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US3803622A - Hf dual-feed corner reflector antenna - Google Patents

Hf dual-feed corner reflector antenna Download PDF

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Publication number
US3803622A
US3803622A US00357045A US35704573A US3803622A US 3803622 A US3803622 A US 3803622A US 00357045 A US00357045 A US 00357045A US 35704573 A US35704573 A US 35704573A US 3803622 A US3803622 A US 3803622A
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planes
lambda
antenna
edges
flared
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US00357045A
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J Thornton
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US Department of Navy
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    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q19/00—Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic
    • H01Q19/10—Combinations 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
    • H01Q19/12—Combinations 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
    • H01Q19/17—Combinations 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 comprising two or more radiating elements
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q15/00—Devices for reflection, refraction, diffraction or polarisation of waves radiated from an antenna, e.g. quasi-optical devices
    • H01Q15/14—Reflecting surfaces; Equivalent structures
    • H01Q15/18—Reflecting surfaces; Equivalent structures comprising plurality of mutually inclined plane surfaces, e.g. corner reflector
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q5/00—Arrangements for simultaneous operation of antennas on two or more different wavebands, e.g. dual-band or multi-band arrangements
    • H01Q5/40—Imbricated or interleaved structures; Combined or electromagnetically coupled arrangements, e.g. comprising two or more non-connected fed radiating elements
    • H01Q5/45—Imbricated or interleaved structures; Combined or electromagnetically coupled arrangements, e.g. comprising two or more non-connected fed radiating elements using two or more feeds in association with a common reflecting, diffracting or refracting device

