US2189283A - Beacon aerial - Google Patents
Beacon aerial Download PDFInfo
- Publication number
- US2189283A US2189283A US182675A US18267537A US2189283A US 2189283 A US2189283 A US 2189283A US 182675 A US182675 A US 182675A US 18267537 A US18267537 A US 18267537A US 2189283 A US2189283 A US 2189283A
- Authority
- US
- United States
- Prior art keywords
- radiating
- beacon
- horizontal
- horizontally polarized
- component
- 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
Links
- 238000010586 diagram Methods 0.000 description 7
- 230000005855 radiation Effects 0.000 description 5
- 239000004020 conductor Substances 0.000 description 4
- 230000010287 polarization Effects 0.000 description 4
- 230000005284 excitation Effects 0.000 description 2
- 238000010276 construction Methods 0.000 description 1
- 230000003292 diminished effect Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000008520 organization Effects 0.000 description 1
- 230000003071 parasitic effect Effects 0.000 description 1
- 230000010363 phase shift Effects 0.000 description 1
Images
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q19/00—Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic
- H01Q19/28—Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using a secondary device in the form of two or more substantially straight conductive elements
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S1/00—Beacons or beacon systems transmitting signals having a characteristic or characteristics capable of being detected by non-directional receivers and defining directions, positions, or position lines fixed relatively to the beacon transmitters; Receivers co-operating therewith
- G01S1/02—Beacons or beacon systems transmitting signals having a characteristic or characteristics capable of being detected by non-directional receivers and defining directions, positions, or position lines fixed relatively to the beacon transmitters; Receivers co-operating therewith using radio waves
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S3/00—Direction-finders for determining the direction from which infrasonic, sonic, ultrasonic, or electromagnetic waves, or particle emission, not having a directional significance, are being received
- G01S3/02—Direction-finders for determining the direction from which infrasonic, sonic, ultrasonic, or electromagnetic waves, or particle emission, not having a directional significance, are being received using radio waves
- G01S3/04—Details
- G01S3/08—Means for reducing polarisation errors, e.g. by use of Adcock or spaced loop antenna systems
-
- 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
- H01Q1/32—Adaptation for use in or on road or rail vehicles
- H01Q1/325—Adaptation for use in or on road or rail vehicles characterised by the location of the antenna on the vehicle
- H01Q1/3275—Adaptation for use in or on road or rail vehicles characterised by the location of the antenna on the vehicle mounted on a horizontal surface of the vehicle, e.g. on roof, hood, trunk
Definitions
- beacon aerials have to be erected upon metallic surfaces of finite dimensions.
- theproblem may consist in erecting or rigging up a radio range aerial upon the roof or top of a vehicle or to build a radio range equipment on the roof of a building. Because of the finite dimension of the base surface or ground sheet, standing waves arise thereon, and these result in a horizontal component in the field intensity.
- ultra-short-wave beacons comprising two keymodulated reflector dipoles in an arrangement presenting mirror-image relationship to the guide beam or radio beacon course
- the two horizontal components of the two side diagrams present a phase shift in reference to each other according to whether the right-hand or the left-hand refiector is closed, that is, elliptically polarized Waves occur in each of the two side diagrams by virtue of reflection relative to the vertical plane of symmetry which contains also the guide beam.
- the example consisting of the simplest receiving antenna, that is, the vertical dipole, may be cited 'to prove that, in the presence of an inclination of the dipole, the radio beacon course or guide 1 beam apparently shifts, and it is evident that consequently an airplane flying along curves and fitted with an antenna being perfectly vertically polarized in horizontal flying positionwould experience a corresponding shift of the guide beam as a function of its flying position.
- the radio beacon course or guide 1 beam apparently shifts, and it is evident that consequently an airplane flying along curves and fitted with an antenna being perfectly vertically polarized in horizontal flying position would experience a corresponding shift of the guide beam as a function of its flying position.
- the antenna subject to more complicated polarization as aresult of its metallic masses, etc., and this also results in a shift of the guide beam in a way as indicated.
- Figure 1 is a vector diagram explanatory of my invention
- Figure 2 is a plan View of an embodiment of my invention
- Figures 3, 4 and 5 are elevational views of modifications of my invention.
- Fig. 1 illustrates the situation in a plane of symmetry containing the guide beam.
- the vertical components V1 and VB: of the two side diagrams are in agreement, and this is true also, in so far as size or quantity is concerned.
