US3373434A - Lightweight antenna formed from net of dielectric cord, having metalized sectors thereon - Google Patents

Lightweight antenna formed from net of dielectric cord, having metalized sectors thereon Download PDF

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US3373434A
US3373434A US415003A US41500364A US3373434A US 3373434 A US3373434 A US 3373434A US 415003 A US415003 A US 415003A US 41500364 A US41500364 A US 41500364A US 3373434 A US3373434 A US 3373434A
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antenna
cords
net
dielectric
metalized
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US415003A
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John J Lorenzo
George O Nagel
Schwartzman Leon
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Sperry Corp
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Sperry Rand Corp
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    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q9/00Electrically-short antennas having dimensions not more than twice the operating wavelength and consisting of conductive active radiating elements
    • H01Q9/04Resonant antennas
    • H01Q9/16Resonant antennas with feed intermediate between the extremities of the antenna, e.g. centre-fed dipole
    • H01Q9/26Resonant antennas with feed intermediate between the extremities of the antenna, e.g. centre-fed dipole with folded element or elements, the folded parts being spaced apart a small fraction of operating wavelength
    • H01Q9/27Spiral antennas
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/08Means for collapsing antennas or parts thereof
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/36Structural form of radiating elements, e.g. cone, spiral, umbrella; Particular materials used therewith
    • H01Q1/38Structural form of radiating elements, e.g. cone, spiral, umbrella; Particular materials used therewith formed by a conductive layer on an insulating support

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  • This invention relates to lightweight, inexpensive, and readily transportable antennas, and more particularly relates to multi-element antennas whose individual elements are formed by metallized segments on a plurality of lengths of dielectric cord, said metalized segments and the lengths of dielectric cord being arranged in a predetermined pattern on a suitable supporting frame to form a desired antenna array.
  • Another object of this invention is to provide a multielement antenna array which is readily transportable in small, compact, and lightweight units.
  • a further object of the invention is to provide a multielement antenna array that is inexpensive to manufacture, easy to construct, and is subject to slight wind loading as compared to other known multi-element antenna arrays.
  • a further object of this invention is to provide a light- Weight antenna that is comprised of lengths or strands of dielectric cord that are supported on a frame and provided with metalized segments that are arranged appropriately along the lengths of cords to form an array, or arrays of elements that are necessary to provide a desired antenna pattern.
  • FIGS. 1 and 2 are perspective and top views, respectively, of an antenna constructed in accordance with the present invention.
  • FIG. 3 is a detailed illustration of the frame or supporting structure for supporting the dielectric cords
  • FIGS. 4 and 5 are graphs illustrating the antenna pattern and voltage standing wave ratio (v.s.w.r.), respectively, of an antenna constructed in accordance with the teachings of this invention.
  • FIG. 6 is an illustration of an alternative embodiment of an antenna constructed in accordance wtih the teachings of this invention.
  • FIGS. 1 and 2 an antenna that successfully fulfilled the above objects is illustrated in FIGS. 1 and 2.
  • This antenna is comprised of a plurality of Yagi antennas positioned side-by-side and excited in the proper phases to produce a desired radiation pattern.
  • the antenna is comprised of a gridlike arrangement of dielectric cords or strands wherein the lengths of cords 11-16 are secured to the end rods 19 and 20.
  • the transversely-extending cords 2228 are either tied to cords 11-16 or the two groups of cords may be wound together in the maner of a fish net.
  • the cords 11-16, 22-28 are made from a dielectric material such as Dacron or wound fiberglass that have low stretch characteristics and high tensile strengths.
  • the end rods 19 and 20 are made of lightweight fiberglass tubing.
  • the elements of each Yagi array are comprised of short metalized conductive segments such as the segments 30-35 on the respective cords 11-16.
  • the dielectric cords may be metalized at the desired segments to form the elements by crimping or bonding aluminum or copper foil to the cords, by applying adhesive metallic tape, by applying metallic paint, or by weaving metallic thread into the cord.
  • the net-like arrangement of the cords is supported on the antenna mast 38 in its stretched-out position by the supporting rods 4643 which lie beneath the plane containing the cords.
