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1. Field
The technology of the present application relates to patch antennas, and more specifically to low profile partially loaded patch antenna.
2. Background
Satellite communications currently requires a radio frequency antenna that operates over one or more frequencies. Many conventional antennas can be used in the appropriate frequencies for satellite communications, such as for example, conventional planar inverted-F antennas, patch antennas, microstrip antennas, etc. However, as satellite usage has increased, companies have begun demanding better performance from antennas while at the same timerestricting the antenna profile.
Several conventional antennas such as the monopole, dipole, inverted-F, and other could be used to meet the performance requirements for satellite communications.
However, these designs are often taller than the desired profile and taking meansures to lower the height results in lowering the efficiency. A conventional patch antenna has a relatively low profile and is a good candidate, but its footprint at frequencies in the appropriate ranges (for example, 100-200 MHz) is very large, often larger than the space allowed or available. Its possible to reduce the profile by providing a high dielectric constant between the ground plane and the patch. This avenue has several drawbacks including the fact that the large dielectric material is heavy and costly to both manufacture and ship.
Thus, against this background, it would be desirable to provide a low profile antenna.
To attain the advantages of and in accordance with the purpose of the present invention, a low profile antenna is provided. The low profile antenna comprises a radiating element arranged over a ground plane. The radiating element has a feed connection that can be either directly or indirectly coupled. The radiating element has a plurality of radiating edges. The radiating edges are selectively loaded with a dielectric, wherein the profile of the antenna fits in the available space.
The foregoing and other features, utilities and advantages of the invention will be apparent from the following more particular description of a preferred embodiment of the invention as illustrated in the accompanying drawings
The above and other objects and advantages of the present invention will be apparent upon consideration of the following detailed description, taken in conjunction with the accompanying drawings, in which like reference characters refer to like parts throughout, and in which:
The word “exemplary” is used herein to mean “serving as an example, instance, or illustration.” Any embodiment described herein should be construed as “exemplary,” unless explicitly stated otherwise, whether it is specifically referred to as exemplary or not, and is not necessarily to be construed as preferred or advantageous over other embodiments.
The technology of the present application will know be described with specific reference to
Referring first to
Radiating element 102 has a ground facing side 102g. A distance d separates the ground plane from the radiating element. Antenna 100 also comprises a feed connection 106. Radiating element 102 may be supported over ground plane 104 using any number of conventional techniques, but as shown four corner supports 110 are shown. In practice, antenna 100 would likely be provided in a housing (not specifically shown) and the supports could be provided as part of the molded housing. Radiating element 102 may be supported by dielectric elements 112 instead of either the housing or support posts 110 as shown.
Extending downward from the radiating edges of antenna 100 are dielectrics elements 112. Dielectrics elements 112 are coupled to radiating element 102 on the ground facing side 102g and extend to or toward the ground plane 104 Dielectric elements 112 must be closely coupled to radiating element 102 as well as ground plane 104 to achieve the desired reduction of resonant frequency for satellite operating ranges.
As shown, radiating element 102 has a length L and a width W. Dielectric elements 112 have a length L1 and W1 less than length L and width W such that the volume occupied by dielectric elements 112 is substantially less than the volume defined by L×W×d.
In order to provide a multi-band radio frequency antenna, radiating element 102 is sized such that L≠W. Orthogonal patch modes are driven and antenna 100 is resonant at two distinct frequencies determined by L and W. Slots 114 are optional and shown in phantom. Varying the length of slots 114 alters the effective dimensions of the patch edges and allows fine tuning of the resonant frequencies. The lengths of slots 114 have much less impact on the resonant frequencies than do the dimensions L and W of radiating element 102. While slots 114 are shown as essentially straight slots, slots 114 may be any number of shapes and sizes depending on operational requirements of the antenna 100. For example, slots 114 may be any straight, L-shaped, meandering, or the like. Also, slots 114 do not need to be identical on each edge. Varying the feed position relative to the edges of radiating element 102 allow the two resonances to be matched. Alternatively, an additional matching network 116 could be provided.
While shown as rectangular, radiating element 102 may comprise different shapes, such as square, triangular, octagonal, etc. Generally speaking, the number of dielectric elements will correspond to the number of radiating edges associated with radiating element 102. One exemplary embodiment of the technology comprises an antenna in a footprint of approximately 275 mm by 325 mm having operating frequencies between 137-138 MHz and 148-150 MHz. Using a radiating element of approximately 200 mm by 250 mm with a dielectric elements having an ∈r equal to approximately 100 and dimensions of approximately 100 mm by 22 mm by 15 mm, it was found the overall height of antenna 100 was no more than 23 mm including a housing component. Thus, as can be seen by this overall profile of this exemplary antenna is relatively low. In this exemplary embodiment the dielectric elements are bonded to radiating element 102 and ground plane 104 using conductive tape. Varying the conductivity of the tape changes the Q-factor (and therefore bandwith) of the antenna. Wider bandwidth can be provided by lowering the conductivity of the tape. However, wider bandwidth comes at the expense of lower efficiency. Varying the conductivity of the tape also effects the impedance seen at the edges of radiating element 102 and ultimately the point at which the antenna feed should be placed for best matching.
Referring now to
The previous description of the disclosed embodiment is provided to enable any person skilled in the art to make or use the present invention. Various modifications to these embodiments will be readily apparent to those skilled in the art, and the generic principles defined herein may be applied to other embodiments without departing from the spirit or scope of the invention. Thus, the present invention is not intended to be limited to the embodiments shown herein but is to be accorded the widest scope consistent with the principles and novel features disclosed herein.
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