US3305870A - Dual mode horn antenna - Google Patents
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- US3305870A US3305870A US301683A US30168363A US3305870A US 3305870 A US3305870 A US 3305870A US 301683 A US301683 A US 301683A US 30168363 A US30168363 A US 30168363A US 3305870 A US3305870 A US 3305870A
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- 230000004323 axial length Effects 0.000 description 1
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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
- H01Q13/025—Multimode horn antennas; Horns using higher mode of propagation
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- This invention relates in general to antenna systems and more particularly to apparatus for producing and radiating a beam of electromagnetic wave energy containing a plurality of modes.
- Horn antennas have been employed for many years to radiate electromagnetic wave energy from a waveguide into free space. These types of antennas are readily adaptable for use with waveguides since they not only serve to match the impedance of the waveguide to the impedance of free space, but also to produce a directive 'wave pattern.
- horn antennas have been of rectangular cross section because of the attendant simple transition to a standard rectangular waveguide. Moreover, use of a rectangular waveguide together with a rectangular horn antenna allows the plane of polarization of the microwave energy to remain fixed.
- Horn antennas of conical cross section operating in the dominant TE mode, have a beamwidth which is more nearly equal in the E and H planes than rectangular or square horns operating in their dominant modes, and these antennas are particularly desirable in applications where a variety of polarizations are needed.
- conical horn antennas have not been more widely utilized because of the high side lobe levels characteristic of their radiation patterns which have been incompatible for certain applications.
- the antenna of the present invention provides a radiation pattern of equal beamwidths in the E and H plane and further characterized by having greatly suppressed side lobes.
- Electromagnetic wave energy in the dominant mode is transferred from a circular waveguide to a cylindrical transition section of waveguide wherein a portion of the energy is converted into energy of a higher order mode. Energy in both modes then propagates from the transition section into a conical horn antenna and hence into 'free space.
- a source of microwave energy in the dominant TE mode is tied into an input circular waveguide.
- the waveguide is abruptly connected to one end of a circular transition section of waveguide having a diameter larger As the energy in the dominant TE mode enters the transition section, due to the abrupt transition a portion of the TE mode energy is converted to the higher order TM mode.
- the other end of the transition section is connected to a conical horn antenna 3,305,870 Patented Feb. 21, 1967 and has the same diameter as the end of the horn antenna to which it is connected.
- the horn antenna then flares outwardly at a fixed angle for a predetermined length.
- the two modes Since the two modes have different phase velocities, they travel down the transition section and horn antenna in an out of phase relationship. However, the length and diameter of the transition section, as well as the length and flare angle of the horn antenna, are so selected that the main beam of both modes will radiate into free space in phase. The resultant combination of the main beams of the two mode results in a radiation pattern having substantially equal beamwidth in the E and H planes and a very low side lobe level.
- FIG. 1 is a side view, partly in section, of a novel antenna system in accordance with this invention
- FIG. 2 is the electric field pattern of the TE mode in a circular waveguide in a plane perpendicular to the axis of the circular waveguide;
- FIG. 3 is the electric field pattern of the TM mode in a circular waveguide in a plane perpendicular to the axis of the circular waveguide;
- FIG. 4 is a three-dimensional radiation pattern, partially cut away, for the TE mode emanating fromthe horn antenna of FIG. 1;
- FIG. 5 is a three-dimensional radiation pattern, partially cut away, for the TM mode emanating from the horn antenna of FIG. 1.
- FIG. 1 a microwave antenna system which is used to transmit a radiation pattern employing an embodiment of the novel apparatus in accordance with this invention.
- the antenna system contains a source 12 of dominant TE mode electromagnetic wave energy connected to an input end of a circular waveguide 14 having an inner diameter D
- the other end of the waveguide 14 is con nected to one end of a cylindrical transition section of waveguide 16.
- the section 16 has an axial length L;- and an inner diameter D
- the section contains an end plate 18 having an aperture into which one end of waveguide 14 fil's and completes an abrupt transition between the waveguide 14 and section 16.
- the other end of the section 16 is connected to a horn antenna 24 havinga length L
- the end of the antenna connected to the section has the same inner diameter D as the section.
- the horn antenna is flared outwardly at an angle a towards its output end until it reaches an inner diameter D
- the source 12 which may be any conventional microwave generator feeds signals in the dominant TE mode into the circular waveguide 14.
- the electric field pattern of the TE mode in a circular waveguide is shown in FIG. 2.
- the abrupt transition in diameter between the waveguide 14 and section 16 causes a portion of the TE mode energy to be converted into higher order TM mode energy.
- the electric field pattern of the TM mode in a circular waveguide is shown in FIG. 3.
