The present disclosure relates to systems for receiving and transmitting signals, and in particular to an electrically small low profile antenna and methods for producing same.
Low profile sensor nodes are useful in many applications, including structural health monitoring and diagnostic testing. With regard to structural health monitoring, low profile antennas in sensor nodes can gather information about an aircraft in real-time, including airframe characteristics (e.g., hoop stress, shear stress, compression, corrosion resistance, bending, torsion, crack growth, high local loads, longitudinal stress and impacts). With regard to diagnostic testing, low profile antennas in sensor nodes can be used for worker safety and aircraft condition monitoring on the factory floor.
Unmanned aerial vehicles (UAVs) typically need light weight antennas with low radar cross sections and low air drag for improved efficiency. Also, like other aircraft, UAV surfaces are typically either metallic or a carbon fiber material, which are conductive in nature and may change the behavior of an antenna.
Existing planar antennas including co-planar microstrip feed and pin feed antennas are inherently bandwidth-limited due to their resonant nature. Furthermore, patch antennas based on existing dielectric materials have very small bandwidths at lower frequencies (i.e., <900 MHz) making them undesirable for low frequency applications. due to existing dielectric materials limit the operating frequencies of patch antennas. What is needed is a low profile antenna with enhanced bandwidth characteristics. There is also a need for low profile antennas with reduced size and weight to permit their installation in a greater number of candidate locations and applications.
To address the requirements described above, this document discloses an electrically small antenna and a method for producing same. One embodiment is evidenced by a low profile antenna, comprising: circuit board that has a composite laminate, formed of a magnetic material. The composite laminate has at least one antenna element disposed on a top surface of the composite laminate, a conductive ground plane disposed on a bottom surface of the composite laminate, and a conductor, extending through the composite laminate between the top surface and the bottom surface of the composite laminate, the conductor forming a microstrip feed extending from an antenna input to the antenna element.
In one embodiment the at least one antenna element comprises an antenna element portion and a slot; and at least a portion of the microstrip feed is disposed within the composite laminate between the slot and the bottom surface conductive ground plane. In another embodiment, the top surface comprises an array of a plurality of antenna elements, each comprising an associated slot, and at least a portion of the microstrip feed is disposed within the composite laminate between each of the array of the plurality of antenna elements and the bottom surface conductive ground plane. In a still further embodiment, the conductor further forms one or more power dividers disposed between the at least a portion of the microstrip feed disposed under each of the array of the plurality of antenna elements. In any of the foregoing embodiments, the composite laminate may have a thickness of, for example, 500 mil (0.5 inches) and the magnetic material a relative permittivity of, for example, 37-38.
Another embodiment is evidenced by a method of forming a low profile antenna, comprising: disposing at least one conductive antenna element on a top surface of a first magnetic layer, disposing a conductor on a top surface of a second magnetic layer or a bottom surface of the first magnetic layer, laminating the first magnetic layer and the second magnetic layer. Upon lamination, the conductor extends from an antenna input to under the conductive antenna element; and at least a portion of the conductor forms a microstrip between the second magnetic layer and the bottom surface conductive ground plane. Still another embodiment is evidence by a low profile antenna, formed by the method steps described above.
Referring now to the drawings in which like reference numbers represent corresponding parts throughout:
In the following description, reference is made to the accompanying drawings which form a part hereof, and which is shown, by way of illustration, several embodiments. It is understood that other embodiments may be utilized, and structural changes may be made without departing from the scope of the present disclosure.
In this disclosure, a bandwidth-enhanced low profile antenna is presented. Bandwidth is enhanced by using an aperture coupled antenna element with an inclusive slot, microstrip feed network, and lower ground plane. The antenna element and lower ground plane enclose a magnetic medium. The inclusive slot decreases the axial ratio and increases the circular polarization bandwidth, which is desirable for lower power loss due to misalignment between transmitter and receiver antennas. The lower ground plane minimizes any change in the antenna's electrical behavior due to the presence of conductive surfaces; better known as “surface agnostic” behavior.
The antenna comprises a number of features which can be characterized by a number of embodiments. Such features may also be combined in selected embodiments as disclosed further herein. One feature is that the antenna has an embedded RF microstrip network electrically coupled to a lower ground plane for efficient signal propagation and simplification of planar arraying. Another feature is that the antenna has a lower ground plane to minimize any change in the antenna's electrical behavior due to conductive surfaces. Still another feature is that the antenna uses aperture coupled antenna elements for simplistic feeding, planar arraying, reduction of antenna failure due to flexure, and simplified fabrication. A further feature is that the antenna utilizes a low-loss magnetic medium that results in an electrically small antenna (i.e., antenna wavelength in magnetic medium much shorter than equivalent wavelength in free-space) with high impedance bandwidth. A still further feature is that the antenna can utilize thin RF dielectrics for low profile applications due to the use of an aperture coupled feed. Still another feature is that the antenna is circularly polarized with increased bandwidth by using aperture coupled antenna elements with inclusive slots to lower power loss due to misalignment between transmitter and receiver antennas.
