|Publication number||US3176301 A|
|Publication date||Mar 30, 1965|
|Filing date||Feb 14, 1963|
|Priority date||Feb 14, 1963|
|Publication number||US 3176301 A, US 3176301A, US-A-3176301, US3176301 A, US3176301A|
|Inventors||Evans Carey A, Wellons Richard S|
|Original Assignee||Evans Carey A, Wellons Richard S|
|Export Citation||BiBTeX, EndNote, RefMan|
|Patent Citations (9), Referenced by (17), Classifications (9)|
|External Links: USPTO, USPTO Assignment, Espacenet|
March 9 R. s. WELLONS ETAL 3,173,301
PLURAL HORNS AT FOCUS OF PARABOLIC REFLECTOR WITH SHIELDS TO REDUCE SPILLOVER AND SIDE LOBES Filed Feb. .14, 1965 ATTOR Y5 3,176,301 PLURAL HORNS AT FOCUS F PARABOLIC RE- FLECTOR WITH SHIELDS TO REDUCE SPILL- OVER AND SIDE LOBES Richard S. Wellons, Arlington, Mass., and Carey A. Evans, Huntington, N.Y., assignors, by mesne assignments, to the United States of America as represented by the Secretary of the Navy Filed Feb. 14, 1963, Ser. No. 258,968 8 Claims. (Cl. 343-782) This invention relates to antenna systems for the radiation of ultra-high frequency electromagnetic energy and more particularly to an antenna shielding arrangement as applied to generally parabolic reflectors for the directive and eflicient propagation of such electromagnetic energy.
Present day antenna systems of the parabolic reflector variety as used with, for example, radar, perform quite satisfactorily in their ability to track and locate distant targets. The solid angle subtended by the radiated beam of these antennas is sufliciently small so as to permit their when celestial targets are considered. Testing of various antenna systems has revealed that extensive difficulties exist in attempting to attain the necessary accuracy in moon tracking. It has been determined that a large part of this difficulty is due to spillover lobes of the antenna. That is, the distortion of the solid angle through which the active antenna radiator is able to view the surrounding terrian directly and to accept energy from such terrain. This is a common fault of paraboloidal antennas and it results in the reception and transmission of energy from or toward directions where such transmission or reception is unwanted or spurious.
It is therefore an object of this invention to provide an inexpensive, simple, eflicient shielding arrangement for an antenna system to minimize the spillover lobes normally attendant in such antennas.
An additional object is to provide shielding for parabolic antenna systems and to improve the operation of the same, which may also be applied to existing antennas with a minimum of expense.
Other objects and advantages will appear from the following description of an example of the invention, and the novel features will be particularly pointed out in the appended claims.
The single figure of an illustrated embodiment of this invention shows a metallic reflector 10 shaped generally in a paraboloid which type reflectors are well known in the art. The leading or forward portion 11 of the reflector 10 is distorted from the generally parabolic shape of the central portion of reflector and assumes a cylindrical configuration. The same arrangement may be obtained by extending the leading reflector edge or by affixing to a parabolic antenna a cylindrical co-extensive strip. This extension or shield constitutes only a small or minor portion of the antenna surface as compared with the parabolic portion and under certain installation conditions, its forward length is limited as, for example, by the radome where clearance is required. The reflector shield is substantially coaxial with respect to the reflector axis 12.
Disposed in front of the reflector and in the focal plane 13 thereof is the active element of the antenna which in United States Patent O this particular embodiment is made up of four feed horns 14. The horns are symmetrically arranged about the focus of the reflector so that two are in the vertical plane on opposite sides of the axis while the other two are similarly arranged in the horizontal. The horns are positioned at the vertices of a square with the reflector axis at the center and are equidistant therefrom. The energy emitted by the horns is directed toward the reflector as also is the energy impinging on the reflector directed thereby toward the horns. Although the supporting structure for the reflector 10 and for the horns has not been illustrated, these structures are well known and presently used in the art.
Disposed symmetrically about the axis 12 and enclosing the feed horns is a cylindrical metallic shield 15. Since it is essential that the surface of the reflector 11 viewed by the horns be kept to a maximum and the spillover a minimum, the dimensions or" this shield 15 must be properly proportioned to obtain superior results. In order to determine these dimensional parameters, namely, the diameter of the cylindrical shield and the location of its leading edge 16, a pair of projection lines are drawn from one pair of opposite feed horns. One line is drawn from any of the feed horns, in this case, for example, horn 14a, to the closest point 18 thereto along the boundary 17 between portion 11 of the reflector and the central portion thereof. The other line is projected from that feed horn diametrically opposite the first mentioned horn, in this case horn 14b, to a point along the free edge of the portion 11 nearest the point 18. The intersection of these two lines 19 and 20 determines the minimum diameter of the shield 15 while the first mentioned line 19 determines the closest disposition of the edge 16 of shield 15 to the reflector 10.
