|Publication number||US3135960 A|
|Publication date||Jun 2, 1964|
|Filing date||Dec 29, 1961|
|Priority date||Dec 29, 1961|
|Publication number||US 3135960 A, US 3135960A, US-A-3135960, US3135960 A, US3135960A|
|Inventors||Kaiser Jr Julius A|
|Original Assignee||Kaiser Jr Julius A|
|Export Citation||BiBTeX, EndNote, RefMan|
|Patent Citations (7), Referenced by (18), Classifications (9)|
|External Links: USPTO, USPTO Assignment, Espacenet|
June 2, 1964 J. K SPIRAL MODE SELECTOR ARCHIMEDEAN AJSETK J CIRCUIT FOR A TWO-WIRE SPIRAL ANTENNA Filed Dec. 29, 1961 SIG/VAL J'IGNAL SOURCE sol/RC5 A 5 United States Patent 3,135,960 SPIRAL MGBE SELECTQR ClltilUlT FOR A TWG- WRE ARfiHIR/EDEAN SPEAK. ANTENNA Julius A. Kaiser, in, Keusingtou, Md assignor to the United States of America as represented by the Secretary of the Army Filed Dec. 2%, 1962, Ser. No. 1635559 2 Claims. (Cl. 343-%58) (Granted under Title 35, US. (lode (1952), see. 266) The invention described herein may be manufactured and used by or-for the Government for governmental purposes without the payment to me of any royalty time on.
This invention relates generally to spiral antennas and is more specifically directed to a two-wire Archimedean spiral antenna in which any desired radiation mode can be selected.
The spiral antenna, although a relatively recent development, has received much at ention because of its broad-band characteristics which make it eminently suitable for radar countermeasures, as well as other related fields. When a spiral antenna is energized at its input terminals, it radiates a broad circularly polarized beam to either side of the spiral. Each radiated beam is normal to the plane of the spiral, and the sense of circularity of polarization of the beam on one side corresponds to the winding sense of the spiral as viewed from the opposite side. Accordingly, the two radiated beams are identical except that the rotational sense of polarization of the radiated field on one side is the opposite of that on the other. In most applications, however, it is desirable that the spiral radiate to one side only. This is readily accomplished by appropriately backing the spiral on one side by a ground plane or cavity.
I have discovered that the spiral antenna can be excited in any one of a plurality of transmission modes, characterized as the 1st, 2nd, 3rd, 4th, etc. modes. Although this description will be limited to the 1st and 2nd modes, it should be realized that a spiral antenna can also be excited in an infinite number of higher order modes. Such an antenna is extremely useful for radar scanning, and can also be utilized as a simultaneous transmit-receive device by transmitting in one mode and receiving in another.
Accordingly, an object of this invention is to provide a circuit for energizing a spiral antenna in any preselected radiation mode.
A further object of this invention is to simultaneously energize a spiral antenna in a plurality of transmission modes.
These and other objects, features, and advantages of this invention will be apparent from the following specification taken in conjunction with the drawings, in which:
FIG. 1 is a diagrammatic representation of an Archimedean spiral antenna;
FIG. 2 represents a schematic diagram of the instant invention, and
FIG. 3 is a side view of the assembled components of the invention.
The two-wire spiral antenna behaves generally as though it were a two-wire transmission line which gradually, by virtue of its spiral geometry, transforms itself into a radiating structure or antenna. It is well known that a two-wire transmission line of narrow spacing relative to wavelength and of any length yields a negligible amount of radiation when excited at its terminals. This is due to the fact that the currents in the two wires of the line at any normal cross-section are always 180 out-ofphase so that radiation from one line is elfectively cancelled by the radiation from the other.
Suppose now that a twowire transmission line is formed into the spiral configuration of FIG. 1. Let P be a point on one wire of the transmission line at a distance measured along the wire from the input terminal A. Then the point Q on the other wire at the same distance from the input terminal A is situated diametrically opposite the point P with respect to the center 0, and both P and Q lie on the same circle centered at O. This implies that the point P and its neighboring point P on the other wire directly alongside P lie at such distances from A and B respectively, that the difference of these distances is precisely the arc length QP along the spiral. If Ar, the spacing between wires, is much smaller than r, the arc length QP is approximately equal to vrr. This difference in Wire lengths is constant regardless of the number of turns within r, provided only that the spacing between wires is uniform.
