US2548655A - Directive dielectric guide antenna - Google Patents

Directive dielectric guide antenna Download PDF

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US2548655A
US2548655A US665027A US66502746A US2548655A US 2548655 A US2548655 A US 2548655A US 665027 A US665027 A US 665027A US 66502746 A US66502746 A US 66502746A US 2548655 A US2548655 A US 2548655A
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horn
plane
guide
mode
modes
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US665027A
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Cassius C Cutler
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AT&T Corp
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Bell Telephone Laboratories Inc
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Priority to US665027A priority patent/US2548655A/en
Priority to FR943949D priority patent/FR943949A/en
Priority to GB10376/47A priority patent/GB644376A/en
Priority to DEP28883A priority patent/DE826317C/en
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    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q13/00Waveguide horns or mouths; Slot antennas; Leaky-waveguide antennas; Equivalent structures causing radiation along the transmission path of a guided wave
    • H01Q13/02Waveguide horns
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01PWAVEGUIDES; RESONATORS, LINES, OR OTHER DEVICES OF THE WAVEGUIDE TYPE
    • H01P1/00Auxiliary devices
    • H01P1/16Auxiliary devices for mode selection, e.g. mode suppression or mode promotion; for mode conversion
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q19/00Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic
    • H01Q19/10Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using reflecting surfaces
    • H01Q19/12Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using reflecting surfaces wherein the surfaces are concave
    • H01Q19/13Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using reflecting surfaces wherein the surfaces are concave the primary radiating source being a single radiating element, e.g. a dipole, a slot, a waveguide termination
    • H01Q19/134Rear-feeds; Splash plate feeds

Definitions

  • FIG. 5 is a diagrammatic representation of FIG. 5.
  • This invention relates to directive antenna systems and particularly to directive horn antennas.
  • a sectoral horn flared in the I-I-plane has, by reason of symmetry, no even order modes, but may have several odd modes such as the TEIO, TEso and TE50 modes; and these modes may have unfavorable phase and amplitude relations at the mouth aperture.
  • the sectoral horn heretofore employed for energizing a fan-beam passive member such as a rectangular or elliptical paraboloidal reflector, has two separated phase centers or 001 and hence the phasing at the mouth aperture is distorted. More specifically, the focus in the plane of the long mouth aperture dimension of the sectoral horn is at the throat aperture, whereas the focus in the plane of the short mouth aperture dimension is at the mouth aperture and,
  • a box or unflared horn antenna comprises a rectangular dielectric guide having at one end a large horn mouth aperture and at the other end a wall containing an iris constituting a throat aperture.
  • a small rectangular guide connects the throat'aperture to a transmitter or receiver.
  • the H-plane transverse dimension of the small guide is sufficiently narrow to permit only the TE10 mode, whereas the corresponding dimension of the large guide is wide enough to support both the T1210 and the TE30 modes.
  • the actual length of the large guide and the ratio of the H-plane dimensions of the guides. are critically selected, such that the two modes combine in the horn mouth aperture to produce a substantially fiat wave front.
  • Fig. 1 is a perspective view of a box or twomode horn antenna constructed in accordance with the invention
  • Figs. 2, 3 and 4 are mode diagrams, and Fig. 5 is an amplitude curve, all used in explaining the embodiment of Fig. 1;
  • Fig. 6 is a perspective view of another embodiment of the invention.
  • Fig. 7 is a perspective view of an embodiment of the invention comprising a fan-beam reflector and a front feed dual-mode horn;
  • Fig. 8 is an H-plane sectional view of the front feed two-mode 0r dual-mode horn utilized in the system of Fig. 7;
  • Figs. 9 and 10 are measured directive. patterns for the system of Fig. I;
  • Fig. 11 is a perspective View of an embodiment of the invention comprising a fan-beam reflector and a rear feed dual-mode horn;
  • Figs. 12 and 13 are, respectively, E-plane and H-plane sectional views of the rearfeed dualmode horn employed in the system of Fig. 11, and
  • Figs. 1 4 and 15 are measured directive patterns for the system of Fig. 11. a
  • the wave and mode symbols, for example, the symbol T Em, usedherein are the same as those given on page 395 of the textbook Electromagnetic Waves" by S. A. Schelkunoff and now more or less universally adopted in the art. Formerly, TE and TM waves were designated H and E waves, respectively.
  • reference numeral I denotes a translation device, such as a transmitter or a receiver
  • numeral 2 designates arelatively small open ended rectangular dielectric guide connected thereto and having an axis 3.
  • the guide 2 comprises two narrow parallel longitudinal metallic walls 4, 5, two wide metallic longitudinal walls 6, 1 and the dielectric medium 8 bounded by the aforesaid four walls.
  • the particular medium utilized in the embodiment of Fig. l is air but, as is well known, other dielectric substances, such as solid dielectric material, may be employed'in place of the air dielectric.
  • the narrow walls 4, 5 are parallel to the electric polarization E, and hence perpendicular to the magnetic polarization H, of the TE waves conveyed by the guide or, stated diiierently, walls 4, 5 and walls 6, I are parallel to the E-plane and the H-plane, respectively.
  • Numeral 9 denotes a dual-mode box horn comprising a relatively large rectangular dielectric guide having a longitudinal axis 3, narrow longitudinal E-plane walls [0, wide longitudinal H- plane walls I I, an open end l2 constituting a horn mouth aperture and an end orthroat wall 13 having a central iris l4 constituting a throat aperture.
  • the dual-mode horn 9 is directly connected to guide 2, the iris M and the open end of guide 2 being coincident.
  • the walls 4 and I have equal transverse E- plane dimensions, 0, whereas the transverse H- plane' dimension, 1111, of guide 2 is smaller than the-corresponding dimension, 1.02, of the horn 9.
