Around-the-mast rotary annular antenna feed coupler

An annular rotary antenna feed coupler especially for around-the-mast use, as on shipboard. A housing in the general shape of a cylinder with a central axial opening essentially concentric with the axial center line of the housing contains a circumferential distribution of a number of fixed axially elongated, conductive loops each with a feed port. Radially spaced therefrom, a second, group of elongated conductive loops circumferentially distributed about a circle of different radius as compared to the aforementioned fixed loops is rotatably mounted. A corresponding plurality of ports, one for each rotating loop, is also provided, and input and output combiner/divider devices, one for the fixed and another for the rotating sub-assemblies serve to combine all ports into a single fixed and a single rotating port. Mechanically, the rotating combiner/divider rotates with the antenna array with which it operates.

BACKGROUND OF THE INVENTION 
The invention relates to microwave systems generally, and more particularly 
to an RF feed operative between fixed transmit/receive apparatus and a 
rotating antenna array, or the like. 
DESCRIPTION OF THE PRIOR ART 
The general problem of providing a rotating RF transmission line joint 
between a rotating antenna system and fixed transmitter, receiver and 
signal processing apparatus is nearly as old as the radar art itself. 
Various forms of such rotating joints or couplings have been developed and 
are known in this art. A few of these include the rotating circular 
waveguide joint, the rotating coaxial coupling, and various hybrid 
arrangements in which there are one or more transitions from one 
transmission line medium to another. 
The unique problem in shipboard radar arises when, for reasons intended to 
minimizing antenna blockage from ship superstructure, a rotating antenna 
is essentially mounted at the top of a mast. In such cases, it is 
particularly useful to provide some form of around-the-mast coupler, a 
part of which rotates with the antenna array and a part of which remains 
fixed for connection to the fixed apparatus, typically a transmitter, 
receiver and other signal processing equipment. One form of such a coupler 
is described in U.S. Pat. application Ser. No. 40,325 filed May 18, 1979, 
and is entitled "Around-The-Mast Rotary Coupler." That patent application 
is assigned to the assignee of the present application. In it, two 
matching, annular, cellular rings rotate with respect to each other. The 
cells of each of these rings are actually waveguide sections and energy 
transfer is effected during rotation. 
One inherent problem associated with the aforementioned rotary coupler is 
this same fact, namely that the individual cells of the annular rings are 
in effect short sections of waveguides, and are therefore subject to the 
low frequency cut-off characteristic of waveguide. This means that, for 
relatively low microwave frequencies, the cross-sectional dimensions of 
these waveguide cells become relatively large. The result in size, weight 
and cost factors can be disadvantageous. 
Of further interest in the prior art is U.S. Pat. application Ser. No. 
77,850, filed Sept. 21, 1979 and entitled "Loop Coupler Commutating Feed." 
In that disclosure, the concept of fixed and rotating loops coupling to 
each other is presented and could be adapted to the rotary coupler use, 
however its diameter is relatively large since the loops are radially 
oriented. More importantly, however, it is not adapted to the 
around-the-mast configuration, and is essentially useful as background 
hereto because of the basic, coupled, elongated loop concept which it 
discloses in common with the invention herein. 
Also of interest is backgound is U.S. Pat. application Ser. No. 19,481, 
filed Mar. 12, 1979 and entitled "Large Scale Low-Loss Combiner and 
Divider." That device, which does not involve moving parts is not a 
coupler per se, and is not directly applicable to the around-the-mast 
rotary coupler application, but like the aforementioned U.S. Pat. 
application Ser. No. 77,850 employs magnetically coupled elongated loops 
in independent input/output groups. 
All three of the aforementioned background patent applications are assigned 
to the same assignee as is the present invention. 
In consideration of the background art and the particular problem to be 
solved, the manner in which the invention advances the state of this art 
will be understood as this description proceeds. 
SUMMARY 
It may be said to have been the general objective of the present invention 
to provide a compact, around-the-mast, rotary coupler for transferring 
radio frequency signals between the rotating antenna and fixed associated 
circuitry through magnetic loop coupling. The apparatus of the invention 
is constructed around a central axial opening of circular cross-section 
for around-the-mast installation. Within a conductive housing, an annular 
chamber is provided into which a first group of fixed, elongated, 
conductive loops are installed, these loops extending generally axially 
about the full 360.degree. cross-section. A rotatable assembly provides a 
second group of similar loops, these being mounted on a rotatable assembly 
so that they revolve as a group about a common center with respect to the 
fixed loops in radial juxtaposition therewith. The fixed loops in the 
representative embodiment to be described hereinafter, are on the inside, 
i.e. laterally tangent to a smaller circle than are the rotating loops 
which are laterally tangent to a somewhat larger circle. 
