EP0024685B1 - Hybrid mode waveguiding member and hybrid mode feedhorn antenna - Google Patents
Hybrid mode waveguiding member and hybrid mode feedhorn antenna Download PDFInfo
- Publication number
- EP0024685B1 EP0024685B1 EP19800104951 EP80104951A EP0024685B1 EP 0024685 B1 EP0024685 B1 EP 0024685B1 EP 19800104951 EP19800104951 EP 19800104951 EP 80104951 A EP80104951 A EP 80104951A EP 0024685 B1 EP0024685 B1 EP 0024685B1
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- Prior art keywords
- wire
- mode
- section
- helical
- hybrid mode
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01P—WAVEGUIDES; RESONATORS, LINES, OR OTHER DEVICES OF THE WAVEGUIDE TYPE
- H01P3/00—Waveguides; Transmission lines of the waveguide type
- H01P3/12—Hollow waveguides
- H01P3/127—Hollow waveguides with a circular, elliptic, or parabolic cross-section
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01P—WAVEGUIDES; RESONATORS, LINES, OR OTHER DEVICES OF THE WAVEGUIDE TYPE
- H01P1/00—Auxiliary devices
- H01P1/16—Auxiliary devices for mode selection, e.g. mode suppression or mode promotion; for mode conversion
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q13/00—Waveguide horns or mouths; Slot antennas; Leaky-waveguide antennas; Equivalent structures causing radiation along the transmission path of a guided wave
- H01Q13/02—Waveguide horns
- H01Q13/0208—Corrugated horns
Definitions
- the present invention relates to a hybrid mode waveguiding member of the type as defined in the preamble clause of claim 1 and a hybrid mode feedhorn antenna.
- Hybrid mode corrugated horn antennas have been in use in the microwave field for a number of years.
- Various techniques for forming the corrugated horn antennas have been used to provide certain advantages.
- U.S. Patent 3,732,571 discloses a microwave horn aerial which is corrugated on its inner surface, defining a tapered waveguide mouth area, with at least one spiro-helical projection which can be produced by a screw cutting operation with a single start spiro-helical groove or by molding on a mandrel which can be withdrawn by unscrewing it.
- a circular waveguide feedhorn which includes corrugated slots on the inner wall surface, the width of the slots abruptly changing from a smaller value in the portion near the axis of the waveguide to a larger value in the remaining portion of the slot.
- the problem remaining in the prior art is to provide a hybrid-mode waveguiding member of a design which is inexpensive to fabricate, provides simplified mode coupling of the TE" mode to the HE '1 mode, and is operative over a very wide frequency bandwidth.
- the helically wound dielectrically coated wire structure changes gauge in each of a plurality of sequential portions thereof to the next smaller gauge as the structure progresses away from the entrance port of the waveguide.
- a second section of the waveguiding member can comprise helical turns of uniform gauge wire or helical turns of decreasing gauge sections as the structure progresses from the first section to the other end of the waveguide.
- the spiro-helical structure is formed from at least one helically wound dielectrically coated wire which has closely spaced turns for a portion of its length and then has the spacings between turns gradually increased as the helix progresses in the waveguide to convert the TE 11 mode to the HE 11 mode and then proceeds towards the other end of the waveguide with a uniform pitch.
- the spiro-helical structure can be formed from a single dielectrically coated wire that is initially flattened and formed in closely spaced edge-wound turns for a portion of its length and then gradually changes to a rounded configuration before continuing with increased spacing between the turns in the mode converting waveguide section and then in a uniform pitch as the helix progresses towards the other end of the waveguide.
- the spiro-helical structure is formed from multiple layers of helically wound dielectrically coated wires in closely spaced turns which gradually reduce to one layer before the spacings between the turns is gradually increased in a linear manner in the waveguide section and then proceed with a uniform pitch as the projection progresses to the other end of the waveguide.
- Fi g. 1 illustrates a helical hybrid-mode feedhorn antenna 10 formed in accordance with an embodiment of the present invention, comprising a first waveguide mode transducer section 12 of uniform cross-section which converts to a tapered waveguide section 14 which is flared outward to form the mouth 16 of feedhorn antenna 10.
- a spiro-helical projection 18 is formed from a helically wound, dielectrically coated, wire structure, which is shown in greater detail in Figs. 2-4, that is bonded to the wire surface of sections 12 and 14 with a dielectric layer 50.
- Feedhorn antenna 10 is shown coupled to a smooth-walled waveguide section 20, which is of a size that is capable of propagating the TE 11 mode in the frequency band of interest, in a manner that the longitudinal axis 22 of waveguide section 20 and feedhorn antenna 10 correspond.
