US3811127A - Antenna for airborne satellite communications - Google Patents

Antenna for airborne satellite communications Download PDF

Info

Publication number
US3811127A
US3811127A US00279590A US27959072A US3811127A US 3811127 A US3811127 A US 3811127A US 00279590 A US00279590 A US 00279590A US 27959072 A US27959072 A US 27959072A US 3811127 A US3811127 A US 3811127A
Authority
US
United States
Prior art keywords
antenna
upper edge
capacitive loading
edge portion
radiating elements
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US00279590A
Inventor
L Griffee
M Anderson
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Collins Radio Co
Original Assignee
Collins Radio Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Collins Radio Co filed Critical Collins Radio Co
Priority to US00279590A priority Critical patent/US3811127A/en
Application granted granted Critical
Publication of US3811127A publication Critical patent/US3811127A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q21/00—Antenna arrays or systems
    • H01Q21/24—Combinations of antenna units polarised in different directions for transmitting or receiving circularly and elliptically polarised waves or waves linearly polarised in any direction
    • H01Q21/26—Turnstile or like antennas comprising arrangements of three or more elongated elements disposed radially and symmetrically in a horizontal plane about a common centre
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00—Details of, or arrangements associated with, antennas
    • H01Q1/27—Adaptation for use in or on movable bodies
    • H01Q1/28—Adaptation for use in or on aircraft, missiles, satellites, or balloons
    • H01Q1/282—Modifying the aerodynamic properties of the vehicle, e.g. projecting type aerials
    • H01Q1/283—Blade, stub antennas
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q9/00—Electrically-short antennas having dimensions not more than twice the operating wavelength and consisting of conductive active radiating elements
    • H01Q9/04—Resonant antennas
    • H01Q9/30—Resonant antennas with feed to end of elongated active element, e.g. unipole
    • H01Q9/42—Resonant antennas with feed to end of elongated active element, e.g. unipole with folded element, the folded parts being spaced apart a small fraction of the operating wavelength
    • H01Q9/43—Scimitar antennas

