Omni directional broadband coplanar antenna element

Information

  • Patent Grant
  • 10424830
  • Patent Number
    10,424,830
  • Date Filed
    Monday, March 6, 2017
    7 years ago
  • Date Issued
    Tuesday, September 24, 2019
    5 years ago
Abstract
The present invention provides an omni-directional antenna element configuration having a compensated radiation pattern. Broadband antenna elements are coplanarly disposed on a suitable planar dielectric material. A single element or antenna comprises a pair of balanced fed radiating microstrip elements symmetrically disposed about the centerline of a balanced signal feed network. Additionally, a pair of pattern augmentation rods positioned on each side of and proximate to the planar dielectric material running longitudinally to the centerline axis of a balanced feed network. Disposed proximate to each radiating element are partially coplanar, frequency bandwidth expanding microstrip lines. The combination of radiating elements together with pattern augmentation rods provides a broad bandwidth omni-directional radiating element suitable for use in multi-element antenna arrays.
Description
BACKGROUND OF THE INVENTION

1. Field of the Invention


The present invention relates in general to radio communication systems and components. More particularly the invention is directed to antenna elements and antenna arrays for radio communication systems.


2. Description of the Prior Art and Related Background Information


Modern wireless antenna implementations generally include a plurality of radiating elements that may be arranged to provide a desired radiated (and received) signal beamwidth and azimuth scan angle. For an omni-directional antenna it is desirable to achieve a near uniform beamwidth that exhibits a minimum variation over 360 degrees of coverage. Differing from highly directional antennas an omni-directional antenna beamwidth is preferably nearly constant in azimuth. Such antennas provide equal signal coverage about them which is useful in certain wireless applications. However it is difficult to maintain a desired broad frequency bandwidth and also provide an omni-directional beamwidth.


Accordingly a need exists for an antenna design which expands the useful frequency bandwidth of an antenna element while providing nearly uniform omni-directional radiation pattern.


SUMMARY OF THE INVENTION

In a first aspect the present invention provides n omni-directional antenna comprising a first radiating element and a second radiating element oriented in generally opposite directions, a first parasitic radiating element configured between the first, and second radiating elements and spaced apart therefrom in a first direction, and a second parasitic radiating element configured between the first and second radiating elements and spaced apart therefrom in a second direction generally opposite to the first direction.


In a preferred embodiment the omni-directional antenna further comprises a generally planar dielectric support structure. The first radiating element and second radiating element are planar dipole radiating elements configured on the planar dielectric support structure. The first and second parasitic radiating elements are configured on opposite sides of the dielectric support structure and spaced apart therefrom. The first and second parasitic radiating elements are preferably spaced an equidistance from respective opposite sides of the dielectric support structure. The first and second parasitic radiating elements may comprise elongated conductive rods. In one embodiment the omni-directional antenna may further comprise third and fourth parasitic radiating elements, configured between the first and second radiating elements and spaced apart therefrom in the first and second directions, respectively. In such an embodiment, the first, second, third and fourth parasitic radiating elements may comprise generally parallel elongated conductive rods. More specifically, in a coordinate system defined such that the first and second directions correspond to opposite directions along a y axis, the first radiating element and second radiating element are oriented in opposite directions along an x axis, and a z axis is defined perpendicular to the x y plane, the generally parallel elongated conductive rods have a length dimension extending in the z direction. The first and third and second and fourth parasitic radiating elements are then preferably aligned along the y direction and symmetrically configured on opposite sides of the x axis. In an alternative configuration the first and third and second and fourth parasitic radiating elements may be respectively aligned along directions parallel to the x axis and symmetrically configured on opposite aides of the x axis.


In another aspect the present invention provides an omni-directional antenna structure comprising a radome, a planar dielectric substrate configured within the radome and having first and second dipole radiating elements configured thereon symmetrically disposed about a feed line, first and second conductive elements configured within the radome symmetrically arranged on opposite sides of the planer dielectric substrate and spaced, apart therefrom and a support structure holding the first and second conductive elements in that configuration.