There are two items of interest that attach to a particular point on the two-wire spiral line: the total diiference in wire lengths of the two-wire line to the point and the circumference or path length of the particular turn on which the point lies. For the circular spiral Where the wires are equally spaced, at a point whose radial distance from the spiral center is r, the difference in line lengths equals TH and the circumference equals 211'). When r is A/ 211-, the phase change is A/ 2 and the circumference is A. Assuming that each wire supports a progressive wave of current and that these current waves are anti-phase at the input terminals A and B, it is clear that the difference in phase of the two current elements at any point PP on the two wire line, measured in radians is- 1r (the input phase ditference)+2wr/ \(1rr). Thusneighboring current elements start anti-phase at the feed points A and B, and gradually come into phase as they proceed outward along the spiral two wire line. When r is 211-, these currents are precisely in phase and radiation is a maximum. Moreover, the condition for precisely iii-phase currents occurs at two points diametrically opposite each other relative to the center 0. 1
Radiation from the spiral then is centered in a ring of turns of one wavelength mean circumference. This property makes the spiral antenna an inherently broadband device, the basic requirement being only that the radius be large enough to allow a half wavelength of phase shift. Also, inasmuch as the radiating ring is a Wavelength in circumeference for all frequencies over whi h the spiral operates, a constant beam width is maintained.
Radiation from the one-wavelength ring as described above is termed the first mode of radiation, because this represents the first occasion for which conditions are correct for radiation. Currents existing beyond the one-wavelength ring will continue experiencing phase change as they progress outward, and assuming the spiral structure is large enough, these currents will be out of phase again at a radius where the circumference is two wavelengths and in phase at the three-wavelength circumference. No radiation occurs from the two-wavelength ring because the currents on adjacent filaments are anti-phase. At the three wavelength ring radiation can occur if currents exist, giving rise to the third mode of radiation. It follows that currents which are anti-phase at the input terminals can excite only the odd modes of radiation. If on the other hand the two center terminals are tied together and excited in some manner, currents start in-phase at the center of the spiral. In progressing outward these currents experience phase change. When the one-wavelength circumference is reached they are anti-phase and no radiation occurs. At the two wavelength circumference, which is defined as the locus of the second radiation mode, the currents are once again in phase, and radiation is once again strong. Currents around the two Wavelength circumference of a circular spiral, are in such phase as to by maximum gain along the axis and 360 phase change per spiral revolution and the second radiation mode is characterized by maximum gain in the plane ofthe spiral and 720 phase change per revolution.
Referring now to the exploded view of FIG. 2 and the assembled side view of FIG. 3 the invention is shown as comprising a two-wire Archimedean spiral antenna 20 consisting of wires and 11. 'Ring network 16 consisting of input terminals 1 and 3, output terminals 2 and 4 and conducting strip 17 is a standard microwave component in which currents entering terminal I arrive at terminals 2 and 4 in phase opposition while currentsentering terminal 3 arrive at terminals 2 and 4 in phase. Metal plate 13 is provided for use as a ground plane to insure launching of the energy onto the spiral. Terminals 2 and 4 of the ring network are connected to the input terminals A and B of the two-wire spiral by the inner conductors 18and 19 of coaxial cables having outer conductors 14 and 15 which are electrically attached to the ground plane 13. Dielectric plate 12 is provided to insulate the ground plate 13 from the antenna when the components are assembled as shown in FIG. 3.
