US2423648A - Antenna - Google Patents
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- Publication number
- US2423648A US2423648A US473674A US47367443A US2423648A US 2423648 A US2423648 A US 2423648A US 473674 A US473674 A US 473674A US 47367443 A US47367443 A US 47367443A US 2423648 A US2423648 A US 2423648A
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- Prior art keywords
- reflector
- cells
- strips
- antenna
- searchlight
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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
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49002—Electrical device making
- Y10T29/49016—Antenna or wave energy "plumbing" making
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49616—Structural member making
- Y10T29/4962—Grille making
Definitions
- the present invention relates to directive antenna systems and, more particularly, to antennas for use in association with searchlights, particularly in so-called radar detection systems.
- directiv antenna systems for use with searchlights have generally been of two classes.
- One class employs a plurality of Yagi type directive radiators mounted around the barrel of the searchlight in positions just outside of the light beam. This is an unwieldly arrangement and not very directive.
- Another class involves the use of a parabolic reflector of wire mesh mounted in front of, and coaxial with, the barrel of the searchlight. Thus the light from the Searchlight could shine through the holes in the wire mesh although with a considerable light loss.
- An object, therefore, of the present invention is the provision of an antenna for use in association with a searchlight.
- Another object of the present invention is the provision of an antenna, as aforesaid, which overcomes the above mentioned disadvantages.
- Still another object of the present invention is the provision of an antenna reflector which is highly light pervious.
- a further object of the present invention is the provision of a light pervious radio wave directive apparatus which has a single sharply directive pattern with a minimum number of subsidiary lobes or ears.
- Still a further object of the present invention is the improvement of radio directive systems.
- an antenna system including a radiator and a parabolic reflector adapted to be mounted over the face of a searchlight, with'out substantially reducing the intensity of the light beam.
- the radio wave reflector is of a cellular construction, the cells being of such depth that the radio frequency energy from the antenna is not radiated through the cells in any substantial amount and of such cross section that th cells cannot act as wave guides. Thus th percentage of solid material in the path of the light beam may be substantially reduced.
- the edges of the cells forming the radio wave are preferably treated to obtain maximum conductivity.
- Figure 1 illustrates a side view partly in section
- Figure 2 illustrates in face view an embodiment of the invention
- Figure 3 illustrates an exploded view of a portion of the reflector of Figures 1 and 2.
- FIG 1 In Figure 1 is shown a searchlight l0 mounted on gimbals I I so that it may be rotated in elevation and in azimuth to illuminate a desired ob ject in the distance.
- searchlights are widely used for aircraft interception purposes. Since the present invention is not concerned with the details of the searchlight, they will not be further illustrated or described.
- the reflector I3 is arranged to be pervious to the light from searchlight IE but at the same time act as a reflector oi" the energy radiated from antenna l2.
- Antenna [2 and its reflector l3 are supported in front of, and in coaxial relationship with, the Searchlight ID by means of suitably arranged supports l5 and IS.
- a transmission line TL is shown as connected to the antenna l2 and is adapted to be connected to suitable radio frequency transducer equipment (not shown).
- the antenna I2 is merely illustrativeof a'general form of radio frestrips are portions of the same parabola and crossing each other at right angles.
- Each strip has a number of parallel spaced slots therein extending half way through the width of the strips. That is, vertical strips 23 may have slots 33 (Fig.
- strips 24 may have slots 34.
- each strip may be assembled somewhat in the manner of an egg crate spacer.
- the construction is shown in somewhat greater detail in Figure 3 wherein short portions of the strips 23, 24 are depicted in somewhat enlarged size and with their curvature somewhat exaggerated.
- the disposition of the slots 33 in strips 23 and cooperating slots 34 in strips 24 andthe manner in which strips 23 fit into slots 34 and strips 24 into slots '33 is herein clearly shown.