Definitions

  • PATENTEB MAY 1 41974 SHEET 2 [IF 2 90 HYBRID ANTENNA FOR AIRBORNE SATELLITE COMMUNICATIONS This invention relates generally to radio antennas, and more particularly to antennas operable in the VHF and UHF ranges for airborne satellite communications.
  • an object of the present invention is an improved VHF/UHF airborne antenna.
  • Another object of the invention is an improved airborne antenna for satellite communication which is operable over a wide frequency range.
  • Yet anotherobject of the invention is a broadband VHF/UHF airborne antenna for satellite communication which is physically compatible with fuselage mounting.
  • Features of the invention include a plurality of radiating elements each comprising a vertical member having a generally arcuate upper edge portion and a capacitive loading portion defining at least approximately a spherical section which is attached to said vertical member along the arcuate upper edge.
  • Four of such radiating elements are supportably positioned orthogonally whereby said spherical sections define at least approximately a larger spherical section.
  • Feed means is provided for feeding said radiating element in phase quadrature.
  • FIG. 1 and FIG. 2 illustrate in perspective prior art antennas used for airborne satellite communication
  • FIG. 3 is a perspective view of an antenna in accordance with the present invention. 7
  • FIG. 4 is an exploded view of one radiating element of the antenna of FIG. 3;
  • FIG. 5 is a plan view of feed means for phase quadrature exciting the antenna of FIG. 3.
  • FIG. 1 and FIG. 2 illustrate in perspective prior art antennas used for airborne satellite communication.
  • FIG. 1 is a turnstile antenna including four orthogonally oriented vertical elements l0, 12, 14, and 1 6 which are supported on support base 18.
  • the turnstile antenna When fed in phase quadrature, the turnstile antenna exhibits a hemispherical radiation pattern with the radiation emanating from each of the vertical radiating elements.
  • Such an antenna has been satisfactorily employed for relatively narrow bands such as, for example, 240-250 MHz.
  • 240-400 MHz for the turnstile antenna to operate satisfactorily over a broader frequency range, 240-400 MHz, for example, the maximum vertical height for each radiating element must be increased from about five inches to over eight inches.
  • the antenna must be mounted in the upper fuselage and enclosed by radome, it will be appreciated that such a broadband antenna is too large for satisfactory mounting on the modern jet aircraft.
  • the prior art crossed-slot antenna of FIG. 2 presents a minimum height profile when mounted to the fuselage of an aircraft, and a hemispherical pattern is generated across the slots between radiating element 20, 22, 24, and 26.
  • an operationally satisfactory broadband crossed-slot antenna becomes too large in horizontal displacement for fuselage mounting.
  • FIG. 3 one embodiment of an antenna in accordance with applicants invention is illustrated in perspective and-includes radiating elements30, 32, 34, and 36 which are orthogonally mounted on base plate 38. These elements are grounded at the outer corners and are shunt fed in phase quadrature approximately halfway toward the center of the antenna by means of a balanced feed system such as,'for example, a combination coaxial cable and stripline.
  • a balanced feed system such as,'for example, a combination coaxial cable and stripline.
  • each radiating element comprises a vertical blade portion 40 which is grounded at the external corner 42 and is fed by coaxial means at corner 44, corner 42 being mounted to the support plate 38 of FIG. 3 and corner 44 being attached to metal conductor 68 and of FIG. 5.
  • the upper edge 46 of blade 40 comprises straight lines which together approximate an arcuate curve which receives by welding or other suitable means a capacitive loading portion comprising members 48 and 50.
  • the capacitive loading portion comprising elements 48 and 50 define at least approximately a spherical section which is attached to the upper arcuate edge of the vertical blade member and along with the other capacitive loading portions of the radiating elements cooperatively define at least approximately a larger spherical section.
  • the antenna of FIG. 3 and FIG. 4 when fed in phase quadrature exhibits a hemispherical radiation pattern which is radiated cross the gaps between the radiating elements 32, 34, 36, and 38, as seen in FIG. 3 and emanating outwardly from the vertical blade member 40 as illustrated in FIG-4.
  • the capacitive loading provided by the spherical sections increases the effective height of each blade member without the necessity for physically enlarging the height.
  • This advantage provided by the present invention allows the broadband antenna to be mounted on the upper fuselage of an aircraft within the physical constraints allowed therefor.
  • coaxial line 60 connects hybrid 62 to a coaxial line positioned on stripline 64 with the outer conductor of coaxial line 64 electrically connected to the metal conductor 68 of the stripline.
  • a like stripline 70 is positioned in alignment with stripline 66 with a gap 72 separating the two striplines.
  • Coaxial line 64 terminates at gap 72 and the center conductor thereof is electrically connected to the metal conductor 74 of stripline 70, thereby causing a 180 phase reversal between the signal in stripline 66 and the signal in stripline 70.
  • Diametrically opposed blades 78 and 80 are mounted above striplines 66 and 70, respectively, and are electrically interconnected therewith whereby blade 78 is excited at the phase, for example, while blade 80 is energized at 180 phase. It will be noted that blades 78 and 80 contact the two striplines at points 79 and 81 away from gap 72. The exact point at which the blade contacts the stripline is a variable parameter used for impedance matching of the blade to a stripline. Similar striplines, not shown, are employed with the 90 output from hybrid 62 to feed the other pair of radiating elements of the antenna.
  • An antenna in accordance with the present invention provides hemispherical coverage over a wide frequency range while being compatible with the physical constraints requisite in mounting in the fuselage'of an aircraft. While the invention has been described with reference to a specific embodiment, the description is illustrative of the invention and is not to be construed as limiting the invention. Various modifications and changes may occur to those skilled in the art without departing from the spirit and scope of the invention as defined by the appended claims.
  • a broadband VHF-UHF airborne antenna for satellite communication comprising four radiating elements, a support base, said radiating elements mounted orthogonally on said support base, each of said radiating elements including a vertical member having an upper edge portion and a capacitive loading portion defining at least approximately a spherical section, said capacitive loading portion being attached to said vertical member along said upper edge portion, said capacitive loading portions of said radiating elements cooperatively defining a larger, at least approximately spherical section, and feed means for electrically feeding said upper edge portion, a generally triangularly shaped capacitive loading portion defining at' least a section of a spherical surface, and means for attaching said capacitive loading portion to said vertical member along said upper edge portion.