, If it were desired to operate the antenna in the first radiation mode for example, current would be fed into arm 1 of the ring network 16. This may be accomplished,
for example, by positioning the switch associated with.
signal source A in the left-hand position and the switch associated with signal source B in the right-hand position. The current would then reach the terminals A and B antiphase and as described above, at the one wavelength circumference the currents would be in phase and radiation would occur. On the other hand, if it weredesired that the antenna operate in the second mode of radiation, current would be fed into terminal 3 of the ring network 16 position. This results in a phenomenon called beam cock. The resultant field obtained from adding the first radiation mode characterized by maximum gain along the axis and 360 phase change per spiral revolution, and the second radiation mode characterized by maximum gain in the plane of the spiral and 720 phase change per revolution, is generally a 'pencil beam that points other than along the spiral axis. The amount of beam cock is dependent upon the relative amplitude of the two radiation modes and the direction is determined from the relative phases. Such a radiation field is desirable in devicessuch as direction finders and radar detectors Where beam directivity is required. a p
Thus, there has been described a circuit which permits a spiral antenna to be operated in any of a plurality of radiation modes either individually or concurrently and which lends itself to a wide varietyof highly useful ap-' plications in the fields of radar, direction finders and simultaneous transmit-receive devices. Itshould be realized that the embodiment described is only exemplary and that many modifications can be made in the instant circuit Without departing from the scope of the invention.v For example, in place of the circular spiral antenna described,
a square spiral or rectangular spiral can similarly be utilized and the same considerations would apply to the operation of these embodiments as those described in connection with the circular spiral.
I claim as my invention:
- 1. A selective .mode spiral antenna system which is adapted to radiate in either odd 'or even modes aiternately or both odd and even modes simultaneously comprising a two-wire Archimedean spiral antenna having two 'input terminals; a ring network having two output'terminals,
a first input terminal which passes applied current to said output terminals in phase opposition, and a second input terminalwhichpas'sesapplied current to said output terminals in phase, two-coaxial cables each having. an outer conductor and an inner conductor, said inner conductors being electrically connected between the output terminals of said ring network and the input terminals of said spiral antenna; a metal ground plane interposed between said ring network and said spiral antenna, said outer conducand the currents would consequently reach terminals A and B in phase. This may be accomplished, for example, by positioning the switches associated with signal sources A and B in the left-hand position. The currents would then be out of phase at the one wavelengthcir cumference and in phase again at the two wavelength circumference where radiation would occur. In 'order' to excite the antenna in a higher-order mode of radiation, such as the third or fourth mode, it would be necessary to provide input terminals further out along the spiral, for example at the two-wavelength circumference. Then, wires 18 and 19 would be attached to these terminals rather than to terminals A' and B and the operation would be similar to that described for the first and second modes. That is, in order to excite the antenna in an odd mode, current would be fed into input terminal 1 of ring network 16 and for the even modes current would be fed, into arm 3 of the ring network. i
It is also possible to simultaneously excite the two-wire spiral in a plurality of transmission modes since adjacent modes are inherently isolated from one another. Thus, the circuit could be utilized as a simultaneous transmitreceive device by transmitting, for example, in the first mode and receivingin the second mode. By the same token, it is possible to transmit in two modes simultaneously such as the first and second modes. This may be accomplished, for example, by positioning the switches associated with signal sources A and B in the right-hand tors being electrically connected to said ground plane; and V V a dielectric insulator interposed between said spiral ank tenna and saidground plane.
2. A spiral antenna system which is capable of elec trically scanning a target area while maintaining the an: tenna in a fixed position comprising a two-wire Archimedean spiral antenna having two input terminals; means for causing said antenna to radiate apencil beam having" a predetermined. orientation with respect to the plane of said spiral; said means comprising a ring network having two output terminals, a first input terminal which passes applied current to said output terminals in'phase .opposi-I tion, and a second input terminal which passes applied current to said output terminals in phase, means connect ing the output terminals of said ring network to the input terminals of said antenna, and means for applying current simultaneously to said first and second input terminals, of
the ring network.
