US2958081A - Unidirectional broadband antenna comprising modified balanced equiangular spiral - Google Patents
Unidirectional broadband antenna comprising modified balanced equiangular spiral Download PDFInfo
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- US2958081A US2958081A US823998A US82399859A US2958081A US 2958081 A US2958081 A US 2958081A US 823998 A US823998 A US 823998A US 82399859 A US82399859 A US 82399859A US 2958081 A US2958081 A US 2958081A
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- 239000004793 Polystyrene Substances 0.000 description 1
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- 230000005540 biological transmission Effects 0.000 description 1
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q11/00—Electrically-long antennas having dimensions more than twice the shortest operating wavelength and consisting of conductive active radiating elements
- H01Q11/02—Non-resonant antennas, e.g. travelling-wave antenna
- H01Q11/08—Helical antennas
- H01Q11/083—Tapered helical aerials, e.g. conical spiral aerials
Definitions
- This invention relates to antennas and, more particularly, it relates to antennas having unidirectional radiation patterns that are essentially independent of frequency over wide bandwidths.
- An antenna which can be made to have a very Wide band of operations in which performance is independent of Wavelength is the balanced equiangular spiral antenna.
- the one specified length for this antenna, the -arm length needvnot be large compared to a wavelength, and in fact need only be comparable to a wavelength at the lowest frequency of operation to obtain performance essentially independent of frequency.
- This antenna comprises two coplanar spiral arms, each arm being defined by two identical equiangular spiral curves, one rotated through a fix-ed angle around the origin (i.e., the central point of the antenna) with respect to the other.
- the arms themselves are also identical in shape, one being rotated through an angle of yabout 180 from the position of the other.
- Planar antennas of this type have broadband bidirectional radiation patterns extending perpendicularly to the plane of the antenna.
- the balanced equiangular spiral antennas described above can be modified to exhibit unidirectional radiation patterns while maintaining the broad bandwidths which such antennas possess.
- the unidirectional radiation patterns are achieved by Wrapping a planar balanced equiangular spiral antenna on the surface of a cone and feeding the antenna at the apex thereof by a feed cable carried along one arm.
- Such antennas exhibit substantially symmetric radiation patterns having a maximum on the antenna ⁇ axis off the apex of the cone.
- Figure l is a plan View of an antenna embodying the features of the invention.
- Figure 2 is a top View of the antenna shown in Figure 1;
- Figures 3, 4, and 5 are typical radiation patterns for the antenna of Figure l.
- Figure 6 is a sketch identifying the coordinate system used in Figures 3, 4, Iand 5.
- the antenna of the invention comprises two spiraling arms 11 and 12 which are wound on the surface of an electrically nonconductve cone 13. As shown, a small portion of the cone near the apex is truncated, since it would be physically impossible to construct this portion of the antenna because of the extremely small size of the arms in this region.
- FIG. 2 the top View, of the antenna of Figure 1, shows a projection thereof on a plane surface.
- the two arms of the antenna are each defined by an equi-angular (or logarithmic) spiral.
- An equiangular spiral is a planeA curve which may be defined by the equation: v
- the equiangular spiral curve derives its name from one of ⁇ its properties, namely, the fact that the angle formed by a radius vector and a tangent to the curve at the Vpoint of intersection with the radius vector, is always constant.
- the inner edge of arm 11 is actually the same curve as that deningthe outer edge, except that yit has been displaced about ⁇ the origin through an angle
- the curves delining arm 12 are identical with those defining arm 11 but have been rotated through (1r radians) and thus have the equations for the outer edge and p4 tem-"6) Kps forthe inner edge.
- a planar antenna having the form depicted in Figure 2 has a bidirectional radiation pattern extending perpen- ⁇ dicularly to the plane of the paper on which the ligure is printed.