Landscapes

  • Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Fluid Mechanics (AREA)
  • Astronomy & Astrophysics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Physics & Mathematics (AREA)
  • Variable-Direction Aerials And Aerial Arrays (AREA)
  • Waveguide Aerials (AREA)

Abstract

A broadband VHF/UHF antenna exhibiting a hemispherical radiation pattern comprising four orthogonally positioned radiating elements and means for feeding the elements in phase quadrature. Each element includes a vertical blade portion and a capacitive loading section attached to the upper edge of the blade portion. The capacitive loading portions define at least approximately a spherical section.

Description

United States Patent 1191 Griffee et al.
[ ANTENNA FOR AIRBORNE SATELLITE COMMUNICATIONS [75] Inventors: Leslie V. Griffee, Dallas; Mardis V.
Anderson, Richardson, both of Tex.
[73] Assignee: Collins Radio Company, Dallas,
Tex.
[22] Filed: Aug. 10, 1972 21 Appl. No.2 279,590
[52] U.S. Cl 343/705, 343/770, 343/797, 343/846 51 1111.01. noi l/28 [58] Field of Search 343/770, 771, 895, 705,
[5 6] References Cited UNITED STATES PATENTS 3,366,963 1 1968 Coff ..343/s95 1111 3,811,127 1451 May 14, 1974 3,015,101 12/1961 Turner et al 343/895 3,641,578 2/1972 Spanos et al..... 343/773 3,701,157 10/1972 Uhrig 343/708 Primary ExaminerEli Lieberman [5 7] ABSTRACT A broadband VHF/UHF antenna exhibiting a hemispherical radiation pattern comprising four orthogonally positioned radiating elements and means for feeding the. elements in' phase quadrature. Each element includes a vertical blade portion and a capacitive loading section attached to the upper edge of the blade portion. The capacitive loading portions define at least approximately a spherical section.
6 Claims,.5 Drawing Figures PATENTEDMAY141974 3.81 1,127
SHEET 1 [IF 2 PRIOR ART 1 10.1 FIG. 2
PATENTEB MAY 1 41974 SHEET 2 [IF 2 90 HYBRID ANTENNA FOR AIRBORNE SATELLITE COMMUNICATIONS This invention relates generally to radio antennas, and more particularly to antennas operable in the VHF and UHF ranges for airborne satellite communications.
The use of satellite communication for aircraft applications has become a reality in governmental and commercial use. Typically, such communication requires an aircraft antenna mounted on the upper fuselage, exhibiting a hemispherical coverage pattern, and operable in the VHF and UHF ranges. Conventional antennas are available for such use, but these antennas are limited in frequency bandwidth due to practical design considerations.
Accordingly, an object of the present invention is an improved VHF/UHF airborne antenna.
Another object of the invention is an improved airborne antenna for satellite communication which is operable over a wide frequency range.
Yet anotherobject of the invention is a broadband VHF/UHF airborne antenna for satellite communication which is physically compatible with fuselage mounting.
Features of the invention include a plurality of radiating elements each comprising a vertical member having a generally arcuate upper edge portion and a capacitive loading portion defining at least approximately a spherical section which is attached to said vertical member along the arcuate upper edge. Four of such radiating elements are supportably positioned orthogonally whereby said spherical sections define at least approximately a larger spherical section. Feed means is provided for feeding said radiating element in phase quadrature.
These and other objects and features of the invention will be more readily apparent from the following detailed description and appended claims when taken with the drawing, in which:
FIG. 1 and FIG. 2 illustrate in perspective prior art antennas used for airborne satellite communication;
FIG. 3 is a perspective view of an antenna in accordance with the present invention; 7
FIG. 4 is an exploded view of one radiating element of the antenna of FIG. 3; and
FIG. 5 is a plan view of feed means for phase quadrature exciting the antenna of FIG. 3.
Referring now to the drawing, FIG. 1 and FIG. 2 illustrate in perspective prior art antennas used for airborne satellite communication. FIG. 1 is a turnstile antenna including four orthogonally oriented vertical elements l0, 12, 14, and 1 6 which are supported on support base 18. When fed in phase quadrature, the turnstile antenna exhibits a hemispherical radiation pattern with the radiation emanating from each of the vertical radiating elements. Such an antenna has been satisfactorily employed for relatively narrow bands such as, for example, 240-250 MHz. However, for the turnstile antenna to operate satisfactorily over a broader frequency range, 240-400 MHz, for example, the maximum vertical height for each radiating element must be increased from about five inches to over eight inches. Considering that the antenna must be mounted in the upper fuselage and enclosed by radome, it will be appreciated that such a broadband antenna is too large for satisfactory mounting on the modern jet aircraft.
The prior art crossed-slot antenna of FIG. 2 presents a minimum height profile when mounted to the fuselage of an aircraft, and a hemispherical pattern is generated across the slots between radiating element 20, 22, 24, and 26. However, an operationally satisfactory broadband crossed-slot antenna becomes too large in horizontal displacement for fuselage mounting.