- Energy in the TE and TM modes are in phase in the transition section 16 at its junction with the waveguide 14.
- the relative phases of the TE and TM modes will vary as energy in the modes begins to travel in the transition section towards the horn antenna because each of the modes has dilferent phase velocities in both the antenna and section. Normally the relative phases of both modes are adjusted to be in phase at the radiating end of the horn antenna 24.
- phase velocities of the TE and TM modes are a function of the diameter of the transition section 16 and the horn antenna 18.
- the diameter of the transition section 16 is chosen as close as possible to cut olf for the TM mode because at near cut off the phase velocity of the mode varies the greatest amount with changes in diameter.
- the phase velocity of the TM mode may be varied over a wide range.
- phase velocity of the TE and TM modes in the section 16 and antenna 24 have been fixed, that is, the diameter of the transition section and the size of the horn antenna connected thereto have been chosen, by merely varying the length of the transition section 16, the relative phase of each of the modes may be easily adjusted so that they radiate at the end of the horn in phase.
- the amount of TE mode energy which will be converted into higher order TM mode energy is dependent upon the relative difference in diameters between the waveguide 14 (D and the transition section 16 (D The greater the difference between these two diameters the greater the amount of TE mode energy which will be converted into TM mode energy.
- the amount of TM mode energy in the transition section is increased by decreasing the diameter of the waveguide 14.
- FIGS. 4 and 5 there are depicted three dimensional representations of the radiation patterns for the TE and TM modes, respectively, which are emanating from the horn antenna 24.
- the main beam 28 of radiation emanating in the TE mode has its greatest amplitude in the direction in which the antenna is pointing.
- the first side lobe 32 of the TE mode is out of phase with the main beam 28 by 180 and is labeled with a negative sign to indicate this fact.
- the second side lobe 34 of the TE mode is 180 out of phase with the first side lobe 32, that is, in phase with the main beam 28.
- adjacent side lobes 36, 38, of the TE mode are 180 out of phase with adjacent side lobes as can be seen in FIG. 4.
- radiation emanating from the TM mode at the output end of the horn antenna 24 comprises a pair of main beams 42, 44, which are in phase with the main beam of radiation 28 of the TE mode and 180 out of phase with the first side lobe 32 of the T13 mode.
- the first side lobe 46 of the TM mode is 180 out of phase with the main beams 42, 44, of the TM mode.
- side lobes 48 and 52 of the TM mode are 180 out of phase with their adjacent side lobes.
- the main beams 28, 42, and 44 add in phase while the side lobe 32 of the TE mode is out of phase With a portion of the main beams 42, 44 of the TM mode.
- the side lobe 32 of the TE mode tends to cancel a portion of the main beams 42, 44 of the TM mode.
- Such a cancellation of power of a portion of the main beams of the TM mode is desirable since the resultant main beam radiation pattern contains equal beamwidth in the E and H planes.
- the side lobes 34 is desirable since the resultant main beam radiation pattern contains equal beamwidth in the E and H planes.
- Diameter of waveguide 14 (D 1.25 inches. Diameter of the transition chamber 16 (D 1.6 inches. Length of transition chamber 16 (L 0.25 inch. Angular opening of the horn 24 (a) 6 Diameter of the mouth of the horn antenna 24 (D 5.4 inches.
- the TM mode does not have any measurable amount of side lobes in the H plane, TE mode side lobes in this plane are not eifectively cancelled. However, the TE mode side lobes in the H plane are usually very small and there is, therefore, no need to suppress them.
- the invention has been described as producing equal beamwidths in both the E and H planes, as can be readily seen by adjusting the relative power of the TE and TM modes, the relative beamwidths in each of these planes can be easily adjusted to a predetermined value.
- E plane and H plane have been used in the specification to designate the planes parallel to the electric field vector, and at right angles to the electric field vector, respectively.
- Apparatus for radiating a beam of electromagnetic energy having a resultant radiation pattern whose magnitudes in both the E and H planes are substantially equal and having a low side lobe level comprising:
- a cylindrical transition section 0 fwaveguide of diameter D having an input end and an output end, the input end of said transition section being abruptly connected to the output end of said feed Waveguide by means of an end plate so that energy in the TE mode will be converted into TM mode energy in the transition section as the microwave energy enters the transition section from said feed Waveguide, the diameter D of said transition section having a cut off wavelength for modes higher than the TM mode at said predetermined frequency;
- a conical horn antenna having an input end and an output end, the input end of said horn antenna having the same diameter as the output end of said transition section and being connected thereto so that electromagnetic Wave energy is transferred to said horn antenna and radiates into free space, the length and diameter of said transition section and the length and the flare angle of said horn antenna being so selected that energy radiating into free space in the TE and TM modes will radiate from the output end of the horn antenna with their main beams in phase.
