US3209361A - Cassegrainian antenna subreflector flange for suppressing ground noise - Google Patents

Cassegrainian antenna subreflector flange for suppressing ground noise Download PDF

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US3209361A
US3209361A US251451A US25145163A US3209361A US 3209361 A US3209361 A US 3209361A US 251451 A US251451 A US 251451A US 25145163 A US25145163 A US 25145163A US 3209361 A US3209361 A US 3209361A
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subreflector
flange
antenna
cassegrainian
edges
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James E Webb
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    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q19/00Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic
    • H01Q19/02Details
    • H01Q19/021Means for reducing undesirable effects
    • H01Q19/026Means for reducing undesirable effects for reducing the primary feed spill-over

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Description

p 28, 1965 JAMES E. WEBB 3,209,361 ADMINISTRATOR OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION CASSEGRAINIAN ANTENNA SUBREFLECTOR FLANGE FOR SUPPRESSING GROUND NOISE Filed Jan. 14, 1963 INVENTOR. PH/L 0. POTTER BY fl zw/z v firm/aw y United States Patent 3,209,361 CASSEGRAINIAN ANTENNA SUBREFLECTOR IliIIAglGE FOR SUPPRESSING GROUND I E James E. Webb, administrator of the National Aeronautics and Space Administration, with respect to an invention of Philip D. Potter Filed Jan. 14, 1963, Ser. No. 251,451 Claims. (Cl. 343-781) This invention relates to antennas and more particularly to an improvement to antennas of the Cassegrainian type.
A Cassegrainian antenna usually comprises a parabolic main reflector dish, a smaller subreflector facing the parabolic reflector, and a horn feed facing the subreflector. When the antenna is used for receiving wavelengths which are of significant size as compared to the size of the antenna, some energy radiated by the surrounding ground strikes the subreflector and enters the horn feed, and this adds noise to the received signal. Similarly, when the antenna is used to transmit energy some of the energy radiated by the horn feed bypasses the subreflector or the main reflector dish, and is lost.
An object of this invention is the provision of structure for substantially minimizing noise in signals received by this antenna.
Another object of this invention is the provision of an improved Cassegrainian antenna which is more eflicient than presently known antennas of this type.
Yet another object of the present invention is the provision of a novel and improved Cassegrainian antenna structure.
These and other objects of the invention may be achieved by providing a flange around the edge portion of the subreflector of a Cassegrainian antenna. The flange makes a smaller angle with the plane of the subreflector than does the edge of the major hyperbolically shaped portion of the subreflector. The optional flange size depends on the frequency being used. The flange not only reduces the noise level of received signals, but also improves the efliciency of the antenna when it is used for transmitting.
The novel features that are considered characteristic of this invention are set forth with particularity in the appended claims. The invention itself, both as to its organization and method of operation, as well as additional objects and advantages thereof, will best be understood from the following description when read in connection with the accompanying drawings, in which:
FIGURE 1 is a side sectional view of a Cassegrainian antenna showing the improvement in accordance with this invention.
FIGURE 2 is a side view of the subreflector and flange in accordance with this invention.
FIGURE 3 is a front elevation view of the subreflector and flange in accordance with this invention.
A Cassegrainian antenna comprises a rotatable pedestal supporting an adjustable mount 12 which supports the main reflector dish 14. The main reflector dish 14 receives microwaves from space and directs them toward a subreflector 16 which reflects them to a horn feed 18, positioned at the center of the main dish 14. A subreflector is usually supported by members 20, extending from the edges of the main dish 14.
The Cassegrainian antenna is used for receiving microwaves, some of which have frequencies for which the wavelengths are not insignificantly small when compared to the sizes of the main dish and the subreflector. Microwaves having these wavelength dimensions which are emitted by the warm surrounding ground area 22, bend around the edges of the main dish 14, strike the subre- 3,209,361 Patented Sept. 28, 1965 flector 16 and are reflected into the horn feed to appear as noise which is added to the received signal.
In accordance with this invention, a conical reflector flange 24 may be mounted on the edge of the subreflector where it is desired to prove an already built antenna, or may be formed integrally with the subreflector when the antenna is made. FIGURES 2 and 3, respectively side and front elevation views of the subreflector and flange, illustrate the position of the flange with respect to the subreflector. The flange also serves to reflect microwaves from the surrounding warm ground 22, into the horn feed 18. However, as represented. by the dotted lines in FIGURE 1, the path 26 from a point 28 on the ground to the subreflector 16 and thereafter to the horn feed 18, is approximately one-half wavelength shorter than a direct path 30 from the same ground point 28 to the flange 24, and then to the horn feed 18. When the two waves arrive at the horn feed they are about one hundred and eighty degrees out of phase and cancel each other out, and the amount of noise is accordingly substantially minimized.