An "equal-path-length" feed arrangement is illustrated and described in 
connection with the implementation of a system employing the loop coupler 
part of the invention. The device of the invention is not subject to low 
frequency cut-off as is the case in waveguide devices, and accordingly can 
be constructed more compactly and with correspondingly higher bandwidth 
capability. Typically, a bandwidth of at least 50 percent is readily 
achievable. The power transfer between the fixed and rotating loop sets is 
relatively constant with rotation except for a periodic power ripple 
caused by reflected power due to the mismatch that occurs as the rotor 
loops pass over the gaps between adjacent fixed loops. If one loop set 
comprises relatively wide loops with minimum gaps between them 
circumferentially, the other set may be relatively narrow in their 
transverse or circumferential dimension and still provide relatively 
constant power transfer except for the aforementioned periodic ripple. 
The details of an embodiment based on the principles of the invention will 
be described hereinafter.

DETAILED DESCRIPTION 
Referring now to FIG. 1, the apparatus of the invention will be seen in 
section with its axial cylindrical central opening emplaced over a mast 
10. The housing 11 will be understood to be generally annular in a plane 
normal to the axial center line of the mast 10 and therefore to the axial 
center-line of the central axial cavity generally congruent with the mast 
10 in the illustration of FIG. 1. 
The cross-section of the housing 11 on either side of the mast 10 will be 
seen to be generally U-shaped in an axial plane, i.e. without the rotating 
assembly generally identified at 16. Within this housing the fixed loops 
or stator loops are distributed circumferentially, typically at 27 in FIG. 
1. The radially outward projection 11A forms a conductive pedestal for 
loop leg 27, the loop being also connected at the lower end to a coaxial 
center conductor 28 passing through a bore 50 in the bottom of housing 11, 
where an external port in the form of a coaxial connector 29 provides a 
connection thereto. The outer conductor of the coaxial connector 29 is 
electrically and mechanically connected to the housing 11 at that point 
and the radially inward wall of housing 11 forms a fixed loop return path. 
The coaxial connector 29 representing one of the fixed loop ports is one 
of the set of first ports referred to hereinafter. In FIG. 2, a 
development of the cylindrically distributed first or fixed loops as well 
as the rotating loops of the second loop set, typically 20 in FIGS. 1 and 
2, is shown. The development showing of FIG. 2 may be considered to be a 
radially inward view taken in the absence of the extended conductive 
cylindrical shell 21 and the housing 11 radially outward wall. Further 
discussion of FIG. 2 will follow during and after the description of FIG. 
1, as appropriate. 
Considering now the rotating assembly generally at 16, this comprises what 
may be referred to as first and second axial sections, the first axial 
section, or lower part as depicted in FIG. 1, comprises the loop leg 20 
with its conductive pedestal 26 connected to the conductive cylindrical 
shell extension 21. The second, or upper part, comprises the stripline 
section between conductive cylindrical shells 33 (from which 21 is 
extended) and 32 on the radially inward side. Insulation portions 17 and 
18 comprise the solid dielectric of the stripline arrangement and 19 is 
the typical center conductor strip which will be seen to be connected to 
loop leg 20. The coaxial connector 12 is one of the plurality of second or 
rotating ports shown as 12, 13, 14 and 15 etc., on FIG. 1A. A metal or 
metalized top strip 49 covers the upper end of the dielectric 17 and 18 
with a clearance opening for the stripline conductor 19 which connected to 
the center conductor of the coaxial fitting 12. The outer conductor of 
coaxial connector 12 is returned to the two, conductive, cylindrical 
shells 32 and 33 which comprise the ground planes for the stripline 
assembly. 
Of course, it will be realized that the rotating assembly includes plural 
circumferentially spaced conductors 19 within the stripline assembly, one 
for each of the circumferentially distributed, rotating loops 20 depicted 
in the development of FIG. 2. 
Bearings 30 and 31 provide mechanical support and alignment with rotational 
freedom for the entire rotating assembly 16. It will be realized, however, 
that since axial and radial alignment and stability of the loop legs 20 
and 27 with respect to each other is important in the obtaining of stable 
and predictable operation of the device. Accordingly, those of skill in 
this art will realize that additional bearings may be necessary. For 
example, an additional, radially outward bearing similar to 11 might be 
provided through the same wall of the housing farther down towards the 
choke aperture 25. Similarly on the radially inward side, the annular 
tongue 23 can be of sufficient thickness to provide for a bearing therein. 
Other expedient's of course are available, such as the provision of a much 
thicker stripline top plate 49 which might extend radially in both 
directions over the top ends of housing 11 to provide an additional 
function of axial constraint as well as electrical continuity between the 
outer conductor of coaxial connector 12 and the conductive cylindrical 
walls 32 and 33. Since mechanical support and variation thereof are well 
within the ordinary skill of this art, it is not thought to be necessary 
to discuss bearing support of the rotating assembly 16 any further. 
In order to "close" the annular chamber housing the loops in a radio 
frequency sense, folded double quarter-wave chokes are built-in to the 
housing as indicated, these have the effect of producing radio frequency 
short circuit points at 24 and 25. The choke cavities and tongues 22 and 
23 defining these cavities are of course annular in shape extending the 
full 360.degree. in the plane normal to the center line of mast 10 in FIG. 
1. The operation of folded double quarter-wave choke devices is well 
understood in art of microwave devices. 