- Apparatus for radiating electromagnetic wave energy having a substantially equal beamwidth in the E and H planes and having a low sidelobe level comprising:
- a circular input waveguide having an input end and an output end
- a cylindrical transition section of waveguide having an input end and an output end and the same longitudinal axis as said input waveguide, but having a larger diameter than the input waveguide, the output end of said input waveguide being connected to the input end of said transition section by means of an end plate in a plane normal to said longitudinal axis, whereby, due to the abrupt transition between said input waveguide and said transition section, a portion of said TE rnode energy will be converted into TM mode energy;
- a conical horn antenna having an input end and an output end, said antenna input end having the same diameter as the transition section :and being connected to the output end thereof, the length and diameter of said transition section and the length and the flare angle of said horn antenna being chosen so that energy in the TE and TM modes are substantially in phase at the output end of said antenna.
- a microwave antenna system comprising in combination:
- a circular waveguide having an input end and an output end
- a cylindrical transition section of waveguide for converting a portion of said TE mode into energy in the TM mode, said section having a diameter larger than said input waveguide and having an input end and an output end, the input end of said transition section being connected to the output end of said waveguide so as to form an abrupt transition for electromagnetic wave energy travelling in said waveguide;
- a conical horn antenna having an input end of equal diameter as said transition section and connected thereto and having an output end having a diameter greater than said input end wherein electromagnetic wave energy is radiated into free space at said output end of said antenna;
- the length and the diameter of said transition section and the length and the flare angle of said horn antenna having parameters that allow the main beams wave energy having a resultant radiation pattern whose 5 magnitude in both the E plane and H plane are similar,
- a conical horn antenna having a substantially circular cross section and having an input end and an output end;
- a source of electromagnetic wave energy at a predetermined frequency for introducing signals in the TE mode into the input end of said feed waveguide;
- a cylindrical transition section of waveguide having an input end and an output end, the output end of said feed waveguide being connected to the input end of said transition section by an abrupt transition, the diameter of said transition section being large enough so that the TM mode can prop-agate therein at said predetermined frequency, and the output end of said transition chamber being connected to the input end of said horn antenna.
- a circular waveguide having an input end and an output end
- a conical horn antenna connected to the output end of said transition section, the length and the diameter of said transition section and the length and flare angle of said conical horn antenna being chosen so that the main beam emanating into free space from said horn antenna of both said TE and TM modes are in phase.
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Description
Feb. 21, 1967 JAMES E. WEBB 3,305,870
ADMINISTRATOR OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION DUAL MODE HORN ANTENNA Filed Aug. 12, 1963 2 Sheets-Sheet 1 I N VEN TOR Philip D. Potter ATTORNEY Feb. 21, 1967 J E WE B 3,305,870
ADMINISTRATOR OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION DUAL MODE HORN ANTENNA Filed Aug. 12, 1963 2 Sheets-Sheet 2 INVENTOR PAH/3 12 P177727? ATTORNEY I than the input waveguide.
United States Patent C) ice 3,305,870 DUAL MODE HORN ANTENNA James E. Webb, Administrator of the National Aeronautics and Space Administration, with respect to an invention of Philip D. Potter, Tujunga, Calif.
Filed Aug. 12, 1963, Ser. No. 301,683 6 Claims. (Cl. 343786) This invention relates in general to antenna systems and more particularly to apparatus for producing and radiating a beam of electromagnetic wave energy containing a plurality of modes.
The invention described herein was made in the performance of work under a NASA contract and is subject to the provisions of Section 305 of the National Aeronan-tics and Space Act of 1958, Public Law 85568 (72 Stat. 435; 42 USC 2457).
Horn antennas have been employed for many years to radiate electromagnetic wave energy from a waveguide into free space. These types of antennas are readily adaptable for use with waveguides since they not only serve to match the impedance of the waveguide to the impedance of free space, but also to produce a directive 'wave pattern.
Heretofore, most horn antennas have been of rectangular cross section because of the attendant simple transition to a standard rectangular waveguide. Moreover, use of a rectangular waveguide together with a rectangular horn antenna allows the plane of polarization of the microwave energy to remain fixed.
A. recent development in horn antennas which results in a radiation pattern having both equal beamwidth and low side lobes is the diagonal horn antenna. All cross sections through the diagonal horn antenna are square. For small flare angles of the horn antenna, the mode of propagation within the horn is such that the electric field vector is parallel to one of the diagonals of the antenna. The resulting radiation pattern possesses almost equal beamwidth in the E and H planes. Side lobe level for the diagonal horn antenna, however, has a theoretical limit of 31.5 decibels.