When the antenna is used for the purpose of transmitting, some of the energy emitted from the horn feed 18 which is then reflected from the subreflector 16, bends around the edges of the main dish 14 and is lost, since. it is not reflected back by the main dish. The flange 24 also reflects energy past the edge of the main dish 14 but this operates to cancel out the bent rays from the subreflector 16. This prevents the loss of this energy to the surrounding ground and increases antenna efliciency. Also, some of the energy from the horn feed 18 which passes around the subreflector and would ordinarily be lost, hits the flange 24, and is reflected toward the main dish to further increase antenna efliciency.
The size of the flange 24, and its angle with respect to the axis of the subreflector 16, are adjusted until the noise level is reduced to a small amount, while the efficiency of the antenna is still large. In FIGURE 2, 0 is the angle between the flange 4 and the plane of the subreflector, and a is the angle between a target to the subreflector and the plane of the subreflector. It is found in practice that, with a Cassegrainian antenna operating at a given frequency, a flange having an inner to outer radius difference of two wavelengths at an angle 0 of about three fourths the size of the angle at will reduce the noise level to a low level while maintaining a high antenna efliciency. Specifically, it is found that a Cassegrainian antenna with a main dish 14 of 8.5 feet in diameter subtending an angle 7 of one hundred twentytwo degrees (shown by the dotted lines in FIG. 1), and having a subreflector 16 with a diameter of 0.8 feet, with an edge making an angle 0c of 24.4 degrees with the plane of the subreflector, and receiving and transmitting at a frequency of 9.6 kmc., that a fiange having a rim of 0.2 feet between inner and outer radii and making an angle 0 of 18.4 degrees with the plane of the subreflector 16, will reduce the noise to almost a minimum while increasing the efliciency to near its maximum.
A flange having a shape other than conical may be used to achieve the same or a somewhat better effect, though the conical shape is very simple to manufacture. Any of these shapes will involve a departure from the hyperbolic shape of the typical Cassegrainian subreflector (which is the shape for best results with very small wavelengths compared to antenna size, as with visual light). The main element of the departure, in accordance with this invention, is a rim or flange portion on the subreflector, which makes a smaller angle with the plane of the subreflector than a target to the edge of the major hyperbolically shaped portion of the subreflector. As was previously pointed out, instead of a flange, the subreflector may be enlarged to include a rim portion of the proper shape to make the subreflector and flange comprise a single article.
Accordingly, there has been shown and described herein a novel, and improved Cassegrainian antenna.
I claim:
1. The improvement in a Cassegrainian antenna having a subreflector with a curved reflecting face and defining a plane with the edges of said curved reflecting face, said improvement comprising a reflecting flange extending radially from the curved reflecting face and making an angle with the plane defined by the edges of said curved reflecting face which is smaller than the angle made by the portion of the curved reflecting face near the edge thereof with said plane, the radial length of said reflecting flange being on the order of an integral number of wavelengths of the frequency at which said antenna is used.
2. The improvement in a Cassegrainian antenna of the type having a subreflector with a curved reflecting face and defining a plane with the edges of said face, said improvement comprising a flange extending from the edge of said curved reflecting face, said flange having an inner to outer radius difference on the order of two wavelengths at the frequency with which said antenna is employed, said flange making an angle with the plane defined by the edges of said face which is less than the angle made by the material of said subreflector adjacent to said edges with said plane.
3. A Cassegrainian antenna subreflector comprising a central region having a curved reflecting face, and a peripheral region comprising a flange extending from the edge of said curved reflecting face, said curved reflecting face defining a plane with the edges thereof, the inner and outer radius of said flange differing by substantially two wavelengths of the frequency at which said antenna is employed, said flange making an angle with the plane defined by the edges of said subreflector which is substantially three fourths of the angle made 4. by the material around the edges of said subreflector with said plane.
4. In a Cassegrainian antenna of the type having a parabolic main reflector dish, a smaller subreflector facing the parabolic reflector and a horn feed facing the subreflector, and wherein signals outside of the target of said main reflector dish are reflected by said subreflector to said horn feed as noise signals, the improvement comprising flange means extending outwardly from the edge of said subreflector for reflecting signals received from the locations outside of the target of said main reflector to said horn feed one hundred and eighty degrees out of phase with said signals reflected to said horn feed by said subreflector received from said locations outside of said main reflector to cause a cancellation of said noise signals.
5. A Cassegrainian antenna comprising a parabolic main reflector dish, a smaller subreflector facing the parabolic reflector and a horn feed facing said subreflector, said subreflector including a flange extending from the edges thereof, said flange extending radially a distance on the order of twice the wavelength at the frequency of operation of said antenna, said flange making an angle with the plane defined by the edges of said subreflector which is on the order of three fourths of the angle made by the material of the subreflector near its edges with the plane defined by the edges of said subreflector.
References Cited by the Examiner UNITED STATES PATENTS 2,342,721 2/44 Boerner 343-781 2,477,694 8/49 Gutton 343-837 2,895,131 7/59 Butler 343-840 3,071,770 1/63 Wilkes 343840 HERMAN KARL SAALBACH, Primary Examiner. ELI LIEBERMAN, Examiner.