  • One end of each of the rods 4tl41 is releaseably secured to an end of the end rod 20, and their other ends are secured by means of pivot joints to a yoke 45 secured to the mast 38.
  • the other two supporting rods 42 and 43 are secured in like manner to support the end rod 19.
  • Support rods 40-43 also are made of fiberglass tubing, and as illustrated in FIG. 3, are provided with telescoping joints to-49, thereby permitting the entire supporting structure to be telescoped and folded into a small, compact unit that is readily transported.
  • Suitable locking means 6164 are associated with the telescoping joints 46 19.
  • the net-like structure is sup ported from above by the dielectric cords 56-53 which extend from the top of mast 38 to the respective corners of the end rods 19 and 20.
  • These supporting cords also are made from a dielectric material such as Dacron or fiberglass.
  • the antenna mast 38 also may be of fibergalss tubing, thus further minimizing the overall weight of the entire antenna assembly.
  • each Yagi antenna such as the element 34
  • the driven elements of each Yagi antenna are excited by means of a suitable connection to a section of coaxial transmission line 60.
  • 3 driven elements may be excited from a phase and amplitude determining network to obtain the excitation that is required to produce a desired radiation pattern.
  • one or more similar array of Yagi antennas may be mounted below the one illustrated in FIG. 1 so as to add further beam-shaping capabilities to the antenna.
  • the structure and means of mounting the additional arrays will be substantially identical to those described above. Because of the very light weight of the antenna structure and the openness of its structure, i.e., no large surfaces, the antenna offers very low wind resistance and therefore is physically stable even in relatively high winds when the antenna mast is properly supported by guy wires, as is conventional in the art.
  • the assembly and erection of the antenna array illustrated in FIG. 1 is a relatively simple matter.
  • the various components will be separately packaged for transportation.
  • end rods 19 and with the dielectric cords 1116, and 22-28 secured thereto may be rolled into a tight bundle.
  • the yoke 45 and supporting rods 4043, FIG. 3 will be separately packaged, as will the sections of antenna mast 38.
  • end rods 19 and 20 and the lengths of cords 1116 and 22-28 will be unrolled and stretched out into their rectangular shape.
  • the supporting rods 4043 then are raised and extended to the approximate desired lengths. The extent to which supporting rods 40-43 may be raised is limited by appropriate stops 70-73, FIG.
  • Yoke 45 next is inserted over the end of the top section of mast 38 and is secured to the mast by suitable clamping means, and the end rods 19 and 20 are secured to the supporting rods 40-43.
  • the supporting cords 56-53 next are attached to the ends of end rods 19 anw 20 and are secured to the top of the end section of mast 38.
  • Final adjustments then are made to the lengths of the supporting rods 40-43 and to the supporting cords 50-53 to assure the correct planar alignment of the dielectric cords forming the antenna array and to assure that the lengths of dielectric cord are taut.
  • the assembled antenna array then is secured to the remainder of the mast 38 and the mast is erected in the usual manner.
  • an antenna was constructed in the manner illustrated in FIG. 1, having a rectangular shape with dimensions of 4 feet x 12 feet, and including an array of 8 Yagi antennas, each antenna having 12 director elements and one reflector element. The elements were formed by securing aluminum tape at the appropriate positions on the dielectric cord. The excited element of each antenna was fed from a power divider network that excited the 8 antennas with a Tschebysheff amplitude distribution.
  • the Yagi antennas were designed in accordance with standard antenna theory which is discussed in many standard texts. For operation in the L-band portion of the frequency spectrum, and with no particular attempt to maximize the antenna design, the radiation pattern that was obtained is illustrated in FIG. 4, and the measured voltage standing wave ratio (v.s.w.r.) is illustrated in FIG. 5. The entire weight of the operable array of antennas, including all hardware, mast, and transmission line feed system, was approximately 13 pounds.
  • a rectangular grid-like arrangement of the dielectric cords is not the only possible arrangement for these cords within a supporting frame comprised of the fiberglass tubing, nor is the array of Yagi antennas the only type of array that can be constructed by means of metalized segments on the dielectric cord.