  • the dimensions 101 and we each have, preferably but not necessarily, minimum and maximum values, as measured in wavelengths, M, in the air dielectric medium 8, that is, in free space; the ratio of the aforesaid dimensions being judiciously chosen, and the axial length, L, of the dual-mode horn 9 being critically selected.
  • the dimensions 201 and um are preferably chosen in accordance with the following relations:
  • the horn 9 will support higher modes, such as the amplitude of mode 15.
  • the horn mouth aperture the horn 9 must be properly dimensioned. Even order H-plane modes, such as the TEzo mode, are not excited in either the guide 2 or horn 9, inasmuch as these dielectric paths are symmetrical about an E- plane containing the axis 3. Also so that a complet E-plane mode is not supported in guide 2 or horn 9.
  • H-plane modes such as the TEzo mode
  • a TE-lO wave mode l5 of relatively large amplitude in guide 2, Fig. 2 enters the dual-mode horn 9 through the throat aperture l 4 and produces at the junction or throat wall i3 a TE10 mode I6, of smaller amplitude, Fig. 3, and, by reason of the value of dimension we and the abrupt expansion (uh to we) in the I-I-plane dimension, initiates a TEso mode H of small amplitude. Since modes l6 and I!
  • the modes [6 and H are oppositely phased.
  • A1 is the amplitude of the 'I'Elio mode [6
  • A3 is the amplitude of the TEso'mode H
  • A is the amplitude ratio of the two modes so that at throat I3 the wave front H3 in the H- plane, Fig. 3, resulting from the algebraic addition of modes 1% and I1, is curvilinear rather than linear.
  • the wave is convex rather than fiat.
  • V1 Vfi (10)
  • M is the guide wavelength at the TEio mode l6
  • A3 is the guide wavelength at the 'IEso mode ll.
  • the amplitudes A1 and A3, and the amplitude ratio A may be obtained by making a Fourier analysis of the incident field at the junction l3 and considering only the first two terms.
  • R and A may each have any practical value greater than zero and less than unity, a value of R in the order of 0.4 to 0.8, corresponding to a value of A in the order of 0.7 to 0.2, is particularly satisfactory.
  • the operation is, by reason of the reciprocity theorem, the converse of the transmitting operation.
  • the incoming wave establishes similarly phased TEIO and TEco modes in the horn mouth aperture l2. By reason of the horn length L, these modes are rendered in opposite phase at the throat aperture 14 and a. strong TE'm wave is initiated in guide 2 and conveyed to the receiver 1.
  • the narrow walls I0 of the dual mode, horn 9 may be flared and, also if desired, the wide walls ll may be flared.
  • the flaring may be advantageously utilized to secure optimum energization of the passive member.
  • the antenna system 20 comprises a quasi-elliptical paraboloidal reflector 2
  • the quasi-elliptical contour of the reflector eliminates the so-called corner minor lobes which are present in the pattern of the conventional rectangular parabolic reflector.
  • Numeral 23 denotes the axi of the reflector 2
  • the horn 22 has a mouth aperture 24 and is connected through an iris 25 to a front feed dielectric guide 26.
  • the E-plane dimension of the iris 25 is slightly less than the E-plane dimensionof guide 26.
  • the H-plane dimension, 101, of iris 25 and the I-l-plane dimension, we, of the horn 22 are properly selected, as explained in connection with Fig. 1.
  • Guide 26 is connected to a translation device I which serves as a support for the reflector 2!.
  • a dielectric window 2! is positioned near the mouth aperture 24 of the dual-mode horn 22 and is rigidly secured to the horn by means of the metallic members 28 and the bolts 29.
  • Numeral 3! denotes a tuning plug in guide 26 and numeral 3
  • the reference letter L denotes the actual length of the dual mode horn 22.
  • the phase velocity in air is different from that in the window so that, if the window is thick, this difference must be taken into account in determining the value of L.
  • the window is usually relatively thin so that the above-mentioned difference in velocities may be disregarded in determining L.
  • a TEm mode is produced in guide 2 by device I and the energy, after passing through the iris 25, appears in the horn 22 in the form of the two modes T1310 and TEso.
  • the two modes produce a flat front in the mouth aperture of the dual mode horn 22. Since the wave front in the mouth aperture is airisto minor axis, for example, 1:3 to 1 :5.
  • the front of the wave arriving at the reflector is fairly spherical, as is desired.
  • the mouth aperture simulates a point source.
  • the beam produced by the dualmode horn 22 is of the horizontal fan-beam type, the beam being wider in the E-plane than in the-H-plane, and therefore suitable for illuminating in an optimum manner the quasi-elliptical reflector 2
  • the shape of the wave front impinging upon the reflector is dependent primarily upon the relative phasing of the diverse wavelets forming the front, whereas the shape of the beam is dependent primarily on the relative amplitudes of the wavelets.
  • reference numerals 32 and 33 denote, respectively, the measured Eplane and H-plane directive patterns of a front-fed dual-mode horn 22 actually constructed and tested at a design wavelength of 3.2 centimeters.
  • Numerals 34 and 35 denote, respectively, the measured E-plane and H-plane patterns for the complete system comprising a born 22 and a quasi-elliptical reflector 2
  • numeral 35 denotes the major lobe
  • numerals 3T designate the minor lobes
  • numerals 38 denotes the half power angular width of the major lobe. As shown in Fig.
  • the half power widths 38 of the major lobes 36 in the E-plane and I-I-plane patterns 32 and 33 are respectively about '70 and 21 degrees and hence, as stated above, the beam of the horn is of the fan type. As compared to the fan-beams of feed horns of the prior art, the fan-beam is more pronounced, that is, the lobe width ratio is greater. Hence the dualmode horn is especially suitable for use with an elliptical reflector having a pronounced fanbeam characteristic, that is, an elliptical reflector having a relatively large ratio of major The minor lobes 3'! of the horn patterns 32 and 33 are at least decibels down and therefore negligible. As shown in Fig.