Horn antennas of conical cross section, operating in the dominant TE mode, have a beamwidth which is more nearly equal in the E and H planes than rectangular or square horns operating in their dominant modes, and these antennas are particularly desirable in applications where a variety of polarizations are needed. However, conical horn antennas have not been more widely utilized because of the high side lobe levels characteristic of their radiation patterns which have been incompatible for certain applications.
In order to overcome these attendant disadvantages in the prior art antennas, the antenna of the present invention provides a radiation pattern of equal beamwidths in the E and H plane and further characterized by having greatly suppressed side lobes. Electromagnetic wave energy in the dominant mode is transferred from a circular waveguide to a cylindrical transition section of waveguide wherein a portion of the energy is converted into energy of a higher order mode. Energy in both modes then propagates from the transition section into a conical horn antenna and hence into 'free space.
More specifically, according to an embodiment of the invention, a source of microwave energy in the dominant TE mode is tied into an input circular waveguide. The waveguide is abruptly connected to one end of a circular transition section of waveguide having a diameter larger As the energy in the dominant TE mode enters the transition section, due to the abrupt transition a portion of the TE mode energy is converted to the higher order TM mode. The other end of the transition section is connected to a conical horn antenna 3,305,870 Patented Feb. 21, 1967 and has the same diameter as the end of the horn antenna to which it is connected. The horn antenna then flares outwardly at a fixed angle for a predetermined length. Since the two modes have different phase velocities, they travel down the transition section and horn antenna in an out of phase relationship. However, the length and diameter of the transition section, as well as the length and flare angle of the horn antenna, are so selected that the main beam of both modes will radiate into free space in phase. The resultant combination of the main beams of the two mode results in a radiation pattern having substantially equal beamwidth in the E and H planes and a very low side lobe level.
The advantages of this invention, both as to its construction and mode of operation, will be readily appreciated as the same become 'better understood by reference to the following detailed description when considered in connection with the accompanying drawings in which like referenced numerals designate like parts throughout the figures and wherein:
FIG. 1 is a side view, partly in section, of a novel antenna system in accordance with this invention;
FIG. 2 is the electric field pattern of the TE mode in a circular waveguide in a plane perpendicular to the axis of the circular waveguide;
FIG. 3 is the electric field pattern of the TM mode in a circular waveguide in a plane perpendicular to the axis of the circular waveguide;
FIG. 4 is a three-dimensional radiation pattern, partially cut away, for the TE mode emanating fromthe horn antenna of FIG. 1; and
FIG. 5 is a three-dimensional radiation pattern, partially cut away, for the TM mode emanating from the horn antenna of FIG. 1.
Referring now to the drawings, there is shown in FIG. 1 a microwave antenna system which is used to transmit a radiation pattern employing an embodiment of the novel apparatus in accordance with this invention.
The antenna system contains a source 12 of dominant TE mode electromagnetic wave energy connected to an input end of a circular waveguide 14 having an inner diameter D The other end of the waveguide 14 is con nected to one end of a cylindrical transition section of waveguide 16. The section 16 has an axial length L;- and an inner diameter D The section contains an end plate 18 having an aperture into which one end of waveguide 14 fil's and completes an abrupt transition between the waveguide 14 and section 16. The other end of the section 16 is connected to a horn antenna 24 havinga length L The end of the antenna connected to the section has the same inner diameter D as the section. The horn antenna is flared outwardly at an angle a towards its output end until it reaches an inner diameter D The source 12 which may be any conventional microwave generator feeds signals in the dominant TE mode into the circular waveguide 14. The electric field pattern of the TE mode in a circular waveguide is shown in FIG. 2. When the electromagnetic wave energy in the waveguide 14 reaches the end plate 18 and enters the section 16, the abrupt transition in diameter between the waveguide 14 and section 16 causes a portion of the TE mode energy to be converted into higher order TM mode energy. The electric field pattern of the TM mode in a circular waveguide is shown in FIG. 3.
Energy in the TE and TM modes are in phase in the transition section 16 at its junction with the waveguide 14. The relative phases of the TE and TM modes will vary as energy in the modes begins to travel in the transition section towards the horn antenna because each of the modes has dilferent phase velocities in both the antenna and section. Normally the relative phases of both modes are adjusted to be in phase at the radiating end of the horn antenna 24.
The phase velocities of the TE and TM modes are a function of the diameter of the transition section 16 and the horn antenna 18. The diameter of the transition section 16 is chosen as close as possible to cut olf for the TM mode because at near cut off the phase velocity of the mode varies the greatest amount with changes in diameter. Thus, by minutely changing the diameter of the transition section, the phase velocity of the TM mode may be varied over a wide range. Once the phase velocity of the TE and TM modes in the section 16 and antenna 24 have been fixed, that is, the diameter of the transition section and the size of the horn antenna connected thereto have been chosen, by merely varying the length of the transition section 16, the relative phase of each of the modes may be easily adjusted so that they radiate at the end of the horn in phase.
