US2031065A - Antenna - Google Patents

Antenna Download PDF

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Publication number
US2031065A
US2031065A US690355A US69035533A US2031065A US 2031065 A US2031065 A US 2031065A US 690355 A US690355 A US 690355A US 69035533 A US69035533 A US 69035533A US 2031065 A US2031065 A US 2031065A
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US
United States
Prior art keywords
aerials
radiators
wires
antenna system
antenna
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
US690355A
Inventor
Posthumus Klaas
Pol Balthasar Van Der
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.)
RCA Corp
Original Assignee
RCA Corp
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
Priority to BE363173D priority Critical patent/BE363173A/xx
Priority to GB23704/29A priority patent/GB319267A/en
Priority to FR680502D priority patent/FR680502A/en
Application filed by RCA Corp filed Critical RCA Corp
Priority to US690355A priority patent/US2031065A/en
Priority to US40204A priority patent/US2066900A/en
Application granted granted Critical
Publication of US2031065A publication Critical patent/US2031065A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q21/00Antenna arrays or systems
    • H01Q21/06Arrays of individually energised antenna units similarly polarised and spaced apart
    • H01Q21/08Arrays of individually energised antenna units similarly polarised and spaced apart the units being spaced along or adjacent to a rectilinear path
    • H01Q21/12Parallel arrangements of substantially straight elongated conductive units

Definitions

  • Figure 1 shows an antenna having two feeders 2, 4 to which the aerials 6 are connected.
  • the aerials are spaced one wave length apart so that they are in phase. This is necessary to secure a directional effect at right angles to the plane of the aerials and this is so in the case with all the aerial systems claimed.

Landscapes

  • Variable-Direction Aerials And Aerial Arrays (AREA)
  • Near-Field Transmission Systems (AREA)