- the horizontal, components H1 and Hit though the horizontal components because of reflection are displaced in phase an angle'of degrees. At this point, therefore, the guide beam will be found with an antenna subject to purely vertical polarization.
- the receiving dipole is turned about a horizontal axis, the result is that for one of the 'side'diagrams it will fall more in the direction of the resultant R1 or Rn of the two field intensity components, and for the other side diagram farther away from this direction.
- the undesired horizontal component is compensated in the radio beacon course and optionally also in other directions at least dimininshed by the aid'of a supplementary radiation presenting predominantly horizontal polarization.
- This supplementary radiation may be produced by exicting, together with the others, one ormore auxiliary radiators mounted at suitable points, the excitation being at the frequency and rate of the keying of the.
- auxiliary radiators should preferably be disposed symmetrically in reference to the radio beacon course plane.
- Fig. 2 An'illustrative embodiment of the-invention'is shown in Fig. 2.
- base area F On a base area F, assumed to be rectangular, is mounted in the center the energy-fed vertical rod' A, while laterally in reference thereto are mounted the two keymodulated reflector rodsRi and R2. The, guide beam will then be in a position at right angles to the line connecting the three rods.
- each of the reflector dipoles R1 and R2 a small horizontal radiator as indicated at H1 and H2, respectively, with phase shifting means P1 and P2, respectively, being provided at the junction point.
- the said phase shifters and the length of the auxiliary horizontal bars should be so chosen that in the beacon course the field intensity diagram of the horizontal component attains a minimum value.
- the contact members T1 and T2, Fig. 3 represent the reversing switch means for the reflector dipoles.
- Fig. 4 isshown an exemplified embodiment in which the compensation of the horizontal component is obtained by radiation-coupled auxiliary. radiators H1 and H2, while the embodiment of Fig. 5 comprises energy-fed radiators which are-associated with thesame feeder lead S. as the chief radiator, and'which, if desired, may be keyed. alternately. Also in this organization phase shifting means may be included as shown in Figure 3.
- abeacon antenna system comprising a vertical radiating system for radiating a vertically. polarized beam, of radiant energy, said. radiating system being mounted on aground sheet of finite area whereby a horizontally polarized component of said beam is produced, the
- a beacon antenna system comprising .a vertical radiating system for radiating a vertically vpolarized beam, said radiating. system being mounted on a ground sheet of finite area whereby a horizontally polarized component of said beam isproduced and means for radiating a horizontally polarized wave of such amplitude and phase that the said horizontally polarized component is neutralized.
- a beacon antenna system comprising a vertical radiating system for radiating a vertically polarized beam, said radiating system being mounted on a ground sheet of finite area whereby a horizontally polarized component of said beam is produced and means for radiating a horizontally polarized wave of such amplitude and phase that the said horizontally polarized component is neutralized in the direction of said beam.
- a beacon antenna system comprising a vertical radiating system for radiating a vertically polarized beam, said radiating system being mounted on a ground sheet of finite area whereby a horizontally polarized component of said beam is produced and means for radiating a'horizontally polarized wave of such amplitude and phase thatthe said horizontally polarized component is neutralized, said means comprising a plurality of horizontal conductors disposed in a vertical plane passing through said radiating system and at right angles to said beam.
- a beacon antenna system comprising a vertical radiating system for radiating. a vertically polarized beam, said radiating system being mounted on a ground sheet of finite area whereby a horizontally polarized component of said beam isproduced and means for radiating a horizontally polarized wave of such amplitude and phase that the said horizontally polarized component is neutralized, said means comprising a plurality of horizontal. conductors disposed in a vertical plane passing through said radiating system and at right angles to said beam and means for energizing said conductors.
- a beacon antenna system comprising a vertical radiating system for radiating a vertically polarized beam, said radiating system being mounted on a groundsheet of finite area whereby a horizontally polarized component of said beam is produced and means for radiating a horizontally polarized Wave of such amplitude and phase that the said horizontally polarized component is neutralized, said means comprising a plurality of horizontal parasitic radiators disposed in a plane passing through said radiating system and at right angles to said beam.
- a beacon antenna system comprising a vertical radiating system for radiating a vertically polarized beam, said radiating system being mounted on a ground sheet of finite area whereby a horizontally polarized componentof said beam is produced and a plurality of horizontal conductorsdisposed in a plane passing through said radiating systemat right angles to said beam and means for energizing said conductors with a wave of such amplitude and phase that the horizontally polarized component of said beam is neutralized.