- conductive bridge pieces 35 are placed at each point of intersection of the component strips. They may be soldered or welded in place and, preferably, the entire inner edge portions 32 of the strips 23 and the bridge pieces 35, if not the entire structure, are plated with some highly conductive metal such as copper or silver.
- the crosssectional dimensions of each of the cells must be too small to pass radio waves according to wave guide action. This may be obtained by making the distances X and Y between adjacent slots 33 and adjacent slots 34 less than one-half of the operating wavelength.
- each of the strips 23 and 24 may be made as large as necessary to obtain the desired attenuation of radio frequency energy without in any way afiecting the transmission of light from the searchlight ill because all of the useful light from searchlight I3 is in the form of parallel rays in a direction parallel to the axis of the cells of reflector l3.
- typical dimensions of an embodiment of the invention may be as follows: the distances X and Y may be 2 inches, while the width Z of strips 23 and 24 may be 4 inches.
- the thickness of the strips may be of the order of to 12 mils.
- the reflector of the present invention may have as little as 5 percent of the absorption of the wire mesh reflector.
- the radio wave energy passing through the reflector composed of conductive. strips is reduced to a negligible. value compared to that passing through the wire mesh reflector.
- the strips I 3 instead of being made of metal may be constructed of a thin plastic or plywood veneer 4 coated with metal foil or sprayed with a coating of metal.
- a directive antenna system including a. diator and a parabolic reflector, said parabolic reflector being comprised of a plurality of conductive walled cells arranged with their lengths parallel to the'axis of said reflector, the lengths of said cells being such that substantial energy from said radiator is not radiated therethrough and said cells having transverse dimensions such that substantial energy is not propagated therethrough by wave guide action.
- a directive antenna system including a radiator and parabolic reflector, said parabolic reflector being comprised of a plurality of conductive walled cells arranged with their lengths parallel to the axis of said reflector, the lengths of said cells being such that substantial energy from said radiator is not radiated therethrough and said cells having transverse dimensions substantially less than one half of the operating wavelength.
- a directive antenna system including a radiator and a parabolic reflector, said parabolic reflect-or being comprised of aplural-ity of conductive walled cells arranged with their lengths parallel to the axis of said reflector, said cells having transverse dimensions such that substantial energy is not propagated therethrough by wave guide action.
- a directive antenna system including a. radiator and a parabolic reflector, said parabolic reflector being comprised of a plurality of conductive walled cells arranged with their lengths parallel to the axis of said reflect-or, said cells having transverse dimensions substantially less than one half of the operating wavelength.
- a light pervious reflector for radio Wave energy including a wall in the form of a plurality of conductive walled, open ended cells having their lengths transverse to the face of said reflector and said cells having transverse dimensions so related to the wavelength of the radiant ener y, such reflector is adapted to reflect that substantial energy is not propagated therethrough by wave guide action and the length of said cells being so related to said wavelength that radio wave energy is not substantiall radiated therethrough.
- a light pervious reflector for radio wave energy including a wall in the form of a plurality of conductive walled cells having their lengths transverse to the face of said reflector and said cells having transverse dimensions substantially less than one half of the wavelength of said energy.
- Aparabolic reflector for radio wave energy including a plurality of flat. parabolic shaped strips of metal arranged on edge in a mutually crossing relationship to form a, plurality of cells, the transverse dimensions of said cells being less than one half of the operating wavelength whereby substantial wave energyxis not propagated therethrough.
- a reflector for radio wave energy including a plurality of flat conductive strips arranged on edge in a mutually crossing relationship to form a plurality of cells, the transverse dimensions of said cells being less than one half of the operating wavelength whereby substantial radio wave energy is not propagated therethrough.
- a parabolic reflector for radio wave energy including a plurality of fiat parabola shaped strips of metal arranged on edge in a mutually crossing relationship to form a plurality of cells, the transverse dimensions of said cells being less than one half of the operating wavelength whereby substantial radio wave energy is not propagated therethrough and cross-shaped metallic clips conductively connected to said strips at each crossing point.
