None.
The present invention relates to tunable antennas, and more particularly to a parallel plate antenna that is tunable.
U.S. Pat. No. 8,228,243 discloses a parallel plate antenna designed for use in a field-deployed shielded room. Specifically, the antenna is designed to determine a radio-frequency (RF) “leakiness” of a room. Such leakiness generally occurs at holes, ports, windows, etc., made in the walls or roof of the room. The disclosed antenna is placed in a room to be evaluated and measures RF energy associated with test pulses directed toward the room from a location outside the room.
The parallel plate antenna is compact and effective, but has a fixed resonant frequency thereby limiting the value of the antenna beyond specific applications.
Accordingly, it is an object of the present invention to provide a tunable antenna.
It is a further object of the present invention to provide a tunable parallel plate antenna.
In order to attain the objects of the present invention, a tunable antenna is provided which comprises a base and a support coupled to the base and extending perpendicular thereto. The antenna also comprises a hollow tube coupled to the base and extending perpendicular thereto. The support and hollow tube oppose one another and are spaced apart from one another.
The antenna also includes a plurality of plates spaced apart and parallel to one another. Each plate has a connected end and an unconnected end such that each plate is coupled only at the connected end to one of the supports and hollow tubes and extends out to the unconnected end thereof. One of the plates located furthest from the base extends past the hollow tube and is spaced apart therefrom.
A shaft has a first end coupled to the base, extends through the hollow tube and the one plate extending past the hollow tube such that the second end of the shaft is spaced apart from the one plate extending past the hollow tube. A tuning piston is coupled to the shaft and is adapted for movement along the shaft and within the hollow tube.
A tuning plate is coupled to the second end of the shaft. Each of the support, hollow tube, plates, shaft, tuning piston, and tuning plate are electrically conductive. The shaft, tuning piston, hollow tube, and tuning plate are also electrically coupled. The shaft is electrically isolated from the one plate extending past the hollow tube.
Other objects, features and advantages of the present invention will become apparent upon reference to the following description of the preferred embodiments and to the drawings, wherein corresponding reference characters indicate corresponding parts throughout the several views of the drawings and wherein:
Referring now to the drawings and more particularly to
Unless otherwise stated herein, the various parts of the antenna 10 need to be electrically conductive. Such electrical conductivity can be achieved by using solid metals for the various parts, metal-coated non-conductive substrates for the various parts, etc., without departing from the scope of the present invention.
The antenna 10 includes a base 20, a support 30 coupled to the base and extending perpendicularly therefrom. The antenna also includes a hollow tube 40 coupled to the base 20 and extending perpendicularly therefrom to an open end 42 and such that the support 30 and the hollow tube oppose one another in a spaced-apart fashion.
The antenna 10 also comprises a series of parallel plates 50 with each plate coupled to one of the supports 30 and with a hollow tube 40 extending perpendicularly away therefrom in a cantilevered fashion. That is, each plate 50 is connected on one end 50A thereof to the support 30 or the hollow tube 40 and is unconnected on another end 50B of the plate. Unless otherwise stated, the term “coupled” as used herein refers to mechanical and electrical coupling. It is to be understood that a variety of coupling or attachment schemes could be used without departing from the scope of the present invention.
The base 20 provides mechanical support for the support 30 and the hollow tube 40. Furthermore, the base 20 serves as an attachment point to an electrical ground plane (not shown) for the antenna 10. Each of the support 30 and the hollow tube 40 can have one or more plates 50 coupled thereto with the plates being alternately connected to the support or the hollow tube. The number of plates 50 shown in the figures is exemplary and is not to be considered as a limitation of the present invention. One of the plates 50 located closest to the base 20 defines a feed point 60 to which an antenna feed 62 is coupled. The antenna feed 62 can be conical (as shown), cylindrical, a plate, etc., without departing from the scope of the present invention.
The antenna 10 also includes a resonant frequency tuning mechanism that cooperates with the hollow tube 40 and one of the plates 50. More specifically, the plate 50 that is part of the tuning mechanism is located furthest from the base 20, and extends from the support 30 past the hollow tube 40 as the plate passes an open top 42 of the hollow tube in a spaced-apart fashion to define a gap region 70 defining the aperture of the antenna 10.
The tuning mechanism includes a shaft 80 supported on one end 80A thereof by the base 20 or another support mechanism (not shown) coupled to the base. A tuning piston 82 is coupled to the shaft 80 for movement within the hollow tube 40 while being electrically coupled to the hollow tube. A tuning plate 84 is coupled to the shaft 80 at an opposing end 80B.