- a suitable transition from the TE 11 mode to the HE 11 mode is obtained in section 12, and as shown in greater detail in Fig. 2, by starting the helical projection 18 adjacent waveguide 20, which is at the TE '1 mode end of section 12, with closely spaced helical turns of a dielectrically coated wire of a first gauge as, for example, 18 gauge.
- a number of closely spaced helical turns of a dielectrically coated wire of a second gauge smaller than the first gauge as, for example, a 20 gauge wire continue helical projection 18 in portion III.
- helical projection 18 in section 12 continues with closely spaced helical turns formed from dielectrically coated wire which reduce in gauge in each adjacent portion as, for example, 22 and 24 gauge wire, respectively.
- the outer diameter of the spiral structure is tapered as the helix progresses away from the TE 11 mode signal entrance port.
- portions II to V in Fig. 2 is an arbitrary value and merely of sufficient length to provide a smooth transition area for continuity of the TE" mode between portion I in waveguide 20 and portion II in section 12 of feedhorn antenna 10, and mode conversion to the HE 11 mode in portions III to V.
- the edges 26 of the helical turns 18 should also be an extension of the inner wall 28 of waveguide 20 to avoid reflective surfaces for the propagating TE" mode signal.
- the remaining closely spaced helical turns of projection 18 in section 12 can be formed from a wire of the smaller gauge used in, for example, portion V or the last portion of the mode conversion area.
- the use of a large gauge wire to form the helical turns in portion II of Fig. 2 substantially increases the capacitance between adjacent turns and, therefore, substantially reduces the coupling per wavelength of the propagating signal into the resonant chamber formed by the dielectric layer 50.
- the reduction in gauge of the wires in portions III to V alters the capacitance between adjacent turns in the successive portions in a manner to cause the mode conversion from the TE 11 mode to the HE 11 mode.
- the remaining portion in sections 12 and 14 provides primarily the proper conductive path for the HE 11 mode and the impedance match for launching the converted mode from mouth 16 of feedhorn antenna 10 into space.
- FIG. 3 One method for forming the projection 18 in section 14 is shown in Fig. 3 where projection 18 is formed from a single gauge dielectrically coated wire with uniform pitch, closely spaced, helical turns.
- FIG. 4 An alternative method for forming projection 18 in section 14 is shown in Fig. 4 where projection 18 can comprise portions, in section 14, which comprise dielectrically coated wire of a different gauge in each subsection which reduce in gauge between subsections as the helix progresses towards mouth 16.
- portion VI may. be formed from, for example, 26 gauge dielectrically coated wire and adjacent portion VII may be formed from 28 gauge dielectrically coated wire.
- a reason for providing an occasional reduction in wire gauge as the helix progresses towards the mouth 1 6 of the feedhorn antenna 10 is to achieve a smooth transition to obtain an ideal taper of the energy distribution at the mouth 16 of antenna feedhorn 10 in all planes in order to reduce wall currents that radiate sidelobe energy to a minimal value at the mouth 16 of feedhorn antenna 10.
- Construction of the helical arrangement of Figs. 1-4 can be accomplished by winding the different gauge wires on a suitable mandrel. When the helical turns have been completely formed, a uniform thickness homogenous layer of dielectric material 50 is bonded to the wires and then enclosed in a conductive sheath 48. The combined thickness 51 of dielectric layer 50 and helix wires 18 capacitive loading should be approximately an electrical quarter wavelength at some nominal medium frequency in the operating frequency band.
- the outer sheath wall 48 can comprise any suitable conductive material.
- the final feedhorn antenna 10 structure can then be coupled to waveguide 20 by any suitable means, as for example, a flange (not shown).
- Fig. 5 illustrates an alternative method for constructing antenna feedhorn 10.
- the helical structure is formed of different gauge dielectrically coated wires as described hereinbefore for Figs. 1-4.
- a layer 50 of foam dielectric is next deposited on the wire structure and the wire and foam layer 50 enclosed in a conductive sheath 48.
- the central portion of feedhorn antenna 10 between the inner edges of the helical turns is filled with a dielectric foam 55 which has a permittivity which approximates the permittivity of the propagation medium in waveguide 20. For example, if air is the medium in waveguide 20 with a permittivity of 1.0, then the dielectric foam 55 should have a permittivity as close to 1.0 as possible.
- Fig. 6 illustrates a hybrid mode waveguide 70 formed in the same manner as shown in Figs. 1-4 and described hereinbefore for feedhorn antenna 10 except that waveguide section 12 continues with the same uniform cross-section in section 72 as found in section 12 instead of converting to a flared section 14 as found in antenna 10.
