US2540518A - Directional antenna - Google Patents
Directional antenna Download PDFInfo
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- US2540518A US2540518A US627469A US62746945A US2540518A US 2540518 A US2540518 A US 2540518A US 627469 A US627469 A US 627469A US 62746945 A US62746945 A US 62746945A US 2540518 A US2540518 A US 2540518A
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- Prior art keywords
- reflector
- antenna
- radiator
- parabola
- directive
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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
- H01Q19/18—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 having two or more spaced reflecting surfaces
- H01Q19/19—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 having two or more spaced reflecting surfaces comprising one main concave reflecting surface associated with an auxiliary reflecting surface
- H01Q19/192—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 having two or more spaced reflecting surfaces comprising one main concave reflecting surface associated with an auxiliary reflecting surface with dual offset reflectors
Definitions
- This invention relates to directive antennas, and more particularly to improvements in antenna systems of the type including curved or parabolic reflector means for providing directivity.
- Another object is to provide an antenna of the described type wherein a relatively large reflector may be used without incurring the disadvantages inherent in similar systems of prior art type.
- an antenna system of the described type which is simple to design and construct, and will meet typical performance requirements with a single narily less than one hundred wavelengths in diameter. This results in interaction between the radiator and reflector, since the radiator is large enough to intercept an appreciable fraction of the beam produced by the reflector, and also because there is appreciable direct radiation from the source which forms an interference pattern with the energy from the focusing reflector.
- the distance F is generally chosen so that direct radiation from the primary radiator in the forward direction is in phase with the energy from the reflector, this arrangement usually having the most favorable antenna pattern. If the distance is chosen to be 3k at a particular operating frequency an increase in operating frequency of 8 percent will cause the distance F to be 3%.
- Figure l is a schematic diagram of a prior art antenna system including parabolic reflector means
- FIG. 2 is a schematic diagram of an antenna system in accordance with the present invention
- Figure 3 is a perspective view of an antenna system embodying this invention.
- a typical prior art antenna comprises a half wave doublet I disposed at the focus of a reflector 3 in the shape of a parabola of rotation.
- the reflector l is in the form of a, section of a circular parabola, and does not include the vertex (indicated at 3) of the parabola.
- a directive antenna i i is disposed at the focal point of the reflector t, which mouth opening and may be designed with the rel- I atively short focal length of one-quarter wavelength without introducing polarization difliculties.
- a cylindrical parabola l5 with the radiator 3 along the focal line obviates this difliculty.
- the larger reflector 1 is illuminated by the small antenna H, providing a very sharp beam parallel to the axis of the paraboloid. This. beam misses the antenna H entirely, so that no energy can be returned from the reflector l to the antenna H.
- the directivity is substantially the same as that which would be obtained (but only at the design frequency) with a complete circular paraboloid having a mouth area equal to that of the section '1.
- FIG 3 shows the principal details of a typical embodiment of the present invention.
- the main reflector 7 comprises a screen of expanded metal or the like, secured by spot-welding to a supporting structure including curved ribs H and 19 mounted on a bracework structure, designated generally by the reference numeral 2!.
- the auxiliary reflector i5 is similarly constructed and supported by the structure 22.
- the reflector i5 is in the form of a cylindrical parabola, with its focal line horizon-
- the radiator l3 comprises a horizontal doublet with its element supported by the transmission line It by which it is connected to the feed system.
- a line balance convertor I6 is provided behind the reflector l5 for coupling the line M to a coaxial feed line 23.
- the antenna, ll, comprising the radiator !3 and reflector I5 may be of the type described in U. S. Patent No. 2,430,353 issued November 4, 1947, to Robert W. Masters, and entitled Antenna.
- the operation of the system of Figure 3 is the same as that of the system of Figure 2.
- the beam emitted from the reflector l is horizontally polarized, since the doublet l3 and the reflector l5 are disposed horizontally.
- the directive antenna ll may be a directive array, rather than a simple dipole and reflector.
- the reflector I5 need not be a parabolic, but may even be a flat screen, depending upon the particular design and performance requirements.
- the present invention contemplates the use of a reflector in the form of a portion of a paraboloid, with the vertex omitted, illuminated by a directive antenna at its focus.
- the beam formed by the reflector does not impinge on the primary radiation source, thus avoiding impedance variations and enabling broad-band operation.
- a directive antenna system including a reflector in the form of a portion of a paraboloid, said portion excluding the vertex of said paraboloid, radiator means near the focus of said reflector, and an auxiliary reflector adjacent said radiator means and oriented to direct radiation from said radiator means substantially only to said first-mentioned reflector, said radiator and said auxiliary reflector being located outside the beam formed by said parabolic reflector.
