Satellite antenna

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Description

FIG. 1 is a perspective view of the satellite antenna, depicted in a deployed configuration, and showing the azimuth assembly, and the reflector and the feed assembly extending from the azimuth assembly;

FIG. 2 is a perspective view of the satellite antenna, opposite to that shown in FIG. 1;

FIG. 3 is a side view of the satellite antenna shown in FIG. 1;

FIG. 4 is a side view of the satellite antenna, opposite to that shown in FIG. 3;

FIG. 5 is a front elevation of the satellite antenna shown in FIG. 1;

FIG. 6 is a rear elevation of the satellite antenna shown in FIG. 1;

FIG. 7 is a top plan view of the satellite antenna shown in FIG. 1;

FIG. 8 is a bottom plan view of the satellite antenna shown in FIG. 1;

FIG. 9 is a perspective view of the satellite antenna, depicted in a stowed configuration;

FIG. 10 is a perspective view of the satellite antenna, opposite to that shown in FIG. 9;

FIG. 11 is a side view of the satellite antenna shown in FIG. 9;

FIG. 12 is a side view of the satellite antenna, opposite to that shown in FIG. 11;

FIG. 13 is a front elevation of the satellite antenna shown in FIG. 9;

FIG. 14 is a rear elevation of the satellite antenna shown in FIG. 9;

FIG. 15 is a top plan view of the satellite antenna shown in FIG. 9; and,

FIG. 16 is a bottom plan view of the satellite antenna shown in FIG. 9.

The radio mounting holes provided in the feed assembly are depicted as small dots to indicate that they do not form part of the design. The mounting holes provided in the support arms of the reflector are depicted as small dots to indicate that they do not form part of the design. The perimeter of the recessed surface provided in the reflector is depicted using a broken line to indicate that the recessed surface does not form part of the design. Other features are also depicted using broken lines to indicate that they do not form part of the design.

Claims

The ornamental design for a satellite antenna, as shown and described.

Referenced Cited
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Patent History
Patent number: D696649
Type: Grant
Filed: Mar 15, 2011
Date of Patent: Dec 31, 2013
Assignee: C-Com Satellite Systems Inc. (Ottawa)
Inventors: Matthew Siemers (Ottawa), Ewan Smith (Ottawa)
Primary Examiner: John Windmuller
Application Number: 29/387,567