1. Field of the Invention
This invention relates to microwave reflector antennas. More particularly, the invention relates to a Radio Frequency (RF) seal for the joint between the feed and main reflector/antenna base of a reflector antenna.
2. Description of Related Art
Self supported feed assemblies typically include a subreflector supported proximate a focal point of the main reflector by a feed waveguide coupled to a mounting hub fastened to an antenna base that also supports the main reflector. A joint between the main reflector/antenna base and the mounting hub creates an RF leakage path to the rear of the reflector antenna that generates signal backlobes known to degrade the reflector antenna signal pattern. A vertex plate is commonly applied to the proximal end of the feed waveguide and/or mounting hub to improve the overall return loss of the antenna.
Prior reflector antennas typically apply a plurality of conductive seal(s), such as a spring ring(s) and/or conductive grease, to seal the joint and/or area between the vertex plate and the main reflector/antenna base. Conductive grease application is time-consuming and may be difficult for installation personnel to correctly apply in exposed reflector antenna mounting environments, such as high atop radio towers. Also, conductive grease application may require skin protection for the installation personnel, further complicating application.
Competition in the reflector antenna market has focused attention on improving electrical performance and minimization of overall manufacturing, inventory, distribution, installation and maintenance costs. Therefore, it is an object of the invention to provide a reflector antenna feed assembly mounting hub joint seal that overcomes deficiencies in the prior art.
The accompanying drawings, which are incorporated in and constitute a part of this specification, illustrate embodiments of the invention, where like reference numbers in the drawing figures refer to the same feature or element and may not be described in detail for every drawing figure in which they appear and, together with a general description of the invention given above, and the detailed description of the embodiments given below, serve to explain the principles of the invention.
The inventors have developed a cavity conforming conductive and/or RF absorbent compressible gasket arrangement that eliminates the prior requirement for multiple RF seals and/or application of conductive grease, significantly reducing manufacture and assembly requirements for a reflector antenna.
A first exemplary embodiment is demonstrated in
The gasket 17 may be provided as a portion of compressible material with an outer diameter greater than at least a periphery of the mating surfaces between the feed hub 7 and the antenna base 5 and lesser than the outer diameter of the vertex plate 15. For ease of initial assembly, the gasket 17 may be dimensioned for retention in a stretch fit around the outer surface of the feed hub 7. Upon insertion of the feed hub 7 into the antenna base 5, the gasket 17 is compressed within a cavity between the vertex plate 15, feed hub 7 and antenna base 5, for example via tightening of fasteners such as screws or bolts (not shown) extending through the antenna base 5 into mounting hole(s) 19 of the feed hub 7.
The gasket 17 may be formed from a compressible conductive and/or RF absorbent material. Alternatively, the gasket 17 material may be a compressible media coated with RF absorbent material and/or conductive material. An example of a suitable compressible material coated with an RF absorbent is urethane foam with a gradient lossy coating such as C-Ram AR, by Cuming Microwave, of Avon Mass., USA. The gasket 17 may be cost effectively formed by cutting or stamping gasket(s) 17 of desired dimensions out of bulk sheets of the selected material.
The compression of the gasket 17 form fills the cavity between the outer diameter of the feed hub 7, the vertex plate 13 and the antenna base 5, as best shown in
The compression of the gasket 17 may be primarily in a direction parallel to a longitudinal axis of the feed, reducing deformation of the gasket 17 in a direction normal to the longitudinal axis such that the gasket 17 does not extend beyond the diameter of the vertex plate 13 when compressed.
One skilled in the art will appreciate that, in addition to improving the electrical performance of the assembled reflector antenna, the gasket 17 arrangement also enables significant manufacturing, delivery, installation and/or maintenance efficiencies as manufacture, inventory, delivery and assembly of multiple conventional point sealing gaskets and/or conductive grease are eliminated.
Where in the foregoing description reference has been made to materials, ratios, integers or components having known equivalents then such equivalents are herein incorporated as if individually set forth.
While the present invention has been illustrated by the description of the embodiments thereof, and while the embodiments have been described in considerable detail, it is not the intention of the applicant to restrict or in any way limit the scope of the appended claims to such detail. Additional advantages and modifications will readily appear to those skilled in the art. Therefore, the invention in its broader aspects is not limited to the specific details, representative apparatus, methods, and illustrative examples shown and described. Accordingly, departures may be made from such details without departure from the spirit or scope of applicant's general inventive concept. Further, it is to be appreciated that improvements and/or modifications may be made thereto without departing from the scope or spirit of the present invention as defined by the following claims.
Filing Document | Filing Date | Country | Kind | 371c Date |
---|---|---|---|---|
PCT/IB2009/054921 | 11/5/2009 | WO | 00 | 7/30/2010 |
Number | Name | Date | Kind |
---|---|---|---|
2694778 | Rowland et al. | Nov 1954 | A |
2945229 | Klauser | Jul 1960 | A |
4689637 | Ochiai et al. | Aug 1987 | A |
4876554 | Tubbs | Oct 1989 | A |
5714963 | Cox | Feb 1998 | A |
5870062 | Cox | Feb 1999 | A |
6137449 | Kildal | Oct 2000 | A |
6429826 | Karlsson et al. | Aug 2002 | B2 |
6522305 | Sharman | Feb 2003 | B2 |
6985120 | Lewry et al. | Jan 2006 | B2 |
20050017916 | Lewry et al. | Jan 2005 | A1 |
20090207095 | Kimura et al. | Aug 2009 | A1 |
Number | Date | Country |
---|---|---|
0136817 | Apr 1985 | EP |
0817307 | Jan 1998 | EP |
0859427 | Aug 1998 | EP |