In a preferred embodiment of the omni-directional antenna structure the first and second conductive elements may comprise conductive rods extending parallel to the feed line. The support structure may comprise first and second nonconductive support plates mounted within the radome and coupled to opposite ends of the conductive rods. The omni-directional antenna structure may further comprise third and fourth conductive elements configured within the radome and symmetrically arranged on opposite sides of the planar dielectric substrate and spaced apart therefrom.


In another aspect the present invention provides an omni-directional antenna structure comprising a radome, a planar dielectric substrate configured within the radome and having first and second dipole radiating elements configured thereon symmetrically disposed about a feed line and oriented to provide a radiation beam pattern in opposite azimuth directions, and means configured within the radome for parasitically augmenting the radiation beam pattern to provide substantially omni-directional azimuth radiation pattern.


In a preferred embodiment of the omni-directional antenna structure the means for parasitically augmenting the radiation beam pattern comprises symmetrically configured conductive elements on opposite sides of the dielectric substrate. As one example, the antenna operational radio frequency (RF) may be approximately 3.30 GHz to 3.80 GHz. The conductive elements may be spaced apart from the dielectric substrate by a distance of about 360 to 440 mils. The conductive elements may comprise conductive rods of diameter between about 160 to 250 mils. The conductive elements may comprise dual rods configured on each side of the dielectric substrate.


Further features and advantages of the present invention will be appreciated from the following detailed description of the invention.





BRIEF DESCRIPTION OF THE DRAWINGS


FIG. 1 is a top planar view and selected planar cross-sections of an omni-directional antenna element in accordance with the invention.



FIG. 2 is an XY cross sectional view of an antenna element in accordance with the invention utilizing a dual tube configuration, mounted inside a radome tube.



FIG. 2A is an XY cross sectional view of an antenna element in accordance with the invention utilizing a quad horizontal tube configuration, mounted inside a radome tube.



FIG. 2B is an XY cross sectional view of an antenna element in accordance with the invention utilizing quad vertical tube configuration, mounted inside a radome tube.



FIG. 3 is a left sided perspective view of an antenna element in accordance with the invention.



FIG. 4 is a right sided perspective view of an antenna element in accordance with the invention.



FIG. 4A is a vertically oriented perspective view of an antenna element in accordance with the invention.



FIG. 5 is a graph showing input return loss for a dual 190 mil tube configuration, as a function of spacing (R1 range of 360 to 440 mil) from the dielectric plane surface.



FIG. 6 is a graph showing input return loss for a dual tube configuration, as a function of tube diameter (160 to 250 mil) placed R1=440 mils from the surface of the dielectric plane.



FIG. 7 is a graph showing azimuth gain ripple as a function of a dual (190 mil) tube placement (R1=360 to 560 mils) above the surface of the dielectric plane.





DETAILED DESCRIPTION OF THE INVENTION

One object of the present invention is to provide dielectric based coplanar antenna elements which have broad frequency bandwidth and are easy to fabricate using conventional PCB processes. The present invention may preferably utilize a radiating element structure described in patent application Ser. No. 12/212,533 filed Sep. 17, 2008 and provisional patent application No. 60/994,557 filed Sep. 20, 2007, the disclosures of which are incorporated herein by reference in their entirety. In addition to coplanar radiating elements the present invention preferably takes advantage of pattern augmentation rods positioned in near proximity to the dielectric plane, equidistant to each surface side. To achieve an omni-directional radiation pattern a pair of symmetrically opposing radiating elements are preferably fed by a balanced feed network structure. The balanced feed structure provides equal signal division for each radiating element to achieve a symmetric radiation pattern. Additionally, a broad band balun is used to convert between a balanced feed network and an unbalanced, coaxial feed network.


In carrying out these and other objectives, features, and advantages of the present invention, a broad bandwidth antenna element is provided for use in a wireless network system.


Next a preferred embodiment of the present invention will be described. Reference will be made to the accompanying drawings, which assist in illustrating the various pertinent features of the present invention. In certain instances herein chosen for illustrating the invention, certain terminology is used which will be recognized as being employed for convenience and having no limiting significance. For example, the terms “horizontal”, “vertical”, “upper”, “lower”, “bottom” and “top” refer to the illustrated embodiment in its normal position of use. Some of the components represented in the drawings are not necessarily to scale, emphasis instead being placed upon clearly illustrating the principles of the present invention.