The amount of TE mode energy which will be converted into higher order TM mode energy is dependent upon the relative difference in diameters between the waveguide 14 (D and the transition section 16 (D The greater the difference between these two diameters the greater the amount of TE mode energy which will be converted into TM mode energy. As a practical matter, since it is desirable to make the diameter of the transition section as close to cut off for the TM mode as possible, the amount of TM mode energy in the transition section is increased by decreasing the diameter of the waveguide 14.
Referring now to FIGS. 4 and 5, there are depicted three dimensional representations of the radiation patterns for the TE and TM modes, respectively, which are emanating from the horn antenna 24. In FIG. 4 the main beam 28 of radiation emanating in the TE mode has its greatest amplitude in the direction in which the antenna is pointing. The first side lobe 32 of the TE mode is out of phase with the main beam 28 by 180 and is labeled with a negative sign to indicate this fact. The second side lobe 34 of the TE mode is 180 out of phase with the first side lobe 32, that is, in phase with the main beam 28. Further, adjacent side lobes 36, 38, of the TE mode are 180 out of phase with adjacent side lobes as can be seen in FIG. 4.
In FIG. 5, radiation emanating from the TM mode at the output end of the horn antenna 24 comprises a pair of main beams 42, 44, which are in phase with the main beam of radiation 28 of the TE mode and 180 out of phase with the first side lobe 32 of the T13 mode. The first side lobe 46 of the TM mode is 180 out of phase with the main beams 42, 44, of the TM mode. Further, side lobes 48 and 52 of the TM mode are 180 out of phase with their adjacent side lobes.
When the electromagnetic wave energy from the TE mode is combined with the electromagnetic wave energy from the TM mode, that is, the radiation patterns of FIGS. 4 and are added, the main beams 28, 42, and 44 add in phase while the side lobe 32 of the TE mode is out of phase With a portion of the main beams 42, 44 of the TM mode. Thus, the side lobe 32 of the TE mode tends to cancel a portion of the main beams 42, 44 of the TM mode. Such a cancellation of power of a portion of the main beams of the TM mode is desirable since the resultant main beam radiation pattern contains equal beamwidth in the E and H planes. Moreover, the side lobes 34. 36, and 38 will be 180 out of phase with their counterpart side lobes 46, 48, and 52 of the TM mode and will tend to cancel each other, thus reducing the strength of the side lobes in the resulting radiation pattern. While only the major side lobes of each mode have been depicted in FIGS. 4 and 5, other lobes are present in the radiation pattern, but these modes will also tend to cancel. It should be noted that the relative strength of the TE and TM modes 4 which yields the most suppressed side lobes is also the ratio which yields equal beamwidths in the E and H planes.
As an example, it has been found that side lobes can be greatly suppressed and equal beamwidths obtained along the E and H planes for a frequency of 9600 megacycles for the following dimensions:
Diameter of waveguide 14 (D 1.25 inches. Diameter of the transition chamber 16 (D 1.6 inches. Length of transition chamber 16 (L 0.25 inch. Angular opening of the horn 24 (a) 6 Diameter of the mouth of the horn antenna 24 (D 5.4 inches.
Because the TM mode does not have any measurable amount of side lobes in the H plane, TE mode side lobes in this plane are not eifectively cancelled. However, the TE mode side lobes in the H plane are usually very small and there is, therefore, no need to suppress them.
Further, although the invention has been described as producing equal beamwidths in both the E and H planes, as can be readily seen by adjusting the relative power of the TE and TM modes, the relative beamwidths in each of these planes can be easily adjusted to a predetermined value.
As is conventional, the terms E plane and H plane have been used in the specification to designate the planes parallel to the electric field vector, and at right angles to the electric field vector, respectively. 7
It should be understood that the foregoing disclosure relates only to preferred embodiments of the invention and that it is intended to cover all changes and modifications of the examples in the invention herein chosen for the purposes of the disclosure which do not constitute departures from the spirit and scope of the invention. What is claimed and desired to be secured by Letters Patent is:
1. Apparatus for radiating a beam of electromagnetic energy having a resultant radiation pattern whose magnitudes in both the E and H planes are substantially equal and having a low side lobe level comprising:
a source of electromagnetic wave enery at a predetermined frequency;
a circular feed waveguide of diameter D and having an input end and an output end;
means for coupling said source of electromagnetic wave energy at said predetermined frequency in the TE mode into the input end of said feed waveguide;
a cylindrical transition section 0 fwaveguide of diameter D having an input end and an output end, the input end of said transition section being abruptly connected to the output end of said feed Waveguide by means of an end plate so that energy in the TE mode will be converted into TM mode energy in the transition section as the microwave energy enters the transition section from said feed Waveguide, the diameter D of said transition section having a cut off wavelength for modes higher than the TM mode at said predetermined frequency; and
a conical horn antenna having an input end and an output end, the input end of said horn antenna having the same diameter as the output end of said transition section and being connected thereto so that electromagnetic Wave energy is transferred to said horn antenna and radiates into free space, the length and diameter of said transition section and the length and the flare angle of said horn antenna being so selected that energy radiating into free space in the TE and TM modes will radiate from the output end of the horn antenna with their main beams in phase.