  • the radiating antennas need not be of the endfire type as is the Yagi antenna, but broadside arrays may be constructed by supporting the lengths of dielectric cord with the metalized segments thereon in a plane that is perpendicular to the ground.
  • An example of this latter type of array is illustrated in FIG. 6 wherein the grid or net-like pattern of flexible dielectric cords is tautly supported between the end members 82 and 83.
  • the end members 82 and 83 in turn are supported by the masts 84 and 85, the masts being properly supported by the guy ropes, as illustrated.
  • the antenna array that is formed on the net-like pattern 80 is comprised, for illustrative purposes, of two spiral antennas 86 and 87.
  • the spiral antenna 86 is formed by the continuous conductive elements 86' and 86 which may be formed by applying flexible conductive tape or conductive paint, for example, along selected paths formed on the dielectric cords of the net-like pattern 80.
  • a transmission line may be connected to the respective elements 86' and 86" at the feed points 88 at the center of the spiral 86.
  • spiral antenna 87 is comprised of the continuous conductive elements 87' and 87" which may be connected to a transmission line at the feed points 89.
  • the end members 82 and 83, as well as the sections of the masts 84 and may be made of lightweight fiberglass tubing, and the flexible dielectric cords of the net-like pattern 80 may be of the same materials as previously mentioned in the description of FIG. 1.
  • the broadside radiating array will have little wind resistance because of the very open and porous nature of the net-like pattern 80.
  • the net-like pattern 80 and the end members 82 and 83 may be detached from the masts 84 and 85 and may be rolled into a small and lightweight package for easy transport.
  • a lightweight antenna comprising a first group of dielectric cords disposed in a common plane in parallel-spaced apart relationship
  • conductive segments placed along respective cords of said net-like structure to provide the elements of an antenna having a shape conforming to the contour of said respective cords.

Description

-March 12, 1968 LORENZO T 3,373,434
LIGHTWEIGHT ANTENNA FORMED FROM NET OF DIELECTRIC CORD, HAVING METALIZED SECTORS THEREON Filed Dec. 1. 1964 3 Sheets-Sheet 1 & O 2 E 2a 27 26 25 24 23 22 F I e. 2.
JOHN J. LORENZO GEORGE O. NAOE'L LEON SCHWARTZMA/V A I TOR/VE Y March 12, 1968 J. J. LORENZO ETAL LIGHTWEIGHT ANTENNA FORMED FROM NET OF DIELECTRIC Filed Dec. 1, 1964 Fuss.-
CORD, HAVING METALIZED SECTORS THEREON 3 Sheets-Sheet 2 INVENTORS JOHN J. LORENZO GEORGE 0. NA GEL LEON SCHWARTZ/MAN BY $2.. bam zw RESPONSE (d b) VSWR March 12, 1968 .1. J. LORENZO ETAL 3,373,434
LIGHTWEIGHT ANTENNA FORMED FROM NET ORDIELECTRIC com), HAVING METALIZED SECTORS THEREON Filed Dec. 1, 1964 3 Sheets-Sheet 3 FREQUENCY (MC) INVENTORS JOHN J. LURE/V20 q kw. H. 16
United States Patent M LIGHTWEIGHT ANTENNA FORMED FROM NET 0F DIELECTRIC CORD, HAVING METALHZED SECTORS THEREON John .l. Lorenzo, Rosedale, George 0. Nagel, Massapequa Park, and Leon Schwartzman, Brooklyn, N.Y., assignors to Sperry Rand Corporation, Great Neck, N.Y., a corporation of Delaware Filed Dec. 1, 1964, Ser. No. 415,003 1 Claim. (Cl. 343879) ABSTRACT OF THE DISCLOSURE A lightweight portable antenna having a collapsible support member comprising a net-like structure of dielectric cords. Selected ones of the cords are covered by conductive segments to provide the elements of an antenna having a shape conforming to the contour of the selected cords of the net-like support structure.
This invention relates to lightweight, inexpensive, and readily transportable antennas, and more particularly relates to multi-element antennas whose individual elements are formed by metallized segments on a plurality of lengths of dielectric cord, said metalized segments and the lengths of dielectric cord being arranged in a predetermined pattern on a suitable supporting frame to form a desired antenna array.