FIG. 1 shows a top (XY planar view) view of a coplanar omni directional antenna element, 100, according to an exemplary implementation, which utilizes a substantially planar dielectric material 12. Additional antenna elements exterior of dielectric plate 12 are omitted from this figure for clarity and will be described later. Two broad bandwidth radiating elements 10a and 10b are disposed symmetrically on each side of dielectric material 12 about the Y axis. Construction of such radiating elements 10a and 10b employs a method which prints or attaches thin metal conductors directly on top 12a and bottom 12b sides of a dielectric substrate 12, such as a PCB (printed circuit board). The square dielectric plate 12 is dimensioned to fit all necessary conductors in a manner which is not only compact but which provides a desired radiation pattern, frequency response and bandwidth over the desired frequency. In an exemplary embodiment the desired radio frequency (RF) is approximately 3.30 GHz to 3.80 GHz while coplanar omni-directional antenna element, 100 is constructed utilizing commercially available PCB material manufactured by Taconic, specifically Taconic RF-35, with εr=3.5 and thickness=30 mills. Alternative dielectric substrates (PCB material) 12 are possible provided that properties of such substrate are chosen in a manner to be compatible with commonly available PCB processes; alternatively metal conductor attachment to the dielectric substrate can be achieved through various means known to the skilled in the art.


As shown, omni-directional antenna element 100 is provided with an upper dielectric 12a (12b is a lower side of a dielectric) side RF unbalanced input-output port 106. Input RF signals are further coupled over balun 104 structure (details are omitted). A balun is an electromagnetic structure for interfacing balanced impedance device or circuit, such as an antenna, with an unbalanced impedance, such as coaxial cable or microstrip line. In its common use a balanced signal comprises a pair of symmetrical signals which are equal in magnitude and opposite in phase (180 degrees). In contrast, an unbalanced impedance may be characterized by a single conductor for supporting the propagation of unbalanced (i.e., asymmetrical) signals relative to a second conductor (i.e., ground). Numerous balun structures are known to those skilled in the art for converting the unbalanced to balanced signals and vice versa.


Thereafter, balanced RF signals are coupled onto 50 Ohm balanced impedance transmission line 102 (bottom side transmission line 112 is not visible) which is connected to 50 to 25 Ohm balanced ¼λ transformer comprising co-aligned bi-planar transmission lines 108, 118. Conventional implementation of a ¼λ transformer can readily utilize 35.3 Ohm characteristic impedance microstrip lines. Radiating elements' 10a, 10b characteristic load impedance is not the same as a conventional (73 Ohms) dipole known in the art. Instead, load impedance function of several variables such as parasitic coupling element spacing (30, 28) and mutual overlap o1, pattern augmentation rods 206, 208 positioning and diameter as well as several other variables to a lesser degree. Utilizing commercially available computer software (HFSS), radiating element 10a and 10b are optimized as a unit to provide an omni-directional radiation pattern as well as suitable load impedance (50 Ohms). Having 50 ohm load impedance greatly simplifies the feeding (110a-120a and 110b-120b) structure for each radiating element 10a, 10b. In a preferred implementation 50 Ohm balanced microstrip line (110a-120a and 110b-120b) pairs are used to feed respective radiating elements (10a, 10b) from the end of the ¼λ transformer 108, 118 from a common node (not labeled). The lengths of the 50 Ohm balanced microstrip line (110a-120a and 110b-120b) pairs also are, optimized to provide an omni-directional pattern among other parameters. Alternative feed implementations are possible that may provide additional benefits or circuit simplification.


A detailed description of a preferred embodiment of radiating element 10 can be found in patent application Ser. No. 12/212,533 filed Sep. 17, 2008 and provisional patent application No. 60/994,557 filed Sep. 20, 2007 the disclosures of which are incorporated herein by reference in their entirety. This embodiment provides a broadband capability as described in the above applications. Alternative designs for radiating elements 10 can be employed, however, especially where broad bandwidth is not important and a variety of radiating element designs will be possible as known to those skilled in the art.


