Field
[0001] The present invention relates to the field of antennas, particularly antenna for
use in Radar systems. It finds particular, but not exclusive utility in the field
of marine Radar systems i.e. those installed on ships.
Background to the present invention
[0002] Most or many ships are equipped with at least one Radar system, used for navigation
and/or other purposes. In particular, military vessels are frequently equipped with
a weapons system Radar which is provided to locate, identify and possibly track possible
threats. The complexity and functionality of such a weapons system Radar is far greater
than that of a relatively simple navigational Radar system.
[0003] In typical prior art systems, the Radar antenna rotates to sweep signals across the
location and is affixed to an upper portion of a high mast on the vessel. It is desirable
to position the antenna as high as possible to give optimal range coverage and to
avoid any other parts of the vessel from obscuring the transmit or receive Radar signal.
[0004] A problem with such an arrangement is that the antenna typically has a mass of several
hundred kilograms. The mass of the system is due to prior art antennas incorporating
a good deal of the Radio Frequency (RF) equipment within the antenna housing. Typically,
this RF equipment includes one or more of transmitters, receivers, duplexers, filters
and associated processing equipment.
[0005] The signals from the RF equipment are passed to digital processing systems, using
one or more complex rotating joints which allow electrical continuity between the
rotating antenna housing and the connected circuits.
[0006] Having a large, heavy rotating mass situated atop a mast, often at the highest point
of the vessel, poses problems - not least in terms of stability, installation and
maintenance - and there is a general desire to reduce the mass of the rotating part
of the Radar system as far as possible. Prior art techniques have tended to concentrate
on designing out as much mass from the RF equipment and housing, but there is a limit
to how much mass can be eliminated from the antenna housing by these means.
[0007] Embodiments of the present invention aim to address these and other problems with
prior art Radar antennas, whether mentioned herein or not.
Summary of the Invention
[0008] According to an aspect of the present invention, there is provided an antenna sub-array
for use in an antenna array comprising a plurality of such sub-arrays, comprising:
a stripline for signal distribution, the stripline defining a plurality of signal
pathways from a common feed point to a plurality of radiating elements, wherein the
stripline is housed in a first support structure located a distance away from a first
surface of a ground plane structure.
[0009] Preferably. the first support structure comprises a foam material having predefined
dielectric properties.
[0010] Preferably, the predefined dielectric properties include having a dielectric constant
substantially equal to that of air.
[0011] Preferably, the stripline is located in a channel in the first support structure
and held in position above the first surface of the ground plane structure by a button
formed from the same material as the first support structure.
[0012] Preferably, affixed to a second surface of the ground plane structure is a second
support structure.
[0013] Preferably the first and second support structures are different materials.
[0014] Preferably, the stripline and the radiating elements are integrally formed.
[0015] Preferably, the first support structure comprises a plurality of channels arranged
to receive a cooling fluid for cooling the stripline and radiating elements.
[0016] According to a further aspect of the present invention, there is provided an antenna
array comprising a plurality of sub-arrays according to the first aspect.
[0017] According to a still further aspect of the present invention, there is provided a
method of manufacturing an antenna array, comprising the steps of: providing a plurality
of sub-arrays, each according to the first aspect; assembling the plurality of sub-arrays
in a layered arrangement and securing each sub-array to a neighbouring sub-array with
an adhesive substance; curing said adhesive to form a unitary antenna array.
[0018] According to a still further aspect of the present invention, there is provided a
method of cooling an antenna sub-array, according to the first aspect, comprising
the steps of: providing a channel in a portion of the sub-array, said channel housing
at least some Radio Frequency components; and forcing a cooling fluid into the channel
via a first aperture, such that the cooling fluid passes through the channel and is
exhausted at a second aperture.
[0019] Preferably, the first aperture is proximal to a Radio Frequency connector of the
sub-array.
[0020] Preferably, the second aperture is proximal to one or more of the plurality of radiating
elements.
[0021] Preferably the channel is provided in the first support structure, which houses the
stripline.
