US2270314A - Corner reflector antenna - Google Patents
Corner reflector antenna Download PDFInfo
- Publication number
- US2270314A US2270314A US316625A US31662540A US2270314A US 2270314 A US2270314 A US 2270314A US 316625 A US316625 A US 316625A US 31662540 A US31662540 A US 31662540A US 2270314 A US2270314 A US 2270314A
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- antenna
- conductors
- corner reflector
- angle
- members
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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
- H01Q19/106—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 using two or more intersecting plane surfaces, e.g. corner reflector antennas
Definitions
- This invention relates to antennas and especially to an antenna which is placed near the corner of a pair of intersecting wave reflecting surfaces.
- the corner reflector antenna exhibits a sharply &
- the beam width can be varied by changing the angle between the reflecting surfaces, the beam becoming sharper as the angle is decreased. Corner angles of about 90 or less are both practical and desirable. Since the reflecting surfaces are planes, the array may be made cheaply and may be arranged for folding to make transportation easy.
- One of the objects of the invention is to provide means for radiating. a sharply defined directive radio field. Another object is to provide an efiicient, compact, directive antenna array. Another object is to provide a foldable reflector and antenna array. An additional object is to provide an adjustable corner reflector antenna array.
- Figures 1 and 2 are plan and perspective views, respectively, of a corner reflector antenna
- Figures 3 and 4 are perspective and plan views, respectively, of a modified corner reflector
- Figure 5 is a graph illustrating the field pattern of a 90 corner reflector antenna
- Figure 6 is a perspective view of a foldable corner reflector antenna array.
- a pair'of wave reflecting surfaces I, 3, of conductive sheets are arranged to intersect at an angle of 90.
- antenna located in the plane bisecting the angle.
- antenna can be connected or coupled to the transmitter or receiver by any of the methods well-known to the art, such as for example, by two parallel, twisted or concentric conductors.
- the distance S from the point of intersection to the antenna 5 is not critical, but may be between 0.1 and 0.5 of the operating wave length. Assuming infinite sheets of perfectly conducting material intersecting at 90 and a spacing S of 0.15 wave length, the calculated field pattern is shown by the broken line curve 1 of Fig. 5. The measured curve 9 is obtained by the modified array of Figs. 3 and 4.
- a plurality of vertical conductors H are arranged on a wooden frame.
- the conductors may be connected together by crossconnecting wires, I2, as'shown, or these may be omitted.
- the conductors adjacent to the corner were spaced 3 inches and the conductors more remote from the corner 6 inches for an operating wave length corresponding to a frequency of 56 to 60 megacycles per second.
- the lengths of the reflecting sides, L were 6 feet and the width, W, 10 feet 6 inches.
- the distance S equalled 32 inches.
- the opening for 90 was approximately 8 feet 6 inches.
- the directive pattern for this array is represented by the curve 9 of Figure 5. It should be understood that diminishing the distance S will increase the directivity at a somewhat diminished gain. At S equal to 0.3x a measured gain of 7.5 db. was obtained over a single half wave antenna.
- the pattern may be varied by moving the antenna toward one of the wave reflecting members.
- a modified antenna is shown in Fig. 6.
- the reflecting surfaces are a plurality of rods l3 which are supported on hinged members l5.
- Thelength of each rod is preferably one-half or more of the operating wavelength.
- the hinged members may be conductive or non-conductive. is not critical, but, for example, spacings of the order of 0.1 to 0.2 of the operating wavelengthcan be used.
- the antenna I1 is arranged on a support I9 which may be clamped on the hinged member I5 to maintain the desired angle; This arrangement may be folded readily to make the array easy to transport and easy to erect. Any of the foregoing arrays may be used for receiving. or transmitting either vertically or horizontally polarized radio waves. 7
- the invention has been described. as a corner reflector antenna in which plane reflecting surfaces are arranged to intersect at an angle of the order of 90 orv less.
- An antenna is arranged in the plane bisecting the angle of intersection and ate; distance of not less'than' 0.1 of the operating wavelength from the intersection.
- the reflecting surfaces or members may be formed by sheets, screens, or rod like reflectors.
- the device may be' readily" folded and transported.