With reference to FIG. 2 a radome 200 with rod support(s) 210 is presented in addition to (along Y Axis) ZX planar view of dielectric plate 12. Rod support(s) 210 may be a suitable lightweight nonconductive material, for example such as Teflon or an RF transparent plastic. Supports 210 may have a planar shape as shown or other suitable shape to fit within radome 200. Proximate to, and running along longitudinal axis of the dielectric plate 12 are radiation pattern augmentation rods 206 and 208, positioned above and below top 12a and bottom 12b surface of dielectric plate 12 and attached to supports 210. The two radiation pattern augmentation rods 206 and 208 are symmetrical about the x-axis, and disposed equidistantly R1 from the surface of the dielectric. Preferably, the two radiation pattern augmentation rods 206 and 208 are constructed using conductive material, such as aluminum and the like. For additional weight and cost savings plastic rods with metallic surface treatment can be utilized, while metal based rods can utilize a thin wall metal tube or an extrusion instead of solid metal rod material. Therefore, the term rod as used herein covers all such variations and is not limited to a solid or a precisely cylindrical shape.


It will be appreciated by those skilled in the art that the conductive rods 206, 208 parasitically couple to the electromagnetic field of radiating elements 10a, 10b and have currents induced on their surface thereby becoming parasitic radiating elements. This provides an augmentation of the beam pattern from that of the elements 10 alone. More specifically, absent the radiation pattern augmentation rods 206 and 208 the beam pattern of radiating elements 10a, 10b would be bidirectional in nature, directed along the +/−x direction of FIG. 2. With the addition of the radiation pattern augmentation rods 206 and 208 the beam pattern becomes substantially omni-directional. Since the radiation pattern augmentation rods 206 and 208 operate as parasitic elements no feed network is required to supply the rods. Also, a ground plane is not:necessary. As a result the omni-directional antenna can be light weight and inexpensive relative to other omni-directional antenna designs.


Performance of the omni-directional antenna 100 element equipped with a pair of radiation pattern augmentation rods 206 and 208 can be further modified which may provide improved performance in some applications. A single rod, can be replaced with pair of similarly constructed rods on each side of dielectric plate 12 to form a quad rod implementation. Quad rod implementations can be oriented horizontally (FIG. 2A) or vertically (FIG. 2B). It is also possible to replace a single pairing of rods (206a, b and 208a, b) with a single piece extrusion or the like and variations in shape may be provided from the rod or tube illustrated.


Preferred dimensions for a 3.30 GHz to 3.80 GHz embodiment with 50 impedance source 106 impedance are as follows.
















Element
Dimension
Min (mills)
Max (mills)
Typical (mills)



















24, 26
W1
86
90
88


24, 26
L1
66
67
66.4


28, 30
W2
105
120
112


28, 30
L2
570
580
576


30 <−> 26
s1
90
94
92


28 <−>30
O1
252
264
258


110, 120
W3
86
90
88


110, 120
L3
540
550
544


108, 118
W4
135
139
137


108, 118
L4
475
485
480


206, 208
R1
400
540
440


206, 208
d1
150
200
190


206a-b, 208a-b
R2
460
560
520


206a-b, 208a-b
H1
190
240
200


206a-b, 208a-b
d2
150
200
190


206a-b, 208a-b
R3
340
400
360


206a-b, 208a-b
V1
80
140
100


206a-b, 208a-b
d3
60
120
100









Results employing exemplary parameters were obtained. FIG. 5 is a graph showing input return loss for a dual 190 mil tube configuration, as a function of spacing (R1 range 360 to 440 mil) from the dielectric plane surface. FIG. 6 is a graph showing input return loss for a dual tube configuration, as a function of tube diameter (160 to 25 mil) placed R1=440 mils from the surface of the dielectric plane. FIG. 7 is a graph showing azimuth gain ripple as a function of a dual (190 mil) tube placement (R1=360 to 560 mils) above the surface of the dielectric plane.


