US3896450A - Hardened antenna element cover - Google Patents

Hardened antenna element cover Download PDF

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Publication number
US3896450A
US3896450A US508584A US50858474A US3896450A US 3896450 A US3896450 A US 3896450A US 508584 A US508584 A US 508584A US 50858474 A US50858474 A US 50858474A US 3896450 A US3896450 A US 3896450A
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Prior art keywords
antenna element
dipole
post
cover
posts
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Expired - Lifetime
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US508584A
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Nancy D Fitzroy
Ronald L Mann
Henry B Gerling
John D Reale
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United States Department of the Army
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United States Department of the Army
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    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/42Housings not intimately mechanically associated with radiating elements, e.g. radome

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Abstract

A hardened cover to provide weather protection (rain and thermal radiation) to an antenna element of a radar system. The antenna element includes a pair of dipoles in normal relation. Each dipole assembly includes a solid and hollow post, a cross-over wire extends between the posts to connect to a dipole arm carried on each post. The hardened cover is comprised of polytetrafluoroethylene (Teflon) filled laminated fiberglass which can be classed as an ablative material.

Description

raw-75 Patent mi United States Fitzroy et al.
[ July 22, 1975 HARDENED ANTENNA ELEMENT COVER Inventors: Nancy D. Fitzroy, Schenectady;
Ronald L. Mann; Henry B. Gerling, both of North Syracuse; John D. Reale, Syracuse, all of N.Y.
The United States of America as represented by the Secretary of the Army, Washington, DC.
Filed: Sept. 23, 1974 Appl. No.: 508,584
Assignee:
US. Cl 343/797; 343/872 Int. Cl. H01Q 1/42 Field of Search 343/797, 872, 873
References Cited UNITED STATES PATENTS Uhrig 343/797 Primary ExaminerEli Lieberman Attorney, Agent, or Firm-Lawrence A. Neureither; Joseph H. Beumer; Harold W. Hilton [57] ABSTRACT A hardened cover to provide weather protection (rain and thermal radiation) to an antenna element of a radar system. The antenna element includes a pair of dipoles in normal relation. Each dipole assembly includes a solid and hollow post, a cross-over wire extends between the posts to connect to a dipole arm carried on each post. The hardened cover is comprised of polytetrafluoroethylene (Teflon) filled laminated fiberglass which can be classed as an ablative material.
2 Claims, 2 Drawing Figures PATENTEDJUL22 ms 3,896,450
FIG. I
HARDENED ANTENNA ELEMENT COVER BACKGROUND OF THE INVENTION Prior antenna elements of a radar system used ceramic type material where dielectric materials were required. The use of ceramics in a complex configuration was judged to be incompatible with a nuclear environment. The most severe nuclear effect imposed on the assembly is thermal radiation. A material investigation program was undertaken to facilitate selection of materials suitable for a radome window. Three classes of material were investigated; opaque materials which can char, opaque materials which can sublime and ceramic materials having high thermal conductivity. Analyses of ceramic materials subjected to the thermal radiation environment indicated that the ceramic which could best withstand thermal shock was marginal with regard to resistance to crack. The analyses considered only a simple model which did not contain stress riser, external loading or support boundary constraints. Due to the mounting constraint and complex geometry with regard to thermal shock, ceramic type materials were judged to be inadequate for a small cover design.
For orientations where thermal radiation is incident on two element posts, a large temperature differential can exist from the front to the rear of each exposed post. Due to the thermal expansion property of the metal post, the posts want to bend toward those posts shaded from the radiation. Since the heated posts are connected to the relatively cooler shaded posts, by means of the element cover, contact surface forces are imposed on the cover. Analyses of this thermal loading situation indicated that external loads on the element cover could be as high as 3,000 pounds. This boundary loading along with the direct absorption of the thermal radiation requires a unique element cover design.