- the waveguide 70 when completed in a manner similar to feedhorn antenna 10, is coupled between an entrance waveguide 20 and a utilization means (not shown).
- Those field components are functions of r, ⁇ and z, and Z o is the free space impedance of approximately 377 ohms.
- the wires are supported off the conducting wall by a dielectric material such as epoxy and the susceptance y z is directly proportional to the dielectric constant of the medium that supports the helical wires inside the conducting wall. While this fact helps to increase the bandwidth over which y z is large at the input to the hybrid mode matching section, it has the opposite affect at the output where it is desired that y z be small. As a consequence, the helical horn would have to have a larger aperture at the output than the corresponding corrugated horn.
- Fig. 7 illustrates a helical hybrid-mode feedhorn antenna 10 formed in accordance with another embodiment of the present invention comprising a circular waveguide mode transducer section 12 of uniform diameter which converts to a conical waveguide horn section 14 which is flared outward to form the mouth 16 of feedhorn antenna 10.
- a spiro-helical projection 18 is formed from a helically wound dielectrically coated wire, which is shown in greater detail in Figs. 8 and 9, which is bonded to the inner surface of sections 12 and 14 with dielectric layer 50.
- Feedhorn antenna 10 is shown coupled to a circular waveguide section 20, which is of a size that is capable of propagating the TE" mode in the frequency band of interest, in a manner that the longitudinal axis 22 of waveguide section 20 and feedhorn antenna 10 correspond.
- a suitable transition from the TE" mode to the HE,, mode is obtained in such embodiment by starting with a round dielectrically coated wire which is partially flattened in a rolling mill and then edge-wound in closely spaced helical turns in the area adjacent to circular waveguide 20 which is at the TE,, mode end of circular waveguide section 12. Flattening of this wire to produce the helical turns substantially increases the capacitance between adjacent turns and, therefore, substantially reduces the leakage per wavelength of the propagating signal into dielectric layer 50.
- the flattening of the wire is gradually reduced starting at the input TE 11 mode end adjacent waveguide 20 to a round cross-section of closely spaced turns.
- a No. 15 gauge Formex (Registered Trade Mark) copper wire is used to form the helical turns of portions II to IV of Fig. 8
- the wire may initially be flattened to dimensions of, for example, approximately 0.74 by 1.96 millimeters which changes gradually to a round cross-section.
- the outer diameter of the spiral structure of Fig. 8 is tapered as the helix progresses away from the TEll mode signal entrance port.
- edges 26 of the helical turns 18 should also be an extension of the inner wall 28 of circular waveguide 20 to avoid reflective surfaces for the propagating signal.
- section 12 shown by portions IV and V of Fig. 8 includes a helical winding with a tapered pitch which starts with a zero spacing and gradually has the spacings between turns increased in a linear manner.
- the remainder of the helical turns in section 12 and in section 14 are of uniform pitch of, for example, approximately 3 wire diameters center-to- center as shown in Fig. 9. Therefore, in portions II to V of Fig.
- the continuity of the TE 11 mode is preserved in a smooth transition between waveguide 20 and horn antenna 10 and the TE 11 mode is converted to the HE 11 mode by the gradually increased spacing between the helical turns while the conical section 14 provides a proper impedance match with its uniform tapered helical turns for launching the converted mode from the mouth 16 of feedhorn antenna 10 into space.
- Fig. 10 An alternative and preferred method for forming the feedhorn antenna 10 in accordance with the present invention is shown in Fig. 10.
- a multi-layer helical wire structure is formed in the area 30 which is equivalent to portions II to IV of Fig. 8.
- a round dielectrically coated wire is first formed in a helix of closely spaced turns for the length of area 30 and then in area 32 the spacings between the helical turns are gradually increased in a linear manner.
- Wire 38 continues its helical spiral for the remainder of section 12 and in section 14, in the manner shown in Fig. 9, with a uniform pitch.
- a second layer of helical turns of dielectrically coated wire 40 is superimposed on top of the helical turns of wire 38 starting at waveguide 20 and extending for most of the length of transition area 30. Additional layers of helical turns of dielectrically coated wire are then superimposed on top of wires 38 and 40 with each layer extending for a lesser distance along area 30 so as to effectively form a taper 44 along the ends of the layers.
- the number of layers of wire in transition area 30 is arbitrary and should be of a sufficient number to provide a low enough surface impedance for propagating the TE" mode. In forming the arrangement of Fig. 10 it was found that preferably at least four layers should be used and that each additional layer of wire improved the performance substantially by providing less leakage per wavelength.