2. Apparatus in accordance with claim 1 wherein the ratio of the diameters D D are selected so that a predetermined amount of energy in the TE mode is converted into TM mode energy.
3. Apparatus for radiating electromagnetic wave energy having a substantially equal beamwidth in the E and H planes and having a low sidelobe level comprising:
a circular input waveguide having an input end and an output end;
means for feeding a source of TE mode electromagnetic wave energy into the input end of said circular waveguide;
a cylindrical transition section of waveguide having an input end and an output end and the same longitudinal axis as said input waveguide, but having a larger diameter than the input waveguide, the output end of said input waveguide being connected to the input end of said transition section by means of an end plate in a plane normal to said longitudinal axis, whereby, due to the abrupt transition between said input waveguide and said transition section, a portion of said TE rnode energy will be converted into TM mode energy;
and a conical horn antenna having an input end and an output end, said antenna input end having the same diameter as the transition section :and being connected to the output end thereof, the length and diameter of said transition section and the length and the flare angle of said horn antenna being chosen so that energy in the TE and TM modes are substantially in phase at the output end of said antenna.
4. A microwave antenna system comprising in combination:
a circular waveguide having an input end and an output end;
means for feeding a source of electromagnetic wave energy in the TE mode into the input end of said circular waveguide;
:a cylindrical transition section of waveguide for converting a portion of said TE mode into energy in the TM mode, said section having a diameter larger than said input waveguide and having an input end and an output end, the input end of said transition section being connected to the output end of said waveguide so as to form an abrupt transition for electromagnetic wave energy travelling in said waveguide;
a conical horn antenna having an input end of equal diameter as said transition section and connected thereto and having an output end having a diameter greater than said input end wherein electromagnetic wave energy is radiated into free space at said output end of said antenna;
the length and the diameter of said transition section and the length and the flare angle of said horn antenna having parameters that allow the main beams wave energy having a resultant radiation pattern whose 5 magnitude in both the E plane and H plane are similar,
comprising:
a conical horn antenna having a substantially circular cross section and having an input end and an output end;
a feed Waveguide of circular diameter having an input and an output end;
a source of electromagnetic wave energy :at a predetermined frequency for introducing signals in the TE mode into the input end of said feed waveguide; and
a cylindrical transition section of waveguide having an input end and an output end, the output end of said feed waveguide being connected to the input end of said transition section by an abrupt transition, the diameter of said transition section being large enough so that the TM mode can prop-agate therein at said predetermined frequency, and the output end of said transition chamber being connected to the input end of said horn antenna.
6. In combination:
a circular waveguide having an input end and an output end;
means for feeding electromagnetic wave energy in the TE mode into said input end of said circular waveguide;
means connected to the output end of said waveguide for converting a portion of said TE mode energy in said circular waveguide to TM mode energy, said means comprising a transition section of waveguide having a diameter larger than said circular waveguide; and
.a conical horn antenna connected to the output end of said transition section, the length and the diameter of said transition section and the length and flare angle of said conical horn antenna being chosen so that the main beam emanating into free space from said horn antenna of both said TE and TM modes are in phase.
References Cited by the Examiner UNITED STATES PATENTS 2,283,935 5/1942 King 343786 X 2,774,067 12/1956 Bollinger 343783 X 2,881,432 4/1959 Hatkin 343--783 X 2,918,673 12/1959 Lewis et a1. 343786 3,205,498 9/1965 Child 3332l X ELI LIEBERMAN, Primary Examiner.