In the use of radio communications and radar systems, both civilian and military, it often is required that the operating location be frequently changed, and it also is often desirable that the equipment be transportable to rather remote locations that are not accessible by heavy vehicles. These factors make it desirable to have lightweight, compact and readily transportable operating equipment. In systems that utilize a shaped antenna pattern, the antenna structure required to obtain the desired pattern can become quite bulky, heavy, and require considerable time to set up and take down, thus constituting a major factor in the usefulness of the system for particular applications.
It therefore is an object of this invention to provide a lightweight, readily transportable antenna that may be set up and taken down with a minimum of effort.
Another object of this invention is to provide a multielement antenna array which is readily transportable in small, compact, and lightweight units.
A further object of the invention is to provide a multielement antenna array that is inexpensive to manufacture, easy to construct, and is subject to slight wind loading as compared to other known multi-element antenna arrays.
A further object of this invention is to provide a light- Weight antenna that is comprised of lengths or strands of dielectric cord that are supported on a frame and provided with metalized segments that are arranged appropriately along the lengths of cords to form an array, or arrays of elements that are necessary to provide a desired antenna pattern.
These and other objects and advantages of the present invention, which will become more apparent from a read ing of the following specification and claims, are achieved in an illustrated embodiment of the invention by providing a rectangularly-shaped grid or net-like arrangement of dielectric cords that are supported in a stretched-out fashion on a suitable supporting frame or structure. The lengths of cord are provided with metalized segments along their lengths, these segments being appropriately spaced and arranged to form the various elements of a particular antenna array, or an array of arrays. Various ones of the rnetalized segments are connected to transmis- 3,373,434 Patented Mar. 12, 1968 sion lines which provide the necessary excitation of the elements to produce the desired radiating and receiving antenna pattern. The supporting frame is secured to an antenna mast and the assembly comprises a lightweight structure that offers little wind resistance, is easily erected, and readily transportable in small lightweight packages when disassembled.
The antenna of this invention will be described by re ferring to the accompanying drawings, wherein:
FIGS. 1 and 2 are perspective and top views, respectively, of an antenna constructed in accordance with the present invention;
FIG. 3 is a detailed illustration of the frame or supporting structure for supporting the dielectric cords;
FIGS. 4 and 5 are graphs illustrating the antenna pattern and voltage standing wave ratio (v.s.w.r.), respectively, of an antenna constructed in accordance with the teachings of this invention; and
FIG. 6 is an illustration of an alternative embodiment of an antenna constructed in accordance wtih the teachings of this invention.
Referring now in more detail to the drawings, an antenna that successfully fulfilled the above objects is illustrated in FIGS. 1 and 2. This antenna is comprised of a plurality of Yagi antennas positioned side-by-side and excited in the proper phases to produce a desired radiation pattern. Physically, the antenna is comprised of a gridlike arrangement of dielectric cords or strands wherein the lengths of cords 11-16 are secured to the end rods 19 and 20. To assure the maintenance of proper spacing between cords 11-16 the transversely-extending cords 2228 are either tied to cords 11-16 or the two groups of cords may be wound together in the maner of a fish net. The cords 11-16, 22-28 are made from a dielectric material such as Dacron or wound fiberglass that have low stretch characteristics and high tensile strengths. The end rods 19 and 20 are made of lightweight fiberglass tubing. The elements of each Yagi array are comprised of short metalized conductive segments such as the segments 30-35 on the respective cords 11-16. The dielectric cords may be metalized at the desired segments to form the elements by crimping or bonding aluminum or copper foil to the cords, by applying adhesive metallic tape, by applying metallic paint, or by weaving metallic thread into the cord.