- Construction of the helical arrangements of Figs. 7-10 can be accomplished by winding the wire 18 or 38 on a suitable mandrel and securing both ends. Additional layers of wire can be wound on the initial turns for forming the structure of Fig. 10.
- a uniform thickness homogeneous layer of dielectric material 50 is bonded to the wire 18 or 38 and then enclosed in a conductive sheath 48.
- the combined thickness 51 of dielectric layer 50 and helix wire 18 capacitive loading should be approximately an electrical quarter wavelength at the lowest operating frequency.
- the outer shield wall 48 can comprise any suitable conductive material.
- the final feedhorn 10 structure can then be coupled to waveguide 20 by any suitable means, as for example, a flange (not shown).
- Fig. 11 illustrates a circular hybrid mode waveguide 70 formed in the same manner as that shown in Figs. 7-10 and described hereinbefore for feedhorn antenna 10 except that circular waveguide section 10 continues with the same uniform diameter in section 72 as found in section 12 instead of converting to a conical section 14 as found in feedhorn antenna 10.
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Description
- The present invention relates to a hybrid mode waveguiding member of the type as defined in the preamble clause of claim 1 and a hybrid mode feedhorn antenna.
- Hybrid mode corrugated horn antennas have been in use in the microwave field for a number of years. Various techniques for forming the corrugated horn antennas have been used to provide certain advantages. For example, U.S. Patent 3,732,571 discloses a microwave horn aerial which is corrugated on its inner surface, defining a tapered waveguide mouth area, with at least one spiro-helical projection which can be produced by a screw cutting operation with a single start spiro-helical groove or by molding on a mandrel which can be withdrawn by unscrewing it.
- In U.S. Patent 3,754,273, a circular waveguide feedhorn is disclosed which includes corrugated slots on the inner wall surface, the width of the slots abruptly changing from a smaller value in the portion near the axis of the waveguide to a larger value in the remaining portion of the slot.
- In U.S. Patent 4,106,026, a corrugated horn of the exponential type is disclosed with corrugations whose depth decreases exponentially from the throat of the horn towards its mouth.
- The article "Conversion of Wave Modes in a Waveguide with Smoothly Varying Impedance of the Walls" by N. P. Kerzhentseva in Radio Engineering and Electronic Physics, Vol. 16, No. 1, 1971, discloses the use of corrugations and rings to achieve a converter.
- In the typical prior art arrangements, construction is generally complicated and expensive and coupling to a dominant mode waveguide is difficult and limited in bandwidth.
- The problem remaining in the prior art is to provide a hybrid-mode waveguiding member of a design which is inexpensive to fabricate, provides simplified mode coupling of the TE" mode to the HE'1 mode, and is operative over a very wide frequency bandwidth.
- In accordance with the present invention the foregoing problem is solved for a hybrid-mode waveguiding member of the type under discussion with the features as defined in the characterizing clause of claim 1.
- In accordance with one embodiment of the present invention, the helically wound dielectrically coated wire structure changes gauge in each of a plurality of sequential portions thereof to the next smaller gauge as the structure progresses away from the entrance port of the waveguide. A second section of the waveguiding member can comprise helical turns of uniform gauge wire or helical turns of decreasing gauge sections as the structure progresses from the first section to the other end of the waveguide.
- In accordance with another embodiment of the invention, the spiro-helical structure is formed from at least one helically wound dielectrically coated wire which has closely spaced turns for a portion of its length and then has the spacings between turns gradually increased as the helix progresses in the waveguide to convert the TE11 mode to the HE11 mode and then proceeds towards the other end of the waveguide with a uniform pitch.
- In one aspect of the present invention, the spiro-helical structure can be formed from a single dielectrically coated wire that is initially flattened and formed in closely spaced edge-wound turns for a portion of its length and then gradually changes to a rounded configuration before continuing with increased spacing between the turns in the mode converting waveguide section and then in a uniform pitch as the helix progresses towards the other end of the waveguide.
- In another aspect of the present invention, the spiro-helical structure is formed from multiple layers of helically wound dielectrically coated wires in closely spaced turns which gradually reduce to one layer before the spacings between the turns is gradually increased in a linear manner in the waveguide section and then proceed with a uniform pitch as the projection progresses to the other end of the waveguide.
- In the drawings, like numerals represent like parts in the several views:
- Fig. 1 illustrates a helical hybrid mode feedhorn antenna in accordance with an embodiment of the present invention;
- Fig. 2 illustrates in cross-section a portion of the first section of the waveguide body of the feedhorn antenna of Fig. 1 or the waveguide of Fig. 6 showing the spiro-helical projection or structure in accordance with one embodiment of the present invention.