- the gain over a half-Wave antenna with the samepower input may be from 7 to 12' or more decibels; the directivity may be increased by decreasing'the angle or the antenna spacing.
- the square corner reflector having an aperture of one-half the wavelength is equal in gain and directivity to a parabolic reflector having twice the aperture and a. focus to vertex spacing of about one-quarter wave-length.
- a corner reflector antenna including a pair of planewave reflecting members arranged to intersect at an angle, said. members having a length and width of the. order of six-tenths of an operating. wave length, means for adjusting said angle. to a predetermined value of not more than 90, and an antenna located between said.
- a foldable antenna array including a p1urality of conductors, a pair of mounting members hinged at one end and each carrying in a row some of said plurality of conductors arranged in parallel to each other, an antenna, and a supporting member securing said mounting members in spaced relation and carrying said antenna between said two rows of conductors.
- a foldable antenna array including a plurality of conductors having a length of not less than half the operating wave length of said array,, a pair of mounting members hinged to each other at one end and carrying said conductors arranged in parallel to each other to form two intersecting planes of wave reflecting members, an antenna, and a supporting member carrying said antenna and securing said members in spaced relation at points intermediate their ends.
- a foldable antenna array including a plurality of conductors, a pair of mounting members hinged at one end to form an angle of not more than and each carrying in a row some of said plurality of conductors arranged in. parallel to each other, an antenna, and a supporting member securing said mounting members in spaced relation and carrying said antenna between said two rows of conductors.
- a foldable antenna array including a plurality of conductors having a length of not less than half the operating wave length of said array, a pair. of mounting members hinged to each other at one end and carrying said conductors arranged in parallel to each other to form two planes. of Wave reflecting members intersecting at an angle of not more than 90,
- an antenna and a supporting member carrying said antenna and securing said members in spacedrelation at points intermediate their ends.
- a corner reflector antenna including in combination a pair of reflectors intersecting at an angle of 90 degrees. or less, said reflectors each including a plurality of parallel conductors of substantially the same length, means for sup porting said conductors at substantially their centers and substantially in. planes, an antenna, and a third supporting means for supporting said antenna parallel to said planes and substantially midway between them at a point of not less than .1 or more than .5 of the operating wave length from said intersection.
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- Aerials With Secondary Devices (AREA)
Description
Jan. 20, 1942. J. D. KRAUS 2,279,314
CORNER REFLECTOR ANTENNA Filed Jan. 31, 1940 FEG 6 3nventor John D. ifrawa.
Patented Jan. 20, 1942 UNITED STATES PATENT OFFICE CORNER REFLECTOR ANTENNA John D. Kraus, AnnArbor, Mich.
Application January 31, 1940, Serial No. 316,625
6 Claims. (Cl. 250-11) This invention relates to antennas and especially to an antenna which is placed near the corner of a pair of intersecting wave reflecting surfaces.
The use of reflecting surfaces to direct the waves from or to an antenna is old. In general these surfaces have been of parabolic form with the antenna located at or near the focus. The surfaces have been constructed of solid conductive sheets, metal screening, or a plurality of parallel conductors. In U. S. Patent 1,745,342, Yagi discloses an antenna which includes a plurality of rod reflectors and directors. The reflectors are arranged to form either a curved surface or two intersecting flat surfaces; the directors are in line with the direction of maximum radiation; and the antenna is located in the plane forming the opening of the reflecting surface. Another example of the prior art is found in U. S. Patent No. 741,622 which issued October 20, 1903, to S. G. Brown.
While the prior art devices produce directive radiation patterns, it has been discovered that sharply defined patterns may be obtained by 10- cating an antenna adjacent the corner of a pair of intersecting reflecting surfaces and preferably in the plane bisecting the angle between the surfaces. The term corner reflector antenna has been used to describe such an antenna array.
The corner reflector antenna exhibits a sharply &
defined beam. The beam width can be varied by changing the angle between the reflecting surfaces, the beam becoming sharper as the angle is decreased. Corner angles of about 90 or less are both practical and desirable. Since the reflecting surfaces are planes, the array may be made cheaply and may be arranged for folding to make transportation easy.