The net-like arrangement of the cords is supported on the antenna mast 38 in its stretched-out position by the supporting rods 4643 which lie beneath the plane containing the cords. One end of each of the rods 4tl41 is releaseably secured to an end of the end rod 20, and their other ends are secured by means of pivot joints to a yoke 45 secured to the mast 38. The other two supporting rods 42 and 43 are secured in like manner to support the end rod 19. Support rods 40-43 also are made of fiberglass tubing, and as illustrated in FIG. 3, are provided with telescoping joints to-49, thereby permitting the entire supporting structure to be telescoped and folded into a small, compact unit that is readily transported. Suitable locking means 6164 are associated with the telescoping joints 46 19.
As illustrated in FIG. 1, the net-like structure is sup ported from above by the dielectric cords 56-53 which extend from the top of mast 38 to the respective corners of the end rods 19 and 20. These supporting cords also are made from a dielectric material such as Dacron or fiberglass.
Because of the extreme light weight of the antenna array, the antenna mast 38 also may be of fibergalss tubing, thus further minimizing the overall weight of the entire antenna assembly.
The driven elements of each Yagi antenna, such as the element 34, are excited by means of a suitable connection to a section of coaxial transmission line 60. The
3 driven elements may be excited from a phase and amplitude determining network to obtain the excitation that is required to produce a desired radiation pattern.
If desired, one or more similar array of Yagi antennas may be mounted below the one illustrated in FIG. 1 so as to add further beam-shaping capabilities to the antenna. The structure and means of mounting the additional arrays will be substantially identical to those described above. Because of the very light weight of the antenna structure and the openness of its structure, i.e., no large surfaces, the antenna offers very low wind resistance and therefore is physically stable even in relatively high winds when the antenna mast is properly supported by guy wires, as is conventional in the art.
The assembly and erection of the antenna array illustrated in FIG. 1 is a relatively simple matter. The various components will be separately packaged for transportation. For example, end rods 19 and with the dielectric cords 1116, and 22-28 secured thereto may be rolled into a tight bundle. Similarly, the yoke 45 and supporting rods 4043, FIG. 3, will be separately packaged, as will the sections of antenna mast 38, In the assembly process, end rods 19 and 20 and the lengths of cords 1116 and 22-28 will be unrolled and stretched out into their rectangular shape. The supporting rods 4043 then are raised and extended to the approximate desired lengths. The extent to which supporting rods 40-43 may be raised is limited by appropriate stops 70-73, FIG. 3, that are associated with the respective pivot joints that secure them to yoke 45. Yoke 45 next is inserted over the end of the top section of mast 38 and is secured to the mast by suitable clamping means, and the end rods 19 and 20 are secured to the supporting rods 40-43. The supporting cords 56-53 next are attached to the ends of end rods 19 anw 20 and are secured to the top of the end section of mast 38. Final adjustments then are made to the lengths of the supporting rods 40-43 and to the supporting cords 50-53 to assure the correct planar alignment of the dielectric cords forming the antenna array and to assure that the lengths of dielectric cord are taut. The assembled antenna array then is secured to the remainder of the mast 38 and the mast is erected in the usual manner.
In practice, an antenna was constructed in the manner illustrated in FIG. 1, having a rectangular shape with dimensions of 4 feet x 12 feet, and including an array of 8 Yagi antennas, each antenna having 12 director elements and one reflector element. The elements were formed by securing aluminum tape at the appropriate positions on the dielectric cord. The excited element of each antenna was fed from a power divider network that excited the 8 antennas with a Tschebysheff amplitude distribution. The Yagi antennas were designed in accordance with standard antenna theory which is discussed in many standard texts. For operation in the L-band portion of the frequency spectrum, and with no particular attempt to maximize the antenna design, the radiation pattern that was obtained is illustrated in FIG. 4, and the measured voltage standing wave ratio (v.s.w.r.) is illustrated in FIG. 5. The entire weight of the operable array of antennas, including all hardware, mast, and transmission line feed system, was approximately 13 pounds.
It will be understood that a rectangular grid-like arrangement of the dielectric cords is not the only possible arrangement for these cords within a supporting frame comprised of the fiberglass tubing, nor is the array of Yagi antennas the only type of array that can be constructed by means of metalized segments on the dielectric cord.