- Fig. 3 illustrates in cross-section a portion of the flared section of the feedhorn antenna of Fig. 1 showing the projection or structure comprising only helical turns of uniform gauge wire;
- Fig. 4 illustrates in cross-section a portion of the flared section of the feedhorn antenna of Fig. 1 showing the projection or structure comprising helical turns of wire which decrease in gauge in adjacent portions as the projection progresses towards the mouth of the feedhorn;
- Fig. 5 illustrates a helical hybrid mode feedhorn antenna similar to Fig. 1 wherein the helical wire structure is supported in the center and bonded to the conductive sheath with a foam dielectric;
- Fig. 6 illustrates a helical waveguide similar to the feedhorn antenna of Fig. 1 capable of converting the TEll mode to the HE" mode and supporting the latter mode in accordance with one embodiment of the present invention;
- Fig. 7 illustrates a helical hybrid mode feedhorn antenna in accordance with another embodiment of the present invention;
- Fig. 8 illustrates in cross-section a portion of the circular waveguide section of the feedhorn antenna of Fig. 7 or waveguide of Fig. 11, respectively, showing one arrangement of the spiro-helical projection in accordance with the other embodiment of the present invention;
- Fig. 9 illustrates in cross-section a portion of the feedhorn antenna of Fig. 7 where the circular section converts into the conical section;
- Fig. 10 illustrates in cross-section a portion of the circular waveguide section of the feedhorn antenna of Fig. 7 or waveguide of Fig. 12 respectively, showing an alternative arrangement of the spiro-helical projection of Fig. 8 in accordance with a further embodiment of the present invention; and
- Fig. 11 illustrates a helical hybrid mode waveguide in accordance with the other embodiment of the present invention.
- Fig. 1 illustrates a helical hybrid-
mode feedhorn antenna 10 formed in accordance with an embodiment of the present invention, comprising a first waveguidemode transducer section 12 of uniform cross-section which converts to atapered waveguide section 14 which is flared outward to form themouth 16 offeedhorn antenna 10. A spiro-helical projection 18 is formed from a helically wound, dielectrically coated, wire structure, which is shown in greater detail in Figs. 2-4, that is bonded to the wire surface ofsections dielectric layer 50.Feedhorn antenna 10 is shown coupled to a smooth-walled waveguide section 20, which is of a size that is capable of propagating the TE11 mode in the frequency band of interest, in a manner that thelongitudinal axis 22 ofwaveguide section 20 andfeedhorn antenna 10 correspond. - In accordance with one embodiment of the present invention, a suitable transition from the TE11 mode to the HE11 mode is obtained in
section 12, and as shown in greater detail in Fig. 2, by starting thehelical projection 18adjacent waveguide 20, which is at the TE'1 mode end ofsection 12, with closely spaced helical turns of a dielectrically coated wire of a first gauge as, for example, 18 gauge. As shown in Fig. 2, after a number of turns of the exemplary 18 gauge wire in portion II, a number of closely spaced helical turns of a dielectrically coated wire of a second gauge smaller than the first gauge as, for example, a 20 gauge wire continuehelical projection 18 in portion III. Portions IV and V of Fig. 2 illustrate thathelical projection 18 insection 12 continues with closely spaced helical turns formed from dielectrically coated wire which reduce in gauge in each adjacent portion as, for example, 22 and 24 gauge wire, respectively. In essence, the outer diameter of the spiral structure is tapered as the helix progresses away from the TE11 mode signal entrance port. - The overall length of portions II to V in Fig. 2 is an arbitrary value and merely of sufficient length to provide a smooth transition area for continuity of the TE" mode between portion I in
waveguide 20 and portion II insection 12 offeedhorn antenna 10, and mode conversion to the HE11 mode in portions III to V. Theedges 26 of thehelical turns 18 should also be an extension of theinner wall 28 ofwaveguide 20 to avoid reflective surfaces for the propagating TE" mode signal. Once the mode conversion from the TE11 mode to the HE11 mode has been achieved in portions II to V ofsection 12 by the gradual reduction of wire gauge in the closely spaced helical turns ofprojection 18, the remaining closely spaced helical turns ofprojection 18 insection 12 can be formed from a wire of the smaller gauge used in, for example, portion V or the last portion of the mode conversion area. - The use of a large gauge wire to form the helical turns in portion II of Fig. 2 substantially increases the capacitance between adjacent turns and, therefore, substantially reduces the coupling per wavelength of the propagating signal into the resonant chamber formed by the
dielectric layer 50. The reduction in gauge of the wires in portions III to V alters the capacitance between adjacent turns in the successive portions in a manner to cause the mode conversion from the TE11 mode to the HE11 mode. The remaining portion insections mouth 16 offeedhorn antenna 10 into space. - One method for forming the
