Very low mass or ultra-lightweight (ULW) antenna designs are desired for some applications, such as, by way of example only, space applications including micro-satellite radar applications. Conventional antenna array and transmission line technology provides significant weight and other challenges to use in such ULW arrays.
A transmission line structure for propagating electromagnetic energy, includes a transmission line conductor trace, a first dielectric foam layer and a second dielectric foam layer. The conductor trace is sandwiched between the first foam layer and the second foam layer. A first ground plane layer and a second ground plane layer sandwich the first foam layer, the conductor trace and the second foam layer. A plurality of mode suppression metallic element portions pass through the first ground plane layer, the first foam layer, the second foam layer and the second ground plane layer in a generally transverse arrangement.
Features and advantages of the disclosure will readily be appreciated by persons skilled in the art from the following detailed description when read in conjunction with the drawing wherein:
In the following detailed description and in the several figures of the drawing, like elements are identified with like reference numerals. The figures are not to scale, and relative feature sizes may be exaggerated for illustrative purposes.
The foam layers 54, 56 are in turn sandwiched between ground planes 58 and 60. The ground planes may be formed, in one embodiment, by a copper metalized layer on a face sheet or substrate, e.g., a liquid crystal polymer (LCP) substrate, such as R/Flex® 3600 copper-clad LCP marketed by the Rogers Corporation.
Unsupported cyanate ester film adhesive (0.015 psf) may be used as an adhesive to bond the layers of the stack-up together in an exemplary embodiment. Other adhesives may be alternatively be used, such as silicone CV-2500 and epoxy EA 9396.
In another exemplary embodiment, the ground planes 58 and 60 are formed by layers of metal deposited directly on the outwardly facing surfaces of the foam layers 54 and 56, e.g. by an evaporation technique such as electron beam (“e-beam”) evaporation of a metal such as aluminum. This eliminates the weight and RF loss of the adhesive and the LCP carrier of the ground plane layers fabricated by copper-clad LCP.
The stripline transmission line structure may be used to implement various circuits, e.g., as part of an antenna array.
Associated with the foam-loaded stripline structures is a technique to provide trace isolation and parallel plate mode suppression. In a typical PWB microstrip transmission line structure, isolation and mode suppression are accomplished by inserting plated vias in the substrate to electrically connect the top and bottom ground planes at precise points. Two methods of mode suppression suitable for foam-loaded stripline structures include copper stitching, and plated vias in the foam layers.
Foam stitching accomplishes trace isolation and mode suppression by electrically connecting the top and bottom ground planes of the foam stack-up with copper wire or ribbon. The wire may be “sewn” through the foam stack up and bonded in place. The vertical vias or stitch segments may be placed to form conductive boundary walls or picket structures along a stripline conductor or to surround a vertical via to form a coaxial cage-like structure around the via and form a vertical interconnect.
Methods to stitch the foam stack-up include hand sewing through pre-placed holes, and machine sewing using, for example, an industrial sewing machine. Hand sewing involves the use of a needle threaded with the copper wire or ribbon, and inserting the needle and wire through the pre-formed holes in the stack-up. An exemplary machine suitable for machine sewing is the Singer 17U with a long beak high point shuttle, which minimizes damage to the wire and stripline assembly. Hand sewing allows for more precise stitch placement while the machine is considerably more efficient. Stitch bonding processes included hand solder, solder re-flow with paste and pre-forms, conductive epoxy and tape.
Plating vias in the foam stack-up may also be employed as an effective method for mode suppression and trace isolation in a foam stripline transmission line structure. An exemplary process may employ sputter deposition to metallize the interior of pre-drilled holes, or e-beam evaporation. In an exemplary application, e.g. for a 0.130″ thick transmission line stack-up structure, sputter deposition may be preferred to e-beam evaporation as it allows for a wider angle of attack and better coating of the walls of the holes.
In an exemplary embodiment, the radiator assembly 110 is electrically connected to two RF feed circuits provided by the structure 130, by feed pins 140 which extend in a transverse direction to the structure 130. The feed pins are electrically connected to baluns formed in the radiator assembly 110, and to the respective ones of the RF feed circuits formed in the structure 130 by pin heads 140A.
The structure 140 defines first and second RF feeds 130-1 and 130-2, which respectively provide feed circuits for the orthogonal radiator sticks 112 and 114. Each of the feed circuits may be fabricated as a foam layer stack-up, similar to that depicted in
Feed circuit 130-2 includes dielectric foam spacer layers 132, 134, and a center RF circuit layer 142 located between the foam spacer layers. Upper and lower ground plane layers 144, 146 are disposed outside the foam spacer layers.
In an exemplary embodiment, the layers of the structure 110 and the structure 130 may be assembled together with the aid of tooling such as fixture 160, and the layers secured together with adhesive such as, for example, RS-4A adhesive film marketed by YLA, Inc., Benicia, Calif. Exemplary materials for the structure 130 include Rohacell 31-HF-HT foam for the foam spacer layers, 0.001 inch thick LCP with 0.0007 inch thick copper traces as the RF circuit layers, and 0.001 inch thick KaptonE® substrate with 0.00035 inch thick copper cladding as the ground plane layers. These specific layer materials and thicknesses are intended only as examples.
In the exemplary embodiment of
Although the foregoing has been a description and illustration of specific embodiments of the invention, various modifications and changes thereto can be made by persons skilled in the art without departing from the scope and spirit of the invention as defined by the following claims.
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| Number | Date | Country | |
|---|---|---|---|
| 20110221649 A1 | Sep 2011 | US |