- a cone 13 of a suitable electrically insulating material such as styrofoam, as shown inv Figure l, the radiation pattern of the antenna becomes unidirectional with the maximum lying olir the apex of the cone, as shown in Figure 6, 1
- the performance of the conical antenna of the invention is not dependent on the constants given in the equations to any marked degree. Except for the fact that the more tightly wound antennas have somewhat smoother and slightly more rotationally symmetric patterns (determined by the value given to a), the rate of spiral rotation has only a secondary effect on the shape of the radiation pattern. Likewise, the value of K may vary considerably without seriously affecting the performance of the antenna.
- the arms of the antenna are made of an electrically conducting material, suitably sheet copper, aluminum, or the like.
- the feed cable 14 comprises a coaxial cable carried by one of the arms, e.g., 12, the outer conductor of the cable being bonded to the arm and the inner conductor being electrically connected to the other arm (i.e., 11) at the vertex.
- a dummy feed cable 16 may be bonded to arm 11 in a manner similar to that used with cable 14. This method of feeding the antenna and the dummy cable are not an essential requirement of the invention but are helpful in achieving the maximum bandwidth of which the antenna is capable.
- the antennas of the invention can be constructed in any suitable manner.
- a preferred method is by drawing the outline of the arms on the development of the cone, which drawing is then transferred by a silk screen process to a rthin copper-clad Teflon impregnated glass cloth. After forming the arms by etching away the undesired portions of the copper cladding, the base material is formed into a cone and the arms are soldered along the joint.
- the cone thus formed can be supported by any of the well-known materials which are eicient insulators at high frequencies, such as polystyrene. Since the cone of insulating material is not an essential part of the antenna and is used only to support the arms, it can be eliminated if -the arms are made of a rigid material, such as a sheet of copper strong enough to support its own weight.
- the upper frequency limit of the band of operation for the antennas of the invention is determined by the fineness of the construction of the spiral at the feed point, i.e., at the vertex of the cone. Since equiangular spiral curves converge to a point as a limit at the origin, it is necessary in a practical structure to terminate 4the central portion in a small straight or tapered section.
- the upper cut-off frequency of the antenna is the frequency at which the truncated apex of the cone becomes approximately 1A wavelength in diameter. As an example, for a termination of the apex at a l-inch diameter the upper frequency limit is approximately 3000-4000 mc.
- the operating bandwidth is at the control of the designer.
- the low frequency limits are affected by the length and the width of the arms of the antennas and hence the diameter of the base of the cone, and are independent of the upper frequency limit.
- the low frequency limit can be lowered by increasing the arm length and/ or by increasing the width of the arms.
- an apex diameter of 1A wavelength at the highest frequency of operation and a base diameter of approximately /s wavelengths at the lowest frequency of operation should provide patterns with a front to back ratio of l5 db or greater and essentially circularly polarized radiation.
- the antennas of the invention have arms each edge of which is defined by an equiangular spiral, so that the width of each arm constantly increases at increasing distances from the apex of the cone, it is also possible to construct practical antennas having advantageously wide bandwidths in which the width of the arm is constant or essentially constant.
- antennas in which the arms consist of coaxial cables alone, arranged to follow equiangular spiral paths have acceptable patterns, although they may not have as low a frequency capability for any given antenna size as the wider true equiangular spiral structures.
- These wire versions of the antenna can most conveniently be constructed from rigid wall coaxial cable and are advantageous for use at the UHF and VHF frequencies.
- the beamwidth for the pattern as shown in Figure 5 at 2000 mc is 70i2 for Eq) polarization and i3 for Ep polarization for any angle 1.
- the average beamwidths of ⁇ the same antenna on a 30 cone ( Figure 4) are approximately 80 and 100.
- Antennas in accordance with the invention can be made to have bandwidths of l0 to Z0 or more to l over which the radiation patterns and input impedance are essentially constant.
- these are balanced antennas and a balanced feed is necessary for optimum performance.
- the feed may be brought in perpendicular to the antenna by a balanced feed line or by an unbalanced line and balancing transformer or balun.
- the bandwidth of this latter method depends upon the bandwidth of the balun.
- the rapid decay of the current along the arms makes possible the previously mentioned highly useful method of feeding the balanced antenna with an unbalanced transmission line.