  • the half power 'widths 38 of major lobes 35' of the E and H- plane patterns 34 and 35, for the entire system, are 2.2 and 5 degrees, respectively, and the beam
  • the reflector fanbeam Fig. is in a sense the converse of the horn fan-beam, Fig. 9, since in Fig. 9 the beam is wide in the E-plane and narrow in the H- plane whereas, in Fig. 10, the beam is narrow in the E-plane and wide in the H-plane.
  • the antenna system 40 comprises a quasi-elliptical reflector 2
  • is positioned at the focus of the reflector and is connected to a rear feed dielectric guide 42 having an H-plane dimension, 201.
  • encloses the open end of guide 42 and comprises the three brass plates 43, 44 and 45, the rubber gasket 46, the dielectric plate 5'! and the brass plate 48, all held securely by brass screws 5
  • Numeral 54 denotes a threaded plug for tuning the chamber 50
  • numerals 55 denote reflective wedges positioned in slots 56 and attached to the top and bottom walls of guide 26.
  • the critical horn length L extends from the open guide end .or throat aperture to the mouth aperture 53.
  • the length L as measured in guide Wavelengths for the TEm mode dilfers a half wavelength, or a multiple thereof, from the length as measured in guide wavelengths for the T1530 mode.
  • a TEm mode is produced in guide 52 and the energy, after passing through the iris or open end, appears in each of guides 5
  • the two modes produce a substantially flat wave front in each of the two horn mouth apertures 53, and a spherical Wave front is projected toward thereflector 25.
  • the wedges 55 function to direct the wavelets emitted by the apertures toward the outermost or central peripheral portions of the left-half and the right-half of the reflector 2
  • reference numerals 5i and 58 denote, respectively the measured E-plane and H-plane directive patterns of a-rear feed dual-mode horn 4
  • the half -power widths 38 of the major lobes of the E-plane and H-plane dual-mode patterns 5'? and 58 are, respectively, about 20 and 50 degrees, respectively, and the horn beam is of the fan type.
  • the minor lobes 31 of patterns 5'! and 58 are about I! decibels down and therefore negligible.
  • , Fig. 11 is especially suitable for use with an elliptical reflector having a large ratio of major axis to minor axis, for example, 113 to 1:5.
  • the half power widths 38 of the major lobes 36 of the E and I-l-plane patterns 59 and 60, for the complete system are 2 and 5.1 degrees respectively and the beam is therefore of the fan type.
  • the minor lobes 31 of patterns 59 and B0 are more than 23 decibels down and therefore negligible.
  • a box or two-mode horn for transmitting or receiving a combined TEm and TEzo wave, .said horn comprising a first dielectric guide for conveying only a TEm wave mode and a second guide connected thereto for conveying said wave ,mode and a TEao wave mode, said wave modes having different guide wavelengths, the difference between the length of said second guide as measured in guide wavelengths at one of said modes and the length of said second guide as measured in guide wavelengths at the other mode being a half wavelength.
  • a front feed two-mode horn antenna system for transmitting or receiving TE waves, said system comprising a first dielectric guide and a second dielectric guide each having E and H- plane walls, said second guide having an end wall and an iris in said end wall, said first guide being 9 electrically connected to said second guid through said iris, the I-I-plane Walls of said second guide being wider than the I-I-plane Walls of said first guide, the difference between the length of said second guide as measured in guide wavelengths for the TEM) mode and the length of said second guide as measured in guide wavelengths for the TEso mode being a half wavelength, or an odd multiple thereof.
  • a rear feed two-mode horn antenna system comprising a main dielectric guide having an open end, a resonant chamber enclosing the end of said guide, a pair ofv auxiliary guides connected to said chamber and each having an antenna aperture, said main and auxiliary guides being parallel and having given I-I-plane dimensions, the I-I-plane dimensions of said auxiliary guides being greater than that of the main guide and such as to permit the conveyance of 'IEm and TEso wave modes, the difference between the distance from said open end to each aperture as measured in guide wavelengths for the TEm mode and said distance as measured in guide wavelengths for the TEao mode being a half wavelength.
  • a paraboloidal reflector having a focal point and a quasi-elliptical periphery, the ratio of the major axis to the minor axis of said periphery being in the order of 5:1 to 3:1, a two-mode horn at said focal point for radiating or receiving a wave including a TE component and a TE'so component, a guide connecting said horn to a translation device, said horn having at least one rectangular mouth aperture facing said reflector, said horn and aperture each having an, I-I-plane dimension extending parallel to said minor axis, the axial length of said horn as measured in guide wavelengths for the TEm component being a half Wavelength different from said length as measured in guide wavelengths for the TE30 component.
  • a paraboloidal reflector having a focal point and a quasi-elliptical periphery, an unflared dual-mode horn at said focal point, said horn having a single mouth aperture facing said reflector and transverse E and H- plane walls, a dielectric guide having E- and H-plane walls extending across a portion of said reflector and attached to said horn, an iris in an E-plane wall of said guide for electrically connecting said guide and horn, the I-I-plane walls of said horn being wider than the I-I-plane walls of said guide and Wider than the H-plane dimension of said iris.
  • a paraboloidal reflector having a focal point and a quasi-elliptical periphery, a rectangular guide extending through said reflector and having an open end near the focus of said reflector, a resonant chamber enclosing the end of said guide, a pair of auxiliary guides connected to said chamber and each having an antenna aperture facing said reflector, the difference in the distance from said open end to each antenna aperture as measured in guide wavelengths for the TEm mode and said distance as measured in guide wavelengths for the 'IExo mode being a half wavelength or an odd multiple thereof.