No information exists on the phenomenological behavior of ablative materials subjected to combined thermal and surface force loading. To develop a design compatible with loading conditions it was necessary to conduct tests in a simulated thermal environment. The present cover of polytetrafluoroethylene filled laminated fiberglass successfully withstood the environment. While material ablated from the external surfaces of the cover, little effect was experienced on the interior which contained the cross-over wires. The material remained stable with no apparent warpage. This is an extremely important characteristic when one is concerned with sealing requirements. This material exhibits a unique self-cleaning behavior in that the laminates tend to ablate away in layers and leave a clean surface. The primary function of the fiberglass is to provide the required reinforcement while the primary function of the Teflon is to provide the thermal protection.
SUMMARY OF THE INVENTION The hardened cover of the present invention is disposed to provide weather protection (rain and thermal conditions) for elements of a radar system. The elements are a pair of dipoles in normal relation. Each dipole assembly includes a base disposed for support of a pair of posts having a dipole arm carried thereby. One post is hollow and the second post is solid. Each dipole arm is supported by respective hollow and solid posts. The feed is carried in the hollow post and each post is in normal relation to the base. The dipole arms are disposed in annular relation to the base. The cross-over wires, cross over each other in spaced relation, to connect respective arms of each dipole. The cover of polytetrafluoroethylene filled laminated fiberglass includes a substantially inverted conical portion and an upper member secured to the tops of each post.
BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 is a top view of the antenna elements and cross-over wires with the cover removed.
FIG. 2 is an elevational sectional view of the antenna elements taken along line 22 of FIG. 1, showing the cover in place.
DESCRIPTION OF THE PREFERRED EMBODIMENT As shown in FIG. 1 an antenna element 10 for a radar includes four posts 12, 14, 16, and 18, spaced apart. A plurality of dipole arms 20, 22, 24, and 26 are secured to posts 12, 14, 16, and 18, respectively. A base 28 supports the posts. Posts 12 and 14 are solid and posts 16 and 18 are hollow. A first cross-over wire 30 connects diopole arms 20 and 24. A second crossover wire 32 crosses under wire 30 and connects dipole arms 22 and 26. The cross-over wires are secured to the solid posts by screws 34 and to the conductor 33 in the hollow posts by screws 36. Conductor 33 is the feed for the antenna element.
To protect the antenna element against rain and thermal radiation, a cover assembly 37 is positioned atop the antenna element. Cover assembly 37 includes a lower substantially frusto-conical member 38 having an annular flanged portion 40, and an upper flat plate 42. Plate 42 and section 38 are secured to the antenna element by screws 44. The posts are provided with a cut back portion 46, as shown in FIG. 2, to receive the conical surfaces of frusto-conical member 38 therebetween.
The cover assembly consists of glass cloth impregnated with a polytetrafluoroethylene resin compound or binder. Some such polytetrafluoroethylene filled laminated fiberglass are identified as Dilecto sheets by the Budd Company, and Fluorglas by Dodge Industries.
We claim:
1. In an antenna element including a pair of dipole assemblies, cover means for protecting said element against rain and thermal radiation comprising:
a. a frusto-conical member mounted on top of said dipole assemblies; and,
b. an upper plate mounted on top of said frustoconical member;
c. said plate and said frusto-conical member comprised of polytetrafluoroethylene filled laminated fiberglass.
2. An assembly as set forth in claim 1 wherein said dipole assemblies include a pair of dipoles each comprised of a solid and hollow post having a dipole arm extending therefrom and a cross-over wire extending from each said hollow and solid post, said cross-over wires being disposed in crossed, spaced relation.