projection 18 insection 14 is shown in Fig. 3 whereprojection 18 is formed from a single gauge dielectrically coated wire with uniform pitch, closely spaced, helical turns. An alternative method for formingprojection 18 insection 14 is shown in Fig. 4 whereprojection 18 can comprise portions, insection 14, which comprise dielectrically coated wire of a different gauge in each subsection which reduce in gauge between subsections as the helix progresses towardsmouth 16. For example, in Fig. 4, portion VI may. be formed from, for example, 26 gauge dielectrically coated wire and adjacent portion VII may be formed from 28 gauge dielectrically coated wire. A reason for providing an occasional reduction in wire gauge as the helix progresses towards the mouth 1 6 of thefeedhorn antenna 10 is to achieve a smooth transition to obtain an ideal taper of the energy distribution at themouth 16 ofantenna feedhorn 10 in all planes in order to reduce wall currents that radiate sidelobe energy to a minimal value at themouth 16 offeedhorn antenna 10. - Construction of the helical arrangement of Figs. 1-4 can be accomplished by winding the different gauge wires on a suitable mandrel. When the helical turns have been completely formed, a uniform thickness homogenous layer of
dielectric material 50 is bonded to the wires and then enclosed in aconductive sheath 48. The combinedthickness 51 ofdielectric layer 50 andhelix wires 18 capacitive loading should be approximately an electrical quarter wavelength at some nominal medium frequency in the operating frequency band. Theouter sheath wall 48 can comprise any suitable conductive material. Thefinal feedhorn antenna 10 structure can then be coupled to waveguide 20 by any suitable means, as for example, a flange (not shown). - Fig. 5 illustrates an alternative method for constructing
antenna feedhorn 10. In Fig. 5, the helical structure is formed of different gauge dielectrically coated wires as described hereinbefore for Figs. 1-4. Alayer 50 of foam dielectric is next deposited on the wire structure and the wire andfoam layer 50 enclosed in aconductive sheath 48. To ensure the positioning of the helical wire structure once the mandrel has been removed, the central portion offeedhorn antenna 10 between the inner edges of the helical turns is filled with adielectric foam 55 which has a permittivity which approximates the permittivity of the propagation medium inwaveguide 20. For example, if air is the medium inwaveguide 20 with a permittivity of 1.0, then thedielectric foam 55 should have a permittivity as close to 1.0 as possible. - Fig. 6 illustrates a
hybrid mode waveguide 70 formed in the same manner as shown in Figs. 1-4 and described hereinbefore forfeedhorn antenna 10 except thatwaveguide section 12 continues with the same uniform cross-section insection 72 as found insection 12 instead of converting to a flaredsection 14 as found inantenna 10. Thewaveguide 70, when completed in a manner similar tofeedhorn antenna 10, is coupled between anentrance waveguide 20 and a utilization means (not shown). - Effecting a smooth transition between the TE11 mode and the HE11 mode requires that the boundary conditions on the inner wall of the waveguide be matched at the interface of the smooth
walled waveguide 20 and the hybrid mode structure. These boundary conditions are best described by considering the normalized anisotropic wall susceptance defined below. - In equations (1) the cylindrical coordinate system is used where z is the direction of propagation, r=a is the radius at the inner wall of the waveguide, Eφ and Hφ are respectively the electric and magnetic components of the field polarized in the φ direction, and Ez and Hz are the field components polarized in the z direction. Those field components are functions of r, φ and z, and Zo is the free space impedance of approximately 377 ohms. In the smooth
walled waveguide 20, the tangential electric fields are identically zero at the conducting surface, r=a, implying that in the TE11 mode, yφ=y2=∞. In order that the pure hybrid mode, the HE11 mode, propagate, the susceptance values required are yφ=∞ but yz=o. Therefore, a matching section is required such that yz gradually changes from a very large value yz> 1 to a very small value yz< 1 for a larger band of frequencies. - In the prior art corrugated feedhorns, the requirement on yz is met at the interface between the smooth walled waveguide and the corrugated horn matching section by standing waves in the slots. However, the bandwidth over which a good match is obtained is limited by the fact that the resonance in the slots is frequency sensitive. Ring-loading the corrugations as found in US-A-3754273 cited in the present Prior Art description adds a capacitance to the wall susceptance y, such that the condition that the yz be large for a good match to the TE11 mode is met for a much larger bandwidth. Since Eφ is required to go to zero at the teeth edges at r=a, yo=∞.