Claims (1)
- 6. IN COMBINATION: A CIRCULAR WAVEGUIDE HAVING AN INPUT END AND AN OUTPUT END; MEANS FOR FEEDING ELECTROMAGNETIC WAVE ENERGY IN THE TE11 MODE INTO SAID INPUT END OF SAID CIRCULAR WAVEGUIDE; MEANS CONNECTED TO THE OUTPUT END OF SAID WAVEGUIDE FOR CONVERTING A PORTION OF SAID TE11 MODE ENERGY IN SAID CIRCULAR WAVEGUIDE TO TM11 MODE ENERGY, SAID MEANS COMPRISING A TRANSITION SECTION OF WAVEGUIDE HAVING A DIAMETER LARGER THAN SAID CIRCULAR WAVEGUIDE; AND A CONICAL HORN ANTENNA CONNECTED TO THE OUTPUT END OF SAID TRANSITION SECTION, THE LENGTH AND THE DIAMETER OF SAID TRANSITION SECTION AND THE LENGTH AND FLARE ANGLE OF SAID CONICAL HORN ANTENNA BEING CHOSEN SO THAT THE MAIN BEAM EMANATING INTO FREE SPACE FROM SAID HORN ANTENNA OF BOTH SAID TE11 AND TM11 MODES ARE IN PHASE.
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US301683A US3305870A (en) | 1963-08-12 | 1963-08-12 | Dual mode horn antenna |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US301683A US3305870A (en) | 1963-08-12 | 1963-08-12 | Dual mode horn antenna |
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| US3305870A true US3305870A (en) | 1967-02-21 |
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Cited By (22)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3324423A (en) * | 1964-12-29 | 1967-06-06 | James E Webb | Dual waveguide mode source having control means for adjusting the relative amplitudesof two modes |
| US3413641A (en) * | 1966-05-05 | 1968-11-26 | Bell Telephone Labor Inc | Dual mode antenna |
| US3413642A (en) * | 1966-05-05 | 1968-11-26 | Bell Telephone Labor Inc | Dual mode antenna |
| US3500258A (en) * | 1968-12-18 | 1970-03-10 | Bell Telephone Labor Inc | Wave mode converter |
| FR2021758A1 (en) * | 1968-10-28 | 1970-07-24 | Hughes Aircraft Co | |
| FR2021757A1 (en) * | 1968-10-28 | 1970-07-24 | Hughes Aircraft Co | |
| FR2118848A1 (en) * | 1970-12-22 | 1972-08-04 | Thomson Csf | |
| US3815139A (en) * | 1973-04-16 | 1974-06-04 | Prodelin Inc | Feed horns for reflector dishes |
| FR2389248A1 (en) * | 1977-04-28 | 1978-11-24 | Andrew Corp | CORNET FOR HYPERFREQUENCY ANTENNAS |
| US4442437A (en) * | 1982-01-25 | 1984-04-10 | Bell Telephone Laboratories, Incorporated | Small dual frequency band, dual-mode feedhorn |
| USD283129S (en) | 1983-06-30 | 1986-03-25 | Miralite International, Inc. | Microwave feed horn |
| US4788553A (en) * | 1983-04-06 | 1988-11-29 | Trw Inc. | Doppler radar velocity measurement apparatus |
| US4962384A (en) * | 1986-03-06 | 1990-10-09 | Walker Charles W E | Microwave antenna apparatus |
| US5017937A (en) * | 1986-03-25 | 1991-05-21 | The Marconi Company Limited | Wideband horn antenna |
| US20100238082A1 (en) * | 2009-03-18 | 2010-09-23 | Kits Van Heyningen Martin Arend | Multi-Band Antenna System for Satellite Communications |
| US20110068988A1 (en) * | 2009-09-21 | 2011-03-24 | Monte Thomas D | Multi-Band antenna System for Satellite Communications |
| US20120186747A1 (en) * | 2011-01-26 | 2012-07-26 | Obama Shinji | Plasma processing apparatus |
| US9520637B2 (en) | 2012-08-27 | 2016-12-13 | Kvh Industries, Inc. | Agile diverse polarization multi-frequency band antenna feed with rotatable integrated distributed transceivers |
| US11493622B1 (en) | 2018-02-08 | 2022-11-08 | Telephonics Corp. | Compact radar with X band long-distance weather monitoring and W band high-resolution obstacle imaging for landing in a degraded visual environment |
| USD1003875S1 (en) * | 2021-04-15 | 2023-11-07 | Nan Hu | Corrugated feed horn antenna |
| USD1006800S1 (en) * | 2021-04-29 | 2023-12-05 | Nan Hu | Dual linear polarization conical horn antenna |
| USD1008234S1 (en) * | 2021-04-21 | 2023-12-19 | Nan Hu | Corrugated feed horn antenna |
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| US2283935A (en) * | 1938-04-29 | 1942-05-26 | Bell Telephone Labor Inc | Transmission, radiation, and reception of electromagnetic waves |