A finite element model analysis of this 2×2 array designed to operate near 350 MHz with an antenna element 106 diameter of 80 mm and two layers of 250 mil thick MAGTREX 555 provides an antenna gain of −3.5 dBi and an electrical impedance bandwidth of 120 MHz or 34%, and weighs only about 7.1 lbs. For comparison, a DPV-95 dipole antenna operating 225 to 400 MHz has a length of 177 in., 0 dBi gain, and antenna weight of −37.5 lbs. Although the foregoing illustrates a 2×2 array, the array may be non-square and may have a greater or lesser number of antenna elements 106.
Similarly, a 2×2 array such as that illustrated in
Turning now to
In block 304, a conductor 116 is disposed on a top surface of a second magnetic layer 103B, or alternatively, on a bottom surface of the first magnetic layer 103A. This is illustrated in
In block 306, the first magnetic layer 103A and the second magnetic layer 103B are laminated. Upon lamination, the conductor 116 extends from an antenna input to a location under the conductive antenna element 106 and at least a portion of the conductor 116 forms a microstrip with the second magnetic layer 103B and the bottom surface conductive ground plane 107. This is shown in
The foregoing steps illustrate the creation of one antenna element 106 on the RF circuit board 101. In other embodiments, the antenna 100 comprises an array of antenna elements 106 such as the 2×2 array of antenna elements illustrated in
Furthermore, in any combination or all of the foregoing operations, the disposition of conductive material on the magnetic layers 103A and 103B may be accomplished by additive methods such as printing or film deposition of suitable conductive materials (e.g., silver, copper, etc.) to the appropriate surface of the dielectric. Deposition of conductive material may also be accomplished by combined additive and subtractive methods such as laser etching, milling, or wet etching. Hence, the conductive materials may be deposited on the entire surface of the magnetic layer(s) and unwanted portions etched away. For example, the top of the first magnetic layer 103A may be formed by disposing a conductive material along the entire top surface, then etching or otherwise removing the conductive material from the slot 106B and the area surrounding the conductive antenna element portion 106A.
The lamination of the first magnetic layer 103A and the second magnetic layer 103B, can be accomplished by disposing an adhesive film 524 between the first magnetic layer 103A and the second magnetic layer 103B. Should portions of the adhesive film 524 be removed to achieve the structure shown in
The foregoing antenna 100 can be used to transmit and/or receive (transceive) signals. In transmission, signals provided to the feed created by conductor 116 are transformed into a transmitted RF signal by antenna elements 106 and associated structures. In reception, RF signals are provided to the antenna elements 106 and associated structures and transformed into a received signal at the conductor 116. For example, referring again to
Generally, the computer 802 operates under control of an operating system 808 stored in the memory 806, and interfaces with the user to accept inputs and commands and to present results through a graphical user interface (GUI) module 818A. Although the GUI module 818B is depicted as a separate module, the instructions performing the GUI functions can be resident or distributed in the operating system 808, the computer program 810, or implemented with special purpose memory and processors. The computer 802 also implements a compiler 812 which allows an application program 810 written in a programming language such as COBOL, C++, FORTRAN, or other language to be translated into processor 804 readable code. After completion, the application 810 accesses and manipulates data stored in the memory 806 of the computer 802 using the relationships and logic that was generated using the compiler 812. The computer 802 also optionally comprises an external communication device such as a modem, satellite link, Ethernet card, or other device for communicating with other computers.
In one embodiment, instructions implementing the operating system 808, the computer program 810, and the compiler 812 are tangibly embodied in a computer-readable medium, e.g., data storage device 820, which could include one or more fixed or removable data storage devices, such as a zip drive, floppy disc drive 824, hard drive, CD-ROM drive, tape drive, etc. Further, the operating system 808 and the computer program 810 are comprised of instructions which, when read and executed by the computer 802, causes the computer 802 to perform the operations herein described. Computer program 810 and/or operating instructions may also be tangibly embodied in memory 806 and/or data communications devices 830, thereby making a computer program product or article of manufacture. As such, the terms “article of manufacture,” “program storage device” and “computer program product” as used herein are intended to encompass a computer program accessible from any computer readable device or media.
Those skilled in the art will recognize many modifications may be made to this configuration without departing from the scope of the present disclosure. For example, those skilled in the art will recognize that any combination of the above components, or any number of different components, peripherals, and other devices, may be used.
This concludes the description of the preferred embodiments of the present disclosure.
The foregoing description of the preferred embodiment has been presented for the purposes of illustration and description. It is not intended to be exhaustive or to limit the disclosure to the precise form disclosed. Many modifications and variations are possible in light of the above teaching. It is intended that the scope of rights be limited not by this detailed description, but rather by the claims appended hereto.
Number | Name | Date | Kind |
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4070676 | Sanford | Jan 1978 | A |
5001492 | Shapiro | Mar 1991 | A |
5400042 | Tulintseff | Mar 1995 | A |
5767808 | Robbins | Jun 1998 | A |
5914693 | Takei | Jun 1999 | A |
6384785 | Kamogawa | May 2002 | B1 |
20190312358 | Rogers | Oct 2019 | A1 |
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Number | Date | Country | |
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20200099122 A1 | Mar 2020 | US |