The concepts, systems, circuits, devices and techniques described herein relate generally to radio frequency (RF) circuits and more particularly to RF antennas.
As is known in the art, in array antennas, performance is often limited by the size and bandwidth limitations of the antenna elements which make up the array. Improving the bandwidth while maintaining a low profile enables array system performance to meet bandwidth and scan requirements of next generation of communication applications, such as software defined or cognitive radio. These applications also frequently require antenna elements that can support either dual linear or circular polarizations.
As is also known, attempts have been made to fabricate low profile antenna elements and array antennas. Such array antennas include an array of tightly coupled dipole elements which approximates the performance of an ideal current sheet, as well as so-called “bunny ear” antennas, and tightly coupled patch arrays. While these antenna element designs are all low profile, they either fail to operate over a desired bandwidth or present significantly increased complexities to provide feed structures necessary to support either dual linear or circular polarizations (e.g. requiring external components difficult to fit within the unit cell of an array antenna). Other antenna elements, such as Vivaldi notch antenna elements, can provide a relatively wide bandwidth, but are not low profile.
It would, therefore, be desirable to provide an antenna element and an array antenna having a relatively low profile and which is responsive to either dual linear or circular polarization over a wide frequency bandwidth and scan volume.
Described herein is an antenna element having an integrated balun/feed assembly. The antenna element may also be provided having an integrated balun/feed and radome (the combination of which is referred to herein as a radiating element). Such an antenna element and/or radiating element is suitable for use in wideband (WB) or ultra wideband (UWB) phased array antenna applications. Such an antenna element and array of such antenna elements may be suitable for use in applications and designs requiring fractional bandwidths of greater than 3:1 and that would benefit from not having an explicit (separate) balun in the feed structure. The antenna element with integrated balun/feed and radome is suitable for use in applications requiring a low antenna profile (i.e. a combined antenna element and radome assembly having a reduced height).
Such an antenna element and antenna array is suitable for use in applications where performance improvements, including volumetric improvements and installation height reductions, may be desired.
In accordance with the concepts, systems and circuits described herein, a dual polarization current loop radiator includes a metal patch radiator in a phased array Dielectrically spaced from a shaped metal tower which is conductively attached to a Metal backplane. The backplane provides a groundplane for the radiating element. A pair of feed circuits, each comprised of a vertical conductor and a feed line, are coupled to the patch radiator. The dual polarization current loop radiator is responsive to RF signals within a frequency band of interest through two different coupling mechanisms as follows. RF signals coupled or otherwise provided to the feed circuits are coupled in the desired radiating mode. The feed circuits (i.e. the feed lines and vertical conductors) guide current to feed points by guiding them along the sidewalls of the shaped metal tower. At lower frequencies within the band of interest, RF signals are coupled (i.e. either received by or emitted by) from the feed points to the patch element. At higher frequencies within a band of interest, RF signals are coupled from the feed points into the desired radiating mode via a guided path slotline mode formed within the current loop radiator structure between the feed circuit and the vertical wall of the shaped metal tower. Thus, the radiator supports two radiation mechanisms: a first radiation mechanism due to the patch element and a second radiation mechanism due to the guided path. The two radiation mechanisms are seamless (i.e. there is a seamless transition between these two different types of radiation) which leads to a significant increase in operational bandwidth and scan of the radiator.
With this particular arrangement, a compact patch radiator suitable for use in a phased array antenna is provided.
A plurality of antenna elements provided in accordance with the concepts and structures described herein results in an array antenna operable over a wide bandwidth and scan volume while maintaining a relatively low profile. In one embodiment, an array antenna provided in accordance with the concepts and structures described herein provides broadside performance over a frequency range of about 2.4 GHz to about 17.6 GHz at a height (or profile, including all radome and balun spacings and components) of about one inch above the metal backplane.
The height (or profile) for such a complete radiator/radome/balun combination is relatively low compared with the profile of prior art antenna elements and array antennas having similar operating characteristics.
In accordance with the concepts described herein, for applications requiring less bandwidth, the antenna height may be reduced to less than one inch. For example, n an antenna having a bandwidth from 2.4-17.6 GHz (i.e. a fractional 7.33:1 bandwidth) if it is desired to operate, for example in the frequency range of about 6 GHz to about 17.6 GHz, the antenna could be provided having a height approximately or about 0.4″. If, however, it was desired to only operate in the range of about 12 GHz to about 18 GHz, the antenna could be provided having a height of about 0.2″. These examples assume the scan performance required remains the same. If the scan angles required are reduced, the height can be reduced further. Furthermore, the scan performance degrades gracefully providing performance out to 70 degrees in both E- and H-planes. The antenna element described herein also provides good isolation and cross-polarization performance over scan.