Landscapes
- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Radar, Positioning & Navigation (AREA)
- Computer Networks & Wireless Communication (AREA)
- Aerials With Secondary Devices (AREA)
- Variable-Direction Aerials And Aerial Arrays (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE205573X | 1936-12-22 | ||
DE200237X | 1937-02-20 |
Publications (1)
Publication Number | Publication Date |
---|---|
US2189283A true US2189283A (en) | 1940-02-06 |
Family
ID=25758519
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US182675A Expired - Lifetime US2189283A (en) | 1936-12-22 | 1937-12-31 | Beacon aerial |
US200370A Expired - Lifetime US2218707A (en) | 1936-12-22 | 1938-04-06 | Antenna array |
Family Applications After (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US200370A Expired - Lifetime US2218707A (en) | 1936-12-22 | 1938-04-06 | Antenna array |
Country Status (3)
Country | Link |
---|---|
US (2) | US2189283A (en:Method) |
CH (1) | CH205573A (en:Method) |
NL (1) | NL54201C (en:Method) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2449999A (en) * | 1942-10-30 | 1948-09-28 | Standard Telephones Cables Ltd | Antenna system for defining glide paths |
US2713164A (en) * | 1945-05-21 | 1955-07-12 | Itt | Direction finding system |
US20040115346A1 (en) * | 2002-09-23 | 2004-06-17 | Woolley Scott J. | Closure sealant dispenser |
US20050158467A1 (en) * | 2003-07-08 | 2005-07-21 | Buckley Ian J. | Variable fluid dispenser |
US20100049357A1 (en) * | 2002-09-23 | 2010-02-25 | Computrol, Inc. | Rotary Machine with Separately Controllable Stations |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3383694A (en) * | 1965-02-15 | 1968-05-14 | Carll F. Strohmeyer Jr. | Rotatable directional antenna attachment for use with a vertical antenna rod |
US7348933B2 (en) * | 2000-03-10 | 2008-03-25 | Wifi Plus, Inc. | Compact multi-polarized antenna for portable devices |
US6496152B2 (en) * | 2000-03-10 | 2002-12-17 | Jack Nilsson | Dual polarized antenna |
US7138956B2 (en) * | 2002-11-14 | 2006-11-21 | Wifi-Plus, Inc. | Apparatus and method for a multi-polarized ground plane beam antenna |
US7236129B2 (en) * | 2002-11-14 | 2007-06-26 | Wifi-Plus, Inc. | Apparatus and method for a multi-polarized antenna |
US7030831B2 (en) * | 2002-11-14 | 2006-04-18 | Wifi-Plus, Inc. | Multi-polarized feeds for dish antennas |
-
0
- NL NL54201D patent/NL54201C/xx active
-
1937
- 1937-12-13 CH CH205573D patent/CH205573A/de unknown
- 1937-12-31 US US182675A patent/US2189283A/en not_active Expired - Lifetime
-
1938
- 1938-04-06 US US200370A patent/US2218707A/en not_active Expired - Lifetime
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2449999A (en) * | 1942-10-30 | 1948-09-28 | Standard Telephones Cables Ltd | Antenna system for defining glide paths |
US2713164A (en) * | 1945-05-21 | 1955-07-12 | Itt | Direction finding system |
US20040115346A1 (en) * | 2002-09-23 | 2004-06-17 | Woolley Scott J. | Closure sealant dispenser |
US7179333B2 (en) | 2002-09-23 | 2007-02-20 | Computrol, Inc. | Closure sealant dispenser |
US20070110896A1 (en) * | 2002-09-23 | 2007-05-17 | Computrol, Inc. | Closure sealant dispenser |
US20100049357A1 (en) * | 2002-09-23 | 2010-02-25 | Computrol, Inc. | Rotary Machine with Separately Controllable Stations |
US8261631B2 (en) | 2002-09-23 | 2012-09-11 | Computrol, Inc. | Rotary machine with separately controllable stations |
US20050158467A1 (en) * | 2003-07-08 | 2005-07-21 | Buckley Ian J. | Variable fluid dispenser |
US20090294472A1 (en) * | 2004-07-08 | 2009-12-03 | Computrol, Inc. | Fluid Dispensing Actuator |
Also Published As
Publication number | Publication date |
---|---|
US2218707A (en) | 1940-10-22 |
NL54201C (en:Method) | |
CH205573A (de) | 1939-06-30 |
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