One of the objects of the invention is to provide means for radiating. a sharply defined directive radio field. Another object is to provide an efiicient, compact, directive antenna array. Another object is to provide a foldable reflector and antenna array. An additional object is to provide an adjustable corner reflector antenna array.
The invention will be described by referring to the accompanying drawing in' which Figures 1 and 2 are plan and perspective views, respectively, of a corner reflector antenna; Figures 3 and 4 are perspective and plan views, respectively, of a modified corner reflector; Figure 5 is a graph illustrating the field pattern of a 90 corner reflector antenna; and Figure 6 is a perspective view of a foldable corner reflector antenna array.
Referring to Figs. 1 and 2, a pair'of wave reflecting surfaces I, 3, of conductive sheets are arranged to intersect at an angle of 90. An antenna 5, which may be a half wave dipole, is
located in the plane bisecting the angle. antenna can be connected or coupled to the transmitter or receiver by any of the methods well-known to the art, such as for example, by two parallel, twisted or concentric conductors. The distance S from the point of intersection to the antenna 5 is not critical, but may be between 0.1 and 0.5 of the operating wave length. Assuming infinite sheets of perfectly conducting material intersecting at 90 and a spacing S of 0.15 wave length, the calculated field pattern is shown by the broken line curve 1 of Fig. 5. The measured curve 9 is obtained by the modified array of Figs. 3 and 4.
Since perfect conductors of inflnite'extent can not be obtained in practice, an efficient and inexpensive compromise may be provided as shown in Figs. 3 and 4. A plurality of vertical conductors H are arranged on a wooden frame. The conductors may be connected together by crossconnecting wires, I2, as'shown, or these may be omitted. By way of example, the conductors adjacent to the corner were spaced 3 inches and the conductors more remote from the corner 6 inches for an operating wave length corresponding to a frequency of 56 to 60 megacycles per second. The lengths of the reflecting sides, L, were 6 feet and the width, W, 10 feet 6 inches. The distance S equalled 32 inches. The opening for 90 was approximately 8 feet 6 inches. The directive pattern for this array is represented by the curve 9 of Figure 5. It should be understood that diminishing the distance S will increase the directivity at a somewhat diminished gain. At S equal to 0.3x a measured gain of 7.5 db. was obtained over a single half wave antenna.
By way of example the following table gives the dimensions for a square corner antenna reflector operated at 56 to 60 mc., for various values of S which may be used.
S in wave- "S" in Side length,
lengths et L in feet 0.15 2 7" 4 to 6' 0.20 3' 5" 5 t0 8' 0. 25 4' 3 6 to 10' 0.30 5 1 7 to 12' The pattern may be varied by moving the antenna toward one of the wave reflecting members.
A modified antenna is shown in Fig. 6. In this arrangement the reflecting surfaces are a plurality of rods l3 which are supported on hinged members l5. Thelength of each rod is preferably one-half or more of the operating wavelength. The hinged members may be conductive or non-conductive. is not critical, but, for example, spacings of the order of 0.1 to 0.2 of the operating wavelengthcan be used. The antenna I1 is arranged on a support I9 which may be clamped on the hinged member I5 to maintain the desired angle; This arrangement may be folded readily to make the array easy to transport and easy to erect. Any of the foregoing arrays may be used for receiving. or transmitting either vertically or horizontally polarized radio waves. 7
Thus the invention has been described. as a corner reflector antenna in which plane reflecting surfaces are arranged to intersect at an angle of the order of 90 orv less. An antenna is arranged in the plane bisecting the angle of intersection and ate; distance of not less'than' 0.1 of the operating wavelength from the intersection. The reflecting surfaces or members may be formed by sheets, screens, or rod like reflectors. The device may be' readily" folded and transported. The gain over a half-Wave antenna with the samepower input may be from 7 to 12' or more decibels; the directivity may be increased by decreasing'the angle or the antenna spacing. By way of. example, the square corner reflector having an aperture of one-half the wavelength is equal in gain and directivity to a parabolic reflector having twice the aperture and a. focus to vertex spacing of about one-quarter wave-length.