Definitions

  • ABSTRACT A high frequency, corner reflector antenna comprising two screens of vertical wires positioned at right angles to each other and two active elements located therebetween.
  • the device is operable over a frequency bandwidth of 4:1 and can provide an azimuth pattern beamwidth of 45.
  • the active elements comprise moderate-Q radiators tunable over a 2:1 frequency range whereby two frequencies can be transmitted simultaneously without the use of multicouplers.
  • corner reflector antennas to foucs and reflect electromagnetic energy is well-known.
  • the antenna normally comprises two conductive planes intersecting at any angle up to 180, and is usually excited by a dipole radiator or a monopole erected over a conducting plane whereby the antenna has a high-gain and moderate bandwidth.
  • the use of more than one active element within a corner reflector to increase the bandwidth is believed to be new in the art.
  • the antenna most commonly used for HP communications is the horizontal rhombic antenna which has a useful bandwidth limited to the ratio of 2:1 by the allowable radiation pattern variations and tolerable side lobe level.
  • the rhombic antenna is best suited for longdistance, point-to-point circuits where low elevationangle radiation is desirable.
  • the dual-feed corner reflector to be disclosed is better suited for variablelength circuits where broader and more consistent vertical patterns are desirable.
  • rhombic antennas designed for elevation angles inevitably have a narrow main horizontal lobe.
  • the nominal azimuth half-power beamwidth of the dual feed corner reflector is 45 over a 4:1 frequency range, enabling a broader sector to be monitored and thereby being less sensitive to normal signal variations in the horizontal plane.
  • Experimental studies have shown that at least two rhombic antennas would be required to cover the 4:1 bandwidth covered by a single dual-feed corner reflector antenna of the type to be described herein.
  • SUMMARY HF antenna apparatus comprising a dual-feed, corner reflector antenna. Flared, wire grids are connected to a corner reflector structure consisting of two conductive planes with intersect at 90" A pair of moderate-Q antennas are positioned. symmetrically within the 90 angle in such a manner that two frequencies can be transmitted simultaneously without use of a multicoupler.
  • FIG. 1 is an isometric view of the novel antenna to be described hereinafter;
  • FIG. 2 is a top view of the antenna of FIG. 1;
  • FIG. 3 is a side view of the right-hand side of the antenna of FIGS. 1 and 2;
  • FIGS. 4 and 5 represent azimuthal directivity voltage patterns achieved with the antenna of FIG. 1;
  • FIGS. 6 and 7 represent vertical-plane voltage patterns achieved as above.
  • FIG. 1 represents a dualfeed corner reflector antenna 10 embodying the present inventive concept.
  • the antenna has the capability of covering a 4:1 frequency bandwidth with a halfpower azimuth beamwidth of 45.
  • Two moderate-Q antennas, 12 and 14 are used as the active radiators, each covering a 2:1 frequency range.
  • the arrangement shown allows simultaneous transmissions of two -KW peak signals without the use of multicouplers. One transmission is within the upper octave frequency range and the other is within the adjacent lower octave range.
  • the gain obtainable on beam over perfect ground is 11 to 16 dBs relative to an isotropic radiator.
  • the comer reflector 10 comprises two wire screens or grids, l6 and 18, which intersect at the apex 19 at right angles with respect to each other.
  • the screens 20 and 24 intersect with the screens 16 andl8 at the apexes 21 and 23, respectively, and at an angle of 10 with respect to each other.
  • the apexes 21 and 23 are a distance of about 0.21 A from the apex 19.
  • a second pair of flared screen portions 22 and 24 are positioned at an angle of 20 with respect to the first flared pair 20 and 24, respectively, and at a distance of about 0.24 A from the apex 19.
  • FIG. 2 is a simplified top view of the antenna of FIG. 1. As'can be seen, the active elements l2 and 14 are symmetrically located between the screens 16 and 18 at about 0.0. About 96 wires are required and as shown, they are connected by horizontal wires at the top and mid-points. The flare portion 22 (and 26) comprise six horizontal wires spaced as shown in FIG. 2 and connected at the top by horizontal wires.
  • the grid configuration and the spacings between the vertical wires of the flare portions-22 and 26 are different from those of the remaining portions to produce the necessary pattern-broadening effects at these frequencies.
  • Experimental pattern measurements were made on various configurations of the antenna, from which the following observations were made. Increasing the length of the reflector narrowed the patterns, while increasing the width of the aperture had a broadening effect. Controlling the leakage of energy to the reflectors sides enables patterns at specific frequency ranges to be changed, and pattern beamwidth at specific ranges of frequencies could also be increased by increasing the width of the corner at specific distances from the apex,
  • a dual-feed corner reflector antenna for use as a high frequency transmitting antenna where omnidirectional azimuthal radiation is not necessary nor desirable and directive gain can be used.
  • the antenna can be used to provide enhanced signal strength of both sky wave and ground wave for a given sector and to provide enhanced sky wave coverage for ranges as close as 180.
  • the antenna can also be used to direct an antenna beam along a heavily used route for ship/shore/ship communications.
  • An HF antenna comprising:
  • a corner reflector antenna comprising two rectangular conductive planes intersecting at an angle of with respect to each other;
  • first flared conductive planes electrically connected to the edges of said two conductive planes parallel to the intersecting edges thereof and intersecting said edges at an angle of approximately 10;
  • said pair of active elements comprise first and second moderate-Q antennas positioned 0.12) and 033A from the intersection of said two conductive planes whereby said antenna can simultaneously transmit two frequencies over a frequency bandwidth of 4:1 and with an azimuth pattern beamwidth of 45.

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  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Aerials With Secondary Devices (AREA)
  • Variable-Direction Aerials And Aerial Arrays (AREA)

Abstract

A high frequency, corner reflector antenna comprising two screens of vertical wires positioned at right angles to each other and two active elements located therebetween. The device is operable over a frequency bandwidth of 4:1 and can provide an azimuth pattern beamwidth of 45*. The active elements comprise moderate-Q radiators tunable over a 2:1 frequency range whereby two frequencies can be transmitted simultaneously without the use of multicouplers.