- the cable is bonded to the ground screen between the arms of the metal structure and is carried to the origin where the center conductor is tied to the opposite arm. Since the ends of the antenna arms do not carry appreciable antenna currents except at the very lowest frequency of operation, the arms themselves act as an infinite balun, the feed terminals are isolated from ground in a balanced manner and the outside of the feed cable beyond the antenna arm does not carry a significant amount of antenna current. However, as the frequency of operation is decreased a point will be reached where the presence and location of this cable alters the radiation pattern. This frequency, however, is below that at which the antenna should be expected to operate satisfactorily. In order to compensate for the presence of the feed cable insofar as possible, a dummy cable may be placed on the other arm to maintain physical symmetry.
- the input impedance of the antennas of the invention remains relatively constant over a wider frequency range than the usable pattern bandwidth.
- a unidirectional broadband antenna comprising two substantially identical electrically conducting elements wound so as to lie on a conical surface, each of said elements having at least one edge which projected on a plane perpendicular to the axis of said conical surface is substantially in the form of an equiangular spiral, the first of said elements being displaced from the second of said elements by rotation through an angle of about 180.
- a unidirectional broadband antenna comprising two substantially identical electrically conducting elements wound so as to lie on a conical surface, each of said elements being defined by a pair of curves which when projected on a plane perpendicular to the axis of said conical surface have the form of equiangular spirals, the rst of said elements being displaced from the second of said elements by rotation about the axis of said conical surface through an angle of about 180.
- a unidirectional broadband antenna comprising two substantially identical elements formed of a thin electrically conducting sheet material, said elements being wound so as to lie on a conical surface, the irst of said elements being partially defined by the curves having the equations lf asind 91:106( 2) and i l
- the antenna of claim 5 which is fed at the apex by a feed cable which is carried on one of said elements.
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Description
Oct. 25, 1960 J. D. DYSON UNIDRECTIONAL BROADBAND ANTENNA COMPRISING 2 Sheets-Sheet 2 United States Patent C) UNIDIRECTIONAL BROADBAND ANTENNA COM- PRISING MODIFIED BALANCED EQUIANGU- LAR SPIRAL John D. Dyson, Champaign, Ill., assigner to University of Illinois Foundation, a corporation of Illinois Filed June 30, 1959, Ser. No. 823,998
8 Claims. (Cl. 343-895) This invention relates to antennas and, more particularly, it relates to antennas having unidirectional radiation patterns that are essentially independent of frequency over wide bandwidths.
It .is known that if the shape of an antenna were such that it could be specified entirely by angles, the antenna would make an ideal broadband radiator, since its operation would be theoretically independent of frequency. All antennas which meet this criterion, however, are infinite in extent, so that it is necessary to specify at least one length for an 4antenna of finite size. By making this one length very large compared with the wavelength of operation of a given antenna, it is possible in some cases to achieve antenna performance which is practically independent of wavelength over wide bandwidths.
An antenna which can be made to have a very Wide band of operations in which performance is independent of Wavelength is the balanced equiangular spiral antenna. The one specified length for this antenna, the -arm length, needvnot be large compared to a wavelength, and in fact need only be comparable to a wavelength at the lowest frequency of operation to obtain performance essentially independent of frequency. This antenna comprises two coplanar spiral arms, each arm being defined by two identical equiangular spiral curves, one rotated through a fix-ed angle around the origin (i.e., the central point of the antenna) with respect to the other. The arms themselves are also identical in shape, one being rotated through an angle of yabout 180 from the position of the other. Planar antennas of this type have broadband bidirectional radiation patterns extending perpendicularly to the plane of the antenna.
It has now been discovered that the balanced equiangular spiral antennas described above can be modified to exhibit unidirectional radiation patterns while maintaining the broad bandwidths which such antennas possess. The unidirectional radiation patterns are achieved by Wrapping a planar balanced equiangular spiral antenna on the surface of a cone and feeding the antenna at the apex thereof by a feed cable carried along one arm. Such antennas exhibit substantially symmetric radiation patterns having a maximum on the antenna `axis off the apex of the cone.