I claim asmy invention:
1. A corner reflector antenna including a pair of planewave reflecting members arranged to intersect at an angle, said. members having a length and width of the. order of six-tenths of an operating. wave length, means for adjusting said angle. to a predetermined value of not more than 90, and an antenna located between said.
members and at a distance fromv said. intersection substantially less" than the distance from.
said intersection to the opening of said. mem- F bers.
The spacing between rods 2. A foldable antenna array including a p1urality of conductors, a pair of mounting members hinged at one end and each carrying in a row some of said plurality of conductors arranged in parallel to each other, an antenna, and a supporting member securing said mounting members in spaced relation and carrying said antenna between said two rows of conductors.
3. A foldable antenna array including a plurality of conductors having a length of not less than half the operating wave length of said array,, a pair of mounting members hinged to each other at one end and carrying said conductors arranged in parallel to each other to form two intersecting planes of wave reflecting members, an antenna, and a supporting member carrying said antenna and securing said members in spaced relation at points intermediate their ends.
4. A foldable antenna array including a plurality of conductors, a pair of mounting members hinged at one end to form an angle of not more than and each carrying in a row some of said plurality of conductors arranged in. parallel to each other, an antenna, and a supporting member securing said mounting members in spaced relation and carrying said antenna between said two rows of conductors.
5. A foldable antenna array including a plurality of conductors having a length of not less than half the operating wave length of said array, a pair. of mounting members hinged to each other at one end and carrying said conductors arranged in parallel to each other to form two planes. of Wave reflecting members intersecting at an angle of not more than 90,
an antenna, and a supporting member carrying said antenna and securing said members in spacedrelation at points intermediate their ends.
6'. A corner reflector antenna including in combination a pair of reflectors intersecting at an angle of 90 degrees. or less, said reflectors each including a plurality of parallel conductors of substantially the same length, means for sup porting said conductors at substantially their centers and substantially in. planes, an antenna, and a third supporting means for supporting said antenna parallel to said planes and substantially midway between them at a point of not less than .1 or more than .5 of the operating wave length from said intersection.
JOHN D. KRAUS.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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US316625A US2270314A (en) | 1940-01-31 | 1940-01-31 | Corner reflector antenna |
Applications Claiming Priority (1)
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US316625A US2270314A (en) | 1940-01-31 | 1940-01-31 | Corner reflector antenna |
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US2270314A true US2270314A (en) | 1942-01-20 |
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Cited By (37)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2430568A (en) * | 1942-06-22 | 1947-11-11 | Rca Corp | Antenna system |
US2438987A (en) * | 1944-05-23 | 1948-04-06 | Radio Transmission Equipment L | Radio navigational aid |
US2452767A (en) * | 1946-04-02 | 1948-11-02 | John D Kraus | Broad-band antenna |
US2531432A (en) * | 1948-10-01 | 1950-11-28 | Fed Telecomm Lab Inc | Broad band antenna system |
US2540757A (en) * | 1944-06-16 | 1951-02-06 | Henry J Riblet | Antenna |
US2577469A (en) * | 1946-05-18 | 1951-12-04 | Rca Corp | Antenna |