Further, the radiating antennas need not be of the endfire type as is the Yagi antenna, but broadside arrays may be constructed by supporting the lengths of dielectric cord with the metalized segments thereon in a plane that is perpendicular to the ground. An example of this latter type of array is illustrated in FIG. 6 wherein the grid or net-like pattern of flexible dielectric cords is tautly supported between the end members 82 and 83. The end members 82 and 83 in turn are supported by the masts 84 and 85, the masts being properly supported by the guy ropes, as illustrated. The antenna array that is formed on the net-like pattern 80 is comprised, for illustrative purposes, of two spiral antennas 86 and 87. The spiral antenna 86 is formed by the continuous conductive elements 86' and 86 which may be formed by applying flexible conductive tape or conductive paint, for example, along selected paths formed on the dielectric cords of the net-like pattern 80. A transmission line may be connected to the respective elements 86' and 86" at the feed points 88 at the center of the spiral 86. Similarly, spiral antenna 87 is comprised of the continuous conductive elements 87' and 87" which may be connected to a transmission line at the feed points 89. The end members 82 and 83, as well as the sections of the masts 84 and may be made of lightweight fiberglass tubing, and the flexible dielectric cords of the net-like pattern 80 may be of the same materials as previously mentioned in the description of FIG. 1.
The broadside radiating array will have little wind resistance because of the very open and porous nature of the net-like pattern 80. The net-like pattern 80 and the end members 82 and 83 may be detached from the masts 84 and 85 and may be rolled into a small and lightweight package for easy transport.
While the invention has been described in its preferred embodiments, it is to be understood that the words which have been used are words of description rather than limitation and that changes within the purview of the appended claim may be made without departing from the true scope and spirit of the invention in its broader aspects,
What is claimed is:
1. A lightweight antenna comprising a first group of dielectric cords disposed in a common plane in parallel-spaced apart relationship,
a second group of dielectric cords disposed in said common plane in parallel-spaced apart relationship and extending transversely to said first group,
said two groups of cords intersecting each other and being secured together at their points of intersection to form a net-like structure, and
conductive segments placed along respective cords of said net-like structure to provide the elements of an antenna having a shape conforming to the contour of said respective cords.
References Cited UNITED STATES PATENTS 1,683,270 9/1928 Taylor et al. 343897 X 2,412,562 12/1946 Crawshaw 343-897 X 2,667,577 1/1954 Graziano 343897 X 2,866,195 12/1958 Powlison 343700 3,047,860 7/1962 Swallow et al. 343915 X 3,129,427 4/1964 Dunlavy 343895 X 3,152,330 10/1964 Chatelain 343-895 X 3,276,027 9/1966 Bell et al. 343886 X HERMAN KARL SAALBACH, Primaly Examiner.
W. H. PUNTER, Assistant Examiner.
US415003A 1964-12-01 1964-12-01 Lightweight antenna formed from net of dielectric cord, having metalized sectors thereon Expired - Lifetime US3373434A (en)

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Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3618109A (en) * 1968-07-23 1971-11-02 Granger Associates Antenna construction with effectively extended radiator elements
US4007436A (en) * 1975-07-07 1977-02-08 Her Majesty The Queen In Right Of Canada As Represented By The Minister Of National Defense Self-deploying instrument assembly
US4138682A (en) * 1977-01-24 1979-02-06 Doherty R Michael Cubical quad antennas with spreader-reinforced crossarms
US4186400A (en) * 1978-06-01 1980-01-29 Grumman Aerospace Corporation Aircraft scanning antenna system with inter-element isolators
US4336543A (en) * 1977-05-18 1982-06-22 Grumman Corporation Electronically scanned aircraft antenna system having a linear array of yagi elements