- a directive antenna system including a reflector having a reflecting surface in cross-section in the shape of a portion of a parabola entirely on one side of the parabola axis and excluding the parabola vertex, means to radiate or receive electromagnetic energy substantially at thev focus of the reflector, and an auxiliary reflector arranged to have a radiation pattern with said means which pattern includes substantially only said reflecting surface and excludes substantially all portions outside said surface, said auxiliary reflector being located on the side of the parabol axis opposite the said reflecting portion surface and thereby being located outside the radiation pattern of the system.
- said means to radiate or receive the electromagnetic energy being a dipole
- said auxiliary reflector having a reflecting surface in cross-section in the shape of a parabola with the dipole substantially at its focal point.
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- Aerials With Secondary Devices (AREA)
Description
Feb. 6, 1951 T. M. GLUYAS, JR
DIRECTIONAL ANTENNA Filed Nov. 8, 1945 INVENTOR.
Thom-IE 7. 22 By fi y s Patented Feb. 6, 1951 DIRECTIONAL ANTENNA Thomas M. Gluyas, Jr., Westmont, N. J assignor to Radio Corporation of America, a corporation of Delaware Application November 8, 1945, Serial No. 627,469
3 Claims.
This invention relates to directive antennas, and more particularly to improvements in antenna systems of the type including curved or parabolic reflector means for providing directivity.
The use of parabolic reflectors with antennas is well known, being described in Radio Engineers Handbook, by F. E. Terman, first edition, 1943, published by McGraw Hill Book Company, on page 837 et seq. The sharpness of the directive beam obtained by such a structure is limited ness of the beam, an auxiliary reflector 5 is provided near to and in front of the radiator I.
It is sometimes supposed that the operation of a system such as that of Figure 1 is closely analagous to that of a Searchlight in producing a beam of light. However, this is not the fact, principally because the usual Searchlight reflector has a diameter of millions of wavelengths, while the reflector used with a radio antenna is ordisubstantially only by the size of the reflector.
However, prior art antennas of this type will 0perate efficiently only at the single frequency for which they are designed. At other frequencies, the spacing in wavelengths between the radiator and the reflector varies from its optimum value, introducing variations in the impedance present+ ed by the antenna to its feed system and producing undesirable side lobes in the directive pattern.
Accordingly, it is the principal object of this invention to provide an improved antenna system of the described type capable of operation throughout a relatively wide frequency band with a minimum variation of directive pattern and impedance.
Another object is to provide an antenna of the described type wherein a relatively large reflector may be used without incurring the disadvantages inherent in similar systems of prior art type.
an antenna system of the described type which is simple to design and construct, and will meet typical performance requirements with a single narily less than one hundred wavelengths in diameter. This results in interaction between the radiator and reflector, since the radiator is large enough to intercept an appreciable fraction of the beam produced by the reflector, and also because there is appreciable direct radiation from the source which forms an interference pattern with the energy from the focusing reflector.
The distance F is generally chosen so that direct radiation from the primary radiator in the forward direction is in phase with the energy from the reflector, this arrangement usually having the most favorable antenna pattern. If the distance is chosen to be 3k at a particular operating frequency an increase in operating frequency of 8 percent will cause the distance F to be 3%.
. If the distance 3% gave the most favorable primary radiator, in contradistinction to the r for the cases F=3x and F=3 The impedance usual array of a large number of radiator elements with graded energization and consequent power division and feed system problems.
The invention will be described with reference to the accompanying drawing, wherein:
Figure l is a schematic diagram of a prior art antenna system including parabolic reflector means,
Figure 2 is a schematic diagram of an antenna system in accordance with the present invention, and Figure 3 is a perspective view of an antenna system embodying this invention.
Referring to Figure 1, a typical prior art antenna comprises a half wave doublet I disposed at the focus of a reflector 3 in the shape of a parabola of rotation. In order to minimize direct forward radiation, with consequent loss of sharpfield pattern the frequency change of 8 percent F=3 Ax results in an inferior pattern because the radiation from the primary radiator and the reflector will now be out of phase in the forward direction. Furthermore, if the radiator is matched to the feed line when F=3 then when F=3 Ax the radiator will present a different impedance to the feed line causing a serious mismatch because the phase of the energy returned from the reflector to the radiator will be opposite mismatch caused by the change in frequency will result in standing waves on the feed line and reduced system efficiency.