The present invention has been described primarily in solving the aforementioned problems relating to expanding useful frequency bandwidth of a coplanar antenna element while providing a nearly uniform omni-directional radiation pattern. Furthermore, the description is not intended to limit the invention to the form disclosed herein. Accordingly, variants and modifications consistent with the following teachings, and skill and knowledge of the relevant art, are within the scope of the present invention. The embodiments described herein are further intended to explain modes known for practicing the invention disclosed herewith and to enable others skilled in the art to utilize the invention in equivalent, or alternative embodiments and with various modifications considered necessary by the particular application(s) or use(s) of the present invention.

Claims
  • 1. An antenna structure comprising: a planar substrate comprising a dipole antenna;a first parasitic element separated from, and extending parallel to, a first side of the substrate by a first distance, and a second parasitic element separated from, and extending parallel to, from the first side of the substrate by a second distance; anda third parasitic element separated from, and extending parallel to, a second side of the substrate by a third distance, and a fourth parasitic element separated from, and extending parallel to, the second side of the substrate by a fourth distance,wherein the dipole antenna and the parasitic elements are configured for omni-directional radiation, andwherein the first parasitic element and the fourth parasitic element are symmetrically arranged opposite each other relative to the substrate, andwherein the second parasitic element and the third parasitic element are symmetrically arranged opposite each other relative to the substrate.
  • 2. The antenna structure of claim 1 wherein the dipole antenna is printed on the substrate.
  • 3. The antenna structure of claim 1 wherein the first and second distances and the third and fourth distances are selected for omnidirectional radiation.
  • 4. The antenna structure of claim 1 wherein the first and fourth parasitic elements are substantially the same length and the second and third parasitic elements are substantially the same length.
  • 5. The antenna structure of claim 2 wherein the first distance is less than the second distance and the fourth distance is less than the third distance.
  • 6. The antenna structure of claim 1 wherein the dipole antenna comprises a first radiating element arranged on the first side of the substrate and a second radiating element arranged on the second side of the substrate.
  • 7. The antenna structure of claim 1 wherein the four parasitic elements are arranged at the same height relative to the dipole antenna.
  • 8. The antenna structure of claim 1 wherein an antenna operational frequency is within the frequency band of approximately 3.30 GHz to 3.80 GHz.
  • 9. The antenna structure of claim 1wherein the first parasitic element and the fourth parasitic element are symmetrically arranged directly opposite each other relative to the substrate,wherein the second parasitic element and the third parasitic element are symmetrically arranged directly opposite each other relative to the substrate.
  • 10. A radio frequency base station comprising: a substrate comprising at least one antenna;a first parasitic element separated from, and extending parallel to, a first side of the substrate by a first distance, and a second parasitic element separated from, and extending parallel to, the first side of the substrate by a second distance; anda third parasitic element separated from, and extending parallel to, a second side of the substrate by a third distance, and a fourth parasitic element separated from, and extending parallel to, the second side of the substrate by a fourth distance,wherein the at least one antenna and the parasitic elements are configured for omni-directional radiation, andwherein the first parasitic element and the fourth parasitic element are symmetrically arranged opposite each other relative to the substrate,wherein the second parasitic element and the third parasitic element are symmetrically arranged opposite each other relative to the substrate,wherein the second and third parasitic elements are each spaced substantially the same distance from the substrate, andwherein the first and fourth parasitic elements are each spaced substantially the same distance from the substrate.