Description

April 1951 c. c. CUTLER DIRECTIVE DIELECTRIC GUIDE ANTENNA 4 Sheets-Sheet 1 Filed April 26, 1946 FIG}.
m c F T. $4M I/\ M5 v E E L FIG. 6.
FIG. 5.
lNl/ENTOR CICCUTLER "0.
A T TORNE'V April 10, 1951 c, Q CUTLER 2,548,655
DIRECTIVE DIELECTRIC GUIDE ANTENNA Filed April 26, 1946 I 4 Sheets-Sheet 2 I //v v/v TOR C. C. CU TL E R A 7' TORNEK April 10, 1951 c c T E 2,548,655
DIRECTIVE DIELECTRIC GUIDE ANTENNA Filed April 26, 1946 4 Sheets-Sheet 3 FIG. .9
60 4-0 20 I00 50 6O 40'20 0"20 4O '60 8O IOOIZO l4-Ol50 DEGREES OFFAXIS E-PLANE H-PLANE 0 DEGREES OFF. AXIS wl/f/vrok C C. CUTL ER ATTORNEY April 10, 1951 CUTLER 2,548,655
DIRECTIVE DIELECTRIC GUIDE ANTENNA Filed April 26, 1946 4 Sheets-Sheet 4 FIG. /4
H-PLANE [so [20 so -4o 0 "40 so I20 I60 DEGREES arr AXIS RELATIVE FIELD STRENGTH-DEC/BELS DEGREES OFF AXIS INVENTOR C. C. CU TL ER ATTORNE V Patented Apr. 10, 1951 DIRECTIVE DIELECTRIC GUIDE ANTENNA Cassius C. Cutler, Oakhurst, N. J assignor to Bell Telephone Laboratories, Incorporated,
New
York, N. Y., a corporation of New York Application April 26, 1946, Serial No. 665,027
6 Claims. 1
This invention relates to directive antenna systems and particularly to directive horn antennas.
As is known sectoral, pyramidal and conical horn antennas are widely used for energizing a passive antenna member, such as a parabolic reflector or a lens, and for receiving energy there from. In general, these flared horns are not entirely satisfactory inasmuch as the intensity of the emitted wave at the periphery of the mouth aperture is relatively low, as compared to that at the center of the aperture, and the phase distribution over the aperture is usually not uniform. The undesired amplitude variation and phase distribution are undoubtedly produced by the addition, at the mouth aperture, of diiferent dissimilarly phased wave modes propagated in the horn. To illustrate, a sectoral horn flared in the I-I-plane has, by reason of symmetry, no even order modes, but may have several odd modes such as the TEIO, TEso and TE50 modes; and these modes may have unfavorable phase and amplitude relations at the mouth aperture. In addition, the sectoral horn heretofore employed for energizing a fan-beam passive member, such as a rectangular or elliptical paraboloidal reflector, has two separated phase centers or 001 and hence the phasing at the mouth aperture is distorted. More specifically, the focus in the plane of the long mouth aperture dimension of the sectoral horn is at the throat aperture, whereas the focus in the plane of the short mouth aperture dimension is at the mouth aperture and,
. since these apertures are spaced a distance equal to the axial length of the horn, the wave front emerging from the mouth aperture is not fiat. Again, the horns mentioned above are not especially directive for their size. Accordingly, it now appears desirable to secure a relatively small horn antenna which is suitable for use with a fan-beam passive member and is devoid of the disadvantages inherent in the horn antennas heretofore proposed.
It is one object of this invention to obtain a highly directive horn antenna.
It is another object of this invention to obtain, in a horn antenna, a relatively fiat emergent wave front of substantially uniform amplitude.
It is another object of this invention to combine, in a horn antenna, a plurality of wave modes in an advantageous manner.
It is still another object of this invention to obtain a highly directive horn antenna which is especially suitable for use with a fan-beam passive antenna member.
In accordance with one embodiment of the invention, a box or unflared horn antenna comprises a rectangular dielectric guide having at one end a large horn mouth aperture and at the other end a wall containing an iris constituting a throat aperture. A small rectangular guide connects the throat'aperture to a transmitter or receiver. Assuming TE waves are utilized and considering only the odd H-plane modes, the H-plane transverse dimension of the small guide is sufficiently narrow to permit only the TE10 mode, whereas the corresponding dimension of the large guide is wide enough to support both the T1210 and the TE30 modes. The actual length of the large guide and the ratio of the H-plane dimensions of the guides. are critically selected, such that the two modes combine in the horn mouth aperture to produce a substantially fiat wave front.
The invention will be more fully understood from a perusal of the following specification taken in conjunction with the drawing on which like reference characters denote elements of similar function on which:
Fig. 1 is a perspective view of a box or twomode horn antenna constructed in accordance with the invention;
Figs. 2, 3 and 4 are mode diagrams, and Fig. 5 is an amplitude curve, all used in explaining the embodiment of Fig. 1;
Fig. 6 is a perspective view of another embodiment of the invention;
Fig. 7 is a perspective view of an embodiment of the invention comprising a fan-beam reflector and a front feed dual-mode horn;
Fig. 8 is an H-plane sectional view of the front feed two-mode 0r dual-mode horn utilized in the system of Fig. 7;
Figs. 9 and 10 are measured directive. patterns for the system of Fig. I;
Fig. 11 is a perspective View of an embodiment of the invention comprising a fan-beam reflector and a rear feed dual-mode horn;
Figs. 12 and 13 are, respectively, E-plane and H-plane sectional views of the rearfeed dualmode horn employed in the system of Fig. 11, and
Figs. 1 4 and 15 are measured directive patterns for the system of Fig. 11. a
The wave and mode symbols, for example, the symbol T Em, usedherein are the same as those given on page 395 of the textbook Electromagnetic Waves" by S. A. Schelkunoff and now more or less universally adopted in the art. Formerly, TE and TM waves were designated H and E waves, respectively.
and TE30 modes.