Claims (1)

1. THE IMPROVEMENT IN A CASSEGRAINIAN ANTENNA HAVING A SUBREFLECTOR WITH A CURVED REFLECTING FACE AND DEFINING A PLANE WITH THE EDGES OF SAID CURVED REFLECTING FACE, SAID IMPROVEMENT COMPRISING A REFLECTING FLANGE EXTENDING RADIALLY FROM THE CURVED REFLECTING FACE AND MAKING AN ANGLE WITH THE PLANE DEFINED BY THE EDGES OF SAID CURVED REFLECTING FACE WHICH IS SMALLER THAN THE ANGLE MADE BY THE PORTION OF THE CURVED REFLECTING FACE NEAR THE EDGE THEREOF WITH SAID PLANE, THE RADIAL LENGTH OF SAID REFLECTING FLANGE BEING ON THE ORDER OF AN INTEGRAL NUMBER OF WAVELENGTHS OF THE FREQUENCY AT WHICH SAID ANTENNA IS USED.
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Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3706999A (en) * 1970-08-28 1972-12-19 Campagnie Ind Des Telecommunic Cassegraninian antenna having limited spillover energy
US3965455A (en) * 1974-04-25 1976-06-22 The United States Of America As Represented By The Secretary Of The Navy Focused arc beam transducer-reflector
US3983560A (en) * 1974-06-06 1976-09-28 Andrew Corporation Cassegrain antenna with improved subreflector for terrestrial communication systems
US3990080A (en) * 1975-07-21 1976-11-02 Bell Telephone Laboratories, Incorporated Antenna with echo cancelling elements
US6215453B1 (en) 1999-03-17 2001-04-10 Burt Baskette Grenell Satellite antenna enhancer and method and system for using an existing satellite dish for aiming replacement dish
US6331839B1 (en) 1999-03-17 2001-12-18 Burt Baskette Grenell Satellite antenna enhancer and method and system for using an existing satellite dish for aiming replacement dish
US20150138657A1 (en) * 2013-11-21 2015-05-21 Electronics And Telecommunications Research Institute Antenna apparatus

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2342721A (en) * 1940-01-20 1944-02-29 Boerner Rudolf Parabolic reflector
US2477694A (en) * 1940-06-15 1949-08-02 Csf Radio waves radiators
US2895131A (en) * 1954-09-17 1959-07-14 Raytheon Co Microwave scanning antennas
US3071770A (en) * 1953-07-20 1963-01-01 Wilkes Gilbert Parabolic dish antenna with aperture blocking correction

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2342721A (en) * 1940-01-20 1944-02-29 Boerner Rudolf Parabolic reflector
US2477694A (en) * 1940-06-15 1949-08-02 Csf Radio waves radiators
US3071770A (en) * 1953-07-20 1963-01-01 Wilkes Gilbert Parabolic dish antenna with aperture blocking correction
US2895131A (en) * 1954-09-17 1959-07-14 Raytheon Co Microwave scanning antennas

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3706999A (en) * 1970-08-28 1972-12-19 Campagnie Ind Des Telecommunic Cassegraninian antenna having limited spillover energy
US3965455A (en) * 1974-04-25 1976-06-22 The United States Of America As Represented By The Secretary Of The Navy Focused arc beam transducer-reflector
US3983560A (en) * 1974-06-06 1976-09-28 Andrew Corporation Cassegrain antenna with improved subreflector for terrestrial communication systems
US3990080A (en) * 1975-07-21 1976-11-02 Bell Telephone Laboratories, Incorporated Antenna with echo cancelling elements
US6215453B1 (en) 1999-03-17 2001-04-10 Burt Baskette Grenell Satellite antenna enhancer and method and system for using an existing satellite dish for aiming replacement dish
US6331839B1 (en) 1999-03-17 2001-12-18 Burt Baskette Grenell Satellite antenna enhancer and method and system for using an existing satellite dish for aiming replacement dish
US20150138657A1 (en) * 2013-11-21 2015-05-21 Electronics And Telecommunications Research Institute Antenna apparatus

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