| US2774067A (en) * | 1949-08-17 | 1956-12-11 | Rca Corp | Microwave scanning antenna system |
| US2881432A (en) * | 1954-06-29 | 1959-04-07 | Hatkin Leonard | Conical scanning antenna |
| US2918673A (en) * | 1957-12-12 | 1959-12-22 | Edwin S Lewis | Antenna feed system |
| US3205498A (en) * | 1960-11-30 | 1965-09-07 | North American Aviation Inc | Dual mode radar beacon antenna |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| US2283935A (en) * | 1938-04-29 | 1942-05-26 | Bell Telephone Labor Inc | Transmission, radiation, and reception of electromagnetic waves |
| US2774067A (en) * | 1949-08-17 | 1956-12-11 | Rca Corp | Microwave scanning antenna system |
| US2881432A (en) * | 1954-06-29 | 1959-04-07 | Hatkin Leonard | Conical scanning antenna |
| US2918673A (en) * | 1957-12-12 | 1959-12-22 | Edwin S Lewis | Antenna feed system |
| US3205498A (en) * | 1960-11-30 | 1965-09-07 | North American Aviation Inc | Dual mode radar beacon antenna |
Cited By (25)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3324423A (en) * | 1964-12-29 | 1967-06-06 | James E Webb | Dual waveguide mode source having control means for adjusting the relative amplitudesof two modes |
| US3413641A (en) * | 1966-05-05 | 1968-11-26 | Bell Telephone Labor Inc | Dual mode antenna |
| US3413642A (en) * | 1966-05-05 | 1968-11-26 | Bell Telephone Labor Inc | Dual mode antenna |
| FR2021758A1 (en) * | 1968-10-28 | 1970-07-24 | Hughes Aircraft Co | |
| FR2021757A1 (en) * | 1968-10-28 | 1970-07-24 | Hughes Aircraft Co | |
| US3500258A (en) * | 1968-12-18 | 1970-03-10 | Bell Telephone Labor Inc | Wave mode converter |
| FR2118848A1 (en) * | 1970-12-22 | 1972-08-04 | Thomson Csf | |
| US3815139A (en) * | 1973-04-16 | 1974-06-04 | Prodelin Inc | Feed horns for reflector dishes |
| FR2389248A1 (en) * | 1977-04-28 | 1978-11-24 | Andrew Corp | CORNET FOR HYPERFREQUENCY ANTENNAS |
| US4442437A (en) * | 1982-01-25 | 1984-04-10 | Bell Telephone Laboratories, Incorporated | Small dual frequency band, dual-mode feedhorn |
| US4788553A (en) * | 1983-04-06 | 1988-11-29 | Trw Inc. | Doppler radar velocity measurement apparatus |
| USD283129S (en) | 1983-06-30 | 1986-03-25 | Miralite International, Inc. | Microwave feed horn |
| US4962384A (en) * | 1986-03-06 | 1990-10-09 | Walker Charles W E | Microwave antenna apparatus |
| US5017937A (en) * | 1986-03-25 | 1991-05-21 | The Marconi Company Limited | Wideband horn antenna |
| US20100238082A1 (en) * | 2009-03-18 | 2010-09-23 | Kits Van Heyningen Martin Arend | Multi-Band Antenna System for Satellite Communications |
| US8497810B2 (en) | 2009-03-18 | 2013-07-30 | Kvh Industries, Inc. | Multi-band antenna system for satellite communications |
| US20110068988A1 (en) * | 2009-09-21 | 2011-03-24 | Monte Thomas D | Multi-Band antenna System for Satellite Communications |
| EP2312693A2 (en) | 2009-09-21 | 2011-04-20 | KVH Industries, Inc. | Multi-band antenna system for satellite communications |
| US9281561B2 (en) | 2009-09-21 | 2016-03-08 | Kvh Industries, Inc. | Multi-band antenna system for satellite communications |
| US20120186747A1 (en) * | 2011-01-26 | 2012-07-26 | Obama Shinji | Plasma processing apparatus |
| US9520637B2 (en) | 2012-08-27 | 2016-12-13 | Kvh Industries, Inc. | Agile diverse polarization multi-frequency band antenna feed with rotatable integrated distributed transceivers |
| US11493622B1 (en) | 2018-02-08 | 2022-11-08 | Telephonics Corp. | Compact radar with X band long-distance weather monitoring and W band high-resolution obstacle imaging for landing in a degraded visual environment |
| USD1003875S1 (en) * | 2021-04-15 | 2023-11-07 | Nan Hu | Corrugated feed horn antenna |
| USD1008234S1 (en) * | 2021-04-21 | 2023-12-19 | Nan Hu | Corrugated feed horn antenna |
| USD1006800S1 (en) * | 2021-04-29 | 2023-12-05 | Nan Hu | Dual linear polarization conical horn antenna |
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