The above described difficulties can be met to v a large extent by designing the reflector to make F one-quarter wavelength at the mean frequency of operation. Then a 20 percent change in frequency will be equivalent to a change of 20. percent X2 or only wavelength, and the variation in im-' is to be wavelengths in diameter, and the focal length one-quarter wavelength. The length of the reflector from vertex to mouth will then be about 156 wavelengths, or over 600 times the focal length. The radiator will be so far inside the mouth that the reflector will no longer operate as a simple parabola at all, owing to diverse polarization of the energy following different paths within the reflector, and to the non-uniform illumination due to the nulls 01f the ends of the radiator.
According to the present invention, the reflector l is in the form of a, section of a circular parabola, and does not include the vertex (indicated at 3) of the parabola. A directive antenna i i is disposed at the focal point of the reflector t, which mouth opening and may be designed with the rel- I atively short focal length of one-quarter wavelength without introducing polarization difliculties. A cylindrical parabola l5 with the radiator 3 along the focal line obviates this difliculty.
The larger reflector 1 is illuminated by the small antenna H, providing a very sharp beam parallel to the axis of the paraboloid. This. beam misses the antenna H entirely, so that no energy can be returned from the reflector l to the antenna H. Thus there is no critical relationship to be maintained between the wavelength and the focal length of the main reflector, and efficient operation is obtained throughout a wide frequency band. The directivity is substantially the same as that which would be obtained (but only at the design frequency) with a complete circular paraboloid having a mouth area equal to that of the section '1.
Figure 3 shows the principal details of a typical embodiment of the present invention. The main reflector 7 comprises a screen of expanded metal or the like, secured by spot-welding to a supporting structure including curved ribs H and 19 mounted on a bracework structure, designated generally by the reference numeral 2!. The auxiliary reflector i5 is similarly constructed and supported by the structure 22. In the present illustration, the reflector i5 is in the form of a cylindrical parabola, with its focal line horizon- The radiator l3 comprises a horizontal doublet with its element supported by the transmission line It by which it is connected to the feed system. A line balance convertor I6 is provided behind the reflector l5 for coupling the line M to a coaxial feed line 23. The antenna, ll, comprising the radiator !3 and reflector I5, may be of the type described in U. S. Patent No. 2,430,353 issued November 4, 1947, to Robert W. Masters, and entitled Antenna.
The operation of the system of Figure 3 is the same as that of the system of Figure 2. The beam emitted from the reflector l is horizontally polarized, since the doublet l3 and the reflector l5 are disposed horizontally.
Although the invention has been described with reference to a specific embodiment thereof, it will be apparent without further illustration to those skilled in the art that it is not limited thereto. For example, the directive antenna ll may be a directive array, rather than a simple dipole and reflector. The reflector I5 need not be a parabolic, but may even be a flat screen, depending upon the particular design and performance requirements.
Summarizing briefly, the present invention contemplates the use of a reflector in the form of a portion of a paraboloid, with the vertex omitted, illuminated by a directive antenna at its focus. The beam formed by the reflector does not impinge on the primary radiation source, thus avoiding impedance variations and enabling broad-band operation.
I claim as my invention:
1. A directive antenna system including a reflector in the form of a portion of a paraboloid, said portion excluding the vertex of said paraboloid, radiator means near the focus of said reflector, and an auxiliary reflector adjacent said radiator means and oriented to direct radiation from said radiator means substantially only to said first-mentioned reflector, said radiator and said auxiliary reflector being located outside the beam formed by said parabolic reflector.
2. A directive antenna system including a reflector having a reflecting surface in cross-section in the shape of a portion of a parabola entirely on one side of the parabola axis and excluding the parabola vertex, means to radiate or receive electromagnetic energy substantially at thev focus of the reflector, and an auxiliary reflector arranged to have a radiation pattern with said means which pattern includes substantially only said reflecting surface and excludes substantially all portions outside said surface, said auxiliary reflector being located on the side of the parabol axis opposite the said reflecting portion surface and thereby being located outside the radiation pattern of the system.
3. The system claimed in claim 2, said means to radiate or receive the electromagnetic energy being a dipole, and said auxiliary reflector having a reflecting surface in cross-section in the shape of a parabola with the dipole substantially at its focal point.