Referring to Fig. 1, reference numeral I denotes a translation device, such as a transmitter or a receiver, and numeral 2 designates arelatively small open ended rectangular dielectric guide connected thereto and having an axis 3. The guide 2 comprises two narrow parallel longitudinal metallic walls 4, 5, two wide metallic longitudinal walls 6, 1 and the dielectric medium 8 bounded by the aforesaid four walls. The particular medium utilized in the embodiment of Fig. l is air but, as is well known, other dielectric substances, such as solid dielectric material, may be employed'in place of the air dielectric. The narrow walls 4, 5 are parallel to the electric polarization E, and hence perpendicular to the magnetic polarization H, of the TE waves conveyed by the guide or, stated diiierently, walls 4, 5 and walls 6, I are parallel to the E-plane and the H-plane, respectively.
Numeral 9 denotes a dual-mode box horn comprising a relatively large rectangular dielectric guide having a longitudinal axis 3, narrow longitudinal E-plane walls [0, wide longitudinal H- plane walls I I, an open end l2 constituting a horn mouth aperture and an end orthroat wall 13 having a central iris l4 constituting a throat aperture. The dual-mode horn 9 is directly connected to guide 2, the iris M and the open end of guide 2 being coincident. As shown on the drawing, the walls 4 and I have equal transverse E- plane dimensions, 0, whereas the transverse H- plane' dimension, 1111, of guide 2 is smaller than the-corresponding dimension, 1.02, of the horn 9. As will now be explained, the dimensions 101 and we each have, preferably but not necessarily, minimum and maximum values, as measured in wavelengths, M, in the air dielectric medium 8, that is, in free space; the ratio of the aforesaid dimensions being judiciously chosen, and the axial length, L, of the dual-mode horn 9 being critically selected.
The dimensions 201 and um are preferably chosen in accordance with the following relations:
3) Ag l 5 er order I-I-plane modes such as the TEao and TEso modes; but the I-I-plane dimension wz of the horn 9 is sufliciently large to support the TE10 The dimension we of horn 9 may have any practical maximum value, but ordinarily whereby odd H-plane modes, higher than the TEso mode, are not supported by the horn. As
discussed below, if
the horn 9 will support higher modes, such as the amplitude of mode 15.
the horn mouth aperture, the horn 9 must be properly dimensioned. Even order H-plane modes, such as the TEzo mode, are not excited in either the guide 2 or horn 9, inasmuch as these dielectric paths are symmetrical about an E- plane containing the axis 3. Also so that a complet E-plane mode is not supported in guide 2 or horn 9.
Referring now to Figs. 2, 3 and 4, and considering the transmittin operation, a TE-lO wave mode l5 of relatively large amplitude in guide 2, Fig. 2, enters the dual-mode horn 9 through the throat aperture l 4 and produces at the junction or throat wall i3 a TE10 mode I6, of smaller amplitude, Fig. 3, and, by reason of the value of dimension we and the abrupt expansion (uh to we) in the I-I-plane dimension, initiates a TEso mode H of small amplitude. Since modes l6 and I! are derived from mode I5, the sum of the amplitudes of modes l6 and I1 is approximately equal to At the junction l3, other odd order modes are present dependent upon the value of 1172 but, for the purpose of this explanation, it is assumed that 202 is less than 57m/2 and that only the TEm and 'I'Eso modes exist in the horn 9. Also, at the junction [3, the intermediate loop or alternation of the 'I'E'so mode H and the sole alternation of the TEio mode 16 have similar phases or polarizations, for example, positive, and accordingly, the two end negative alternations of the T1330 mode I! have a phase or polarity opposite that of the TEio mode 16. Hence, generally speaking, at the throat l3 the modes [6 and H are oppositely phased. Also where A1 is the amplitude of the 'I'Elio mode [6 A3 is the amplitude of the TEso'mode H A is the amplitude ratio of the two modes so that at throat I3 the wave front H3 in the H- plane, Fig. 3, resulting from the algebraic addition of modes 1% and I1, is curvilinear rather than linear. Hence, considering the E and H planes, the wave is convex rather than fiat.
Now the phase velocities for the two modes in the air-filled horn 9 are;
A 2 I "t 1 2) and ' V Ve= where v1 is the phase velocity of the TEio mode l6 V3 is the phase velocity of the TEat mode I! V0 is the phase velocity in free space but,
V1 Vfi, (10) Where M is the guide wavelength at the TEio mode l6 and A3 is the guide wavelength at the 'IEso mode ll. Now in order to secure a relatively fiat wave front in the mouth aperture [2 of the horn 9, the axial length L of thehorn must. be
such as to produce a 180-degree relative phase shift between the two modes I6 and II, that is,
All): em T Accordingly, at the horn mouth aperture I2, Fig. 4, the two end loops of the TEco mode I 1 and the single loop of the TEm mode 16 are similarly polarized and the central loop of mode I! is oppositely polarized relative to mode 16, that is, inone sense the two modes are in phase agreement in the mouth aperture l2, by reason of the critically selected physical dimension L. Hence, assuming the amplitude ratio, A, is properly chosen, the modes combine in the mouth aperture l2 to form a fairly linear wave front in the H-plane. In the E-plane, the wave front is fairly linear in the mouth aperture 12, since the E-plane dimension is small. Consequently, in mouth aper: ture 12 the wave front is fiat, whereby atadistance from aperture [2 the front becomes spherical, so that the dual mode horn is particularly suitable for illuminating a paraboloidal reflector or a point focus lens.