By combining the radiating features of the turnstile antenna and the crossed array antenna, applicant has provided a broadband VHF/UHF antenna which is within the physical constraints necessary for use in airborne satellite communications. Referring to FIG. 3, one embodiment of an antenna in accordance with applicants invention is illustrated in perspective and-includes radiating elements30, 32, 34, and 36 which are orthogonally mounted on base plate 38. These elements are grounded at the outer corners and are shunt fed in phase quadrature approximately halfway toward the center of the antenna by means of a balanced feed system such as,'for example, a combination coaxial cable and stripline.
As seen in the exploded view in FIG. 4, each radiating element comprises a vertical blade portion 40 which is grounded at the external corner 42 and is fed by coaxial means at corner 44, corner 42 being mounted to the support plate 38 of FIG. 3 and corner 44 being attached to metal conductor 68 and of FIG. 5. The upper edge 46 of blade 40 comprises straight lines which together approximate an arcuate curve which receives by welding or other suitable means a capacitive loading portion comprising members 48 and 50. As seen in FIG. 3, the capacitive loading portion comprising elements 48 and 50 define at least approximately a spherical section which is attached to the upper arcuate edge of the vertical blade member and along with the other capacitive loading portions of the radiating elements cooperatively define at least approximately a larger spherical section. While in this illustrative embodiment the spherical sections are approximated by adjoining planar sections, and the illustrative embodiment is satisfactorily operational, true spherical sections may be employed. Arm 52 attached to blade 40 in FIG. 4 functions solely for additional support to the cantilevered capacitive load element .48.
As indicated above, the antenna of FIG. 3 and FIG. 4 when fed in phase quadrature exhibits a hemispherical radiation pattern which is radiated cross the gaps between the radiating elements 32, 34, 36, and 38, as seen in FIG. 3 and emanating outwardly from the vertical blade member 40 as illustrated in FIG-4. Advantageously, the capacitive loading provided by the spherical sections increases the effective height of each blade member without the necessity for physically enlarging the height. This advantage provided by the present invention allows the broadband antenna to be mounted on the upper fuselage of an aircraft within the physical constraints allowed therefor.
The method of exciting the radiating elements in phase quadrature as illustrated in the plan view of FIG. 5 is conventional and well known in the art. An input signal is applied to a hybrid which provides two output signals at 90 phase separation, as shown. Referring to the 0 phase output, coaxial line 60 connects hybrid 62 to a coaxial line positioned on stripline 64 with the outer conductor of coaxial line 64 electrically connected to the metal conductor 68 of the stripline. A like stripline 70 is positioned in alignment with stripline 66 with a gap 72 separating the two striplines. Coaxial line 64 terminates at gap 72 and the center conductor thereof is electrically connected to the metal conductor 74 of stripline 70, thereby causing a 180 phase reversal between the signal in stripline 66 and the signal in stripline 70.
Diametrically opposed blades 78 and 80 are mounted above striplines 66 and 70, respectively, and are electrically interconnected therewith whereby blade 78 is excited at the phase, for example, while blade 80 is energized at 180 phase. It will be noted that blades 78 and 80 contact the two striplines at points 79 and 81 away from gap 72. The exact point at which the blade contacts the stripline is a variable parameter used for impedance matching of the blade to a stripline. Similar striplines, not shown, are employed with the 90 output from hybrid 62 to feed the other pair of radiating elements of the antenna.
An antenna in accordance with the present invention provides hemispherical coverage over a wide frequency range while being compatible with the physical constraints requisite in mounting in the fuselage'of an aircraft. While the invention has been described with reference to a specific embodiment, the description is illustrative of the invention and is not to be construed as limiting the invention. Various modifications and changes may occur to those skilled in the art without departing from the spirit and scope of the invention as defined by the appended claims.
I claim:
1. A broadband VHF-UHF airborne antenna for satellite communication comprising four radiating elements, a support base, said radiating elements mounted orthogonally on said support base, each of said radiating elements including a vertical member having an upper edge portion and a capacitive loading portion defining at least approximately a spherical section, said capacitive loading portion being attached to said vertical member along said upper edge portion, said capacitive loading portions of said radiating elements cooperatively defining a larger, at least approximately spherical section, and feed means for electrically feeding said upper edge portion, a generally triangularly shaped capacitive loading portion defining at' least a section of a spherical surface, and means for attaching said capacitive loading portion to said vertical member along said upper edge portion.
5. A radiating element as defined in'claim 4 and including feed means attached to said vertical member for energizing said element.
6. A radiating element as defined by claim 4 wherein said upper edge portion is generally arcuate in configuration.