In FIG. 1A the conductive cylindrical shells which form the ground planes 
for the upper or stripline assembly portion of the rotating assembly 16 
are depicted. The blocks 47 and 48 are merely intended to indicate 
attachment to fixed and rotating structure respectively. That is, 47 
represents the fixed structure of the ship or other platform to which the 
mast 10 is affixed. Block 48 represents the rotating structure including 
the antenna array which would be mounted on the mast 10 above the rotary 
coupler of the invention as depicted in FIG. 1, the rotating structure of 
48 also including whatever drive and support structure would be normally 
included. 
Also shown in FIG. 2 is a method for equal phase or equal path length 
summation of all the individual loop energy transfers. A plurality of 
first fixed couplers, for example four-port, coaxial type couplers include 
39 and 40 in a first group and 37 and 38 in a second group, the latter 
mechanically rotating with the rotor loops such as 20. Couplers 39 and 40 
effectively couple in series into a first main line 42 which has a 
termination 41 and a stationary main line port 43, and individually 
connect, for example, by leads 34 and 36 (coaxial cable normally), to 
fixed loop legs 27 and an adjacent fixed loop in the manner already 
described in connection with FIG. 1. Similarly the rotating ports 
connected to rotating loops such as 20 and an adjacent one thereto are 
connected by leads 33 and 35 (also coaxial cable typically) to four-port 
coaxial couplers 37 and 38 respectively. Thus the second main line 44, 
which physically rotates with the entire rotating superstructure in 
cooperation with the coaxial couplers 37 and 38 etc., provides the 
combination or division of energy so that 45 becomes a rotating port 
connectable to the antenna which is a part of the rotating superstructure. 
The second main line 44 also has a termination or load 46. 
It will be noted that in the showing of FIG. 2, the rotating loops comprise 
narrower loop legs such as 20 as compared to the typical fixed loop leg 
27. This reduces the rotational inertia while limiting flutter in the 
overall power transfer between the terminals 43 and 45 to an acceptable 
level. Since the configuration of the interconnecting coaxial cable 
including 33, 35, 34 and 36 is intended to avoid phase disparity among the 
individual paths between 43 and 45, it follows that some signal energy 
phase disparity can exist between adjacent fixed and adjacent rotating 
loops, however this is not a significant consideration and accordingly the 
fixed loops may be designed with greater relative width and lesser 
circumferential spacing than implied on FIG. 2, that tending to reduce the 
aforementioned power transfer flutter. 
In FIG. 1, it will be noted that the return paths for the loop legs, such 
as 20 and 27 are through the conductive cylindrical shell 21 and the 
radially inner portion of the housing 11. Thus while the loop legs such as 
20 and 27 are discrete, the return paths are mingled in the conductive 
shell 21 and housing 11 respectively. 
Basically, the loop legs 20 and 27 including conductive pedestals 26 and 
11A are electrically one-quarter wavelength, axially measured, however the 
dimensioning is not critical and small variations within ordinary 
mechanical tolerances are not of great significance. 
In lieu of the stripline arrangement of the upper (second) axial section of 
the rotating assembly 16, a coaxial line between 12 and the rotating loop 
leg 20 might be employed as a variation. In that case, the dielectric 17 
and 18 of the stripline configuration might be replaced by solid metal, 
with axial bores, the internal walls of which would provide the outer 
condutors for the coaxial transmission lines thereby formed with 19 etc., 
as its center conductor. The illustrated stripline structure is preferred 
from the point of view of ease of construction and overall lightness, 
since a low-density, dielectric medium can be employed at 17 and 18. 
From an understanding of the invention it will be realized that the fixed 
loops can be placed adjacent the radially outward wall of the housing 11 
rather than the radially inward wall as illustrated. In that alternative 
situation, the rotating loops are similarly reversed, their loop return 
paths being provided by a cylindrical conductive shell extended from 32 
rather than 33. 
Either the stripline or coaxial line medium between coaxial connector 12 
and the loop leg 20 can be easily designed for an impedance match to the 
impedance presented by the loop. The factors affecting loop impedance 
include loop width, ground plane spacing and coupling to a loop of the 
other set (fixed or rotating). The practitioner of skill in this art can 
select the parameters of a particular design to provide proper impedance 
matching, which should be optimum when a rotor loop is centered over one 
of the stator loops. The technical literature including a paper entitled 
"Characteristic Impedance of Broad Side Coupled Strip Transmission Lines" 
by S. Cohn (IEEE Transactions MTT., Vol 8, pp 633-637), summarizes the 
analytical approach through which specific loop parameters may be 
determined. In one embodiment of the invention, the convenient loop 
characteristic impedance of 50 ohms was selected, this being readily 
consistent with the impedances out through the coaxial connectors, 
typically 12 and 29. 
FIG. 3 is self explanatory in depicting the effect of relative rotational 
position between given rotor and stator loops. Circuit accommodations may 
be made if necessary, to avoid the point illustrated at which the coupling 
falls below 3dB. 
Modifications and variations will suggest themselves to those of skill in 
this art, once the invention is understood, accordingly, it is not 
intended that the invention should be regarded as limited to the specific 
embodiment illustrated and described.