The construction of the antennas of the invention will be better understood from the following detailed descrip tion thereof taken in conjunction with the accompanying diagrams in which:
Figure l is a plan View of an antenna embodying the features of the invention;
Figure 2 is a top View of the antenna shown in Figure 1;
Figures 3, 4, and 5 are typical radiation patterns for the antenna of Figure l; and
Figure 6 is a sketch identifying the coordinate system used in Figures 3, 4, Iand 5.
As can be seen from Figures l and 2, the antenna of the invention comprises two spiraling arms 11 and 12 which are wound on the surface of an electrically nonconductve cone 13. As shown, a small portion of the cone near the apex is truncated, since it would be physically impossible to construct this portion of the antenna because of the extremely small size of the arms in this region.
Figure 2, the top View, of the antenna of Figure 1, shows a projection thereof on a plane surface. In such a projection the two arms of the antenna are each defined by an equi-angular (or logarithmic) spiral. An equiangular spiral is a planeA curve which may be defined by the equation: v
where p and are the conventional polar coordinates and a and k are positive constants.
The equiangular spiral curve derives its name from one of `its properties, namely, the fact that the angle formed by a radius vector and a tangent to the curve at the Vpoint of intersection with the radius vector, is always constant. The constant a determines the rate of spiral of the curve and the constant k determines the physical starting point of the curve when =0, as will be apparent to those skilled in the art.
Considering the plane curves shown in 'Figure 2 (that is, the projection of the outlines of the arms of the actual antenna) it will be seen that the outer and inner edges of both arms are defined by the same curve which is rotated Iabout the origin or central point of the figure. Thus, for example, consider the outer edge of arm 11. This curve can be represented by an equation of the form.
The inner edge of arm 11 is actually the same curve as that deningthe outer edge, except that yit has been displaced about `the origin through an angle The equation of the inner edge of arm 11 may therefore be represented by s p2=ke Km where In a similar manner it will be seen that the curves delining arm 12 are identical with those defining arm 11 but have been rotated through (1r radians) and thus have the equations for the outer edge and p4 tem-"6) Kps forthe inner edge.
A planar antenna having the form depicted in Figure 2 has a bidirectional radiation pattern extending perpen-` dicularly to the plane of the paper on which the ligure is printed. By wrapping the arms of the antenna about a cone 13 of a suitable electrically insulating material, such as styrofoam, as shown inv Figure l, the radiation pattern of the antenna becomes unidirectional with the maximum lying olir the apex of the cone, as shown in Figure 6, 1
The curves delining the edges of the arms of the antenna shown inFigure 1 can be described by equations similar 4to those used for the planar version thereof, with the introduction of an additional variable, the cone angle The radial distance along the surface of the cone (extended if required) from the vertex to the outer edge of one arm (e.g., 11) is given by the equation Patented oct. 25, 19st)` where and 44 is the included cone angle. The inner edge of arm 11 is defined by p2: kebw-a) z K' p1 where K e-b The edges of the other arm (i.e., 12) are defined by the equations Par-Pie-b1r (outer edge) and P4=Kpa (inner edge).
It can be seen that for an included cone angle, i/f, of 180 (i.e., the planar form of the antenna) the above equations reduce to the form as previously described.
As in the case of its planar version, the performance of the conical antenna of the invention is not dependent on the constants given in the equations to any marked degree. Except for the fact that the more tightly wound antennas have somewhat smoother and slightly more rotationally symmetric patterns (determined by the value given to a), the rate of spiral rotation has only a secondary effect on the shape of the radiation pattern. Likewise, the value of K may vary considerably without seriously affecting the performance of the antenna.