Claims (6)

1. A broadband VHF-UHF airborne antenna for satellite communication comprising four radiating elements, a support base, said radiating elements mounted orthogonally on said support base, each of said radiating elements including a vertical member having an upper edge portion and a capacitive loading portion defining at least approximately a spherical section, said capacitive loading portion being attached to said vertical member along said upper edge portion, said capacitive loading portions of said radiating elements cooperatively defining a larger, at least approximately spherical section, and feed means for electrically feeding said radiating element in phase quadrature.
2. An airborne antenna as defined in claim 1 wherein said feed means comprises a 90* hybrid and stripline means for feeding said radiating elements at 0* , 90* , 180*, and 270* .
3. An airborne antenna as defined in claim 1 wherein said upper edge portion is generally arcuate in configuration.
4. A radiating element for use in a combination turnstile and crossed-slot airborne satellite communication antenna comprising a vertical planar member having an upper edge portion, a generally triangularly shaped capacitive loading portion defining at least a section of a spherical surface, and means for attaching said capacitive loading portion to said vertical member along said upper edge portion.
5. A radiating element as defined in claim 4 and including feed means attached to said vertical member for energizing said element.
6. A radiating element as defined by claim 4 wherein said upper edge portion is generally arcuate in configuration.
US00279590A 1972-08-10 1972-08-10 Antenna for airborne satellite communications Expired - Lifetime US3811127A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US00279590A US3811127A (en) 1972-08-10 1972-08-10 Antenna for airborne satellite communications

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US00279590A US3811127A (en) 1972-08-10 1972-08-10 Antenna for airborne satellite communications

Publications (1)

Publication Number Publication Date
US3811127A true US3811127A (en) 1974-05-14

Family

ID=23069617

Family Applications (1)

Application Number Title Priority Date Filing Date
US00279590A Expired - Lifetime US3811127A (en) 1972-08-10 1972-08-10 Antenna for airborne satellite communications

Country Status (1)

Country Link
US (1) US3811127A (en)