- a parabolic reflector for radio wave energy a comprised of two sets of parallel flat parabolic and slotted metal sheets, the two sets of sheets 6 being interleaved and joined together to form a single rigid structure.
- a parabolic reflector for radio wave energy comprising two sets of parallel fiat slotted metal sheets, said sheets each having an edge of parabolic curvature, the two sets of sheets being so interleaved and joined together as to form a single rigid structure.
Description
y 1947,- c.- w. HANSELL 3,
- ANTENNA I Filed Jan. 27; 1945v Y z INVENTOR (z/m me: if Aim i514.
' ATTQRNEY Patente d July 8, 1947 ANTENNA Clarence W. Hansell, Rocky Point, N. Y., assignor to Radio Corporation of America, a corporation of Delaware Application January 27, 1943, Serial No. 473,674
11 Claims. 1
The present invention relates to directive antenna systems and, more particularly, to antennas for use in association with searchlights, particularly in so-called radar detection systems. Heretofore known directiv antenna systems for use with searchlights have generally been of two classes. One class employs a plurality of Yagi type directive radiators mounted around the barrel of the searchlight in positions just outside of the light beam. This is an unwieldly arrangement and not very directive. Another class involves the use of a parabolic reflector of wire mesh mounted in front of, and coaxial with, the barrel of the searchlight. Thus the light from the Searchlight could shine through the holes in the wire mesh although with a considerable light loss. The maximum response of the antenna theoretically should be centered about the beam of light from the searchlight but actual tests have indicated that such an arrangement is not sufliciently directive and is responsive to radio signals arriving from undesired directions outside the main beam of the reflector. This causes excessive reflections to be received from objects at short distances from the installation which interferes with satisfactory functioning of the equipment over greater distances. This limits the maximum satisfactory range in some instances to 6 or 8 miles.
It has been observed that the lack of directivity is partly due to the fact that very strong high frequency electric fields exist inside the barrel of the searchlight due to waves passing through the reflector screen and reflecting back and forth between the antenna reflector and the light reflector. This cannot be satisfactorily overcome by increasing the number of wires in the mesh of the radio reflector screen because the leakage of energy through the screen cannot be made satisfactorily small without blocking out an excessive amount of light and adding an excessve amount of weight.
An object, therefore, of the present invention is the provision of an antenna for use in association with a searchlight.
Another object of the present invention is the provision of an antenna, as aforesaid, which overcomes the above mentioned disadvantages.
Still another object of the present invention is the provision of an antenna reflector which is highly light pervious.
A further object of the present invention is the provision of a light pervious radio wave directive apparatus which has a single sharply directive pattern with a minimum number of subsidiary lobes or ears.
Still a further object of the present invention is the improvement of radio directive systems.
The foregoing objects, and others which may appear from the following detailed description, are attained by providing an antenna system including a radiator and a parabolic reflector adapted to be mounted over the face of a searchlight, with'out substantially reducing the intensity of the light beam. In order that the light may not be adversely affected the radio wave reflector is of a cellular construction, the cells being of such depth that the radio frequency energy from the antenna is not radiated through the cells in any substantial amount and of such cross section that th cells cannot act as wave guides. Thus th percentage of solid material in the path of the light beam may be substantially reduced. The edges of the cells forming the radio wave are preferably treated to obtain maximum conductivity.
The novel features which, it is believed, are characteristic of the present invention are pointed out with particularity in the appended claims.
The invention will, however, be more completely understood by reference to the following detailed description, which is accompanied by a drawing in which Figure 1 illustrates a side view partly in section, while Figure 2 illustrates in face view an embodiment of the invention and Figure 3 illustrates an exploded view of a portion of the reflector of Figures 1 and 2.