WO1983000952A1 (en) * 1982-03-26 1983-03-17 Grumman Corp An electronically scanned antenna system having a linear array of endfire elements
US4378558A (en) * 1980-08-01 1983-03-29 The Boeing Company Endfire antenna arrays excited by proximity coupling to single wire transmission line
US4514734A (en) * 1980-05-12 1985-04-30 Grumman Aerospace Corporation Array antenna system with low coupling elements
US5319380A (en) * 1991-08-28 1994-06-07 Telefunken Sendertechnik Gmbh Antenna curtain
US5351062A (en) * 1992-09-08 1994-09-27 General Electric Company Retractable distributed array antenna
US5554999A (en) * 1994-02-01 1996-09-10 Spar Aerospace Limited Collapsible flat antenna reflector
US5787673A (en) * 1992-09-14 1998-08-04 Pirod, Inc. Antenna support with multi-direction adjustability
WO1999019938A1 (en) * 1997-10-09 1999-04-22 Malibu Research Associates, Inc. Low-windload satellite antenna

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Publication number Priority date Publication date Assignee Title
US1683270A (en) * 1923-08-25 1928-09-04 Taylor Marcia Estabrook Radiation receiving conductor
US2412562A (en) * 1943-05-21 1946-12-17 British Celanese Fabric
US2667577A (en) * 1951-07-14 1954-01-26 Motorola Inc Antenna
US2866195A (en) * 1954-02-23 1958-12-23 Neil C Powlison Television receiving antenna
US3047860A (en) * 1957-11-27 1962-07-31 Austin B Swallow Two ply electromagnetic energy reflecting fabric
US3129427A (en) * 1960-05-25 1964-04-14 All Products Company Spiral antenna mounted on openwork support
US3152330A (en) * 1961-03-27 1964-10-06 Ryan Aeronautical Co Multi-spiral satellite antenna
US3276027A (en) * 1962-08-07 1966-09-27 Granger Associates Logarithmic periodic antenna

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1683270A (en) * 1923-08-25 1928-09-04 Taylor Marcia Estabrook Radiation receiving conductor
US2412562A (en) * 1943-05-21 1946-12-17 British Celanese Fabric
US2667577A (en) * 1951-07-14 1954-01-26 Motorola Inc Antenna
US2866195A (en) * 1954-02-23 1958-12-23 Neil C Powlison Television receiving antenna
US3047860A (en) * 1957-11-27 1962-07-31 Austin B Swallow Two ply electromagnetic energy reflecting fabric
US3129427A (en) * 1960-05-25 1964-04-14 All Products Company Spiral antenna mounted on openwork support
US3152330A (en) * 1961-03-27 1964-10-06 Ryan Aeronautical Co Multi-spiral satellite antenna
US3276027A (en) * 1962-08-07 1966-09-27 Granger Associates Logarithmic periodic antenna

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3618109A (en) * 1968-07-23 1971-11-02 Granger Associates Antenna construction with effectively extended radiator elements
US4007436A (en) * 1975-07-07 1977-02-08 Her Majesty The Queen In Right Of Canada As Represented By The Minister Of National Defense Self-deploying instrument assembly
US4138682A (en) * 1977-01-24 1979-02-06 Doherty R Michael Cubical quad antennas with spreader-reinforced crossarms
US4336543A (en) * 1977-05-18 1982-06-22 Grumman Corporation Electronically scanned aircraft antenna system having a linear array of yagi elements
US4186400A (en) * 1978-06-01 1980-01-29 Grumman Aerospace Corporation Aircraft scanning antenna system with inter-element isolators
US4514734A (en) * 1980-05-12 1985-04-30 Grumman Aerospace Corporation Array antenna system with low coupling elements
US4378558A (en) * 1980-08-01 1983-03-29 The Boeing Company Endfire antenna arrays excited by proximity coupling to single wire transmission line
WO1983000952A1 (en) * 1982-03-26 1983-03-17 Grumman Corp An electronically scanned antenna system having a linear array of endfire elements
US5319380A (en) * 1991-08-28 1994-06-07 Telefunken Sendertechnik Gmbh Antenna curtain
US5351062A (en) * 1992-09-08 1994-09-27 General Electric Company Retractable distributed array antenna
US5787673A (en) * 1992-09-14 1998-08-04 Pirod, Inc. Antenna support with multi-direction adjustability
US5554999A (en) * 1994-02-01 1996-09-10 Spar Aerospace Limited Collapsible flat antenna reflector
WO1999019938A1 (en) * 1997-10-09 1999-04-22 Malibu Research Associates, Inc. Low-windload satellite antenna

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