Description

United States Patent [1 1 Thornton [111 3,803,622 [451 Apr. 9, 1974 HF DUAL-FEED CORNER REFLECTOR ANTENNA [75] Inventor: John H. Thornton, San Diego, Calif.
[73] Assignee: The United States of America as represented by the Secretary of the Navy, Washington, DC.
[22] Filed; May 3, 1973 [21] Appl. No.: 357,045
[52] US. Cl. 343/836, 343/914 [51] Int. Cl. H01q 19/28 [58] Field of Search 343/834, 835, 836, 914
[56] References Cited UNITED STATES PATENTS 3,483,563 12/1969 Schroeder 343/835 Primary ExaminerEli Lieberman Attorney, Agent, or Firm-R. S. Sciascia; G. J. Rubens; J. W. McLaren [5 7] ABSTRACT A high frequency, corner reflector antenna comprising two screens of vertical wires positioned at right angles to each other and two active elements located therebetween. The device is operable over a frequency bandwidth of 4:1 and can provide an azimuth pattern beamwidth of 45. The active elements comprise moderate-Q radiators tunable over a 2:1 frequency range whereby two frequencies can be transmitted simultaneously without the use of multicouplers.
4 Claims, 7 Drawing Figures HF DUAL-FEED CORNER REFLECTOR ANTENNA BACKGROUND OF THE INVENTION The use of corner reflector antennas to foucs and reflect electromagnetic energy is well-known. The antenna normally comprises two conductive planes intersecting at any angle up to 180, and is usually excited by a dipole radiator or a monopole erected over a conducting plane whereby the antenna has a high-gain and moderate bandwidth. The use of more than one active element within a corner reflector to increase the bandwidth, however, is believed to be new in the art.
The antenna most commonly used for HP communications is the horizontal rhombic antenna which has a useful bandwidth limited to the ratio of 2:1 by the allowable radiation pattern variations and tolerable side lobe level. The rhombic antenna is best suited for longdistance, point-to-point circuits where low elevationangle radiation is desirable. The dual-feed corner reflector to be disclosed is better suited for variablelength circuits where broader and more consistent vertical patterns are desirable. Furthermore, rhombic antennas designed for elevation angles inevitably have a narrow main horizontal lobe. The nominal azimuth half-power beamwidth of the dual feed corner reflector is 45 over a 4:1 frequency range, enabling a broader sector to be monitored and thereby being less sensitive to normal signal variations in the horizontal plane. Experimental studies have shown that at least two rhombic antennas would be required to cover the 4:1 bandwidth covered by a single dual-feed corner reflector antenna of the type to be described herein.
SUMMARY HF antenna apparatus are disclosed comprising a dual-feed, corner reflector antenna. Flared, wire grids are connected to a corner reflector structure consisting of two conductive planes with intersect at 90" A pair of moderate-Q antennas are positioned. symmetrically within the 90 angle in such a manner that two frequencies can be transmitted simultaneously without use of a multicoupler.
OBJECTS It is the primary object of the present invention to disclose HF antenna apparatus operable over a bandwidth of 4:1 and with a pattern beamwidth'of 45 and capable of simultaneously transmitting two frequencies without use of multicouplers.
Other objects, advantages and novel features of the invention will become apparent from the following detailed description of the invention when considered in' conjunction with the accompanying drawings.
BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 is an isometric view of the novel antenna to be described hereinafter;
FIG. 2 is a top view of the antenna of FIG. 1;
FIG. 3 is a side view of the right-hand side of the antenna of FIGS. 1 and 2;
FIGS. 4 and 5 represent azimuthal directivity voltage patterns achieved with the antenna of FIG. 1; and
FIGS. 6 and 7 represent vertical-plane voltage patterns achieved as above.
DESCRIPTION OF THE PREFERRED EMBODIMENT The configuration shown in FIG. 1 represents a dualfeed corner reflector antenna 10 embodying the present inventive concept. The antenna has the capability of covering a 4:1 frequency bandwidth with a halfpower azimuth beamwidth of 45. Two moderate-Q antennas, 12 and 14, are used as the active radiators, each covering a 2:1 frequency range. The arrangement shown allows simultaneous transmissions of two -KW peak signals without the use of multicouplers. One transmission is within the upper octave frequency range and the other is within the adjacent lower octave range. The gain obtainable on beam over perfect ground is 11 to 16 dBs relative to an isotropic radiator.
The comer reflector 10 comprises two wire screens or grids, l6 and 18, which intersect at the apex 19 at right angles with respect to each other. The screens 20 and 24 intersect with the screens 16 andl8 at the apexes 21 and 23, respectively, and at an angle of 10 with respect to each other. The apexes 21 and 23 are a distance of about 0.21 A from the apex 19.
A second pair of flared screen portions 22 and 24 are positioned at an angle of 20 with respect to the first flared pair 20 and 24, respectively, and at a distance of about 0.24 A from the apex 19.
