Continuous transverse stub (CTS) arrays are disclosed, for example, in U.S. Pat. Nos. 5,926,077; 5,995,055; and 6,075,494. CTS arrays can be implemented as true-time-delay (TTDCTS) apertures employing parallel plate feeds. Typically there are a relatively large number of rails of varying shapes that are fabricated and assembled together in order to realize the aperture/parallel plate feed assembly.
Most antenna applications require two directive (high-gain, narrow bandwidth) beams, each at a different frequency band. In communication applications, the two beams perform the transmit and receive functions. Conventional dish antennas can perform these functions, but require relatively large swept volumes, which is not desirable for an installation that is adversely affected by it, such as an aircraft. Conventional phased arrays also can perform these functions, but include a fully populated lattice of discrete phase-shifters or transmit/receive elements each requiring their own phase and/or power-control lines. The recurring (component, assembly, and test) costs, prime-power, and cooling requirements associated with such electronically controlled phased-arrays can be prohibitive in many applications. In addition, such conventional arrays can suffer from degraded ohmic efficiency (peak gain), poor scan efficiency (gain roll-off with scan), limited instantaneous bandwidth (data rates), and data stream discontinuities (signal blanking between commanded scan positions). These cost and performance issues can be particularly pronounced for physically large and/or high-frequency arrays where the overall phase-shifter/transmit-receive module count can exceed many tens of thousands elements. In addition, when the transmit and receive frequency bands are widely spaced, two arrays can be required, one to perform the transmit function and one for the receive function.
A true-time-delay feed network for a continuous transverse stub antenna array includes a plurality of feed levels, each comprising one or more rails, the feed levels arranged in a spaced, parallel configuration. An open parallel plate region is defined between adjacent ones of the feed levels. The rails of the plurality of feed levels are arranged to form a power divider network unencumbered with septums or wall portions protruding into the open region.
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 different levels of the assembly 10 are illustrated in the cross-sectional view of
The first parallel plate feed level 30 comprises a plurality of spaced rails 32A-32E, spaced apart such that adjacent edges of the rails define slots 34A-34D. Interior rails 32B-32D are identical. End or exterior rails 32A and 32E are truncated versions of the interior rails. The rails are formed with respective pairs of inductive wells or grooves, e.g. grooves 32D-1, 32D-2 formed in rail 32-D, which are discussed more fully below.
The second parallel plate feed level 40 comprises a plurality of spaced rails 42A-42C, spaced apart such that adjacent edges of the rails define slots 44A, 44B. The end rails 42A, 42C are truncated versions of the interior rail 42B. The rails have pairs of wells formed therein as well.
The third parallel plate feed level 50 comprises two rails 52A, 52B, spaced apart such that adjacent edges of the rails form a slot 54A. Each rail has a pair of wells formed therein as well.
The rails of each level can be fabricated as a single unit, or assembled together to form a single unit, reducing the number of parts. The rails have electrically conductive surfaces, and can be fabricated from a metal, e.g. aluminum, by machining, extrusion, or other processes. Alternatively the rails can be fabricated from a plastic material, e.g. by molding or extrusion, and plated with a conductive layer.
The levels 20, 30, 50 and 50 are assembled together in a spaced relationship, as illustrated in
In a transmit mode, RF energy is launched into the slot 54A, e.g. by a line source, and divides into two components which propagate in opposite directions in the parallel plate region 48, thus forming a 1:2 power divider. Energy propagating in the region 48 enters slots 44A, 44B in level 40, and divides into respective components which propagate in the parallel plate region 38, thus forming two 1:2 power dividers. Now the input energy has been divided into four components. The energy propagating in region 38 enters slots 34A-34D in level 30, separating into respective pairs of energy components which propagate in region 28 adjacent the aperture level 20. The input energy has been divided into eight components in region 28, one component for each transverse stub 24A-24H. The respective energy components radiate from the respective stubs. In this exemplary embodiment, the path lengths from the slot 54A to the respective stubs are equal in length, so that the time delay is equal for each path, and the signal components radiated from each slot will be in phase. Of course, on receive, the received signal components at each stub will be combined in phase to provide a single combined signal component at slot 54A.
The assembly 10 makes use of “virtual” shorts that replace a perfect electrical conductor (“PEC”) short wall in the path of propagating waves inside the parallel-plate or rectangular waveguide structures, typically arranged at a 45 degree angle to direct energy from a parallel plate region into a slot communicating with a next level. The virtual short is matched by inductive wells or grooves formed in the parallel plate structure where the propagating wave is confined. The depth, width and the number of wells replacing the PEC short wall are dependent on bandwidth and the separation distance between the walls.
The assembly 10 also makes use of septum-less TEE E-plane power dividers, that do not employ protruding septums in front of the input arm of the TEE. Instead, the protruding septum and its function (matching) can replaced by one or more inductive wells or grooves, e.g. a pair of wells formed in the two co-linear arms of the TEE, if desirable for a particular application. The dimensions of the wells and their distances to the input arm determine the bandwidth and matching properties of the tee.
In some applications, the septum-less TEE power divider as employed in the feed network of the TTDCTS array may not employ matching wells formed in each side arm port. The exemplary embodiment of
A virtual short 130 is also illustrated in
Referring again to
Slots 44A, 44B comprise input arms for septum-less TEE power dividers 46A, 46B, to divide the RF energy entering these power dividers into RF energy components conducted into open channel 38. The energy components from divider 46A enter slots 34A, 34B in feed level 30, and the energy components from divider 46B enter slots 34C, 34D in feed level 30.
A third level of power dividers 56A, 56B, 56C, 56D in turn divides the power from the second level of dividers 46A, 46B into eight RF energy components which are directed into the radiating stubs 24A-24H.
Each of these power dividers of the first, second and third levels of power dividers in this embodiment are septum-less power dividers, i.e. without a septum element protruding into the open channel between levels. These power dividers further include tuning wells formed on the wall opposite the input arm or channel to improve impedance matching. Thus, TEE divider 56 includes a well 57. TEEs 46A, 46B respectively include wells 47A, 47B. TEEs 56A-56D include wells 57A-57D, respectively. Virtual shorts are employed instead of hard shorts extending into the open channels. Thus, for open channel 48, virtual shorts 58A, 58B each comprising a pair of inductive wells formed in the surface of respective rails 52A, 52B, prevent energy entering from input port 57A from passing beyond the shorts. For open channel 38, virtual shorts 48A, 48B are positioned for TEE 46A, and virtual shorts 48C, 48D are positioned for TEE 46B. For open channel 28, virtual shorts 38A, 38B are positioned for TEE 56A, virtual shorts 38C, 38D are positioned for TEE 56B, virtual shorts 38E, 38F are positioned for TEE 56C, and virtual shorts 38G, 38H are positioned for TEE 56D.
It is to be understood that the antenna aperture and parallel plate feed assembly described above is capable of reciprocal operation, i.e. for operation on receive as well as transmit. Thus, while slot 54A is described above in terms of an input port for the assembly, the slot functions as an output port when the assembly is operated on receive.
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.
This invention was made with Government support under Contract No. F30602-96-C-0283 awarded by the Department of the Air Force. The Government has certain rights in this invention.