Brief Description of the Figures
[0022] For a better understanding of the invention, and to show how embodiments of the same
may be carried into effect, reference will now be made, by way of example, to the
accompanying diagrammatic drawings in which:
Figures 1 a and 1 b show rear and front views, respectively, of an antenna sub-array
according to an embodiment of the present invention;
Figure 2 shows a plan view of a stripline in a sub-array according to an embodiment
of the present invention;
Figure 3 shows a cross-section through a sub-array according to an embodiment of the
present invention;
Figure 4 shows an front view of an antenna array according to an embodiment of the
present invention comprising a plurality of sub-arrays; and
Figure 5 shows how a cooling fluid acts to cool the stripline and antenna elements.
Detailed description of preferred embodiment
[0023] Embodiments of the present invention allow an antenna array, for use with a Radar
system, to be constructed from a plurality of individual sub-arrays. The sub arrays
are substantially identical. This provides a great deal of design freedom, and allows
antenna arrays having different functional properties to be created, starting from
a single building block, namely the sub-array.
[0024] The sub-array is arranged to be lightweight and, as such, is constructed, as far
as possible, from lightweight foam materials, which are used to support and house
the feed and radiating components, which carry and transmit the RF signals, respectively.
[0025] At the frequencies used in Radar systems, stripline techniques are often used to
carry and distribute the signals from transmitters and/or receivers to individual
radiating elements, which are arranged to co-operate to produce a desired antenna
performance. Details of the stripline construction and its housing will follow shortly.
[0026] Figure 1a shows a rear perspective view of an antenna sub-array 1 according to an
embodiment of the present invention. The sub-array in this embodiment is formed to
have a substantially rectangular profile in plan view. In terms of its dimensions,
it is significantly larger in width and depth than height, although other configurations
are possible where this may not be the case.
[0027] On its rear surface, as shown in Figure 1a, there is provided an RF connector 2 which
forms a common feed point for connection of the sub-array 1 to the RF equipment (not
shown). The RF connector may be an N-type coaxial connector or any other suitable
form of connector.
[0028] On the front surface, as shown in Figure 1b, there is provided a plurality of individual
radiating elements 3. In the present embodiment, these take the form of identical
dipole elements. In alternative embodiments, the individual radiating elements may
not be identical and may not be dipole elements, but different forms of antenna.
[0029] The dipole elements 3 are integrally formed with the stripline, meaning that the
feed structure and the radiating structure are part of the same physical entity, having
been milled from the same sheet of material. This has advantages in ease of manufacture
and helps to ensure reliable antenna performance. However, in alternative embodiments,
the individual radiating elements may be connected to the stripline feed structure
by respective individual connectors.
[0030] Figure 2 shows a typical stripline 7 layout. The stripline is milled from sheet aluminium
to precise tolerances and, as far as is practicable, from a single sheet of material.
The path length of any particular branch is calculated to achieve a particular phase
relationship between each respective path. For instance, in most cases, it will be
desired to ensure that each individual path length is identical and so certain of
the individual branches may meander or deviate to achieve this. The exact nature of
this meandering not shown here, and will depend on the specification of the antenna
sub-array.
[0031] The stripline 7 is accommodated as shown in Figure 3 which shows a cross-sectional
view through a sub-array 1. On a lower surface of the sub-array, there is a ground
plane 4. This is formed from aluminium1200 foil, 0.2mm thick which is secured to a
layer of structural foam 5, by means of a lightweight adhesive film (such as SA70/100g
adhesive film). The structural foam 5 provides strength and form to the sub-array.
It is chosen to have specified mechanical properties and to be as lightweight as possible,
while still providing the required strength and structure. A suitable lightweight
structural foam material is ROHACELL 31 IG, a polymethacrylimide foam, available from
Evonik industries (
www.evonik.com).
[0032] Secured to the upper surface of the structural foam 5, is a further ground plane
4, identical to the one secured to the lower surface of the structural foam 5.