In Figure 1 is shown a searchlight l0 mounted on gimbals I I so that it may be rotated in elevation and in azimuth to illuminate a desired ob ject in the distance. Such searchlights are widely used for aircraft interception purposes. Since the present invention is not concerned with the details of the searchlight, they will not be further illustrated or described. Over the face of the searchlight is mounted a radio antenna l2'at the focus of a reflector l3. The reflector I3 is arranged to be pervious to the light from searchlight IE but at the same time act as a reflector oi" the energy radiated from antenna l2. Antenna [2 and its reflector l3 are supported in front of, and in coaxial relationship with, the Searchlight ID by means of suitably arranged supports l5 and IS. A transmission line TL is shown as connected to the antenna l2 and is adapted to be connected to suitable radio frequency transducer equipment (not shown). The antenna I2 is merely illustrativeof a'general form of radio frestrips are portions of the same parabola and crossing each other at right angles. Each strip has a number of parallel spaced slots therein extending half way through the width of the strips. That is, vertical strips 23 may have slots 33 (Fig.
3) extending outwardly from the concave edge of each strip, while strips 24 may have slots 34..
extending inwardly from the convex edge-01 each strip. Thus the strips forming the reflector may be assembled somewhat in the manner of an egg crate spacer. The construction is shown in somewhat greater detail in Figure 3 wherein short portions of the strips 23, 24 are depicted in somewhat enlarged size and with their curvature somewhat exaggerated. The disposition of the slots 33 in strips 23 and cooperating slots 34 in strips 24 andthe manner in which strips 23 fit into slots 34 and strips 24 into slots '33 is herein clearly shown.
In order to improve the mechanical strength and the rigidity of the structure, as well as the conductivity of the assembled reflector, conductive bridge pieces 35 are placed at each point of intersection of the component strips. They may be soldered or welded in place and, preferably, the entire inner edge portions 32 of the strips 23 and the bridge pieces 35, if not the entire structure, are plated with some highly conductive metal such as copper or silver. In order to obtain the maximum reflectivity of the reflector the crosssectional dimensions of each of the cells must be too small to pass radio waves according to wave guide action. This may be obtained by making the distances X and Y between adjacent slots 33 and adjacent slots 34 less than one-half of the operating wavelength. The width of each of the strips 23 and 24 may be made as large as necessary to obtain the desired attenuation of radio frequency energy without in any way afiecting the transmission of light from the searchlight ill because all of the useful light from searchlight I3 is in the form of parallel rays in a direction parallel to the axis of the cells of reflector l3. For a reflector 72 inches in diameter operating at a frequency of the order of 1000 megacycles typical dimensions of an embodiment of the invention may be as follows: the distances X and Y may be 2 inches, while the width Z of strips 23 and 24 may be 4 inches. The thickness of the strips may be of the order of to 12 mils. Comparing a reflector thus constructed with a similar reflector constructed of wire mesh of 1 inch spacin the component wires thereof being number 10 gauge having a thickness of 102 mils, it has been found that light absorption of the reflector of the present invention may have as little as 5 percent of the absorption of the wire mesh reflector. The radio wave energy passing through the reflector composed of conductive. strips is reduced to a negligible. value compared to that passing through the wire mesh reflector. If desired, the strips I 3 instead of being made of metal may be constructed of a thin plastic or plywood veneer 4 coated with metal foil or sprayed with a coating of metal.
While I hav illustrated a particular embodiment of .the present invention it should be clearly understood that the invention is not limited thereto since many modifications may be made in the several elements employed and in their arrangement and it is therefore contemplated by the appended claims to cover any such modifications as fall within the spirit and scope of the invention.
I claim:
1. A directive antenna system, including a. diator and a parabolic reflector, said parabolic reflector being comprised of a plurality of conductive walled cells arranged with their lengths parallel to the'axis of said reflector, the lengths of said cells being such that substantial energy from said radiator is not radiated therethrough and said cells having transverse dimensions such that substantial energy is not propagated therethrough by wave guide action. v
A directive antenna system, including a radiator and parabolic reflector, said parabolic reflector being comprised of a plurality of conductive walled cells arranged with their lengths parallel to the axis of said reflector, the lengths of said cells being such that substantial energy from said radiator is not radiated therethrough and said cells having transverse dimensions substantially less than one half of the operating wavelength.