THOMAS M. GLUYAS, JR.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Number Name Date 2,118,419 Scharlau May 24, 1938 FOREIGN PATENTS Number Country Date 678,010 Germany June 24, 1939 463,355 Great Britain Oct. 9, 1935
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Application Number | Priority Date | Filing Date | Title |
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US627469A US2540518A (en) | 1945-11-08 | 1945-11-08 | Directional antenna |
Applications Claiming Priority (1)
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US627469A US2540518A (en) | 1945-11-08 | 1945-11-08 | Directional antenna |
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US2540518A true US2540518A (en) | 1951-02-06 |
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US627469A Expired - Lifetime US2540518A (en) | 1945-11-08 | 1945-11-08 | Directional antenna |
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Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2922161A (en) * | 1954-11-17 | 1960-01-19 | Raytheon Co | Antenna reflectors |
US2975420A (en) * | 1954-10-04 | 1961-03-14 | Telefunken Gmbh | Directional antenna having cosine shaped aperture |
US2996714A (en) * | 1957-12-26 | 1961-08-15 | Edward F Harris | Dish radiator of adjustable polarization |
US3264648A (en) * | 1963-07-02 | 1966-08-02 | Sylvania Electric Prod | Broadband automatic tracking antenna |
US3276022A (en) * | 1964-05-13 | 1966-09-27 | Aeronca Mfg Corp | Dual frequency gregorian-newtonian antenna system with newtonian feed located at common focus of parabolic main dish and ellipsoidal sub-dish |
US3317912A (en) * | 1963-07-29 | 1967-05-02 | Kenneth S Kelleher | Plural concentric parabolic antenna for omnidirectional coverage |
US3407404A (en) * | 1964-10-05 | 1968-10-22 | Bell Telephone Labor Inc | Directive microwave antenna capable of rotating about two intersecting axes |
US3964071A (en) * | 1973-11-28 | 1976-06-15 | Texas Instruments Incorporated | Radar antenna having a screen supported by shaped slats |
US3995275A (en) * | 1973-07-12 | 1976-11-30 | Mitsubishi Denki Kabushiki Kaisha | Reflector antenna having main and subreflector of diverse curvature |
US4005433A (en) * | 1975-12-05 | 1977-01-25 | Hughes Aircraft Company | Small wavelength high efficiency antenna |
US4030103A (en) * | 1975-12-10 | 1977-06-14 | Lockheed Missiles & Space Company, Inc. | Deployable offset paraboloid antenna |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE78010C (en) * | G. VOSS, Köln a. Rh., Schildergasse 22H | Jump wood for bird cages | ||
GB463355A (en) * | 1935-04-29 | 1937-03-30 | Siemens Ag | Improvements in and relating to rotary commutator switching-apparatus for converting electric currents |
US2118419A (en) * | 1931-09-16 | 1938-05-24 | Telefunken Gmbh | Ultrashort wave reflector |
-
1945
- 1945-11-08 US US627469A patent/US2540518A/en not_active Expired - Lifetime
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE78010C (en) * | G. VOSS, Köln a. Rh., Schildergasse 22H | Jump wood for bird cages | ||
US2118419A (en) * | 1931-09-16 | 1938-05-24 | Telefunken Gmbh | Ultrashort wave reflector |
GB463355A (en) * | 1935-04-29 | 1937-03-30 | Siemens Ag | Improvements in and relating to rotary commutator switching-apparatus for converting electric currents |
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2975420A (en) * | 1954-10-04 | 1961-03-14 | Telefunken Gmbh | Directional antenna having cosine shaped aperture |
US2922161A (en) * | 1954-11-17 | 1960-01-19 | Raytheon Co | Antenna reflectors |
US2996714A (en) * | 1957-12-26 | 1961-08-15 | Edward F Harris | Dish radiator of adjustable polarization |
US3264648A (en) * | 1963-07-02 | 1966-08-02 | Sylvania Electric Prod | Broadband automatic tracking antenna |
US3317912A (en) * | 1963-07-29 | 1967-05-02 | Kenneth S Kelleher | Plural concentric parabolic antenna for omnidirectional coverage |
US3276022A (en) * | 1964-05-13 | 1966-09-27 | Aeronca Mfg Corp | Dual frequency gregorian-newtonian antenna system with newtonian feed located at common focus of parabolic main dish and ellipsoidal sub-dish |
US3407404A (en) * | 1964-10-05 | 1968-10-22 | Bell Telephone Labor Inc | Directive microwave antenna capable of rotating about two intersecting axes |
US3995275A (en) * | 1973-07-12 | 1976-11-30 | Mitsubishi Denki Kabushiki Kaisha | Reflector antenna having main and subreflector of diverse curvature |
US3964071A (en) * | 1973-11-28 | 1976-06-15 | Texas Instruments Incorporated | Radar antenna having a screen supported by shaped slats |
US4005433A (en) * | 1975-12-05 | 1977-01-25 | Hughes Aircraft Company | Small wavelength high efficiency antenna |
US4030103A (en) * | 1975-12-10 | 1977-06-14 | Lockheed Missiles & Space Company, Inc. | Deployable offset paraboloid antenna |
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