Cited By (35)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3952310A (en) * 1975-02-20 1976-04-20 Rockwell International Corporation Crossed dipole and slot antenna in pyramid form
US3987458A (en) * 1975-07-25 1976-10-19 The United States Of America As Represented By The Secretary Of The Army Low-profile quadrature-plate UHF antenna
US4031539A (en) * 1975-12-11 1977-06-21 Rca Corporation Broadband turnstile antenna
US4475109A (en) * 1982-01-25 1984-10-02 Rockwell International Corporation Inflatable antenna
FR2589634A1 (en) * 1985-10-30 1987-05-07 Applic Rech Electro Ste Wide band omnidirectional VHF antenna for vehicle or aircraft, and in particular for helicopter
US4675685A (en) * 1984-04-17 1987-06-23 Harris Corporation Low VSWR, flush-mounted, adaptive array antenna
US4847627A (en) * 1987-09-08 1989-07-11 Lockheed Corporation Compact wave antenna system
US4878062A (en) * 1988-07-28 1989-10-31 Dayton-Granger, Inc. Global position satellite antenna
EP0431764A2 (en) * 1989-12-04 1991-06-12 Trimble Navigation Antenna with curved dipole elements
US5068671A (en) * 1988-06-24 1991-11-26 The United States Of America As Representated By The Secretary Of The Air Force Orthogonally polarized quadraphase electromagnetic radiator
US5406292A (en) * 1993-06-09 1995-04-11 Ball Corporation Crossed-slot antenna having infinite balun feed means
US5614917A (en) * 1993-10-04 1997-03-25 Ford Motor Company RF sail pumped tuned antenna
US6356235B2 (en) 1999-09-20 2002-03-12 Motorola, Inc. Ground based antenna assembly
US6499027B1 (en) 1998-05-26 2002-12-24 Rockwell Collins, Inc. System software architecture for a passenger entertainment system, method and article of manufacture
US6512496B2 (en) 2001-01-17 2003-01-28 Asi Technology Corporation Expandible antenna
WO2003058762A1 (en) * 2000-01-27 2003-07-17 George Ploussios Crossed bent monopole doublets
US6618016B1 (en) * 2001-02-21 2003-09-09 Bae Systems Aerospace Inc. Eight-element anti-jam aircraft GPS antennas
US6738026B1 (en) * 2002-12-09 2004-05-18 Centurion Wireless Technologies, Inc. Low profile tri-filar, single feed, helical antenna
US6771226B1 (en) * 2003-01-07 2004-08-03 Northrop Grumman Corporation Three-dimensional wideband antenna
US6782392B1 (en) 1998-05-26 2004-08-24 Rockwell Collins, Inc. System software architecture for a passenger entertainment system, method and article of manufacture
US6807538B1 (en) 1998-05-26 2004-10-19 Rockwell Collins Passenger entertainment system, method and article of manufacture employing object oriented system software
US6813777B1 (en) 1998-05-26 2004-11-02 Rockwell Collins Transaction dispatcher for a passenger entertainment system, method and article of manufacture
US6819291B1 (en) 2003-06-02 2004-11-16 Raymond J. Lackey Reduced-size GPS antennas for anti-jam adaptive processing
US6938258B1 (en) 1998-05-26 2005-08-30 Rockwell Collins Message processor for a passenger entertainment system, method and article of manufacture
US7028304B1 (en) 1998-05-26 2006-04-11 Rockwell Collins Virtual line replaceable unit for a passenger entertainment system, method and article of manufacture
WO2008102406A2 (en) * 2007-02-21 2008-08-28 Clarbruno Vedruccio Circular polarization omnidirectional antenna
US7450082B1 (en) 2006-03-31 2008-11-11 Bae Systems Information And Electronics Systems Integration Inc. Small tuned-element GPS antennas for anti-jam adaptive processing
US7450081B1 (en) 2007-03-12 2008-11-11 Sandia Corporation Compact low frequency radio antenna
US20100073239A1 (en) * 2008-09-25 2010-03-25 Topcon Gps, Llc Compact Circularly-Polarized Antenna with Expanded Frequency Bandwidth
US20100103070A1 (en) * 2007-01-24 2010-04-29 Groupe Des Ecoles Des Telecommunications (Enst Bre Ultra wide band antenna or antenna member
US20100277389A1 (en) * 2009-05-01 2010-11-04 Applied Wireless Identification Group, Inc. Compact circular polarized antenna
US8217850B1 (en) * 2008-08-14 2012-07-10 Rockwell Collins, Inc. Adjustable beamwidth aviation antenna with directional and omni-directional radiation modes
US8618998B2 (en) 2009-07-21 2013-12-31 Applied Wireless Identifications Group, Inc. Compact circular polarized antenna with cavity for additional devices
RU2643700C1 (en) * 2016-11-21 2018-02-05 Акционерное общество "Научно-производственное объединение измерительной техники" Turnstile antenna
US11921225B1 (en) * 2019-09-12 2024-03-05 SeeScan, Inc. Antenna systems for circularly polarized radio signals