[0033] Secured to the upper ground plane 4 is a layer of dielectric foam 6. This is so-called
as this layer of foam has specific dielectric properties, which have an influence
on the properties of the stripline 7. Specifically, the dielectric foam 6 is selected
to have a dielectric constant as near as possible to that of free air. A suitable
dielectric foam is ROHACELL 31 HF, a polymethacrylimide foam, also available from
Evonik Industries. In other embodiments, the dielectric foam may be selected to have
a dielectric constant which is significantly different to that of free air to achieve
different transmission effects.
[0034] The same adhesive film, which is used to secure the lower ground plane 4 to the structural
foam 5, is used to secure the other parts of the sub-array together i.e. it is located
between structural foam 5 an upper ground plane 4, and also between upper ground plane
4 and dielectric foam 6. It is also used to secure each individual sub array to its
neighbouring sub-array when the complete array is constructed, as will be described
shortly.
[0035] The dielectric foam 6 has channels cut into it which conform generally to the arrangement
of the stripline 7, such that the stripline 7 can be accommodated in the channels
and within the thickness of the dielectric foam 6. This is illustrated in the detailed
view of Figure 3 where a channel in the dielectric foam can be seen, in which is situated
the stripline 7. It is supported above the lower ground plane 4 by a button 8 of dielectric
foam. There is a similar or identical button 8 positioned above the lower button so
that the stripline 7 is effectively sandwiched into position and so can maintain a
constant distance between the upper and lower ground planes 4, for its entire length.
This is important in ensuring proper operation of the stripline in feeding RF signals
to the antenna elements 3.
[0036] The antenna elements 3 are arranged to protrude from beyond the front surface of
the sub-array 1.
[0037] In order to create an antenna array 10 for use in a Radar system, a plurality of
individual sub-arrays 1 are coupled together, as shown in Figure 4. In this way, the
lower ground plane 4 of a first sub-array, when placed atop another sub-array, completes
the stripline circuit, by enclosing the stripline 7 between two ground planes.
[0038] In order to complete the stripline circuit for the uppermost sub-array, a ground
plane 4 is affixed atop the dielectric foam 6. A further layer of structural foam
5 may be provided at the very top of the array to protect the stripline 7 disposed
within the uppermost sub-array.
[0039] Once the required number of sub-arrays have been assembled, as shown in Figure 4,
with an adhesive film being used to couple the various layers together, the entire
assembly is cured to form a single unit which is then treated as a single unitary
part, since it may not be disassembled without damaging the components contained therein.
[0040] The curing process involves placing the complete array assembly in an oven at 80°C.
Thermocouples may be provided at various points of the array to ensure that the core
temperature is maintained at the correct level. Then the array is allowed to cool,
during which time it is found that the height of the array assembly reduces by a few
millimetres, typically. However, after about 2 weeks, the height is recovered.
[0041] The selected adhesive film having 100g per square metre weight profile ensures that
the amount of adhesive in the assembly is a known controlled quantity and allows the
stripline and ground plane 4 to interact correctly.
[0042] The number of sub-arrays 1 required to form the antenna array 10 is determined by
the performance requirements of the finished antenna array. Using beam-forming techniques,
which are know in the field of Radar design, the beams formed by the respective sub-arrays
1 can be made to co-operate to give a desired performance. If a lesser degree of performance
is required, then fewer sub-arrays can be included in the antenna array. Therefore,
the modular design approach employed herein lends itself well to flexible design methodologies,
where overall system requirements can be altered relatively straightforwardly.
[0043] Figure 5 shows how the channels formed in the dielectric foam permit a cooling to
be propelled through said channels for the purposes of cooling the stripline and radiating
elements (not shown in Figure 5, for clarity). Cooled air is the preferred cooling
fluid and it is injected into the sub array in the vicinity of the connector 2. The
cooled air flows through the channels in which the stripline 7 is housed, and exits
the sub-array in the vicinity of the radiating elements 3, having cooled the parts
it has contacted along its way. The now warmer air is expelled from the antenna housing
in a continuous flow.
[0044] The buttons 8 which support the stripline and maintain its position between the upper
and lower ground planes are dimensioned to ensure that air can pass through the channels
relatively unimpeded. Given the branching nature of the channels, cooling fluid injected
at a common point, flows along each channel and cools all parts of the antenna array.