Claims (2)

1. In an antenna element including a pair of dipole assemblies, cover means for protecting said element against rain and thermal radiation comprising: a. a frusto-conical member mounted on top of said dipole assemblies; and, b. an upper plate mounted on top of said frusto-conical member; c. said plate and said frusto-conical member comprised of polytetrafluoroethylene filled laminated fiberglass.
2. An assembly as set forth in claim 1 wherein said dipole assemblies include a pair of dipoles each comprised of a solid and hollow post having a dipole arm extending therefrom and a cross-over wire extending from each said hollow and solid post, said cross-over wires being disposed in crossed, spaced relation.
US508584A 1974-09-23 1974-09-23 Hardened antenna element cover Expired - Lifetime US3896450A (en)

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Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4317122A (en) * 1980-08-18 1982-02-23 Rca Corporation Duopyramid circularly polarized broadcast antenna
USD361569S (en) 1994-05-27 1995-08-22 Jervis James W Antenna dome
US5897919A (en) * 1992-05-22 1999-04-27 Furon Company Process for forming microwave transmissive fabric
WO2005020369A1 (en) * 2002-08-23 2005-03-03 Michael Grondin Antenna cover for mobile communications device
WO2005101575A1 (en) * 2004-04-15 2005-10-27 Cellmax Technologies Ab Dipole design
RU2275719C1 (en) * 2004-09-06 2006-04-27 ФГУП "Центральное конструкторское бюро автоматики" Radio-absorbing material
US20100149062A1 (en) * 2008-12-17 2010-06-17 The Boeing Company Dipole for hemispherical coverage antenna
RU2410777C1 (en) * 2009-06-25 2011-01-27 Российская Федерация в лице Министерства промышленности и торговли Российской Федерации (Минпромторг России) Radar absorbing material
US20110025569A1 (en) * 2009-08-03 2011-02-03 Venti Group, LLC Cross-dipole antenna combination
US20110025573A1 (en) * 2009-08-03 2011-02-03 William Ernest Payne Cross-dipole antenna
US20110068992A1 (en) * 2009-08-03 2011-03-24 Venti Group, LLC Cross-dipole antenna configurations
US8624791B2 (en) 2012-03-22 2014-01-07 Venti Group, LLC Chokes for electrical cables
US8803755B2 (en) 2013-01-10 2014-08-12 Venti Group, LLC Low passive intermodulation chokes for electrical cables
US9985363B2 (en) 2013-10-18 2018-05-29 Venti Group, LLC Electrical connectors with low passive intermodulation

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3701157A (en) * 1971-06-03 1972-10-24 Us Air Force Helicopter uhf antenna system for satellite communications

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3701157A (en) * 1971-06-03 1972-10-24 Us Air Force Helicopter uhf antenna system for satellite communications

Cited By (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4317122A (en) * 1980-08-18 1982-02-23 Rca Corporation Duopyramid circularly polarized broadcast antenna
US5897919A (en) * 1992-05-22 1999-04-27 Furon Company Process for forming microwave transmissive fabric
USD361569S (en) 1994-05-27 1995-08-22 Jervis James W Antenna dome
WO2005020369A1 (en) * 2002-08-23 2005-03-03 Michael Grondin Antenna cover for mobile communications device
WO2005101575A1 (en) * 2004-04-15 2005-10-27 Cellmax Technologies Ab Dipole design
US20070200783A1 (en) * 2004-04-15 2007-08-30 Cellmax Technologies Ab Dipole design
US7439927B2 (en) * 2004-04-15 2008-10-21 Cellmax Technologies Ab Dipole design
RU2275719C1 (en) * 2004-09-06 2006-04-27 ФГУП "Центральное конструкторское бюро автоматики" Radio-absorbing material
US8040288B2 (en) * 2008-12-17 2011-10-18 The Boeing Company Dipole for hemispherical coverage antenna
US20100149062A1 (en) * 2008-12-17 2010-06-17 The Boeing Company Dipole for hemispherical coverage antenna
RU2410777C1 (en) * 2009-06-25 2011-01-27 Российская Федерация в лице Министерства промышленности и торговли Российской Федерации (Минпромторг России) Radar absorbing material
US20110025569A1 (en) * 2009-08-03 2011-02-03 Venti Group, LLC Cross-dipole antenna combination
US20110068992A1 (en) * 2009-08-03 2011-03-24 Venti Group, LLC Cross-dipole antenna configurations
US20110025573A1 (en) * 2009-08-03 2011-02-03 William Ernest Payne Cross-dipole antenna
US8289218B2 (en) 2009-08-03 2012-10-16 Venti Group, LLC Cross-dipole antenna combination
US8325101B2 (en) 2009-08-03 2012-12-04 Venti Group, LLC Cross-dipole antenna configurations
US8427385B2 (en) 2009-08-03 2013-04-23 Venti Group, LLC Cross-dipole antenna
US8638270B2 (en) 2009-08-03 2014-01-28 Venti Group, LLC Cross-dipole antenna configurations
US9710576B2 (en) 2009-08-03 2017-07-18 Venti Group, LLC Cross-dipole antenna configurations
US8624791B2 (en) 2012-03-22 2014-01-07 Venti Group, LLC Chokes for electrical cables
US8803755B2 (en) 2013-01-10 2014-08-12 Venti Group, LLC Low passive intermodulation chokes for electrical cables
US9985363B2 (en) 2013-10-18 2018-05-29 Venti Group, LLC Electrical connectors with low passive intermodulation

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