  • 11. The radio frequency base station of claim 10 wherein the at least one antenna is at least one dipole antenna printed on the substrate.
  • 12. The radio frequency base station of claim 10 wherein the first and second distances and the third and fourth distances are selected for omnidirectional radiation.
  • 13. The radio frequency base station of claim 10 wherein the first distance is less than the second distance and the fourth distance is less than the third distance.
  • 14. The radio frequency base station of claim 10 wherein the first parasitic element and the fourth parasitic element are located at the same height relative to the antenna.
  • 15. The radio frequency base station of claim 10 wherein the second parasitic element and the third parasitic element are located at the same height relative to the antenna.
  • 16. The radio frequency base station of claim 11 wherein the at least one dipole antenna comprises a first radiating element arranged on the first side of the substrate and a second radiating element arranged on the second side of the substrate.
  • 17. The radio frequency base station of claim 10 wherein an antenna operational frequency is within the frequency band of approximately 3.30 GHz to 3.80 GHz.
  • 18. The radio frequency base station of claim 10 wherein the substrate, the first and second parasitic elements and the third and fourth parasitic elements are surrounded by a radome.
  • 19. The radio frequency base station of claim 10wherein the first parasitic element and the fourth parasitic element are symmetrically arranged directly opposite each other relative to the substrate,wherein the second parasitic element and the third parasitic element are symmetrically arranged directly opposite each other relative to the substrate.
  • 20. A radio frequency device comprising: an antenna structure including a substrate having configured thereon an antenna;a first parasitic element separated from, and extending parallel to, a first side of the substrate by a first distance, and a second parasitic element separated from, and extending parallel to, the first side of the substrate by a second distance; anda third parasitic element separated from, and extending parallel to, the second side of the substrate by a third distance and a fourth parasitic element separated from, and extending parallel to, the second side of the substrate by a fourth distance,wherein the first parasitic element and the fourth parasitic element are symmetrically arranged opposite each other relative to the substrate,wherein the second parasitic element and the third parasitic element are symmetrically arranged opposite each other relative to the substrate,wherein the first distance is substantially equal to the fourth distance and the second distance is substantially equal to the third distance,wherein the second and third parasitic elements are each spaced substantially the same distance from the substrate, andwherein the first parasitic element and the fourth parasitic element are substantially the same shape.
  • 21. The radio frequency device of claim 20 wherein the at least one antenna and the parasitic elements are configured for omni-directional radiation.
  • 22. The radio frequency device of claim 20 wherein the first parasitic element and the fourth parasitic elements are arranged at substantially the same height with respect to the substrate.
  • 23. The radio frequency device of claim 20 wherein the at least one antenna is at least one dipole antenna printed on the substrate.
  • 24. The radio frequency device of claim 20 wherein the second parasitic element and the third parasitic element are arranged at substantially the same height with respect to the substrate.
  • 25. The radio frequency device of claim 20wherein the first parasitic element and the fourth parasitic element are symmetrically arranged directly opposite each other relative to the substrate,wherein the second parasitic element and the third parasitic element are symmetrically arranged directly opposite each other relative to the substrate.
RELATED APPLICATION INFORMATION