FIG. 2 is a simplified top view of the antenna of FIG. 1. As'can be seen, the active elements l2 and 14 are symmetrically located between the screens 16 and 18 at about 0.0. About 96 wires are required and as shown, they are connected by horizontal wires at the top and mid-points. The flare portion 22 (and 26) comprise six horizontal wires spaced as shown in FIG. 2 and connected at the top by horizontal wires.
The grid configuration and the spacings between the vertical wires of the flare portions-22 and 26 are different from those of the remaining portions to produce the necessary pattern-broadening effects at these frequencies. Experimental pattern measurements were made on various configurations of the antenna, from which the following observations were made. Increasing the length of the reflector narrowed the patterns, while increasing the width of the aperture had a broadening effect. Controlling the leakage of energy to the reflectors sides enables patterns at specific frequency ranges to be changed, and pattern beamwidth at specific ranges of frequencies could also be increased by increasing the width of the corner at specific distances from the apex,
It was further experimentally demonstrated that if two whip radiators were used in the corner simultaneously, pattern splitting and broadening occurred at higher frequencies. Consequently, to reduce the reradiated energy and the pattern distortion, the vertical monopoles were replaced with tunable antennas. The moderate-Q antenna which is characterized by narrow bandwidth was chosen because of its frequency selectivity, low-profile, and adaptability to tuning. The combination of the two moderate-Q radiators producedthe desired'results, with the beamwidth being only slightly narrow at the high frequencies. Adding the 10 flare portions and modifying the grid configuration produced the necessary pattern broadening effects at the frequencies of interest.
Experimental testing also was utilized to determine the optimum number of grid elements required to approach the results obtained with solid copper sheets. The results have previously been described with respect to H6. 3.
Consideration was also given to providing isolation between the radiators since RF energy will be coupled from one moderate-Q radiator to the other because of their proximity. When the two radiators are transmitting simultaneously there will be instants of time when voltage resulting from the coupled power will add in phase within the coaxial transmission line with the voltage of the transmitted signal. Therefore consideration must be given to the voltage rating of the coaxial cable. To reduce the coupling passive filter networks may be used to provide additional isolation'without degrading the performance of each antenna. These networks may be in the form of either transmission line segments or lumped constants.
Thus it can be seen that a dual-feed corner reflector antenna has been disclosed for use as a high frequency transmitting antenna where omnidirectional azimuthal radiation is not necessary nor desirable and directive gain can be used. The antenna can be used to provide enhanced signal strength of both sky wave and ground wave for a given sector and to provide enhanced sky wave coverage for ranges as close as 180. The antenna can also be used to direct an antenna beam along a heavily used route for ship/shore/ship communications.
Obviously many modifications and variations of the present invention are possible in the light of the above teachings. It is therefore to be understood that within the scope of the appended claims the invention may be practiced otherwise than as specifically described.
What is claimed is:
1. An HF antenna comprising:
a corner reflector antenna comprising two rectangular conductive planes intersecting at an angle of with respect to each other;
first flared conductive planes electrically connected to the edges of said two conductive planes parallel to the intersecting edges thereof and intersecting said edges at an angle of approximately 10;
second flared conductive planes electrically connected to the edges of said first flared planes parallel to the intersecting edges thereof and positioned to form an angle of approximately 20 therewith; and,
a pair of active elements electrically connected to said conductive planes and being symmetrically positioned within said 90 angle.
2. The antenna of claim 1 wherein said two conductive planes are 0.21% long, said first planes are 023A, said second planes are 0.53)\ long, and wherein all of said planes are 038A wide.
3. The antenna of claim 2 wherein said two planes and said first planes comprise 96 vertical wires spaced at 0.0M from each other and connected to horizontal wires at the top and mid-point thereof and wherein said second flared planes comprise six vertical wires sequentially spaced at 0.13), 0.1 IL, 0.13)., 0.08)., and 0.08). from the adjacent one of said wires.
4. The antenna of claim 3 wherein said pair of active elements comprise first and second moderate-Q antennas positioned 0.12) and 033A from the intersection of said two conductive planes whereby said antenna can simultaneously transmit two frequencies over a frequency bandwidth of 4:1 and with an azimuth pattern beamwidth of 45.