- Using a helical winding in place of the teeth edges will also require Eφ to go to zero at r=a. However, the windings have been found to add a capacitance to yz much like ring-loading the teeth in a corrugated horn. A standing wave is set up in the space between the
wires 18 and the conductingwall 48 as in the slots of a corrugated horn. - The wires are supported off the conducting wall by a dielectric material such as epoxy and the susceptance yz is directly proportional to the dielectric constant of the medium that suports the helical wires inside the conducting wall. While this fact helps to increase the bandwidth over which yz is large at the input to the hybrid mode matching section, it has the opposite affect at the output where it is desired that yz be small. As a consequence, the helical horn would have to have a larger aperture at the output than the corresponding corrugated horn. The
feedhorn antenna 10 design of Fig. 5, however, would eliminate this problem by using a dielectric foam with a very small relative permittivity to support the windings. This feedhorn antenna would then permit the same size aperture as a corrugated feedhorn. - Fig. 7 illustrates a helical hybrid-
mode feedhorn antenna 10 formed in accordance with another embodiment of the present invention comprising a circular waveguidemode transducer section 12 of uniform diameter which converts to a conicalwaveguide horn section 14 which is flared outward to form themouth 16 offeedhorn antenna 10. A spiro-helical projection 18 is formed from a helically wound dielectrically coated wire, which is shown in greater detail in Figs. 8 and 9, which is bonded to the inner surface ofsections dielectric layer 50.Feedhorn antenna 10 is shown coupled to acircular waveguide section 20, which is of a size that is capable of propagating the TE" mode in the frequency band of interest, in a manner that thelongitudinal axis 22 ofwaveguide section 20 andfeedhorn antenna 10 correspond. - In accordance with the present invention, a suitable transition from the TE" mode to the HE,, mode is obtained in such embodiment by starting with a round dielectrically coated wire which is partially flattened in a rolling mill and then edge-wound in closely spaced helical turns in the area adjacent to
circular waveguide 20 which is at the TE,, mode end ofcircular waveguide section 12. Flattening of this wire to produce the helical turns substantially increases the capacitance between adjacent turns and, therefore, substantially reduces the leakage per wavelength of the propagating signal intodielectric layer 50. - As shown in Fig. 8, the flattening of the wire, as depicted in portions II to IV of Fig. 8, is gradually reduced starting at the input TE11 mode end
adjacent waveguide 20 to a round cross-section of closely spaced turns. For example, if a No. 15 gauge Formex (Registered Trade Mark) copper wire is used to form the helical turns of portions II to IV of Fig. 8, the wire may initially be flattened to dimensions of, for example, approximately 0.74 by 1.96 millimeters which changes gradually to a round cross-section. In essence, the outer diameter of the spiral structure of Fig. 8 is tapered as the helix progresses away from the TEll mode signal entrance port. The overall length of portions II to IV in Fig. 8 is an arbitrary value and is merely of sufficient length to provide a smooth transition area for continuity of the TE11 modes betweenwaveguide 20 and portion II, and mode conversion to the HE11 mode in portions III to V. Theedges 26 of the helical turns 18 should also be an extension of theinner wall 28 ofcircular waveguide 20 to avoid reflective surfaces for the propagating signal. - The next portion of
section 12 shown by portions IV and V of Fig. 8 includes a helical winding with a tapered pitch which starts with a zero spacing and gradually has the spacings between turns increased in a linear manner. The remainder of the helical turns insection 12 and insection 14 are of uniform pitch of, for example, approximately 3 wire diameters center-to- center as shown in Fig. 9. Therefore, in portions II to V of Fig. 8, the continuity of the TE11 mode is preserved in a smooth transition betweenwaveguide 20 andhorn antenna 10 and the TE11 mode is converted to the HE11 mode by the gradually increased spacing between the helical turns while theconical section 14 provides a proper impedance match with its uniform tapered helical turns for launching the converted mode from themouth 16 offeedhorn antenna 10 into space. - An alternative and preferred method for forming the