It should be appreciated that this Summary is provided to introduce a selection of concepts in a simplified form that are further described below in the Detailed Description. This Summary is not intended to identify key features or essential features of the claimed subject matter, nor is it intended to be used to limit the scope of the claimed subject matter.
The foregoing and other objects, features and advantages of the Invention will be apparent from the following description of particular embodiments of the invention, as illustrated in the accompanying drawings in which like reference characters refer to the same parts throughout the different views. The drawings are not necessarily to scale, emphasis instead being placed upon illustrating the principles of the invention.
Described herein are structures and techniques for exciting and propagating electromagnetic waves in wave guiding structures. As used herein, the term “vertical plane” refers to a plane which extends along a length of the wave guiding structure and the term “horizontal plane ” refers to a plane which is perpendicular to the vertical plane.
Referring now to
In the exemplary embodiment of
Unit cell 12 has disposed across one end 12a thereof a backplane 14 which serves as a ground plane while a second end 12b of unit cell 12 is open.
A first conductor 16 having a width W1, a height H1 and a length L1 is disposed in a first vertical plane within unit cell 12. Since conductor 18 is disposed in a vertical plane, first conductor 16 is sometimes referred to as first vertical conductor 16 (or more simply “vertical conductor 18” or “vertical wall 18”). Vertical conductor 16 is electrically coupled to backplane 14. In one embodiment, this is accomplished by placing at least a portion of (e.g. one end of) vertical conductor 18 in physical contact with at least a portion of backplane 14 (e.g. using a ribbon conductor to provide an electrical connection between backplane 14 with vertical conductor 18.
The placement of the vertical walls 16, 16a are controlled by two factors. The first factor is the desire to maximize the bandwidth performances of the balun, particularly at the low frequencies. This is normally done by maximizing the volume between the inside walls of the shaped metal toward and the feed circuit. For this reason, it is desirable for the walls of the shaped metal tower to be thin. The second factor is controlling the impedance of the guided transmission structure formed by the feed circuit and the vertical walls of the shaped metal tower. To maintain a suitable impedance, it is generally desirable for the feed circuit and the vertical wall to be proximate to each other. This proximity also aids in improving isolation and cross-polarization performance.
It should be appreciated that vertical conductor 18 may be provided using a variety of different techniques. For example, vertical conductor 16 may be stamped and attached (e.g. bonded) to backplane 14 (e.g. via an automated pick and place operation). Alternatively, vertical conductor 16 may be formed or otherwise provided as part of backplane 14. Other techniques for providing vertical conductor 16 may, of course, also be used.
A first feed signal path 18(or more simply “feed line 18”) is electrically coupled to vertical conductor 16. The combination of feed line 18 and vertical conductor 16 forms a feed circuit 19. In the exemplary embodiment of
It should be appreciated that although in the exemplary embodiment of
In the exemplary embodiment illustrated in
A horizontal substrate 30 having a metal plate structure 32 provided as part thereof is disposed across the vertical metal structure and spaced apart from, but capacitively coupled to the vertical metal structure 16. Metal plate structure 32 operates as a patch antenna element and contacts feed point 24 of feed circuit 19. In one embodiment, horizontal substrate 30 is provided from a dielectric material having a conductive material disposed on first and second opposing surfaces thereof. In one embodiment, the conductive material on the opposing surfaces of dielectric substrate are electrically coupled by one or more conductive via holes which extend through substrate to electrically couple the conductors disposed on the first and second opposing surfaces of substrate 30. The effective thickness of metal plate 32 is important and can be determined empirically (e.g. determined by iteration), but typically is thickened to improve antenna performance at the lower frequencies within the operational bandwidth of interest.
