higher sidelobes being obtained for the elevation gain
pattern 600 than for the azimuth gain pattern 500. In particular, the uniform excitation
leads to the first sidelobe 604 being at approximately 13dB below the peak 602. As
discussed above with reference to Figure 2a and Figure 2b, it should be understood
that feed designs using unequal splits may be used in some applications. In this case,
one could achieve an antenna aperture where each radiator of the radiator array 104
provides a non uniform illumination, e.g. more energy is output towards the center
of the radiator than at the edges thereof. The gain pattern of such an antenna aperture
would thus comprise a wider main beam and lower sidelobe levels. However, this would
lower the gain of the overall antenna structure. As gain is the principal limiting
factor for aeronautical satellite communications antennas, sidelobe control in the
elevation plane is of limited utility. The reduction in antenna gain would therefore
not provide any additional net benefit for the intended applications.
[0030] Referring back to Figure 1, the antenna aperture 100 illustratively has low loss
and high gain over a large frequency bandwidth. In particular, broadband response
over 50% of the bandwidth may be achieved and the design may be scalable from 5 GHz
to 75 GHz operating frequency. This is particularly desirable for satellite communications
applications where a wideband signal is to be radiated in a single direction regardless
of the input frequency. The antenna aperture 100 may further allow for a minimal number
of radiator elements to be used in the radiator array 104, thus achieving a low profile
and low weight structure having a flat plate, i.e. compact, design. The impact of
an installed system on the operating costs of a device, such as an aircraft, may therefore
minimized while achieving high performance.
[0031] The embodiments of the invention described above are intended to be exemplary only.
The scope of the invention is therefore intended to be limited solely by the scope
of the appended claims.
1. A low profile antenna (100) comprising:
a radiator array (104) comprising a plurality of radiating elements (1061, ..., 106N) arranged linearly along a first direction, each one of the plurality of radiating
elements adapted to radiate along a second direction substantially perpendicular to
the first direction; and
a corporate feed network (108) integrated with the radiator array, the corporate feed
network comprising an input transmission line (1121) adapted to receive an input signal and a plurality of output transmission lines
(112n) each coupled to the input transmission line and to a corresponding one of the plurality
of radiating elements, the input signal adapted to be routed among the plurality of
output transmission lines for delivery to the plurality of radiating elements.
2. The antenna of claim 1, wherein the plurality of radiating elements of the radiator
array are arranged in a single column along the first direction, the first direction
being a vertical direction.
3. The antenna of claim 1 or 2, further comprising a line source (102) adapted to be
coupled to the corporate feed network for supplying the input signal to the input
transmission line.
4. The antenna of claim 3, wherein the line source is a folded reflective line source
(200) adapted to receive a single mode input (202) having a first width and to transform
the single mode input into the input signal, wherein the input signal has a second
width greater than the first width and is continuous along the second direction.
5. The antenna of claim 4, wherein the corporate feed network is adapted to route the
input signal among the plurality of output transmission lines for delivery to the
plurality of radiating elements, thereby causing each one of the plurality of radiating
elements to radiate an output signal that is continuous along the second direction.
6. The antenna of claim 3, wherein the line source is a corporate feed line source adapted
to receive thereat a single mode input having a first width and to transform the single
mode input into the input signal, wherein the input signal comprises a plurality of
discrete sources arranged along the second direction.
7. The antenna of claim 6, wherein the corporate feed network is adapted to route the
input signal among the plurality of output transmission lines for delivery to the
plurality of radiating elements, thereby causing each one of the plurality of radiating
elements to radiate an output signal that is discretized along the second direction.
8. The antenna of any of claims 3 to 7, wherein the corporate feed network further comprises
a plurality of intermediary transmission lines, the input line, the plurality of intermediary
lines, and the plurality of output transmission lines distributed among a plurality
of feed levels.
9. The antenna of claim 8, wherein the plurality of feed levels of the corporate feed
network comprises a first feed level arranged adjacent the line source and a last
feed level arranged adjacent the radiator array, the input transmission line provided
at the first feed level and the plurality of output transmission lines provided at
the last feed level.
10. The antenna of claim 8 or 9, wherein the corporate feed network comprises a plurality
of junctions (116) for arranging the plurality of intermediary lines and the plurality
of output transmission lines in pairs over successive ones of the plurality of feed
levels, each one of the plurality of junctions adapted to receive a first signal and
to output a second and a third signal.
11. The antenna of claim 10, wherein the corporate feed network comprises a plurality
of power dividers each provided at a corresponding one of the plurality of junctions
for dividing a first power of the first signal into a second power of the second signal
and a third power of the third signal, wherein the second power is equal to the third
power, or the second power is different from the third power.
12. The antenna of claim 10 or 11, wherein the corporate feed network comprises a plurality
of power dividers each provided at a corresponding one of the plurality of junctions
for dividing a first power of the first signal into a second power of the second signal
and a third power of the third signal, wherein the second signal has a phase equal
to that of the third signal, or the second signal has a phase different from that
of the third signal.
13. The antenna of any preceding claim, wherein the radiator array and the corporate feed
network are manufactured from a same waveguide piece (110), and optionally wherein
the radiator array is manufactured using one of solid metal extrusions, hollow extrusions,
plastic extrusions, composite extrusions, casting, and molding.
14. A method for manufacturing a low profile antenna (100), the method comprising:
arranging a plurality of radiating elements (1061, ..., 106N) linearly along a first direction to form a radiator array (104), each one of the
plurality of radiating elements adapted to radiate along a second direction substantially
perpendicular to the first direction; and
integrating a corporate feed network (108) with the radiator array, the corporate
feed network comprising an input transmission line (1121) adapted to receive an input signal and a plurality of output transmission lines
(112n) each coupled to the input transmission line and to a corresponding one of the plurality
of radiating elements, the input signal adapted to be routed among the plurality of
output transmission lines for delivery to the plurality of radiating elements.
15. The method of claim 14, wherein linearly arranging the plurality of radiating elements
comprises arranging the plurality of radiating elements in a single column along the
first direction, the first direction being a vertical direction, and/or wherein the
method further comprises coupling a line source (102) to the corporate feed network
for supplying the input signal to the input transmission line.