Stated in another way, on the layout of the reflector and feed horns, the horns being at the focal plane of the refiector and arranged in two pairs, one pair vertical and the other pair horizontal, a line drawn from the near feed horn to the outermost edge of the reflector portion and from the far feed horn to the outermost point on the shield portion. The feed horn shield is so positioned that its edge nearest the reflector falls on the latter line and its diameter is such that the edge thereof falls outside the intersection of these two lines thus giving a complete lineof-sight shielding of the feed horns without shadowing any of the surface of the reflector.
This antenna arrangement has been evaluated and the results indicate satisfactory operation with signals which include those that are randomly polarized. There has been observed a minimum of 10 decibel reduction in spillover with an approximate 0.5 decibel reduction in forward lobe again.
It will be understood that various changes in the details, materials and arrangements of parts (and steps), which have been herein described and illustrated in order to explain the nature of the invention, may be made by those skilled in the art within the principle and scope of the invention as expressed in the appended claims.
1. A shielding arrangement for minimizing the spillover lobes of an antenna system having a generally parabolic reflector and a plurality of feed horns disposed in the focal plane of said reflector which comprises:
(a) a metallic shield coextensive with the edge of said reflector and extending therefrom in the direction of the axis of said reflector toward said focal plane,
(b) a second cylindrical shield coaxial with said axis extending from said focal plane toward said reflector and enclosing said feed horns,
(c) said second shield having a diameter and length proportioned so as to permit illumination of the entire reflector surface by said horns.
2. A shielding arrangement for minimizing the spillover lobes of an antenna system which comprises:
(a) a metallic reflector having a, generally parabolic central portion and a cylindrical outer, portionco-f axial with the axis of said central portion and extending in a direction toward the focal plane of said central portion; a v (b) electromagnetic radiating means disposed in the focal plane of said centralportion, i '7 5 (c) an electrically conducting cylindrical shield dis posed about said radiating means and coaxial with said axis, said shield being of a diameter and length 7 whereby said radiating means may. only illuminate said central portion. Y
3. 'The antenna system according to claim 2, wherein said radiating means is disposedsymmetrically about said axis. l 1
i 4. The antenna system according'to clairn 3,-'wher ein .the other of ,whic'hline's extends from the-diammetrically opposite edge of said radiating means to-the outer edge of ,said' cylindrical outer portion.
6. The antenna systemaccording to claim 5, wherein said radiating means are a plurality'of feed horns disposed I symmetrically about said axis and in said focal plane,
7. A shielding arrangement for minimizing the spillover lobesof an antenna system which comprises:
(a); afgenerally parabolic metallic reflector having an I extended edge portionsubstantially cylindrical and coaxial with the axis ofreflector, (b) four :teed horns supported in the focal plane of said reflector, said horns disposed at thevertices of a,
square and being equidistant from said axis,
i the diameter'of said shield-is such that it is further fro m said axis than the intersection ofa pair of lines one of which extends from the furtherest portion of said radiator from said axis to thebuteredge of said central portion and 5 2o (c) an electrically conducting cylindricalshield coaxial with'said axis enclosing said horns, I (d) the diameter and'length of said shield .being depedent on-the relative positions of two projected lines, (e) one of said lines extending from one horn to the nearest point along the inner edge of-said extended 5 portion of said reflector the other lineextending from the horn diamrnetrically opposite said one horn :to a point onthe outer edge of said extended portion nearest the first said point, a (f)the diameter of said shield being such that it extends outwardly' beyond the intersection of said lines and the edge of said-shield proximate said reflector extending just short of the first of said lines, (g) whereby the entire 'parabolic portion of said reflector maybe illuminated by said feedhorns without g the creation of spillover lobes. 8. The arrangement according to claim 7,' wherein said extended portion constitutes only a small fraction ofthe entire reflecting surface of said reflector. 1
Referencs'Cited by the Examiner UNITED STATES PATENTS' a 2,237,792 5 4/41 'Roosenstein "343- -846 2,460,869 2/49 Brad ;.;343 840 7 2,608,659 8/52 Korman 343-782 52,895,131 7/591 'Butler; 343,4 0 2,918,673 7, 12/59, Lewis'etal. 343-479 7 ",VV'VFOREIGNPATENTS" 675,245 7/52 Great Britain.-. 800,466 8/58- Great Britain.