The amplitudes A1 and A3, and the amplitude ratio A, may be obtained by making a Fourier analysis of the incident field at the junction l3 and considering only the first two terms. The field, fir), at the junction or throat I3 may be expressed fix) =A1 cos ac+A3 cos 3:): Ap cos par: .(13)
where p is an odd integer and m is the normalized distance from the horn axis to the point in question, measured in the magnetic plane. This normalized distance is equal to 1r/2 times the ratio of the distance from the axis to the width we ofthe horn 9. The constants A may be found from where f (x) is the field incident to the junction and is equal to fir). It may be taken as stituting values of 1 and 3 for 21, the values of A1 and As may be obtained and, since higher order modes are not propagated, the first two terms of Equation 13 give the field propagated in the dualmode horn 9. At any point in the horn 9 the amplitude ratio, A, is
As (R l)(cos R) =k= (9R l)(cos 12) Hence, the amplitude ratio A is a function of the ratio R. The curve of Fig. 5 illustrates the relation given by Equation 17. In practice, a ratio R, and therefore a ratio A, are selected such that the central portion of the wave front 19, Fig. 4,
1 is slightly convex or depressed, whereby optimum gain and comparatively low minor lobes are obtained. While, as shown by Fig. 5, R and A may each have any practical value greater than zero and less than unity, a value of R in the order of 0.4 to 0.8, corresponding to a value of A in the order of 0.7 to 0.2, is particularly satisfactory.
In reception, the operation is, by reason of the reciprocity theorem, the converse of the transmitting operation. The incoming wave establishes similarly phased TEIO and TEco modes in the horn mouth aperture l2. By reason of the horn length L, these modes are rendered in opposite phase at the throat aperture 14 and a. strong TE'm wave is initiated in guide 2 and conveyed to the receiver 1.
As shown in Fig. 6, if desired, the narrow walls I0 of the dual mode, horn 9 may be flared and, also if desired, the wide walls ll may be flared. In antenna systems comprising a passive member, such as a parabolic reflector or a lens, and a primary dual-mode horn, the flaring may be advantageously utilized to secure optimum energization of the passive member.
Referring to Figs. 7 and'8 the antenna system 20 comprises a quasi-elliptical paraboloidal reflector 2| of the type disclosed in my copending application Serial No. 546,687, filed July 26, 1944, now Patent No. 2,483,575 issued October 4, 1949, and a single aperture dual-mode horn 22 positioned at the point focus of the reflector. More particularly, the projection of th reflector periphery on a plane perpendicular to the reflector axis is an ellipse. The quasi-elliptical contour of the reflector eliminates the so-called corner minor lobes which are present in the pattern of the conventional rectangular parabolic reflector. Numeral 23 denotes the axi of the reflector 2| and of the dual-mode horn 22. The horn 22 has a mouth aperture 24 and is connected through an iris 25 to a front feed dielectric guide 26. The E-plane dimension of the iris 25 is slightly less than the E-plane dimensionof guide 26. The H-plane dimension, 101, of iris 25 and the I-l-plane dimension, we, of the horn 22 are properly selected, as explained in connection with Fig. 1. Guide 26 is connected to a translation device I which serves as a support for the reflector 2!. A dielectric window 2! is positioned near the mouth aperture 24 of the dual-mode horn 22 and is rigidly secured to the horn by means of the metallic members 28 and the bolts 29. Numeral 3!] denotes a tuning plug in guide 26 and numeral 3| denotes an inclined metallic member or elbow in guide 26. As in Fig. 1, the reference letter L denotes the actual length of the dual mode horn 22. The phase velocity in air is different from that in the window so that, if the window is thick, this difference must be taken into account in determining the value of L. In practice, the window is usually relatively thin so that the above-mentioned difference in velocities may be disregarded in determining L.
The operation of the antenna 20, Figs. '7 and 8, is believed to be obvious in view of the description given above and the disclosures in my above-mentioned copending applications. Briefly, a TEm mode is produced in guide 2 by device I and the energy, after passing through the iris 25, appears in the horn 22 in the form of the two modes T1310 and TEso. By reason of the critical horn length L, and the selected ratio, wz/wi, the two modes producea flat front in the mouth aperture of the dual mode horn 22. Since the wave front in the mouth aperture is airisto minor axis, for example, 1:3 to 1 :5.
' is therefore of the fan type.
fairly flat, the front of the wave arriving at the reflector is fairly spherical, as is desired. In
other words, the mouth aperture simulates a point source. The beam produced by the dualmode horn 22 is of the horizontal fan-beam type, the beam being wider in the E-plane than in the-H-plane, and therefore suitable for illuminating in an optimum manner the quasi-elliptical reflector 2| which produces a vertical fan-beam, as explained in my first-mentioned copending application. While, in Fig. 7, the E and H- 'planes are horizontal and vertical, respectively,
they may of course be reversed or have other quadrature orientations. It may be noted here that the shape of the wave front impinging upon the reflector is dependent primarily upon the relative phasing of the diverse wavelets forming the front, whereas the shape of the beam is dependent primarily on the relative amplitudes of the wavelets.