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3015101A (en) * 1958-10-31 1961-12-26 Edwin M Turner Scimitar antenna
US3366963A (en) * 1964-11-16 1968-01-30 Sperry Rand Corp Reduced-height scimitar antenna
US3641578A (en) * 1970-07-21 1972-02-08 Itt Discone antenna
US3701157A (en) * 1971-06-03 1972-10-24 Us Air Force Helicopter uhf antenna system for satellite communications

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3015101A (en) * 1958-10-31 1961-12-26 Edwin M Turner Scimitar antenna
US3366963A (en) * 1964-11-16 1968-01-30 Sperry Rand Corp Reduced-height scimitar antenna
US3641578A (en) * 1970-07-21 1972-02-08 Itt Discone antenna
US3701157A (en) * 1971-06-03 1972-10-24 Us Air Force Helicopter uhf antenna system for satellite communications

Cited By (42)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3952310A (en) * 1975-02-20 1976-04-20 Rockwell International Corporation Crossed dipole and slot antenna in pyramid form
US3987458A (en) * 1975-07-25 1976-10-19 The United States Of America As Represented By The Secretary Of The Army Low-profile quadrature-plate UHF antenna
US4031539A (en) * 1975-12-11 1977-06-21 Rca Corporation Broadband turnstile antenna
US4475109A (en) * 1982-01-25 1984-10-02 Rockwell International Corporation Inflatable antenna
US4675685A (en) * 1984-04-17 1987-06-23 Harris Corporation Low VSWR, flush-mounted, adaptive array antenna
FR2589634A1 (en) * 1985-10-30 1987-05-07 Applic Rech Electro Ste Wide band omnidirectional VHF antenna for vehicle or aircraft, and in particular for helicopter
US4847627A (en) * 1987-09-08 1989-07-11 Lockheed Corporation Compact wave antenna system
US5068671A (en) * 1988-06-24 1991-11-26 The United States Of America As Representated By The Secretary Of The Air Force Orthogonally polarized quadraphase electromagnetic radiator
US4878062A (en) * 1988-07-28 1989-10-31 Dayton-Granger, Inc. Global position satellite antenna
EP0431764A2 (en) * 1989-12-04 1991-06-12 Trimble Navigation Antenna with curved dipole elements
EP0431764A3 (en) * 1989-12-04 1991-11-13 Trimble Navigation Antenna with curved dipole elements
US5406292A (en) * 1993-06-09 1995-04-11 Ball Corporation Crossed-slot antenna having infinite balun feed means
US5614917A (en) * 1993-10-04 1997-03-25 Ford Motor Company RF sail pumped tuned antenna
US6499027B1 (en) 1998-05-26 2002-12-24 Rockwell Collins, Inc. System software architecture for a passenger entertainment system, method and article of manufacture
US6938258B1 (en) 1998-05-26 2005-08-30 Rockwell Collins Message processor for a passenger entertainment system, method and article of manufacture
US6782392B1 (en) 1998-05-26 2004-08-24 Rockwell Collins, Inc. System software architecture for a passenger entertainment system, method and article of manufacture
US6807538B1 (en) 1998-05-26 2004-10-19 Rockwell Collins Passenger entertainment system, method and article of manufacture employing object oriented system software
US6813777B1 (en) 1998-05-26 2004-11-02 Rockwell Collins Transaction dispatcher for a passenger entertainment system, method and article of manufacture
US7028304B1 (en) 1998-05-26 2006-04-11 Rockwell Collins Virtual line replaceable unit for a passenger entertainment system, method and article of manufacture
US6356235B2 (en) 1999-09-20 2002-03-12 Motorola, Inc. Ground based antenna assembly
WO2003058762A1 (en) * 2000-01-27 2003-07-17 George Ploussios Crossed bent monopole doublets
US6512496B2 (en) 2001-01-17 2003-01-28 Asi Technology Corporation Expandible antenna
US6618016B1 (en) * 2001-02-21 2003-09-09 Bae Systems Aerospace Inc. Eight-element anti-jam aircraft GPS antennas
US6738026B1 (en) * 2002-12-09 2004-05-18 Centurion Wireless Technologies, Inc. Low profile tri-filar, single feed, helical antenna
US20040108964A1 (en) * 2002-12-09 2004-06-10 Mckivergan Patrick Daniel Low profile tri-filar, single feed, helical antenna
US6771226B1 (en) * 2003-01-07 2004-08-03 Northrop Grumman Corporation Three-dimensional wideband antenna
US6819291B1 (en) 2003-06-02 2004-11-16 Raymond J. Lackey Reduced-size GPS antennas for anti-jam adaptive processing
US7450082B1 (en) 2006-03-31 2008-11-11 Bae Systems Information And Electronics Systems Integration Inc. Small tuned-element GPS antennas for anti-jam adaptive processing
US8791872B2 (en) * 2007-01-24 2014-07-29 Groupe des Ecoles des Telecommunications (ENST Bretange) Ultra wide band antenna or antenna member
US20100103070A1 (en) * 2007-01-24 2010-04-29 Groupe Des Ecoles Des Telecommunications (Enst Bre Ultra wide band antenna or antenna member
WO2008102406A2 (en) * 2007-02-21 2008-08-28 Clarbruno Vedruccio Circular polarization omnidirectional antenna
WO2008102406A3 (en) * 2007-02-21 2008-10-23 Clarbruno Vedruccio Circular polarization omnidirectional antenna
US7450081B1 (en) 2007-03-12 2008-11-11 Sandia Corporation Compact low frequency radio antenna
US8217850B1 (en) * 2008-08-14 2012-07-10 Rockwell Collins, Inc. Adjustable beamwidth aviation antenna with directional and omni-directional radiation modes
US8723731B2 (en) 2008-09-25 2014-05-13 Topcon Gps, Llc Compact circularly-polarized antenna with expanded frequency bandwidth
WO2010035104A1 (en) * 2008-09-25 2010-04-01 Topcon Gps, Llc Compact circularly-polarized antenna with expanded frequency bandwidth
US20100073239A1 (en) * 2008-09-25 2010-03-25 Topcon Gps, Llc Compact Circularly-Polarized Antenna with Expanded Frequency Bandwidth
US8106846B2 (en) 2009-05-01 2012-01-31 Applied Wireless Identifications Group, Inc. Compact circular polarized antenna
US20100277389A1 (en) * 2009-05-01 2010-11-04 Applied Wireless Identification Group, Inc. Compact circular polarized antenna
US8618998B2 (en) 2009-07-21 2013-12-31 Applied Wireless Identifications Group, Inc. Compact circular polarized antenna with cavity for additional devices
RU2643700C1 (en) * 2016-11-21 2018-02-05 Акционерное общество "Научно-производственное объединение измерительной техники" Turnstile antenna
US11921225B1 (en) * 2019-09-12 2024-03-05 SeeScan, Inc. Antenna systems for circularly polarized radio signals

