The present inventions relate generally to wireless communications antenna systems. In particular, they relate to improvements in wireless base station antenna connector mountings.
Mobile wireless access antennas, such as cellular sector antennas, are deployed in severe environmental conditions. The operational temperature range for such antennas is typically −40° C. to +70° C., and the antennas are rated to endure wind speeds of up to 240 km/h. Environmental sealing must be maintained through these weather extremes.
In known antennas, RF connectors are often located on a bottom panel, and are connected to coaxial cables one at a time. However, a recent development involves defining an interface with pre-determined locations for blocks of RF connectors, to allow for interconnection of equipment without having to field-install coaxial cable jumpers. See, for example, U.S. application Ser. No. 14/224,369, now U.S. Pat. No. 9,249,593 to Perko et al., which is incorporated by reference. These pre-determined locations for these blind mate blocks of RF connectors must be thermally stable.
A connector assembly for an antenna including an antenna cover according to one aspect of the invention includes a connector mount attachable to an inner structure of the antenna which extends through an opening in the antenna cover with sufficient clearance to permit movement of the antenna cover relative to the connector mount. A sealing structure dimensioned to enclose at least a portion of the connector mount forms a flexible weather resistant seal between the antenna cover and the connector mount that allows movement of the antenna cover relative to the connector mount.
The present invention is described herein with reference to the accompanying drawings, in which embodiments of the invention are shown. This invention may, however, be embodied in many different forms and should not be construed as limited to the embodiments set forth herein. Rather, these embodiments are provided so that this disclosure will be thorough and complete, and will convey the scope of the invention to those skilled in the art.
The terminology used herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the invention. As used herein, the singular forms “a”, “an” and “the” are intended to include the plural forms as well, unless the context clearly indicates otherwise. It will be further understood that the terms “comprises” and/or “comprising,” when used in this specification, specify the presence of stated features, integers, steps, operations, elements, and/or components, but do not preclude the presence or addition of one or more other features, integers, steps, operations, elements, components, and/or groups thereof.
Many different embodiments are disclosed herein, in connection with the description and the drawings. It will be understood that it would be unduly repetitious and obfuscating to literally describe and illustrate every combination and subcombination of these embodiments. Accordingly, the present specification, including the drawings, shall be construed to constitute a complete written description of all combinations and sub combinations of the embodiments described herein, and of the manner and process of making and using them, and shall support claims to any such combination or subcombination.
The reflector 22 is typically fabricated from metal, such as aluminum or steel. The rear cover 16 and radome 18 may be fabricated from a thermo plastic, such as Acrylonitrile Styrene Acrylate (ASA). In a one embodiment, the rear cover 16 and radome 18 comprise a single extrusion. In an alternate embodiment, the rear cover 16 and radome 18 may be separately formed and may be fastened to the reflector or other antenna structure.
Referring to
The coefficient of thermal expansion (CTE) of the ASA radome/rear cover may be approximately 95×10-6/° C., whereas the CTE for the reflector are may be as little as 13×10-6/° C., depending on the metal used for the reflector 22 and the structure on which the antenna is mounted. This mis-match in the rate of expansion of the two components means that adequate clearance must be provided at the openings in the rear cover 16 for the greater rate of expansion of the rear cover 16 relative to the reflector 22. (The relatively high CTE for the rear cover 16 precludes attaching the connector blocks directly to the rear cover, as that may cause misalignment of the connector blocks relative to the mounting brackets of the antenna.) Accordingly, according to one aspect of the present invention, the connector blocks 20 are environmentally sealed to the rear cover with a flexible seal structure 40, while the connector blocks themselves are fixed to the reflector.
Also shown in
When assembled, clearance between the rear cover 16 and connector mounts allows sufficient room for movement of the rear cover relative to the connector mount. However, the seal, being clamped at one end to the rear cover, and clamped at the other end to the connector block, provides weather resistant environmental sealing without restricting movement of the connector block relative to the rear cover.
Although embodiments of the present invention have been described with reference to specific example embodiments, it will be evident that various modifications and changes may be made to these embodiments without departing from the broader spirit and scope of the invention. Accordingly, the specification and drawings are to be regarded in an illustrative rather than a restrictive sense and it is intended that the invention be limited only to the extent required by the appended claims and the applicable rules of law.
The Abstract of the Disclosure is provided to comply with 37 C.F.R. § 1.72(b), requiring an abstract that will allow the reader to quickly ascertain the nature of the technical disclosure. It is submitted with the understanding that it will not be used to interpret or limit the scope or meaning of the claims. In addition, in the foregoing Detailed Description, it can be seen that various features are grouped together in a single embodiment for the purpose of streamlining the disclosure. This method of disclosure is not to be interpreted as reflecting an intention that the claimed embodiments require more features than are expressly recited in each claim. Rather, as the following claims reflect, inventive subject matter may lie in less than all features of a single disclosed embodiment. Thus, the following claims are hereby incorporated into the Detailed Description, with each claim standing on its own as a separate embodiment.
This application is a 35 U.S.C. § 371 national stage application of PCT International Application No. PCT/US2015/057746, filed Oct. 28, 2015, which itself claims priority to the following U.S. Provisional Application pursuant to 35 U.S.C. § 120, U.S. Provisional Application Ser. No. 62/072,078 filed Oct. 29, 2014, the disclosure and content of both of which are incorporated by reference herein in their entireties. The above-referenced PCT International Application was published in the English language as International Publication No. WO 2016/069710 A1 on May 6, 2016.
Filing Document | Filing Date | Country | Kind |
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PCT/US2015/057746 | 10/28/2015 | WO | 00 |
Publishing Document | Publishing Date | Country | Kind |
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WO2016/069710 | 5/6/2016 | WO | A |
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International Search Report and Written Opinion of the International Searching Authority, International Application No. PCT/US2015/057746, dated Jan. 26, 2016. |
Number | Date | Country | |
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20170214133 A1 | Jul 2017 | US |
Number | Date | Country | |
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62072078 | Oct 2014 | US |