The cooling fluid essentially follows the same path as the stripline 7.
[0045] By use of the materials and construction techniques disclosed herein, antenna arrays
of significantly lower mass than prior art antennas can be constructed. Furthermore,
by making use of a plurality of identical sub-arrays, different overall antenna characteristics
and specification can be achieved, without re-designing the entire antenna. Instead,
the desired performance may be achieved by use of an appropriate number of sub-arrays.
[0046] Embodiments of the present invention are able to meet stringent weight requirements
by use of composite manufacturing techniques, which are believed not to have been
used in antenna manufacture before.
[0047] There are no mechanical fixings used in the entire completed array structure, which
helps to keep the weight down and reduces possible points of failure. Indeed, the
competed array is maintenance free and is considered as a single unit once the manufacturing
process is complete.
[0048] Attention is directed to all papers and documents which are filed concurrently with
or previous to this specification in connection with this application and which are
open to public inspection with this specification, and the contents of all such papers
and documents are incorporated herein by reference.
[0049] All of the features disclosed in this specification (including any accompanying claims,
abstract and drawings), and/or all of the steps of any method or process so disclosed,
may be combined in any combination, except combinations where at least some of such
features and/or steps are mutually exclusive.
[0050] Each feature disclosed in this specification (including any accompanying claims,
abstract and drawings) may be replaced by alternative features serving the same, equivalent
or similar purpose, unless expressly stated otherwise. Thus, unless expressly stated
otherwise, each feature disclosed is one example only of a generic series of equivalent
or similar features.
[0051] The invention is not restricted to the details of the foregoing embodiment(s). The
invention extends to any novel one, or any novel combination, of the features disclosed
in this specification (including any accompanying claims, abstract and drawings),
or to any novel one, or any novel combination, of the steps of any method or process
so disclosed.
1. An antenna sub-array for use in an antenna array comprising a plurality of such sub-arrays,
comprising:
a stripline for signal distribution, the stripline defining a plurality of signal
pathways from a common feed point to a plurality of radiating elements, wherein
the stripline is housed in a first support structure located a distance away from
a first surface of a ground plane structure.
2. The antenna sub-array as claimed in claim 1 wherein the first support structure comprises
a foam material having predefined dielectric properties.
3. The sub-array as claimed in claim 2 wherein the predefined dielectric properties include
having a dielectric constant substantially equal to that of air.
4. The sub-array as claimed in any preceding claim wherein the stripline is located in
a channel in the first support structure and held in position above the first surface
of the ground plane structure by a button formed from the same material as the first
support structure.
5. The sub-array as claimed in any preceding claim wherein, affixed to a second surface
of the ground plane structure is a second support structure.
6. The sub-array as claimed in claim 5 wherein the first and second support structures
are different materials.
7. The sub-array as claimed in any preceding claim wherein the stripline and the radiating
elements are integrally formed.
8. The sub-array as claimed in any preceding claim wherein the first support structure
comprises a plurality of channels arranged to receive a cooling fluid for cooling
the stripline and radiating elements.
9. An antenna array comprising a plurality of sub-arrays, each according to a preceding
claim.
10. A method of manufacturing an antenna array, comprising the steps of:
providing a plurality of sub-arrays, each according to any one of claims 1 to 8;
assembling the plurality of sub-arrays in a layered arrangement and securing each
sub-array to a neighbouring sub-array with an adhesive substance; and
curing said adhesive to form a unitary antenna array.
11. A method of cooling an antenna sub-array, according to any one of claims 1 to 8, comprising
the steps of:
providing a channel in a portion of the sub-array, said channel housing at least one
Radio Frequency component; and
forcing a cooling fluid into the channel via a first aperture, such that the cooling
fluid passes through the channel and is exhausted at a second aperture.
12. The method of claim 12 wherein the first aperture is proximal to a Radio Frequency
connector of the sub-array.
13. The method of claim 11 or 12 wherein the second aperture is proximal to one or more
of the plurality of radiating elements.
14. The method of claim 11, 12 or 13 wherein the channel is provided in the first support
structure, which houses the stripline.