The arms of the antenna are made of an electrically conducting material, suitably sheet copper, aluminum, or the like. The feed cable 14 comprises a coaxial cable carried by one of the arms, e.g., 12, the outer conductor of the cable being bonded to the arm and the inner conductor being electrically connected to the other arm (i.e., 11) at the vertex. In order to maintain the physical symmetry of the antenna a dummy feed cable 16 may be bonded to arm 11 in a manner similar to that used with cable 14. This method of feeding the antenna and the dummy cable are not an essential requirement of the invention but are helpful in achieving the maximum bandwidth of which the antenna is capable.
The antennas of the invention can be constructed in any suitable manner. A preferred method is by drawing the outline of the arms on the development of the cone, which drawing is then transferred by a silk screen process to a rthin copper-clad Teflon impregnated glass cloth. After forming the arms by etching away the undesired portions of the copper cladding, the base material is formed into a cone and the arms are soldered along the joint. The cone thus formed can be supported by any of the well-known materials which are eicient insulators at high frequencies, such as polystyrene. Since the cone of insulating material is not an essential part of the antenna and is used only to support the arms, it can be eliminated if -the arms are made of a rigid material, such as a sheet of copper strong enough to support its own weight.
The upper frequency limit of the band of operation for the antennas of the invention is determined by the fineness of the construction of the spiral at the feed point, i.e., at the vertex of the cone. Since equiangular spiral curves converge to a point as a limit at the origin, it is necessary in a practical structure to terminate 4the central portion in a small straight or tapered section. The upper cut-off frequency of the antenna is the frequency at which the truncated apex of the cone becomes approximately 1A wavelength in diameter. As an example, for a termination of the apex at a l-inch diameter the upper frequency limit is approximately 3000-4000 mc.
The operating bandwidth is at the control of the designer. The low frequency limits are affected by the length and the width of the arms of the antennas and hence the diameter of the base of the cone, and are independent of the upper frequency limit. Thus, for example, the low frequency limit can be lowered by increasing the arm length and/ or by increasing the width of the arms. As an example, for a cone angle rl/ of 20, and parameters of the order of K=.85 to .9 and b=.053, an apex diameter of 1A wavelength at the highest frequency of operation and a base diameter of approximately /s wavelengths at the lowest frequency of operation should provide patterns with a front to back ratio of l5 db or greater and essentially circularly polarized radiation.
Although in the preferred form the antennas of the invention have arms each edge of which is defined by an equiangular spiral, so that the width of each arm constantly increases at increasing distances from the apex of the cone, it is also possible to construct practical antennas having advantageously wide bandwidths in which the width of the arm is constant or essentially constant. Thus, for example, antennas in which the arms consist of coaxial cables alone, arranged to follow equiangular spiral paths, have acceptable patterns, although they may not have as low a frequency capability for any given antenna size as the wider true equiangular spiral structures. These wire versions of the antenna can most conveniently be constructed from rigid wall coaxial cable and are advantageous for use at the UHF and VHF frequencies.
The practical results which are obtainable with the antennas of the invention are demonstrated by an antenna defined by the constants 1:0303 and K=0.925 with arms 150 cm. in length. This antenna was wrapped on conical surfaces made of styrofoam, having cone angles ranging from 60 to 20. The radiation patterns obtained with these antennas at a frequency of 2000 mc. are Shown in Figures 3, 4, and 5. Figure 3 shows the radiation pattern for a cone angle of 60, Figure 4, a 30 cone angle, and Figure 5, a 20 cone angle. lt can be seen that as the cone angle drops below 60, there is a marked increase in the ratio of front to back radiation. The absence of back radiation for 1,1/:20 (Figure 5) is evident. For all these antennas there was no basic tilt to the patterns and the lobes were rotationally essentially symmetric. The patterns rotate with frequency but this rotation is masked in the symmetrical structure since the pattern beamwidth is independent of the angle qs. As an example, the beamwidth for the pattern as shown in Figure 5 at 2000 mc, is 70i2 for Eq) polarization and i3 for Ep polarization for any angle 1. The average beamwidths of `the same antenna on a 30 cone (Figure 4) are approximately 80 and 100.