US2622242A (en) * | 1945-05-09 | 1952-12-16 | Freedman Samuel | Tuned microwave reflector |
US2691102A (en) * | 1950-08-14 | 1954-10-05 | Rca Corp | High gain vhf antenna system |
US2714659A (en) * | 1951-07-30 | 1955-08-02 | Rca Corp | Broad band unidirectional antenna |
US2720590A (en) * | 1953-09-08 | 1955-10-11 | Itt | Wedge antenna system for sector operation |
US2801413A (en) * | 1949-03-30 | 1957-07-30 | Bell Telephone Labor Inc | Directive dielectric antennas |
US2813268A (en) * | 1954-07-23 | 1957-11-12 | Joseph V Fisher | Foldable high gain antenna system |
US2897496A (en) * | 1955-01-12 | 1959-07-28 | Rca Corp | Corner reflector antenna |
US2922161A (en) * | 1954-11-17 | 1960-01-19 | Raytheon Co | Antenna reflectors |
US3178713A (en) * | 1961-03-08 | 1965-04-13 | Andrew Corp | Parabolic antenna formed of curved spaced rods |
US4114163A (en) * | 1976-12-06 | 1978-09-12 | The United States Of America As Represented By The Secretary Of The Army | L-band radar antenna array |
US5132699A (en) * | 1990-11-19 | 1992-07-21 | Ltv Aerospace And Defense Co. | Inflatable antenna |
US20040233118A1 (en) * | 2003-05-23 | 2004-11-25 | Jocher Ronald William | Antenna with reflector |
US20050068245A1 (en) * | 2003-09-25 | 2005-03-31 | Cheng-Chung Chen | Reflective signal booster for omini-antenna |
US20050168387A1 (en) * | 2003-09-29 | 2005-08-04 | Greg Tangonan | Mechanically reconfigurable antenna for wireless access points |
US6977624B1 (en) * | 2003-10-17 | 2005-12-20 | Szente Pedro A | Antenna directivity enhancer |
US20070247388A1 (en) * | 2006-01-19 | 2007-10-25 | Kenji Asakura | Antenna device, antenna reflector, and wireless communication unit incorporating antenna |
US20070262912A1 (en) * | 2006-03-31 | 2007-11-15 | Eckwielen Bradley L | Modular digital UHF/VHF antenna |
US7626557B2 (en) | 2006-03-31 | 2009-12-01 | Bradley L. Eckwielen | Digital UHF/VHF antenna |
US20110273352A1 (en) * | 2010-05-05 | 2011-11-10 | You-Cheng You | Antenna Structure |
US9416802B2 (en) | 2012-12-31 | 2016-08-16 | University Of Kansas | Radar energy absorbing deformable low drag vortex generator |
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US9606577B2 (en) | 2002-10-22 | 2017-03-28 | Atd Ventures Llc | Systems and methods for providing a dynamically modular processing unit |
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US9961788B2 (en) | 2002-10-22 | 2018-05-01 | Atd Ventures, Llc | Non-peripherals processing control module having improved heat dissipating properties |
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US10594044B1 (en) | 2019-03-07 | 2020-03-17 | Jon C. Taenzer | Wide-direction antenna |
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-
1940
- 1940-01-31 US US316625A patent/US2270314A/en not_active Expired - Lifetime
Cited By (46)
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US2430568A (en) * | 1942-06-22 | 1947-11-11 | Rca Corp | Antenna system |
US2438987A (en) * | 1944-05-23 | 1948-04-06 | Radio Transmission Equipment L | Radio navigational aid |
US2540757A (en) * | 1944-06-16 | 1951-02-06 | Henry J Riblet | Antenna |
US2622242A (en) * | 1945-05-09 | 1952-12-16 | Freedman Samuel | Tuned microwave reflector |
US2452767A (en) * | 1946-04-02 | 1948-11-02 | John D Kraus | Broad-band antenna |
US2577469A (en) * | 1946-05-18 | 1951-12-04 | Rca Corp | Antenna |
US2531432A (en) * | 1948-10-01 | 1950-11-28 | Fed Telecomm Lab Inc | Broad band antenna system |
US2801413A (en) * | 1949-03-30 | 1957-07-30 | Bell Telephone Labor Inc | Directive dielectric antennas |
US2691102A (en) * | 1950-08-14 | 1954-10-05 | Rca Corp | High gain vhf antenna system |
US2714659A (en) * | 1951-07-30 | 1955-08-02 | Rca Corp | Broad band unidirectional antenna |
US2720590A (en) * | 1953-09-08 | 1955-10-11 | Itt | Wedge antenna system for sector operation |