The present application is a continuation application of U.S. patent application Ser. No. 15/175,448 filed Jun. 7, 2016, which is a continuation application of U.S. patent application Ser. No. 13/470,064 filed May 11, 2012, which is a continuation application of U.S. patent application Ser. No. 12/287,661 filed Oct. 10, 2008, which claims priority under 35 U.S.C. Section 119(e) to U.S. Provisional Patent Application No. 60/998,662 filed Oct. 12, 2007, the disclosures of which are incorporated herein by reference in their entirety.

US Referenced Citations (36)
Number Name Date Kind
4812855 Coe et al. Mar 1989 A
6067053 Runyon et al. May 2000 A
6407719 Ohira Jun 2002 B1
6670923 Kadambi et al. Dec 2003 B1
6741219 Shor May 2004 B2
6747605 Lebaric et al. Jun 2004 B2
6859176 Choi Feb 2005 B2
7132989 Poilasne Nov 2006 B1
7215285 Song et al. May 2007 B2
7224315 Tsai et al. May 2007 B2
7274339 Wu et al. Sep 2007 B2
7298228 Sievenpiper Nov 2007 B2
7391386 Sawaya Jun 2008 B2
7646343 Shtrom Jan 2010 B2
7696943 Chiang Apr 2010 B2
7764245 Loyet Jul 2010 B2
7986280 Semonov Jul 2011 B2
8199064 Semonov et al. Jun 2012 B2
8319686 Park Nov 2012 B2
8405567 Park Mar 2013 B2
9368861 Semonov et al. Jun 2016 B2
20030054855 Kojola et al. Mar 2003 A1
20030218571 Yoon et al. Nov 2003 A1
20030231138 Weinstein Dec 2003 A1
20040061652 Ishihara et al. Apr 2004 A1
20040090371 Rossman May 2004 A1
20040125031 Jo et al. Jul 2004 A1
20040207562 Schadler Oct 2004 A1
20060232492 Sawatani Oct 2006 A1
20060290573 Puente Baliarda et al. Dec 2006 A1
20070109198 Saban et al. May 2007 A1
20080169993 Matsuzawa et al. Jul 2008 A1
20090079653 Semonov et al. Mar 2009 A1
20090096698 Semonov et al. Apr 2009 A1
20120218168 Semonov et al. Aug 2012 A1
20170012360 Semonov et al. Jan 2017 A1
Foreign Referenced Citations (2)
Number Date Country
4155359 Sep 2008 JP
WO2009048614 Apr 2009 WO
Non-Patent Literature Citations (24)
Entry
U.S. Appl. No. 12/287,661, U.S. Pat. No. 8,199,064, filed Oct. 10, 2008, Omni Directional Broadband Coplanar Antenna Element.
U.S. Appl. No. 13/470,064, U.S. Pat. No. 9,368,861, filed May 11, 2012, Omni Directional Broadband Coplanar Antenna Element.
U.S. Appl. No. 15/175,448, filed Jun. 7, 2016, Omni Directional Broadband Coplanar Antenna Element.
“U.S. Appl. No. 12/212,533, Non Final Office Action dated Apr. 28, 2011”, 6 pgs.
“U.S. Appl. No. 12/287,661, Non Final Office Action dated Jan. 19, 2011”, 11 pgs.
“U.S. Appl. No. 12/287,661, Non Final Office Action dated Aug. 3, 2011”, 12 pgs.
“U.S. Appl. No. 12/287,661, Notice of Allowance dated Feb. 15, 2012”, 5 pgs.
“U.S. Appl. No. 12/287,661, Response filed Feb. 2, 2012 to Non Final Office Action dated Aug. 3, 2011”, 4 pgs.
“U.S. Appl. No. 12/287,661, Response filed May 23, 2011 to Non Final Office Action dated Jan. 19, 2011”, 10 pgs.
“U.S. Appl. No. 13/470,064, Advisory Action dated Apr. 29, 2015”, 3 pgs.
“U.S. Appl. No. 13/470,064, Final Office Action dated Feb. 20, 2015”, 11 pgs.
“U.S. Appl. No. 13/470,064, Non Final Office Action dated Jul. 31, 2014”, 9 pgs.
“U.S. Appl. No. 13/470,064, Non Final Office Action dated Sep. 4, 2015”, 7 pgs.
“U.S. Appl. No. 13/470,064, Notice of Allowance dated Feb. 12, 2016”, 8 pgs.
“U.S. Appl. No. 13/470,064, Response filed Jun. 22, 2015 to Advisory Action dated Apr. 29, 2015”, 8 pgs.
“U.S. Appl. No. 13/470,064, Response filed Dec. 1, 2014 to Non Final Office Action dated Jul. 31, 2014”, 8 pgs.
“U.S. Appl. No. 13/470,064, Response Filed Dec. 4, 2015 to Non Final Office Action dated Sep. 4, 2015”, 6 pgs.
“U.S. Appl. No. 13/470,064, Response filed Apr. 20, 2015 to Final Office Action dated Feb. 20, 2015”, 8 pgs.
“U.S. Appl. No. 15/175,448, Non Final Office Action dated Dec. 30, 2016”, 11 pgs.
“International Application Serial No. PCT/US2008/010851, International Search Report dated Nov. 25, 2008”, 1 pg.
“International Application Serial No. PCT/US2008/010851, Written Opinion dated Nov. 25, 2008”, 7 pgs.
“International Application Serial No. PCT/US2008/011655, International Preliminary Report on Patentability dated Nov. 11, 2008”, 7 pgs.
“International Application Serial No. PCT/US2008/011655, International Search Report dated Dec. 10, 2008”, 1 pg.
“International Application Serial No. PCT/US2008/011655, Written Opinion dated Dec. 10, 2008”, 5 pgs.
Related Publications (1)
Number Date Country
20170179578 A1 Jun 2017 US
Provisional Applications (1)
Number Date Country
60998662 Oct 2007 US
Continuations (3)
Number Date Country
Parent 15175448 Jun 2016 US
Child 15451012 US
Parent 13470064 May 2012 US
Child 15175448 US
Parent 12287661 Oct 2008 US
Child 13470064 US