Antennas in accordance with the invention can be made to have bandwidths of l0 to Z0 or more to l over which the radiation patterns and input impedance are essentially constant. In order to obtain the maximum bandwidth, however, it should be noted that these are balanced antennas and a balanced feed is necessary for optimum performance. The feed may be brought in perpendicular to the antenna by a balanced feed line or by an unbalanced line and balancing transformer or balun. The bandwidth of this latter method, of course, depends upon the bandwidth of the balun. The rapid decay of the current along the arms however, makes possible the previously mentioned highly useful method of feeding the balanced antenna with an unbalanced transmission line. The cable is bonded to the ground screen between the arms of the metal structure and is carried to the origin where the center conductor is tied to the opposite arm. Since the ends of the antenna arms do not carry appreciable antenna currents except at the very lowest frequency of operation, the arms themselves act as an infinite balun, the feed terminals are isolated from ground in a balanced manner and the outside of the feed cable beyond the antenna arm does not carry a significant amount of antenna current. However, as the frequency of operation is decreased a point will be reached where the presence and location of this cable alters the radiation pattern. This frequency, however, is below that at which the antenna should be expected to operate satisfactorily. In order to compensate for the presence of the feed cable insofar as possible, a dummy cable may be placed on the other arm to maintain physical symmetry.
The input impedance of the antennas of the invention remains relatively constant over a wider frequency range than the usable pattern bandwidth.
The foregoing detailed description has been given for clearness of understanding only, and no unnecessary limitations should be understood therefrom, as modifications Will be obvious to those skilled in the art.
What is claimed is:
l. A unidirectional broadband antenna comprising two substantially identical electrically conducting elements wound so as to lie on a conical surface, each of said elements having at least one edge which projected on a plane perpendicular to the axis of said conical surface is substantially in the form of an equiangular spiral, the first of said elements being displaced from the second of said elements by rotation through an angle of about 180.
2. The antenna of claim 1 wherein the cone-angle of said conical surface is less than about 60.
3. A unidirectional broadband antenna comprising two substantially identical electrically conducting elements wound so as to lie on a conical surface, each of said elements being defined by a pair of curves which when projected on a plane perpendicular to the axis of said conical surface have the form of equiangular spirals, the rst of said elements being displaced from the second of said elements by rotation about the axis of said conical surface through an angle of about 180.
4. The antenna of claim 2 wherein the cone angle of said conical surface is less than about 5. A unidirectional broadband antenna comprising two substantially identical elements formed of a thin electrically conducting sheet material, said elements being wound so as to lie on a conical surface, the irst of said elements being partially defined by the curves having the equations lf asind 91:106( 2) and i l |11 asin- @-6) Pz=ke( 2) the second of said elements being partially defined by the curves ill la=lfre a sm Low-f) and l x0 p4=ke a sin 5)(15-1-6) where p represents the distance along the conical surface from the apex to any point on one of said curves, e is the natural logarithm base, :,l/ is the cone angle of the conical surface, p is the angle of rotation from a base line in a plane passing through the apex of said conical surface perpendicular to the axis thereof, to the projection in said plane of the line representing the distance p, and a, k and are constants.
6. The antenna of claim 5 wherein gb is an angle of less than about 60.
7. The antenna of claim 5 which is fed at the apex by a feed cable which is carried on one of said elements.
8. Ihe antenna of claim 7 in which a dummy feed cable is carried by the other of said elements.
No references cited.