US2813268A (en) * | 1954-07-23 | 1957-11-12 | Joseph V Fisher | Foldable high gain antenna system |
US2922161A (en) * | 1954-11-17 | 1960-01-19 | Raytheon Co | Antenna reflectors |
US2897496A (en) * | 1955-01-12 | 1959-07-28 | Rca Corp | Corner reflector antenna |
US3178713A (en) * | 1961-03-08 | 1965-04-13 | Andrew Corp | Parabolic antenna formed of curved spaced rods |
US4114163A (en) * | 1976-12-06 | 1978-09-12 | The United States Of America As Represented By The Secretary Of The Army | L-band radar antenna array |
US5132699A (en) * | 1990-11-19 | 1992-07-21 | Ltv Aerospace And Defense Co. | Inflatable antenna |
US9606577B2 (en) | 2002-10-22 | 2017-03-28 | Atd Ventures Llc | Systems and methods for providing a dynamically modular processing unit |
US9961788B2 (en) | 2002-10-22 | 2018-05-01 | Atd Ventures, Llc | Non-peripherals processing control module having improved heat dissipating properties |
US10285293B2 (en) | 2002-10-22 | 2019-05-07 | Atd Ventures, Llc | Systems and methods for providing a robust computer processing unit |
US7215294B2 (en) * | 2003-05-23 | 2007-05-08 | Lucent Technologies Inc. | Antenna with reflector |
US20040233118A1 (en) * | 2003-05-23 | 2004-11-25 | Jocher Ronald William | Antenna with reflector |
US20050068245A1 (en) * | 2003-09-25 | 2005-03-31 | Cheng-Chung Chen | Reflective signal booster for omini-antenna |
US20050168387A1 (en) * | 2003-09-29 | 2005-08-04 | Greg Tangonan | Mechanically reconfigurable antenna for wireless access points |
US6977624B1 (en) * | 2003-10-17 | 2005-12-20 | Szente Pedro A | Antenna directivity enhancer |
US7245266B1 (en) * | 2003-10-17 | 2007-07-17 | Szente Pedro A | Antenna directivity enhancer |
US8384611B2 (en) * | 2006-01-19 | 2013-02-26 | Sony Corporation | Antenna device, antenna reflector, and wireless communication unit incorporating antenna |
US20070247388A1 (en) * | 2006-01-19 | 2007-10-25 | Kenji Asakura | Antenna device, antenna reflector, and wireless communication unit incorporating antenna |
US20070262912A1 (en) * | 2006-03-31 | 2007-11-15 | Eckwielen Bradley L | Modular digital UHF/VHF antenna |
US7911406B2 (en) | 2006-03-31 | 2011-03-22 | Bradley Lee Eckwielen | Modular digital UHF/VHF antenna |
US7626557B2 (en) | 2006-03-31 | 2009-12-01 | Bradley L. Eckwielen | Digital UHF/VHF antenna |
US20080309573A9 (en) * | 2006-03-31 | 2008-12-18 | Eckwielen Bradley L | Modular digital UHF/VHF antenna |
US20110273352A1 (en) * | 2010-05-05 | 2011-11-10 | You-Cheng You | Antenna Structure |
US9478868B2 (en) | 2011-02-09 | 2016-10-25 | Xi3 | Corrugated horn antenna with enhanced frequency range |
US9677580B2 (en) | 2012-12-31 | 2017-06-13 | University Of Kansas | Radar energy absorbing deformable low drag vortex generator |
US9416802B2 (en) | 2012-12-31 | 2016-08-16 | University Of Kansas | Radar energy absorbing deformable low drag vortex generator |
US9450309B2 (en) | 2013-05-30 | 2016-09-20 | Xi3 | Lobe antenna |
CN107004943A (en) * | 2014-07-15 | 2017-08-01 | Xi3有限公司 | System and method for providing frequency sensitivity skin antenna |
US11349201B1 (en) | 2019-01-24 | 2022-05-31 | Northrop Grumman Systems Corporation | Compact antenna system for munition |
US12107326B2 (en) | 2019-01-24 | 2024-10-01 | Northrop Grumman Systems Corporation | Compact antenna system for munition |
US10594044B1 (en) | 2019-03-07 | 2020-03-17 | Jon C. Taenzer | Wide-direction antenna |
US11581632B1 (en) | 2019-11-01 | 2023-02-14 | Northrop Grumman Systems Corporation | Flexline wrap antenna for projectile |
EP4117118A1 (en) * | 2021-07-05 | 2023-01-11 | PhoenixC4i Ltd. | Antenna reflector |
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GB2608612B (en) * | 2021-07-05 | 2023-09-20 | Phoenixc4I Ltd | Antenna reflector |
WO2023220373A3 (en) * | 2022-05-12 | 2023-12-21 | Lunewave Inc. | Radar identification devices, systems, and methods |
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