3'. A directive antenna system, including a radiator and a parabolic reflector, said parabolic reflect-or being comprised of aplural-ity of conductive walled cells arranged with their lengths parallel to the axis of said reflector, said cells having transverse dimensions such that substantial energy is not propagated therethrough by wave guide action.
l. A directive antenna system, including a. radiator and a parabolic reflector, said parabolic reflector being comprised of a plurality of conductive walled cells arranged with their lengths parallel to the axis of said reflect-or, said cells having transverse dimensions substantially less than one half of the operating wavelength.
5. A light pervious reflector for radio Wave energy including a wall in the form of a plurality of conductive walled, open ended cells having their lengths transverse to the face of said reflector and said cells having transverse dimensions so related to the wavelength of the radiant ener y, such reflector is adapted to reflect that substantial energy is not propagated therethrough by wave guide action and the length of said cells being so related to said wavelength that radio wave energy is not substantiall radiated therethrough.
6. A light pervious reflector for radio wave energy including a wall in the form of a plurality of conductive walled cells having their lengths transverse to the face of said reflector and said cells having transverse dimensions substantially less than one half of the wavelength of said energy.
'7. Aparabolic reflector for radio wave energy including a plurality of flat. parabolic shaped strips of metal arranged on edge in a mutually crossing relationship to form a, plurality of cells, the transverse dimensions of said cells being less than one half of the operating wavelength whereby substantial wave energyxis not propagated therethrough.
8. A reflector for radio wave energy including a plurality of flat conductive strips arranged on edge in a mutually crossing relationship to form a plurality of cells, the transverse dimensions of said cells being less than one half of the operating wavelength whereby substantial radio wave energy is not propagated therethrough.
9. A parabolic reflector for radio wave energy, including a plurality of fiat parabola shaped strips of metal arranged on edge in a mutually crossing relationship to form a plurality of cells, the transverse dimensions of said cells being less than one half of the operating wavelength whereby substantial radio wave energy is not propagated therethrough and cross-shaped metallic clips conductively connected to said strips at each crossing point.
10. A parabolic reflector for radio wave energy a comprised of two sets of parallel flat parabolic and slotted metal sheets, the two sets of sheets 6 being interleaved and joined together to form a single rigid structure.
11. A parabolic reflector for radio wave energy comprising two sets of parallel fiat slotted metal sheets, said sheets each having an edge of parabolic curvature, the two sets of sheets being so interleaved and joined together as to form a single rigid structure.