Referring to Figs. 9 and 10, reference numerals 32 and 33 denote, respectively, the measured Eplane and H-plane directive patterns of a front-fed dual-mode horn 22 actually constructed and tested at a design wavelength of 3.2 centimeters. Numerals 34 and 35 denote, respectively, the measured E-plane and H-plane patterns for the complete system comprising a born 22 and a quasi-elliptical reflector 2| as illustrated by Fig. 7. In each pattern numeral 35 denotes the major lobe, numerals 3T designate the minor lobes and numerals 38 denotes the half power angular width of the major lobe. As shown in Fig. 9, the half power widths 38 of the major lobes 36 in the E-plane and I-I- plane patterns 32 and 33 are respectively about '70 and 21 degrees and hence, as stated above, the beam of the horn is of the fan type. As compared to the fan-beams of feed horns of the prior art, the fan-beam is more pronounced, that is, the lobe width ratio is greater. Hence the dualmode horn is especially suitable for use with an elliptical reflector having a pronounced fanbeam characteristic, that is, an elliptical reflector having a relatively large ratio of major The minor lobes 3'! of the horn patterns 32 and 33 are at least decibels down and therefore negligible. As shown in Fig. 10, the half power 'widths 38 of major lobes 35' of the E and H- plane patterns 34 and 35, for the entire system, are 2.2 and 5 degrees, respectively, and the beam The reflector fanbeam Fig. is in a sense the converse of the horn fan-beam, Fig. 9, since in Fig. 9 the beam is wide in the E-plane and narrow in the H- plane whereas, in Fig. 10, the beam is narrow in the E-plane and wide in the H-plane. The
' minor lobes 31 of patterns 34 and 35, are below 19.5 decibels and therefore insignificant.
Referring to Figs. 11, 12 and 13, the antenna system 40 comprises a quasi-elliptical reflector 2| and a dual aperture dual-mode horn 4|. The
' horn 4| is positioned at the focus of the reflector and is connected to a rear feed dielectric guide 42 having an H-plane dimension, 201. The horn 4| encloses the open end of guide 42 and comprises the three brass plates 43, 44 and 45, the rubber gasket 46, the dielectric plate 5'! and the brass plate 48, all held securely by brass screws 5|, 52. Numeral 54 denotes a threaded plug for tuning the chamber 50 and numerals 55 denote reflective wedges positioned in slots 56 and attached to the top and bottom walls of guide 26. As shown on the drawing, the critical horn length L, extends from the open guide end .or throat aperture to the mouth aperture 53. As in the previously described embodiments, the length L as measured in guide Wavelengths for the TEm mode dilfers a half wavelength, or a multiple thereof, from the length as measured in guide wavelengths for the T1530 mode.
7 The operation of the system of Fig. 11 is believed to be apparent in view of the description given above. Briefly a TEm mode is produced in guide 52 and the energy, after passing through the iris or open end, appears in each of guides 5| and 52 in the form of the two modes TE-lO and TEsu. By reason of the critical length L, and the selected ratio, wz/wi, the two modes produce a substantially flat wave front in each of the two horn mouth apertures 53, and a spherical Wave front is projected toward thereflector 25. The wedges 55 function to direct the wavelets emitted by the apertures toward the outermost or central peripheral portions of the left-half and the right-half of the reflector 2|. In reception the converse operation is obtained.
Referring to Figs. 14 and 15, reference numerals 5i and 58 denote, respectively the measured E-plane and H-plane directive patterns of a-rear feed dual-mode horn 4| which was actually constructed in accordance with Figs. 11, 12 and 13, and tested at a design Wavelength of 3.2 centimeters; and numerals 59 and 6|] denote, respectively, the measured E-plane and H-plane patterns for the complete system 40. As shown in Fig. 14, the half -power widths 38 of the major lobes of the E-plane and H-plane dual-mode patterns 5'? and 58 are, respectively, about 20 and 50 degrees, respectively, and the horn beam is of the fan type. The minor lobes 31 of patterns 5'! and 58 are about I! decibels down and therefore negligible. As in the case of the front feed dual-mode horn 22, Fig. '7, the rear feed dual-mode horn 4|, Fig. 11, is especially suitable for use with an elliptical reflector having a large ratio of major axis to minor axis, for example, 113 to 1:5. As shown in Fig. 15, the half power widths 38 of the major lobes 36 of the E and I-l- plane patterns 59 and 60, for the complete system, are 2 and 5.1 degrees respectively and the beam is therefore of the fan type. The minor lobes 31 of patterns 59 and B0 are more than 23 decibels down and therefore negligible.
What is claimed is:
1. A box or two-mode horn for transmitting or receiving a combined TEm and TEzo wave, .said horn comprising a first dielectric guide for conveying only a TEm wave mode and a second guide connected thereto for conveying said wave ,mode and a TEao wave mode, said wave modes having different guide wavelengths, the difference between the length of said second guide as measured in guide wavelengths at one of said modes and the length of said second guide as measured in guide wavelengths at the other mode being a half wavelength.
2. A front feed two-mode horn antenna system. for transmitting or receiving TE waves, said system comprising a first dielectric guide and a second dielectric guide each having E and H- plane walls, said second guide having an end wall and an iris in said end wall, said first guide being 9 electrically connected to said second guid through said iris, the I-I-plane Walls of said second guide being wider than the I-I-plane Walls of said first guide, the difference between the length of said second guide as measured in guide wavelengths for the TEM) mode and the length of said second guide as measured in guide wavelengths for the TEso mode being a half wavelength, or an odd multiple thereof. 1
3. A rear feed two-mode horn antenna system comprising a main dielectric guide having an open end, a resonant chamber enclosing the end of said guide, a pair ofv auxiliary guides connected to said chamber and each having an antenna aperture, said main and auxiliary guides being parallel and having given I-I-plane dimensions, the I-I-plane dimensions of said auxiliary guides being greater than that of the main guide and such as to permit the conveyance of 'IEm and TEso wave modes, the difference between the distance from said open end to each aperture as measured in guide wavelengths for the TEm mode and said distance as measured in guide wavelengths for the TEao mode being a half wavelength.