1,020,692 12/57 Germany,
' 1,048,298 1/59 Germany. HERMANK'ATRLISAALBACH, Primary Examiner.
|Cited Patent||Filing date||Publication date||Applicant||Title|
|US2237792 *||Apr 29, 1939||Apr 8, 1941||Telefunken Gmbh||Antenna system and feeder|
|US2460869 *||Mar 14, 1946||Feb 8, 1949||Rca Corp||Antenna|
|US2608659 *||Jan 10, 1948||Aug 26, 1952||Rca Corp||Antenna for microwave beacons|
|US2895131 *||Sep 17, 1954||Jul 14, 1959||Raytheon Co||Microwave scanning antennas|
|US2918673 *||Dec 12, 1957||Dec 22, 1959||Crawford Carl F||Antenna feed system|
|DE1020692B *||Mar 11, 1957||Dec 12, 1957||Rohde & Schwarz||Richtantenne fuer hochfrequente elektrische Wellen|
|DE1048298B *||Mar 20, 1957||Jan 8, 1959||Deutsche Bundespost||Antennenanordnung mit einem ueber einen Hohlrohrleiter eingespeisten Parabolspiegel|
|GB675245A *||Title not available|
|GB800466A *||Title not available|
|Citing Patent||Filing date||Publication date||Applicant||Title|
|US3314071 *||Jul 12, 1965||Apr 11, 1967||Gen Dynamics Corp||Device for control of antenna illumination tapers comprising a tapered surface of rf absorption material|
|US3680143 *||Jul 1, 1970||Jul 25, 1972||Hughes Aircraft Co||Shaped beam antenna|
|US3716862 *||Feb 24, 1970||Feb 13, 1973||Univ Adelaide||Generation of navigating planes for aircraft landing utilizing parabolic cheese aerial|
|US4005433 *||Dec 5, 1975||Jan 25, 1977||Hughes Aircraft Company||Small wavelength high efficiency antenna|
|US4207573 *||May 17, 1978||Jun 10, 1980||Thomson-Csf||Dual-frequency antenna system with common reflector illuminated by different feeds|
|US4364052 *||Oct 29, 1980||Dec 14, 1982||Bell Telephone Laboratories, Incorporated||Antenna arrangements for suppressing selected sidelobes|
|US4376940 *||Oct 29, 1980||Mar 15, 1983||Bell Telephone Laboratories, Incorporated||Antenna arrangements for suppressing selected sidelobes|
|US4516130 *||Mar 9, 1982||May 7, 1985||At&T Bell Laboratories||Antenna arrangements using focal plane filtering for reducing sidelobes|
|US4626863 *||Sep 12, 1983||Dec 2, 1986||Andrew Corporation||Low side lobe Gregorian antenna|
|US6611238||Nov 6, 2001||Aug 26, 2003||Hughes Electronics Corporation||Method and apparatus for reducing earth station interference from non-GSO and terrestrial sources|
|US6778810||Jan 10, 2000||Aug 17, 2004||The Directtv Group, Inc.||Method and apparatus for mitigating interference from terrestrial broadcasts sharing the same channel with satellite broadcasts using an antenna with posterior sidelobes|
|US6975837||Jan 21, 2003||Dec 13, 2005||The Directv Group, Inc.||Method and apparatus for reducing interference between terrestrially-based and space-based broadcast systems|
|US7257370||Jun 21, 2004||Aug 14, 2007||The Directv Group, Inc.||Method and apparatus for mitigating interference from terrestrial broadcasts sharing the same channel with satellite broadcasts using an antenna with posterior sidelobes|
|US7369809||Oct 30, 2000||May 6, 2008||The Directv Group, Inc.||System and method for continuous broadcast service from non-geostationary orbits|
|US7917080||Jul 11, 2007||Mar 29, 2011||The Directv Group, Inc.||Method and apparatus for mitigating interference from terrestrial broadcasts sharing the same channel with satellite broadcasts using an antenna with posterior sidelobes|
|US20040235418 *||Jun 21, 2004||Nov 25, 2004||Anderson Paul R.|
|US20090004967 *||Jul 11, 2007||Jan 1, 2009||Anderson Paul R|
|U.S. Classification||343/782, 343/841, 343/840, 343/777, 343/779|
|International Classification||H01Q19/10, H01Q19/17|