A top edge of vertical conductor 16 is spaced apart from horizontal conductor 30. The space between the top of vertical conductor 16 and horizontal conductor 30 may either be air-filled or filled with a dielectric material or a non-conductive adhesive material. The purpose of the spacing is so the patch is not shorted to the shaped metal tower. The patch characteristics are sensitive to this distance. Decreasing the distance will increase the capacitance. The distance is chosen as part of the design, which is iterated to find the optimal capacitance value for meeting performance requirements. In one embodiment, the spacing is accomplished using a dielectric spacer 32 having a thickness typically on the order of a few mils. In one exemplary embodiment, dielectric spacer 32 is provided as a dielectric material of the type manufactured by Rogers Corporation and identified as RO4350 having a thickness of about 0.01 inch and having a relative dielectric constant of about 3.66.
As noted above, patch element 32 may be formed on substrate 30 using additive or subtractive techniques as is generally known. For example conductors 32a, 32b may be provided n the substrate 30 by patterning copper patches 32a, 32b on opposing surfaces of substrate 30 and then providing one or more plated through holes generally denoted 34 through the conductors 32a, 32b to provide the effect of a thick metal conductor through substrate 30. Also, electrically coupled to patch element 32 are feed circuit elements 34 and 26 which feed patch 32 described above.
Radiator 10 is responsive to RF signals within a frequency band of interest. through two different coupling mechanisms as follows. RF signals coupled or otherwise provided to the exposed end 17 (
The above described feed circuit 19 may be used to couple an RF signal having a single linear polarization to/from radiator 10.
The exemplary radiator 8 in
As mentioned above, radome 11 is disposed within unit cell 12 over antenna element 10. Radome 11 is provided form a plurality of substrates 38 and 44. In this exemplary embodiment, radome 11 protects antenna element 10 (e.g. from exposure to environmental forces—e.g. wind, rain, etc. . . . ) and also performs an impedance matching function to match the antenna element impedance to free space impedance. Thus, in this exemplary embodiment, the physical and electrical characteristics of the components which make up both antenna element 10 and radome 11 are selected to cooperate in providing radiator 8 having a desired impedance match for RF signals received by and transmitted thereto.
In the exemplary embodiment of
Also, although three layers are shown, those of ordinary skill in the art will appreciate that pixilated assembly 38 may include fewer or greater than three layers The number of layers is a function of performance needs of bandwidth and scan requirements and allowable construction complexity. It could be any number from one layer to dozens of layers. More layers allows for more fine tuning of performance, but at the cost of increased sensitivity to tolerance and complexity of build. In many practical applications, a number of layers in the range of one to five (1-5) will result in an antenna having acceptable performance characteristics.
In one embodiment, pixilated assembly 38 is spaced from surface 32a of a substrate 32 by an air or foam layer 46 having a relative dielectric constant of about 1.0 having a thickness of about 0.05″. Layer 40 of pixilated assembly 38 is provided from a dielectric having relative dielectric constant of about 6.15 and a thickness of about 0.05″. In one particular embodiment, layer 40 may be provided from commercially available material such as RO4360 manufactured by Rogers Corporation. Layer 41 may be provided as air or from a foam substrate having a relative dielectric constant of about 1.0 and having a thickness of about 0.21″. Layer 42 may be provided from a material having a relative dielectric constant of about 2.33 and a thickness of about 0.06″. Layer 42 may be provided, for example, as Arion Clad233 having all copper removed.
Substrate 44 may be provided from a Ce/Quartz material having a relative dielectric constant of about 3.2 and having a thickness of about 0.015″. A bottom surface 44a of a substrate 44 is spaced from a top surface 42a of a substrate 42 by a region 48 having a thickness of about 0.333″. Region 48 may be air filled or may be provided from a foam material having a relative dielectric constant of about 1.0.
As mentioned above, the specific dimensions, dielectric constants and other characteristics mentioned above are exemplary only for operation in a frequency range of about 2.4 to 17.6 GHz. After reading the disclosure herein, those of ordinary skill in the art will understand how to adjust dimensions, dielectric constants and other characteristics of the structures described herein for operation within other frequency ranges.
Referring now to
It should also be appreciated that the holes sizes and patterns of each layer in assembly 38′ need not be the same (i.e. each layer in assembly 38′ may be provided having a unique hole pattern and unique holes sizes. Furthermore, the diameters of each hole on the same layer need not be the same. Different hole size are allowed both layer to layer and within the layer.
Referring now to
Referring now to
Referring now to
Referring now to
Referring now to
while particular embodiments of the present invention have been shown and described, it will be apparent to those skilled in the art that various changes and modifications in form and details may be made therein without departing from the spirit and scope of the invention as defined by the following claims. Accordingly, the appended claims encompass within their scope all such changes and modifications.