Claims (4)

1. An HF antenna comprising: a corner reflector antenna comprising two rectangular conductive planes intersecting at an angle of 90* with respect to each other; first flared conductive planes electrically connected to the edges of said two conductive planes parallel to the intersecting edges thereof and intersecting said edges at an angle of approximately 10*; second flared conductive planes electrically connected to the edges of said first flared planes parallel to the intersecting edges thereof and positioned to form an angle of approximately 20* therewith; and, a pair of active elements electrically connected to said conductive planes and being symmetrically positioned within said 90* angle.
2. The antenna of claim 1 wherein said two conductive planes are 0.21 lambda long, said first planes are 0.23 lambda , said second planes are 0.53 lambda long, and wherein all of said planes are 0.38 lambda wide.
3. The antenna of claim 2 wherein said two planes and said first planes comprise 96 vertical wires spaced at 0.01 lambda from each other and connected to horizontal wires at the top and mid-point thereof and wherein said second flared planes comprise six vertical wires sequentially spaced at 0.13 lambda , 0.11 lambda , 0.13 lambda , 0.08 lambda , and 0.08 lambda from the adjacent one of said wires.
4. The antenna of claim 3 wherein said pair of active elements comprise first and second moderate-Q antennas positioned 0.12 lambda and 0.33 lambda from the intersection of said two conductive planes whereby said antenna can simultaneously transmit two frequencies over a frequency bandwidth of 4:1 and with an azimuth pattern beamwidth of 45*.
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Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0022991A1 (en) * 1979-07-13 1981-01-28 Siemens Aktiengesellschaft Antenna arrangement for masking the side lobe pattern of a highly directional main antenna and its use with a panoramic search radar antenna
US4544928A (en) * 1980-07-16 1985-10-01 General Electric Company Multifrequency reflector antenna
US5977926A (en) * 1998-09-10 1999-11-02 Trw Inc. Multi-focus reflector antenna
RU2185696C1 (en) * 2001-04-28 2002-07-20 Энианс Ко. Лтд. Corner antenna
WO2002097923A1 (en) * 2001-04-28 2002-12-05 Anyans Corner antenna
US6496683B1 (en) * 1998-06-15 2002-12-17 Samsung Electronics, Co., Ltd. Apparatus and method for suppressing frequency interference
CN111430931A (en) * 2020-04-01 2020-07-17 武汉虹信通信技术有限责任公司 Radiation sheet for broadband antenna and broadband antenna

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3483563A (en) * 1965-10-13 1969-12-09 Collins Radio Co Combination vertically-horizontally polarized paracylinder antennas

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3483563A (en) * 1965-10-13 1969-12-09 Collins Radio Co Combination vertically-horizontally polarized paracylinder antennas

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0022991A1 (en) * 1979-07-13 1981-01-28 Siemens Aktiengesellschaft Antenna arrangement for masking the side lobe pattern of a highly directional main antenna and its use with a panoramic search radar antenna
US4544928A (en) * 1980-07-16 1985-10-01 General Electric Company Multifrequency reflector antenna
US6496683B1 (en) * 1998-06-15 2002-12-17 Samsung Electronics, Co., Ltd. Apparatus and method for suppressing frequency interference
US5977926A (en) * 1998-09-10 1999-11-02 Trw Inc. Multi-focus reflector antenna
RU2185696C1 (en) * 2001-04-28 2002-07-20 Энианс Ко. Лтд. Corner antenna
WO2002097923A1 (en) * 2001-04-28 2002-12-05 Anyans Corner antenna
CN111430931A (en) * 2020-04-01 2020-07-17 武汉虹信通信技术有限责任公司 Radiation sheet for broadband antenna and broadband antenna
CN111430931B (en) * 2020-04-01 2022-01-11 武汉虹信科技发展有限责任公司 Radiation sheet for broadband antenna and broadband antenna

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