feedhorn antenna 10 in accordance with the present invention is shown in Fig. 10. There a multi-layer helical wire structure is formed in thearea 30 which is equivalent to portions II to IV of Fig. 8. In forming the helical projection of Fig. 10, a round dielectrically coated wire is first formed in a helix of closely spaced turns for the length ofarea 30 and then inarea 32 the spacings between the helical turns are gradually increased in a linear manner.Wire 38 continues its helical spiral for the remainder ofsection 12 and insection 14, in the manner shown in Fig. 9, with a uniform pitch. Oncewire 38 has been formed as described for traversing the entire length of the inside surface offeedhorn 10, a second layer of helical turns of dielectricallycoated wire 40 is superimposed on top of the helical turns ofwire 38 starting atwaveguide 20 and extending for most of the length oftransition area 30. Additional layers of helical turns of dielectrically coated wire are then superimposed on top ofwires area 30 so as to effectively form ataper 44 along the ends of the layers. In accordance with the present invention, the number of layers of wire intransition area 30 is arbitrary and should be of a sufficient number to provide a low enough surface impedance for propagating the TE" mode. In forming the arrangement of Fig. 10 it was found that preferably at least four layers should be used and that each additional layer of wire improved the performance substantially by providing less leakage per wavelength. - Construction of the helical arrangements of Figs. 7-10 can be accomplished by winding the
wire dielectric material 50 is bonded to thewire conductive sheath 48. The combinedthickness 51 ofdielectric layer 50 andhelix wire 18 capacitive loading should be approximately an electrical quarter wavelength at the lowest operating frequency. Theouter shield wall 48 can comprise any suitable conductive material. Thefinal feedhorn 10 structure can then be coupled towaveguide 20 by any suitable means, as for example, a flange (not shown). - Fig. 11 illustrates a circular
hybrid mode waveguide 70 formed in the same manner as that shown in Figs. 7-10 and described hereinbefore forfeedhorn antenna 10 except thatcircular waveguide section 10 continues with the same uniform diameter insection 72 as found insection 12 instead of converting to aconical section 14 as found infeedhorn antenna 10.
Claims (13)
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US68726 | 1979-08-22 | ||
US06/068,621 US4231042A (en) | 1979-08-22 | 1979-08-22 | Hybrid mode waveguide and feedhorn antennas |
US06/068,726 US4246584A (en) | 1979-08-22 | 1979-08-22 | Hybrid mode waveguide or feedhorn antenna |
US68621 | 1979-08-22 |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0024685A1 EP0024685A1 (en) | 1981-03-11 |
EP0024685B1 true EP0024685B1 (en) | 1984-02-15 |
Family
ID=26749172
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP19800104951 Expired EP0024685B1 (en) | 1979-08-22 | 1980-08-20 | Hybrid mode waveguiding member and hybrid mode feedhorn antenna |
Country Status (2)
Country | Link |
---|---|
EP (1) | EP0024685B1 (en) |
DE (1) | DE3066596D1 (en) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4467292A (en) * | 1982-09-30 | 1984-08-21 | Hughes Aircraft Company | Millimeter-wave phase shifting device |
FR2603425B1 (en) * | 1986-09-02 | 1988-11-10 | Thomson Csf | WAVEGUIDE FILTERING CIRCULAR POLARIZATION |
US4971847A (en) * | 1989-06-02 | 1990-11-20 | Rohm And Haas Company | Multilayered structures |
US11289816B2 (en) | 2017-02-28 | 2022-03-29 | Toyota Motor Europe | Helically corrugated horn antenna and helically corrugated waveguide system |
CN112615161A (en) * | 2020-12-08 | 2021-04-06 | 中国科学院新疆天文台 | 7-millimeter-wave-band broadband small-opening-angle shaped corrugated horn feed source |
US11613931B2 (en) | 2021-07-06 | 2023-03-28 | Quaise, Inc. | Multi-piece corrugated waveguide |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR998819A (en) * | 1949-10-14 | 1952-01-23 | Csf | Improvements in the coupling of linear wave propagation tubes with their input and output circuits |
US2716202A (en) * | 1950-06-20 | 1955-08-23 | Bell Telephone Labor Inc | Microwave amplifier electron discharge device |
US2752494A (en) * | 1951-08-22 | 1956-06-26 | Polytechnic Res And Dev Compan | Wide range resonator |
GB811738A (en) * | 1955-06-28 | 1959-04-08 | Siemens Ag | Improvements in or relating to electromagnetic wave guides |
BE570125A (en) * | 1957-08-23 | |||
US2950454A (en) * | 1958-10-30 | 1960-08-23 | Bell Telephone Labor Inc | Helix wave guide |
-
1980
- 1980-08-20 DE DE8080104951T patent/DE3066596D1/en not_active Expired
- 1980-08-20 EP EP19800104951 patent/EP0024685B1/en not_active Expired
Also Published As
Publication number | Publication date |
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DE3066596D1 (en) | 1984-03-22 |
EP0024685A1 (en) | 1981-03-11 |
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