The present invention relates generally to antennas, and more particularly but not exclusively to multiband antennas structured as a three dimensional solid having a plurality of radiating cavities disposed therein.
A variety of applications exist with a need to feed a single reflector antenna to operate across multiple sub-bands disposed within a bandwidth. Typically such sub-bands are relatively narrowband. For example, many NASA airborne and space science applications have to support multiple electromagnetic sensor instruments that operate through the same shared reflector apertures. The applications may involve, but are not limited to measurements of aerosols, clouds, precipitation, snow water equivalent and wind velocities. Such instruments can include radiometers, active radar devices and scatterometers, and even can be combined with a communication link. Alternatively, the same aperture sharing approach can be used for multiband communication and so on.
Feeds of shared reflectors can be made using a number of horn antennas, viz. one horn for each sub-band. However, only one horn can be in the reflector focus for optimal illumination of the reflector surface. The remaining horns will be off focus and, thus, cannot provide optimal illumination of the reflector surface. Furthermore, the remaining horns may introduce blockage of the reflector. Alternatively, antennas comprising stacked patches using multi-layer circuit boards may also be designed to perform similar functions as reflector feeds; however, the phase center normal to the patch surfaces of such antennas differ depending on which patch is radiating, which may change depending on the frequency bands of operation. The proposed antenna does not suffer from such detuning of the reflector antenna optics over frequency.
Another approach is to employ a broadband array that allows operation on multiple sub-bands with an optimal reflector excitation, because the array feed can be installed in the focus. However, using a broadband array to feed a reflector is not straightforward, because such arrays can operate truly in broadband mode only if they are (1) electrically large and (2) fully excited. A typical array used to feed reflectors can be small to avoid blockage of the reflector. At the same time, small arrays may suffer from edge truncation and severe impedance mismatching. Another factor degrading impedance matching of feed arrays is fragmented excitation, when only a part of array is selectively used to drive particular bands of interest and, thus, those arrays are not fully excited.
In one of its aspects, the present invention provides a multiband antenna in which at least two cavities are present, each dimensioned and configured differently according to the operational wavelength at which the respective cavity is to operate. A first, inner cavity may operate at a first, relatively-higher frequency, while a second cavity may operate at a relatively lower frequency. Each cavity may be excited by two probes from opposite locations which may be differentially fed by a network of feedlines. The feedline network may be provided in a metal base of the multiband feed and may include vertical and horizontal feed network distribution sections. Each cavity may include its own feed network routed inside the body of the antenna. The feedline for each cavity may start at the bottom of the feed structure where, for example, a connector can be placed. The feedline may ascend vertically and then split into two differentially-fed branches using an integrated narrow-band balun or other power divider circuit. Each differentially-fed branch may be routed through several vertical-horizontal paths until reaching a designated cavity, where it may terminate in an open cavity section to excite the cavity.
For example, in one exemplary configuration, the present invention may provide a multiband antenna for operation at two or more selected wavelengths. The multiband antenna may include a first cavity having first sidewalls disposed within the antenna. The first sidewalls may extend upward from the interior of the antenna to an upper surface of the antenna such that the first sidewalls provide a first aperture in the upper surface having an annular shape. A second cavity having second sidewalls may be disposed within the antenna, and the second sidewalls may extend upward from the interior of the antenna to the upper surface of the antenna such that the second sidewalls provide a second aperture in the upper surface having an annular shape. The second aperture may be disposed internally to the first aperture within the upper surface. A first pair of excitation probes may be disposed within the first cavity to drive the cavity. The first pair of excitation probes may each have a length associated therewith, and the difference between the lengths of the probes of the first pair may be one half of a selected operational wavelength. In addition, a second pair of excitation probes may be disposed within the second cavity. The second pair of excitation probes may each have a length associated therewith, and the difference between the lengths of the probes of the second pair may be one half of a second selected operational wavelength. The first cavity may extend from the upper surface into the antenna to a depth which is greater than that of the second cavity.
In a second exemplary configuration, the present invention may provide a multiband antenna for operation at two or more selected wavelengths having a first pair of cavities. The first pair of cavities may include first sidewalls disposed within the antenna, with the first sidewalls extending upward from the interior of the antenna to an upper surface of the antenna such that the first sidewalls provide a first pair of apertures having a rectangular shape in the upper surface. The antenna may also include a second pair of cavities each having second sidewalls disposed within the antenna, with the second sidewalls extending upward from the interior of the antenna to the upper surface of the antenna such that the second sidewalls provide a second pair of apertures having a rectangular shape in the upper surface. The first and second pairs of apertures may each disposed symmetrically on opposing sides of a central line disposed parallel to the longitudinal axes of the apertures, and the antenna may include a first pair of excitation probes disposed within the first pair of cavities.