Similar Documents

Publication Publication Date Title
US3811127A (en) Antenna for airborne satellite communications
US5420596A (en) Quarter-wave gap-coupled tunable strip antenna
US3945013A (en) Double omni-directional antenna
US4675685A (en) Low VSWR, flush-mounted, adaptive array antenna
US5287116A (en) Array antenna generating circularly polarized waves with a plurality of microstrip antennas
US6759990B2 (en) Compact antenna with circular polarization
US4843400A (en) Aperture coupled circular polarization antenna
EP0716774B1 (en) A folded dipole antenna
EP1301967B1 (en) Nested turnstile antenna
US3813674A (en) Cavity backed dipole-slot antenna for circular polarization
US5703600A (en) Microstrip antenna with a parasitically coupled ground plane
EP1118138B1 (en) Circularly polarized dielectric resonator antenna
US3239838A (en) Dipole antenna mounted in open-faced resonant cavity
US4724443A (en) Patch antenna with a strip line feed element
US3818490A (en) Dual frequency array
US6061031A (en) Method and apparatus for a dual frequency band antenna
WO2002050941A2 (en) Diagonal dual-polarized broadband horn antenna
US5270722A (en) Patch-type microwave antenna
US4060810A (en) Loaded microstrip antenna
US4494120A (en) Two element low profile antenna
GB1388230A (en) Frequency extension of circularly polarized antenna
US4438437A (en) Dual mode blade antenna
US5323168A (en) Dual frequency antenna
US3613098A (en) Electrically small cavity antenna
US4516127A (en) Three element low profile antenna