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US823998A US2958081A (en) | 1959-06-30 | 1959-06-30 | Unidirectional broadband antenna comprising modified balanced equiangular spiral |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US823998A US2958081A (en) | 1959-06-30 | 1959-06-30 | Unidirectional broadband antenna comprising modified balanced equiangular spiral |
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| US2958081A true US2958081A (en) | 1960-10-25 |
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| US823998A Expired - Lifetime US2958081A (en) | 1959-06-30 | 1959-06-30 | Unidirectional broadband antenna comprising modified balanced equiangular spiral |
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Cited By (24)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3110030A (en) * | 1961-05-25 | 1963-11-05 | Martin Marietta Corp | Cone mounted logarithmic dipole array antenna |
| US3188643A (en) * | 1960-12-29 | 1965-06-08 | Univ Illinois | Circularly polarized omnidirectional cone mounted spiral antenna |
| US3192529A (en) * | 1961-03-20 | 1965-06-29 | Ryan Aeronautical Co | Multi-helix antenna on inflatable satellite |
| US3241148A (en) * | 1960-04-04 | 1966-03-15 | Mcdonnell Aircraft Corp | End loaded planar spiral antenna |
| US3283332A (en) * | 1964-08-24 | 1966-11-01 | Nussbaum Milton | "null" conical helix |
| US3296536A (en) * | 1960-06-06 | 1967-01-03 | Univ Ohio State Res Found | Combined antenna and tunnel diode converter circuit |
| US3381297A (en) * | 1965-02-11 | 1968-04-30 | Csf | Wide-band goniometer system |
| US3509465A (en) * | 1965-10-22 | 1970-04-28 | Sylvania Electric Prod | Printed circuit spiral antenna having amplifier and bias feed circuits integrated therein |
| DE1541386B1 (en) * | 1965-11-15 | 1970-11-26 | Granger Associates Palo Alto | Broadband spiral antenna |
| US3618114A (en) * | 1968-12-16 | 1971-11-02 | Univ Ohio State Res Found | Conical logarithmic-spiral antenna |
| US3633210A (en) * | 1967-05-26 | 1972-01-04 | Philco Ford Corp | Unbalanced conical spiral antenna |
| FR2299739A1 (en) * | 1975-01-29 | 1976-08-27 | Abreu Joao Do Espirito Santo | HELICOIDAL TYPE ANTENNA |
| US4161737A (en) * | 1977-10-03 | 1979-07-17 | Albright Eugene A | Helical antenna |
| US4525720A (en) * | 1982-10-15 | 1985-06-25 | The United States Of America As Represented By The Secretary Of The Navy | Integrated spiral antenna and printed circuit balun |
| US4559539A (en) * | 1983-07-18 | 1985-12-17 | American Electronic Laboratories, Inc. | Spiral antenna deformed to receive another antenna |
| US4605934A (en) * | 1984-08-02 | 1986-08-12 | The Boeing Company | Broad band spiral antenna with tapered arm width modulation |
| US4630064A (en) * | 1983-09-30 | 1986-12-16 | The Boeing Company | Spiral antenna with selectable impedance |
| US5640170A (en) * | 1995-06-05 | 1997-06-17 | Polhemus Incorporated | Position and orientation measuring system having anti-distortion source configuration |
| US5815122A (en) * | 1996-01-11 | 1998-09-29 | The Regents Of The University Of Michigan | Slot spiral antenna with integrated balun and feed |
| USD481030S1 (en) | 2002-05-28 | 2003-10-21 | Randy L. Larson | CB antenna |
| US20040257298A1 (en) * | 2003-06-18 | 2004-12-23 | Steve Larouche | Helical antenna |
| WO2016056935A1 (en) * | 2014-10-07 | 2016-04-14 | Llc "Topcon Positioning Systems" | Impedance helical antenna forming п-shaped directional diagram |
| RU2730114C2 (en) * | 2020-01-10 | 2020-08-17 | Акционерное общество "Научно-производственное объединение им. С.А. Лавочкина" | Conical spiral antenna and method of its manufacturing |
| RU2813818C1 (en) * | 2023-12-04 | 2024-02-19 | Общество с ограниченной ответственностью "Спутниковые инновационные космические системы" | Conical double-thread helical antenna |