The foregoing summary and the following detailed description of exemplary embodiments of the present invention may be further understood when read in conjunction with the appended drawings, in which:
In one of its aspects, multiband antennas of the present invention may be operable at two or more wavelengths simultaneously by providing a separate radiating cavity for each band at which the antenna is to function. The cavities may be formed in an electrically conductive, e.g., metal base, which may be created by an additive build process, such as that described in U.S. Pat. Nos. 7,012,489, 7,649,432, 7,948,335, 7,148,772, 7,405,638, 7,656,256, 7,755,174, 7,898,356, 8,031,037, 2008/0199656, 2011/0123783, 2010/0296252, 2011/0273241, 2011/0181376, 2011/0210807, the contents of which are incorporated herein by reference.
Each cavity may be dimensioned and configured with regard to the particular operational wavelength the cavity is designed to support. Thus, in a multiband antenna at least two cavities are present, each dimensioned and configured differently according to the operational wavelength at which the respective cavity is to operate. For example, a first cavity of first dimensions may operate at a first frequency, while a second cavity having relatively larger dimensions may operate at a relatively lower frequency (longer wavelength). Each cavity may be excited by two probes from opposite locations which may be differentially fed. It should be appreciated, that while antennas of the present invention may be described as operating in a transmitting/radiating mode, the multiband antennas of the present invention may also operate in a reception mode to receive electromagnetic radiation. Moreover, some cavities may be operating in a radiating mode while others are operating in a reception mode.
Referring now to the figures, wherein like elements are numbered alike throughout.
Additionally, aperture 150 may have a circular or elliptical shape or the annular slots may be meandered in the plane of 122 to increase its electrical length and give more control over operational bands. The aperture dimensions “a” and “b” may desirably be in the range of a fraction of an operational wavelength at which the cavity 140 is designed to operate, to help deter higher order coaxial modes. The gap may desirably be very small; for example, “g” may be 1/10 to 1/100 of the operational wavelength. In addition, the aperture 150 may be offset from an edge of the antenna 100 by a distance “c”. In addition, just as it may be desirable to have the aperture dimensions “a” and “b” be different, it may also be desirable to have a different set of offsets “c” and “d” from the edge of the antenna. Alternatively, the co-located annular slots may be mounted on a larger body such as a vehicular platform or in an environment that closely approximates an infinite ground plane in antenna parlance.
The cavity 140 may be driven by first and second excitation probes 112, 114 which may be disposed at opposing locations within the cavity 140. (The probes 112, 114 may alternatively operate as receivers rather than transmitters.) The excitation probes 112, 114 may be fed by a common feedline 110 in a “T” configuration. The excitation probes 112, 114 and feedline 110 may extend through the volume of the antenna 100 and island 146 in the form of coaxial transmission lines. Other types of transmission lines, such as a stripline in a printed circuit board may be used. In addition, the excitation probes 112, 114 may desirably differ in length by one half of the operational wavelength; that is, there may be an electrical length difference of pi (180°) between the probes 112, 114. In particular, the dimensions “LL” and “LR” may differ by half of the operational wavelength to differentially drive the cavity 140. Alternatively, this phase difference may be created using 180-degree hybrids (e.g., a rat-race hybrid), by using a balun (e.g., a Marchand balun) or by feeding one of the two excitation probes from the exterior side wall, 123, to interior side wall, 122, rather than what is shown. The cavity depth “CD” may desirably be approximately one quarter of the operational wavelength and may be meandered as shown in
Turning then to multiband antennas in accordance with the present invention,
The apertures 250, 252, 254 may have a generally square or rectangular shape and may have a gap width labeled “g”. Alternatively, the apertures 250, 252, 254 may have any shape suitable for radiating or receiving electromagnetic radiation at a desired operational wavelength, such as circular or meandered. Dimensions may be set as exemplified with the single-band antenna 100 of
The cavities 240, 242, 244 may be driven by respective pairs of excitation probes 211/212, 214/215, 217/218, a given pair of which may be disposed on opposing locations within the respective cavity 240, 242, 244. (The probes 211/212, 214/215, 217/218 may alternatively operate as receivers rather than transmitters.) Each probe pair 211/212, 214/215, 217/218 may be fed by a respective feedline 210, 213, 216 in a “T” configuration,
These and other advantages of the present invention will be apparent to those skilled in the art from the foregoing specification. Accordingly, it will be recognized by those skilled in the art that changes or modifications may be made to the above-described embodiments without departing from the broad inventive concepts of the invention. It should therefore be understood that this invention is not limited to the particular embodiments described herein, but is intended to include all changes and modifications that are within the scope and spirit of the invention as set forth in the claims.
This application claims the benefit of priority of U.S. Provisional Application No. 62/268,054, filed on Dec. 16, 2015, the entire contents of which application(s) are incorporated herein by reference.
This invention was made with government support under contract #NNX15CP66P awarded by National Aeronautics and Space Administration (NASA). The government has certain rights in the invention.
Number | Date | Country | |
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62268054 | Dec 2015 | US |