References Cited in the file of this patent UNITED STATES PATENTS 2,1 ,8 Gothe June, 6. 1 2 2,863,145 Turner Dec; 2, 1958 2,947,000 Marston et a1. July 26 1-960 2,953,781 Donnellan et al. Sept. 20,1960
2,990,548 Wheeler 'June 27, 1961 3,019,439 Reis et al. -Jan. 30,1962 3,039,099
Chait et al. June 12,1962
|Cited Patent||Filing date||Publication date||Applicant||Title|
|US2160857 *||Mar 25, 1936||Jun 6, 1939||Telefunken Gmbh||High frequency system|
|US2863145 *||Oct 19, 1955||Dec 2, 1958||Turner Edwin M||Spiral slot antenna|
|US2947000 *||Nov 28, 1958||Jul 26, 1960||Kaiser Jr Julius A||Beacon antenna using spiral|
|US2953781 *||Nov 30, 1959||Sep 20, 1960||Donnellan John R||Polarization diversity with flat spiral antennas|
|US2990548 *||Feb 26, 1959||Jun 27, 1961||Westinghouse Electric Corp||Spiral antenna apparatus for electronic scanning and beam position control|
|US3019439 *||Sep 19, 1957||Jan 30, 1962||Martin Marietta Corp||Elliptically polarized spiral antenna|
|US3039099 *||Jun 25, 1959||Jun 12, 1962||Chait Herman N||Linearly polarized spiral antenna system|
|Citing Patent||Filing date||Publication date||Applicant||Title|
|US3175217 *||Jan 28, 1963||Mar 23, 1965||Kaiser Jr Julius A||Direction finder|
|US3228030 *||Jun 11, 1965||Jan 4, 1966||Gen Dynamics Corp||Shielded antenna|
|US3241148 *||Apr 4, 1960||Mar 15, 1966||Mcdonnell Aircraft Corp||End loaded planar spiral antenna|
|US3445853 *||Jan 12, 1966||May 20, 1969||Us Army||Linear scanning array with adjustable polarizers and hybrids in the coupling network|
|US5343173 *||Jun 28, 1991||Aug 30, 1994||Mesc Electronic Systems, Inc.||Phase shifting network and antenna and method|
|US5495258 *||Sep 1, 1994||Feb 27, 1996||Nicholas L. Muhlhauser||Multiple beam antenna system for simultaneously receiving multiple satellite signals|
|US5619218 *||Jun 6, 1995||Apr 8, 1997||Hughes Missile Systems Company||Common aperture isolated dual frequency band antenna|
|US5646633 *||Apr 5, 1995||Jul 8, 1997||Mcdonnell Douglas Corporation||Microstrip antenna having a plurality of broken loops|
|US5678219 *||Mar 29, 1991||Oct 14, 1997||E-Systems, Inc.||Integrated electronic warfare antenna receiver|
|US5831582 *||Aug 25, 1995||Nov 3, 1998||Easterisk Star, Inc.||Multiple beam antenna system for simultaneously receiving multiple satellite signals|
|US6087999 *||Jan 8, 1998||Jul 11, 2000||E*Star, Inc.||Reflector based dielectric lens antenna system|
|US6107897 *||Jul 7, 1998||Aug 22, 2000||E*Star, Inc.||Orthogonal mode junction (OMJ) for use in antenna system|
|US6160520 *||Mar 22, 1999||Dec 12, 2000||E★Star, Inc.||Distributed bifocal abbe-sine for wide-angle multi-beam and scanning antenna system|
|US6181293 *||Jul 7, 1998||Jan 30, 2001||E*Star, Inc.||Reflector based dielectric lens antenna system including bifocal lens|
|US6198449||Oct 15, 1998||Mar 6, 2001||E*Star, Inc.||Multiple beam antenna system for simultaneously receiving multiple satellite signals|
|US8610515||May 9, 2011||Dec 17, 2013||Northrop Grumman Systems Corporation||True time delay circuits including archimedean spiral delay lines|
|EP0825674A1 *||Feb 24, 1997||Feb 25, 1998||Hisamatsu Nakano||Single-wire spiral antenna|
|EP0825674A4 *||Feb 24, 1997||Oct 7, 1998||Nippon Antena Kabushiki Kaisya||Single-wire spiral antenna|
|U.S. Classification||343/858, 343/895, 333/101, 342/14, 343/876|
|International Classification||H01Q9/27, H01Q9/04|