-
1959
- 1959-06-30 US US823998A patent/US2958081A/en not_active Expired - Lifetime
Non-Patent Citations (1)
| Title |
|---|
| None * |
Cited By (27)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3241148A (en) * | 1960-04-04 | 1966-03-15 | Mcdonnell Aircraft Corp | End loaded planar spiral antenna |
| US3296536A (en) * | 1960-06-06 | 1967-01-03 | Univ Ohio State Res Found | Combined antenna and tunnel diode converter circuit |
| US3188643A (en) * | 1960-12-29 | 1965-06-08 | Univ Illinois | Circularly polarized omnidirectional cone mounted spiral antenna |
| US3192529A (en) * | 1961-03-20 | 1965-06-29 | Ryan Aeronautical Co | Multi-helix antenna on inflatable satellite |
| US3110030A (en) * | 1961-05-25 | 1963-11-05 | Martin Marietta Corp | Cone mounted logarithmic dipole array antenna |
| US3283332A (en) * | 1964-08-24 | 1966-11-01 | Nussbaum Milton | "null" conical helix |
| US3381297A (en) * | 1965-02-11 | 1968-04-30 | Csf | Wide-band goniometer system |
| US3509465A (en) * | 1965-10-22 | 1970-04-28 | Sylvania Electric Prod | Printed circuit spiral antenna having amplifier and bias feed circuits integrated therein |
| DE1541386B1 (en) * | 1965-11-15 | 1970-11-26 | Granger Associates Palo Alto | Broadband spiral antenna |
| US3633210A (en) * | 1967-05-26 | 1972-01-04 | Philco Ford Corp | Unbalanced conical spiral antenna |
| US3618114A (en) * | 1968-12-16 | 1971-11-02 | Univ Ohio State Res Found | Conical logarithmic-spiral antenna |
| FR2299739A1 (en) * | 1975-01-29 | 1976-08-27 | Abreu Joao Do Espirito Santo | HELICOIDAL TYPE ANTENNA |
| US4161737A (en) * | 1977-10-03 | 1979-07-17 | Albright Eugene A | Helical antenna |
| US4525720A (en) * | 1982-10-15 | 1985-06-25 | The United States Of America As Represented By The Secretary Of The Navy | Integrated spiral antenna and printed circuit balun |
| US4559539A (en) * | 1983-07-18 | 1985-12-17 | American Electronic Laboratories, Inc. | Spiral antenna deformed to receive another antenna |
| US4630064A (en) * | 1983-09-30 | 1986-12-16 | The Boeing Company | Spiral antenna with selectable impedance |
| US4605934A (en) * | 1984-08-02 | 1986-08-12 | The Boeing Company | Broad band spiral antenna with tapered arm width modulation |
| US5640170A (en) * | 1995-06-05 | 1997-06-17 | Polhemus Incorporated | Position and orientation measuring system having anti-distortion source configuration |
| US5815122A (en) * | 1996-01-11 | 1998-09-29 | The Regents Of The University Of Michigan | Slot spiral antenna with integrated balun and feed |
| USD481030S1 (en) | 2002-05-28 | 2003-10-21 | Randy L. Larson | CB antenna |
| US20040257298A1 (en) * | 2003-06-18 | 2004-12-23 | Steve Larouche | Helical antenna |
| US7038636B2 (en) * | 2003-06-18 | 2006-05-02 | Ems Technologies Cawada, Ltd. | Helical antenna |
| WO2016056935A1 (en) * | 2014-10-07 | 2016-04-14 | Llc "Topcon Positioning Systems" | Impedance helical antenna forming п-shaped directional diagram |
| US9774089B2 (en) | 2014-10-07 | 2017-09-26 | Topcon Positioning Systems, Inc. | Impedance helical antenna forming Π-shaped directional diagram |
| US9960494B2 (en) | 2014-10-07 | 2018-05-01 | Topcon Positioning Systems, Inc. | Impedance helical antenna forming Π-shaped directional diagram |
| RU2730114C2 (en) * | 2020-01-10 | 2020-08-17 | Акционерное общество "Научно-производственное объединение им. С.А. Лавочкина" | Conical spiral antenna and method of its manufacturing |
| RU2813818C1 (en) * | 2023-12-04 | 2024-02-19 | Общество с ограниченной ответственностью "Спутниковые инновационные космические системы" | Conical double-thread helical antenna |
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