A patch antenna is often utilized as a low-profile and low-cost multi-constellation global navigation satellite system (GNSS) antenna due to its planar configuration and ease of integration with circuit boards. To shrink the size of the antenna, it is well known in the art to use ceramic material as the substrate. Typical considerations of using ceramics are its high DK (ε′, dielectric constant) and low dielectric loss. Depending on the compounds and composites, the DK of the ceramics can vary from the range of approximately 4 to several hundred. To cover the dual-band requirements of a typical GNSS system, two or more stacked patches are required to resonate at each frequency. For circular patches, the fundamental mode of operation is TM11 mode, which has an upper-hemisphere radiation pattern that works well for GNSS applications. Using the well known cavity model, the fundamental mode's resonance frequency is given by
where χ11 represents the first zero of the derivative of the Bessel function, J1′(χ)=0, aeff is the effective radius of the circular patch disk, εeq is the equivalent dielectric constant and c is the speed of light. Using the same material as substrate, the sizes of the two patches are significantly different: the top one resonating at the L1 band is roughly about 77% of the L2 patch at the bottom layer. Therefore, the overall lateral size of the antenna is determined by the bottom radiator. Using ceramic as substrate reduces the size of the antenna, but as a noted disadvantage, it also narrows the bandwidth since the quality factor Q of the resonant antenna is inversely proportional to the volume it physically occupy according to Chu-Harrington limit for electrically small antennas.
The disadvantages of the prior art are overcome by utilizing a stacked patch antenna using an exemplary molded ceramic puck with perforated air-cavities as the substrate. Illustratively, the substrate for the antenna is not completely filled with ceramic, but some part filled with air. The effective permittivity in the perforated dielectric region is determined from the porosity, or void fraction of the perforation, defined as the fraction of the volume of the voids-space over the total bulk volume of the material.
By having a ceramic puck with one or more perforated air cavities, a number of noted advantages are obtained. By introducing perforation to the dielectric substrate for the top layer patch of the stacked antenna, the effective permittivity in the patterned area of the ceramic is reduced so that the L1-band resonance occupied volume is illustratively increased without changing the overall material weight significantly. Through this, the Q-factor decreases and the operation bandwidth is substantially widened. At the same time, the weight of the ceramic is decreased due to the perforation. Further, the electromagnetic field distribution at resonance is changed by the perforation in the substrate. This gives the designer the flexibility to change the size of the patches, and therefore the bandwidth by varying the perforation position, size and pattern.
Using illustrative dual-band stacked patch antenna, only one set of direct feeds to the top patch radiator is applied since the excitation of the bottom patch (L2 band) element is through parasitic coupling. The stacked patch can be modeled by two coupled resonators. The coupling affects the impedance bandwidth of the bottom patch element; therefore the capability of varying the top patch size facilitates possible control over the coupling and the impedance matching.
Further, by manipulating the positions where the cavities are located, the frequency ratio between the high order mode and fundamental mode can be controlled. This is possible as the voltage peaks for different modes of resonating standing waves are located at different regions of the antenna. This is especially useful in the situation where harmonic or higher-frequency radiation needs to be controlled.
The description below refers to the accompanying drawings, of which:
In accordance with an illustrative embodiment of the present invention, the bandwidth of an exemplary ceramic antenna is designable and flexible. Illustratively, this is achieved by molding the ceramic with perforated cavities and using the perforated ceramic as the substrate for an exemplary patch antenna. The reason for perforating cavities, rather than holes, is to keep top-surface of the ceramic unaffected so that the same metallization process as conventional non-perforated ceramic may be used in accordance with illustrative embodiments of the present invention.
The first ceramic layer 110 comprises a cavity 125 that comprises of an air void. Illustratively, the cavity 125 may range in size in accordance with alternative embodiments of the present invention. As such, the description or depiction of the cavity 125 should be taken as exemplary only. Similarly, the second ceramic layer 120 comprises of a second cavity 130 that may range in size in accordance with alternative embodiments of the present invention. Illustratively, both cavities 125, 130 are located on a bottom portion of the respective ceramic layers 110, 120. That is, the cavities 125, 130 are located on a bottom side of the respective ceramic layers. In accordance with an illustrative embodiment of the present invention, a volume of the first cavity 125 is larger than a volume of the second cavity 130. However, in alternative embodiments, the two cavities may have the same and/or differing volumes. As such, the description of the first cavity having a larger volume than the second cavity should be taken as exemplary only.
Additionally one or more through holes 135 are provided to enable feed wires and/or pins to be passed to the first metal layer 105 and/or the second metal layer 115 in accordance with illustrative embodiments of the present invention. In accordance with an illustrative embodiment, there are four (4) through holes 135. However, it should be noted that in alternative embodiments of the present invention varying numbers of through holes may be utilized. As such, the description of four through holes should be taken as exemplary only.
It is expressly contemplated that the principles of the present invention may be implemented in hardware, software, including a non-transitory computer readable media, firmware or any combination thereof. Further, the description of specific sizes and/or numbers of cavities should be taken as exemplary only.
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Number | Date | Country | |
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20170331192 A1 | Nov 2017 | US |