4. In combination, a paraboloidal reflector having a focal point and a quasi-elliptical periphery, the ratio of the major axis to the minor axis of said periphery being in the order of 5:1 to 3:1, a two-mode horn at said focal point for radiating or receiving a wave including a TE component and a TE'so component, a guide connecting said horn to a translation device, said horn having at least one rectangular mouth aperture facing said reflector, said horn and aperture each having an, I-I-plane dimension extending parallel to said minor axis, the axial length of said horn as measured in guide wavelengths for the TEm component being a half Wavelength different from said length as measured in guide wavelengths for the TE30 component.
5. In combination, a paraboloidal reflector having a focal point and a quasi-elliptical periphery, an unflared dual-mode horn at said focal point, said horn having a single mouth aperture facing said reflector and transverse E and H- plane walls, a dielectric guide having E- and H-plane walls extending across a portion of said reflector and attached to said horn, an iris in an E-plane wall of said guide for electrically connecting said guide and horn, the I-I-plane walls of said horn being wider than the I-I-plane walls of said guide and Wider than the H-plane dimension of said iris.
6. In combination, a paraboloidal reflector having a focal point and a quasi-elliptical periphery, a rectangular guide extending through said reflector and having an open end near the focus of said reflector, a resonant chamber enclosing the end of said guide, a pair of auxiliary guides connected to said chamber and each having an antenna aperture facing said reflector, the difference in the distance from said open end to each antenna aperture as measured in guide wavelengths for the TEm mode and said distance as measured in guide wavelengths for the 'IExo mode being a half wavelength or an odd multiple thereof.
CASSIUS C. CUTLER.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Number Name Date 2,129,669 Bowen Sept. 13, 1938 2,206,923 Southworth July 9, 1940 2,232,179 King Feb. 18, 1941 2,255,042 Barrow Sept. 9, 1941 2,283,935 King May 26, 1942 2,396,044 Fox Mar. 5, 1946 2,405,242 Southworth Aug. 6, 1946 2,415,807 Barrow et a1. Feb. 18, 1947 2,416,698 King Mar. 4, 1947
US665027A 1946-04-26 1946-04-26 Directive dielectric guide antenna Expired - Lifetime US2548655A (en)

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BE472577D BE472577A (en) 1946-04-26
US665027A US2548655A (en) 1946-04-26 1946-04-26 Directive dielectric guide antenna
FR943949D FR943949A (en) 1946-04-26 1947-03-25 Directional antenna system
GB10376/47A GB644376A (en) 1946-04-26 1947-04-18 Directive antenna systems
DEP28883A DE826317C (en) 1946-04-26 1948-12-31 Directional radiator with dielectric waveguide

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US2675524A (en) * 1948-03-25 1954-04-13 Emi Ltd Electrical wave guide provided with tuning pistons
US2692984A (en) * 1950-08-30 1954-10-26 Sperry Corp Bridge obstruction marker for radar navigation
US2778016A (en) * 1953-01-23 1957-01-15 Gabriel Co Wave guide antenna
US2809371A (en) * 1954-09-30 1957-10-08 Rca Corp Liquid trap for vertically mounted horn antenna
US10763916B2 (en) * 2017-10-19 2020-09-01 At&T Intellectual Property I, L.P. Dual mode antenna systems and methods for use therewith

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US2206923A (en) * 1934-09-12 1940-07-09 American Telephone & Telegraph Short wave radio system
US2232179A (en) * 1938-02-05 1941-02-18 Bell Telephone Labor Inc Transmission of guided waves
US2255042A (en) * 1939-01-03 1941-09-09 Research Corp Electromagnetic horn
US2283935A (en) * 1938-04-29 1942-05-26 Bell Telephone Labor Inc Transmission, radiation, and reception of electromagnetic waves
US2396044A (en) * 1941-12-10 1946-03-05 Bell Telephone Labor Inc Switching device
US2405242A (en) * 1941-11-28 1946-08-06 Bell Telephone Labor Inc Microwave radio transmission
US2415807A (en) * 1942-01-29 1947-02-18 Sperry Gyroscope Co Inc Directive electromagnetic radiator
US2416698A (en) * 1938-04-29 1947-03-04 Bell Telephone Labor Inc Radiation and reception of microwaves

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US2206923A (en) * 1934-09-12 1940-07-09 American Telephone & Telegraph Short wave radio system
US2129669A (en) * 1937-03-30 1938-09-13 Bell Telephone Labor Inc Guided wave transmission
US2232179A (en) * 1938-02-05 1941-02-18 Bell Telephone Labor Inc Transmission of guided waves
US2283935A (en) * 1938-04-29 1942-05-26 Bell Telephone Labor Inc Transmission, radiation, and reception of electromagnetic waves
US2416698A (en) * 1938-04-29 1947-03-04 Bell Telephone Labor Inc Radiation and reception of microwaves
US2255042A (en) * 1939-01-03 1941-09-09 Research Corp Electromagnetic horn
US2405242A (en) * 1941-11-28 1946-08-06 Bell Telephone Labor Inc Microwave radio transmission
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Publication number Priority date Publication date Assignee Title
US2675524A (en) * 1948-03-25 1954-04-13 Emi Ltd Electrical wave guide provided with tuning pistons
US2692984A (en) * 1950-08-30 1954-10-26 Sperry Corp Bridge obstruction marker for radar navigation
US2778016A (en) * 1953-01-23 1957-01-15 Gabriel Co Wave guide antenna
US2809371A (en) * 1954-09-30 1957-10-08 Rca Corp Liquid trap for vertically mounted horn antenna
US10763916B2 (en) * 2017-10-19 2020-09-01 At&T Intellectual Property I, L.P. Dual mode antenna systems and methods for use therewith

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FR943949A (en) 1949-03-22
BE472577A (en)
DE826317C (en) 1951-12-27

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