CLARENCE W. HANSELL.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Number Name Date 775,846 De Moura Nov. 22, 1904 2,021,790 Kuhn Nov. 19, 1935 2,089,935 Eyring Aug. 17, 1937
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US473674A US2423648A (en) | 1943-01-27 | 1943-01-27 | Antenna |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US473674A US2423648A (en) | 1943-01-27 | 1943-01-27 | Antenna |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2423648A true US2423648A (en) | 1947-07-08 |
Family
ID=23880534
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US473674A Expired - Lifetime US2423648A (en) | 1943-01-27 | 1943-01-27 | Antenna |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2423648A (en) |
Cited By (43)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2522562A (en) * | 1945-04-21 | 1950-09-19 | Rca Corp | Antenna system |
| US2530098A (en) * | 1945-05-03 | 1950-11-14 | Lester C Van Atta | Antenna |
| US2543130A (en) * | 1946-07-03 | 1951-02-27 | Bell Telephone Labor Inc | Reflecting system |
| US2570197A (en) * | 1949-06-16 | 1951-10-09 | John I Bohnert | Dual purpose antenna |
| US2576255A (en) * | 1948-06-15 | 1951-11-27 | Emmett L Hudspeth | Reflecting fabric |
| US2598475A (en) * | 1945-12-17 | 1952-05-27 | Raytheon Mfg Co | Antenna system |
| US2613887A (en) * | 1949-01-07 | 1952-10-14 | Bell Aircraft Corp | Aircraft with radar antenna |
| US2617030A (en) * | 1946-03-21 | 1952-11-04 | Rca Corp | Radio mirror |
| US2636125A (en) * | 1948-04-10 | 1953-04-21 | Bell Telephone Labor Inc | Selective electromagnetic wave system |
| US2639384A (en) * | 1948-12-04 | 1953-05-19 | Coligny Guerric De Pillot De | Method and device for focusing of radiations by means of stationary reflector and refractor gratings |
| US2721940A (en) * | 1946-01-03 | 1955-10-25 | Allen S Dunbar | Antenna |
| DE946237C (en) * | 1952-10-22 | 1956-07-26 | Telefunken Gmbh | Directional antenna arrangement for linear polarization |
| US2763860A (en) * | 1949-12-03 | 1956-09-18 | Csf | Hertzian optics |
| US2790169A (en) * | 1949-04-18 | 1957-04-23 | Itt | Antenna |
| US2854724A (en) * | 1954-11-24 | 1958-10-07 | American Dyewood Company | Molding apparatus |
| US3041604A (en) * | 1957-08-15 | 1962-06-26 | Decca Record Co Ltd | Corner reflector formed of taut flat reflecting elements with resilient peripheral tesion frames |
| US3120640A (en) * | 1961-09-29 | 1964-02-04 | Lab For Electronics Inc | Casing and support for transmitterreceiver |
| US3137000A (en) * | 1959-08-10 | 1964-06-09 | Gen Electric Co Ltd | Quarter-wave reflecting plate with support core of resin-impregnated paper honeycomb |
| US3136674A (en) * | 1959-12-09 | 1964-06-09 | Robert V Dunkle | Method of making electromagnetic wave reflector |
| US3231892A (en) * | 1962-06-26 | 1966-01-25 | Philco Corp | Antenna feed system simultaneously operable at two frequencies utilizing polarization independent frequency selective intermediate reflector |
| US3286270A (en) * | 1964-07-01 | 1966-11-15 | Gen Electric | Collapsible parasol-like reflector utilizing flexible honeycomb shell |
| US3427625A (en) * | 1962-12-14 | 1969-02-11 | Hexcel Corp | Focussing reflector with dimpled surface to scatter infra-red radiation |
| US3483614A (en) * | 1962-12-14 | 1969-12-16 | Hexcel Products Inc | Method for making dimpled honeycomb sandwich |
| US3622780A (en) * | 1970-01-15 | 1971-11-23 | Willie R Mccain | Railway switch target |
| US3683379A (en) * | 1970-10-21 | 1972-08-08 | Motorola Inc | Vehicle control system and equipment |
| US3878506A (en) * | 1973-08-03 | 1975-04-15 | David W Young | Airport lighting and radar reflector combination |
| US3886557A (en) * | 1973-11-28 | 1975-05-27 | Texas Instruments Inc | Radar antenna and method of fabricating same |
