I. Field of the Invention
The invention relates generally to antennas and, more particularly, to a portable antenna which may be used for satellite communications.
II. Description of Relevant Art
There are many situations, particularly in military operations, in which it is desirable to deploy an antenna for high frequency use, such as for satellite communications. Previously, antennas used by the military for satellite communications as well as other high frequency communications are assembled in fixed locations. Such fixed locations, however, are oftentimes not conveniently located, particularly during periods of unexpected troop movements. When this occurs, the previously known satellite terminals must be disassembled, moved to new locations, and then reassembled. Such disassembly and reassembly of the antenna systems, however, is time consuming and oftentimes not practical.
The present invention provides a portable antenna which overcomes the above mentioned disadvantages of the previously known antennas.
In brief, the antenna assembly of the present invention includes an elongated housing open at one end and defining an interior chamber. Preferably, the housing is tubular and cylindrical in shape and closed at its other end.
A telescoping mast has a carrier attached to one end which is slidably received within the housing chamber. The carrier, together with its attached mast, is movable between a storage position, in which the carrier and mast are positioned within the housing chamber, and a deployed position in which the carrier moves to adjacent the open end of the housing and the mast protrudes outwardly from the housing.
A flexible antenna is secured to the mast which is also contained within the housing chamber when in its storage position. However, when the mast moves to its deployed position, the flexible antenna also moves outwardly from the housing chamber and flares into a generally conical shape. The flexible antenna itself is constructed from an electrical insulating material while an electrically conductive material is deposited in a pattern on the flexible antenna to form the radiator for the antenna.
A spring is entrapped between the carrier for the mast and the closed end of the housing. This spring is maintained in a compressed position when the mast with its attached antenna is contained in the storage position within the housing chamber. A catch mechanism, such as a trigger, however, releases the force of the spring which then propels the carrier with its attached mast and antenna outwardly from the open end of the housing and to its deployed position. Preferably, movable struts attached to the housing adjustably support the antenna on a ground surface.
In order to ensure that the antenna forms a conical shape when in its deployed position, preferably a plurality of struts are pivotally connected to the housing carrier and extend through a guide plate at the open end of the housing. Thus, upon deployment of the antenna, the struts extend through openings in the guide plate so that the struts extend outwardly from the housing. However, the position of the holes in the guide plate ensures that, when the antenna is fully deployed, the struts flare outwardly from each other. Furthermore, a free end of the strut is secured to the antenna thus forcing the antenna into a generally conical shape.
A better understanding of the present invention will be had upon reference to the following detailed description when read in conjunction with the accompanying drawing, wherein like reference characters refer to like parts throughout the several views, and in which:
With reference first to
A carrier 20 is axially slidably mounted within the housing chamber 18 and movable between a storage position, illustrated in
With reference to
The radiators 32 may be printed, stitched, or otherwise attached to the substrate 30. A single electrically conductive radiator 32 is illustrated in
The diameter of the antenna 26 will have a substantial effect on the overall weight, stowed size and mechanical design of the assembly 10. Overall, the antenna 26 may have dimensions of around 20 inches in diameter when deployed in some embodiments. The parameters of the antenna design can be selected to satisfy certain performance requirements as desired.
Referring now to
With reference now particularly to
An annular guide plate 46 is connected to the housing adjacent its open end 14. This guide plate 46 includes a plurality of circumferentially spaced openings 48 and one spar 40 extends through each opening 48 in the guide plate 46. These openings 48, however, are spaced radially outwardly from the attachment points of their associated spars 40. Consequently, as the spars 40 move from their stored and to their deployed position, the coaction between the spars 40 and the guide plate openings 48 causes the spars 40 to flare outwardly as shown in
With reference now to
As best shown in
In operation, the antenna is initially in its stored position as illustrated in
When deployment of the antenna 26 is desired, the safety pin 52 is removed and the catch mechanism 50 actuated. Upon actuation, the catch mechanism 50 releases the spring 18 which propels the mast 22, antenna 26, and spars 40 out through the open end 14 of the housing 18. In doing so, the guide plate 46 not only retains the carrier 42 within the housing chamber 18, but also flares the spars 40 outwardly to ensure that the antenna 26 is conical in shape.
The antenna assembly 10 is then positioned as desired, with or without the use of the struts 54, and radio communications may be conducted using the antenna radiator 32 in any conventional fashion. More partially, the antenna may be pointed toward a communication source, such as a satellite. The required elevation and azimuth angles for pointing are functions of the antenna location and the satellite orbital location. An external device or an antenna-mounted chip, with or without a look-up table can be easily devised to be used with the antenna for positioning. Although the lengths of the struts 54 are adjustable and can be used to provide some pointing relative to zenith direction, the pointing can be accomplished, for instance, using a flexible annulated ring connected to the base of the deployed antenna 26. The antenna 10 can be pointed in both azimuth and elevation within limited angular spread. Wider angular movement can be done by adjusting the length of the supporting struts 54 for elevation control, and by rotating the supporting struts 54 for azimuth control. Similar to the annulated joint, a ball-and-socket section can be used at the base of the deployed antenna to provide elevation and azimuth pointing within wide angles. Pre-set marks can be provided on the housing 12 for accurate pointing relative to reference directions.
After use of the antenna assembly 10 has been completed, the mast 22 and antenna 26 may be returned to their storage position by forcing the mast 22 with the antenna 26 back into the interior chamber 18 of the housing 12 until the catch mechanism 50 engages the carrier 20 and retains it within the housing chamber 18. The safety pin 52 is then replaced and the entire antenna assembly 10 is ready for a subsequent deployment when desired.
In other embodiments, the antenna assembly 10 may optionally include light emitting diodes (LEDs) to indicate signal strength, the operational mode, and/or the elevation angle of the antenna.
From the foregoing, it can be seen that the present invention provides a portable antenna for high frequency communications, such as satellite communications, which may be rapidly deployed when desired. Having described my invention, however, many modifications thereto will become apparent to those skilled in the art to which it pertains without deviation from the spirit of the invention as defined by the scope of the appended claims.
This application claims priority of U.S. Provisional Application No. 61/901,283 filed Nov. 7, 2013, the contents of which are incorporated herein by reference.
The invention described herein may be manufactured, used, and licensed by or for the United States Government.
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Number | Date | Country | |
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20160315372 A1 | Oct 2016 | US |
Number | Date | Country | |
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61901283 | Nov 2013 | US |