The tuning mechanism operates to move the tuning piston 82 along the shaft 80 and in the hollow tube 40 as indicated by arrows 86A and 86B to tune the resonant frequency of the antenna 10 at the aperture 70. While a variety of tuning mechanism constructions can be used to generate and control movements in directions 86A and 86B, some non-limiting exemplary constructions will be described herein.
Referring now to
Referring additionally now to
By way of example, if the shaft 80 is a rotating shaft as indicated by a rotational arrow 81, the tuning plate 84 can be coupled to the shaft for rotation in correspondence therewith. In such a case, the tuning plate 84 also functions as a flywheel to maintain smooth rotational movement of the shaft 80 which, in turn, translates to smooth the movements 86A and 86B of the tuning piston 82.
As mentioned above, a variety of constructions can be used to bring about the movements 86A and 86B of the tuning piston 82. With reference to
The shapes of the plates 50 can all be rectangular as shown and described in the afore-mentioned U.S. Pat. No. 8,228,243. However, the present invention is not so limited. For example, the plates 50 between the base 20 and the one plate extending over the hollow tube 40 can be T-shaped as described in U.S. patent application Ser. No. 16/143,593, filed Sep. 27, 2018, the contents of which are incorporated herein by reference.
The ability to change the antenna's resonant frequency is now explained. The internal dimensions of the hollow tube 40, the shaft 80, and the tuning piston 82 are very small as compared to the operating wavelengths of the antenna 10 such that the tuning mechanism behaves as a lumped-element circuit.
To understand the behavior of the tuning mechanism behavior, one can temporarily ignore the elements of the tuning mechanism that are internal to the hollow tube 40. In this state, a complex admittance of value Y1 (Y1=G1+jB1) appears across the aperture 70.
The real part of the admittance (i.e., G1), called the conductance, is a function of antenna geometry and frequency and describes the conversion of stored energy in the parallel plate region into radiation across the aperture 70 and into the surrounding space. The imaginary part of the admittance (i.e., B1), also a function of geometry and frequency is called the susceptance. The susceptance describes the energy storage across the aperture 70. The admittance therefore describes, in total, the imperfect “leakiness” of energy from the parallel plate cavity and into space and is responsible for generating current flow on the external surface of the antenna 10 to thereby form the radiated field.
Adding back the elements of the tuning mechanism that are internal to the hollow tube 40 adds another admittance Y2 (Y2=G2+jB2) in parallel with the admittance Y1 to thereby yield a total admittance Yt across the aperture 70 that is the sum of admittances Y1 and Y2. The movement 86A or 86B of the tuning piston 82 changes the value of Y2, which when combined with Y1, causes a shift in resonant frequency of the antenna 10. The admittance Y2 of the tuning mechanism is formed by the electrostatic coupling to the uppermost plate 50 by means of the tuning plate 84.
The parallel plate region of the antenna 10 is a conveyor of radio-frequency power. In a transmission mode, the feed point 60 is energized with an alternating voltage and a propagating electromagnetic field is established in the region that is “leaked” across the aperture 70 (with an admittance Yt) to generate an external surface distribution of current that, in turn, generates a radiated field. The same action occurs in reception, but in reverse order. When the spacing of the parallel plates 50 is small compared to the operating wavelength; power transfer to and from the aperture 70 is efficient because the fields in the parallel plate region are highly confined.
Referring now to
The advantages of the present invention are numerous. The antenna 10 can be readily tuned to any resonant frequency in a design range of the antenna. Movement of the tuning piston 82 can be affected through a variety of manual, automated, and even remotely-controlled mechanisms.
It will be understood that many additional changes in the details, materials, steps and arrangement of parts, which have been herein described and illustrated in order to explain the nature of the invention, may be made by those skilled in the art within the principle and scope of the invention as expressed in the appended claims.
The foregoing description of the preferred embodiments of the invention has been presented for purposes of illustration and description only. It is not intended to be exhaustive nor to limit the invention to the precise form disclosed; and obviously many modifications and variations are possible in light of the above teaching. Such modifications and variations that may be apparent to a person skilled in the art are intended to be included within the scope of this invention as defined by the accompanying claims.
The invention described herein may be manufactured and used by or for the Government of the United States of America for governmental purposes without the payment of any royalties thereon or therefor.
Number | Name | Date | Kind |
---|---|---|---|
2660675 | Amen | Nov 1953 | A |
20120112977 | Yun | May 2012 | A1 |
20160020521 | Astakhov | Jan 2016 | A1 |