| US3964071A (en) * | 1973-11-28 | 1976-06-15 | Texas Instruments Incorporated | Radar antenna having a screen supported by shaped slats |
| US4247858A (en) * | 1979-05-21 | 1981-01-27 | Kurt Eichweber | Antennas for use with optical and high-frequency radiation |
| US4439774A (en) * | 1980-12-23 | 1984-03-27 | International Telephone And Telegraph Corporation | Antenna reflector with triangulated cellular back structure |
| DE3709053A1 (en) * | 1986-03-19 | 1987-10-01 | Hitachi Ltd | PARABOLIC ANTENNA SHELL |
| US4698638A (en) * | 1985-12-26 | 1987-10-06 | General Dynamics, Pomona Division | Dual mode target seeking system |
| US4801946A (en) * | 1983-01-26 | 1989-01-31 | Mark Antenna Products, Inc. | Grid antenna |
| US4862188A (en) * | 1986-06-24 | 1989-08-29 | Thomson-Csf | Microwave antenna of light weight and small bulk |
| US5003321A (en) * | 1985-09-09 | 1991-03-26 | Sts Enterprises, Inc. | Dual frequency feed |
| EP0559546A1 (en) * | 1992-03-03 | 1993-09-08 | Thomson-Trt Defense | Low cost microwave antenna for transmitter and/or receiver for a vehicle and a headlight light bulb for its realisation |
| US5291212A (en) * | 1992-09-01 | 1994-03-01 | Andrew Corporation | Grid-type paraboloidal microwave antenna |
| FR2703517A1 (en) * | 1993-04-02 | 1994-10-07 | Thomson Csf | Low-cost compact UHF antenna for a vehicle transmitter and/or receiver system |
| USD382566S (en) * | 1996-05-07 | 1997-08-19 | Espey Mfg. & Electronics Corp. | Dual dipole antenna |
| WO1997032357A1 (en) * | 1996-02-29 | 1997-09-04 | Robert Bosch Gmbh | Head-lamp with integrated microwave antenna |
| US5894290A (en) * | 1996-10-09 | 1999-04-13 | Espey Mfg. & Electronics Corp. | Parabolic rod antenna |
| USD418841S (en) * | 1999-03-01 | 2000-01-11 | Espey Mfg & Electronics Corp. | Parabolic slat antenna |
| EP1739787A1 (en) * | 2005-06-22 | 2007-01-03 | Delphi Technologies, Inc. | Directional antenna using a light reflector |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US775846A (en) * | 1901-10-04 | 1904-11-22 | Roberto Landell De Moura | Wireless telegraph. |
| US2021790A (en) * | 1929-08-02 | 1935-11-19 | Butler Kuhn Corp | Antiglare device |
| US2089935A (en) * | 1937-06-05 | 1937-08-17 | Globe & Machine & Stamping Com | Radiator grille construction |
-
1943
- 1943-01-27 US US473674A patent/US2423648A/en not_active Expired - Lifetime
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US775846A (en) * | 1901-10-04 | 1904-11-22 | Roberto Landell De Moura | Wireless telegraph. |
| US2021790A (en) * | 1929-08-02 | 1935-11-19 | Butler Kuhn Corp | Antiglare device |
| US2089935A (en) * | 1937-06-05 | 1937-08-17 | Globe & Machine & Stamping Com | Radiator grille construction |
Cited By (47)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2522562A (en) * | 1945-04-21 | 1950-09-19 | Rca Corp | Antenna system |
| US2530098A (en) * | 1945-05-03 | 1950-11-14 | Lester C Van Atta | Antenna |
| US2598475A (en) * | 1945-12-17 | 1952-05-27 | Raytheon Mfg Co | Antenna system |
| US2721940A (en) * | 1946-01-03 | 1955-10-25 | Allen S Dunbar | Antenna |
| US2617030A (en) * | 1946-03-21 | 1952-11-04 | Rca Corp | Radio mirror |
| US2543130A (en) * | 1946-07-03 | 1951-02-27 | Bell Telephone Labor Inc | Reflecting system |
| US2636125A (en) * | 1948-04-10 | 1953-04-21 | Bell Telephone Labor Inc | Selective electromagnetic wave system |
| US2576255A (en) * | 1948-06-15 | 1951-11-27 | Emmett L Hudspeth | Reflecting fabric |
| US2639384A (en) * | 1948-12-04 | 1953-05-19 | Coligny Guerric De Pillot De | Method and device for focusing of radiations by means of stationary reflector and refractor gratings |
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