Description

Feb. 18, 1936. PQSTHUMUS ET A 2,031,065 ANTENNA Original Filed Sept. 19, 1929 I INVENTORS KLAAS POSTHUMUS EBAYLTHASA VA DER POL ATTORNEY Patented Feb. 18, 1936 UNITED STAES ATENT OFICE ANTENNA Original application September 19, 1929, Serial No. 393,794. Divided and this application September 21, 1933, Serial No. 690,355. In the Netherlands September 19, 1928 5 Claims.
This invention is a. division of our copending application Serial No. 393,794, filed September 19, 1929, and relates to antenna systems for transmitting and receiving wireless signals. More particularly, the invention provides an arrangement in which a pure directional effect is obtained by means of an aerial system utilizing a plurality of aerials or radiators.
According to the invention the height of these aerials is substantially equal to or an odd multiple of the half wave length of the oscillations to be transmitted or received, and the said aerials are energized such that the operative direction is at right angles to the plane in which the aerials are located.
In the preferred embodiment an arrangement is provided in which the spacing of the aerials is a half wave length and each aerial is connected to one of two feeders present such that the energy in all the aerials is in phase. As an alternative, four feeders are provided and each aerial is conected to two feeders such that the energy in all the aerials is in phase. An arrangement may be provided in which the spacing of the aerials is a half wave length and the aerials, which are alternately coupled in opposition, are connected to two central feeders. Alternatively, the spacing of the aerials may be an odd multiple of the half wave length and a single feeder is connected to all the aerials such that the energy in all the aerials is in phase.
The invention will be more clearly understood by reference to the accompanying drawing, in which Figures 1 to 7 inclusive show some embodiments.
Figure 1 shows an antenna having two feeders 2, 4 to which the aerials 6 are connected. The aerials are spaced one wave length apart so that they are in phase. This is necessary to secure a directional effect at right angles to the plane of the aerials and this is so in the case with all the aerial systems claimed.
Figure 2 shows an antenna having likewise two feeders 2, 4.
In this case the aerials 8 are spaced a half wave length apart and as shown in the drawing are each only connected to one of the two feeders so as to ensure uniformity in phase.
The arrangement shown in Figure 3, is identical with that of Figure 2 but for the width of the aerial system which is reduced by the interconnection of coils ID in the feeders such that the spacing of the radiators or aerials is still rangement of Figure 3, the free ends of the aerials 8 shown in Figure 3 being connected to two feeders l4, l6 so that the radiation of energy from the feeders, if any, is balanced by the close proximity of a forward and a backward lead. The pairs of feeders l4, l4 and l6, it are preferably placed close together or they may be separated by an even number of half Wave lengths to get proper radiation addition in a direction perpendicular to their length.
Referring to Figure 5, all the aerials are fed from one single feeder l8 and so are they in Figure 6 which shows the same antenna construction, but for the spacing of the aerials being very small so that in principle all the aerials are simultaneously in phase if their length is a half wave length. That is to say, by bending adjacent half wave lengths, the currents therein, upon which radiation depends, are made to flow in the same direction. As nevertheless the horizontal spacing is to be slightly taken account of, the length of the aerials Will practically be slightly smaller.
Referring to Figure 7, the aerials 2|] are arranged on either side of two central feeders 22; in order to ensure uniformity in phase at a spacing of a half wave length, the aerials must be a1- ternately coupled in opposition to the feeders.
We claim:
1. A directive antenna system comprising a two wire transmission line, the wires of said line being parallel to each other and separated a distance equal to an odd multiple of half the length of the communication wave, parallel radiators transverse of said wires extending between said wires and connected thereto, said radiators being located substantially one wave length apart whereby cophasal energization is effected therein.
2. A directive antenna system comprising a two wire transmission line, the wires of said line being parallel to each other and separated a distance equal to an odd multiple of half the length of the communication wave, parallel radiators transverse of said wires extending between said wires and connected thereto, said radiators being located substantially one wave length apart whereby cophasal energization is effected therein, another similar antenna system located close to said first antenna system so arranged that the corresponding wires of both said transmission lines are in proximity to each other for the cancellation of radiation from the wires of both of said lines, the radiators of said first antenna system being located substantially intermediate the radiators of said second antenna system.
3. A system in accordance with claim 2, char acterized in this, that the radiators of one antenna are separated from the adjacent radiators of the other antenna substantially one half wave length apart.
4. A directive antenna system comprising a two wire transmission line, the wires of said'line being parallel to each other and separated a distance equal to one half the length of the communication wave, parallel radiators transverse of said wires extending between said wires and connected thereto, said radiators being located substantially one wave length apart whereby c0- phasal energization is efiected therein, another similar antenna system located close to said first antenna system so arranged that the corresponding wires of both said transmission lines are in proximity to each other for the cancellation of radiation from the wires of both said lines, the radiators of said first antenna system being located substantially intermediate the radiators of said second antenna system with respect to a.
single plane, adjacent radiators being separated one half wave length apart.
5. A directive antenna system comprising a two wire transmission line, the wires of said line being parallel to each other and separated a distance equal to an odd multiple of half the length of the communication wave, parallel radiators transverse of said wires extending between said wires and connected thereto, said radiators being located substantially one wave length apart whereby cophasal energization is effected therein, another similar antenna system parallel to said first antenna system and separated therefrom an even number of half wave lengths, the radiators of said first antenna system being located substantially intermediate the radiators of said second antenna system with respect to a single plane.
KLAAS POSTI-IUMUS. BALTI-IASAR VAN DER POL.
US690355A 1928-09-19 1933-09-21 Antenna Expired - Lifetime US2031065A (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
BE363173D BE363173A (en) 1928-09-19
GB23704/29A GB319267A (en) 1928-09-19 1929-08-01 Improvements in or relating to aerial systems for transmitting and receiving wireless signals
FR680502D FR680502A (en) 1928-09-19 1929-08-19 Device for transmitting and receiving radio signals by means of an antenna system comprising two or more radiators
US690355A US2031065A (en) 1928-09-19 1933-09-21 Antenna
US40204A US2066900A (en) 1928-09-19 1935-09-12 Antenna

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
NL319267X 1928-09-19
US39379429A 1929-09-19 1929-09-19
US690355A US2031065A (en) 1928-09-19 1933-09-21 Antenna

Publications (1)

Publication Number Publication Date
US2031065A true US2031065A (en) 1936-02-18

Family

ID=32512146

Family Applications (1)

Application Number Title Priority Date Filing Date
US690355A Expired - Lifetime US2031065A (en) 1928-09-19 1933-09-21 Antenna

Country Status (4)

Country Link
US (1) US2031065A (en)
BE (1) BE363173A (en)
FR (1) FR680502A (en)
GB (1) GB319267A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2551171A (en) * 1946-05-31 1951-05-01 Rca Corp Antenna system
US3500426A (en) * 1965-10-22 1970-03-10 Scott & Fetzer Co Magnetically driven antenna array
US6765530B1 (en) 2002-07-16 2004-07-20 Ball Aerospace & Technologies Corp. Array antenna having pairs of antenna elements
EP2332214B1 (en) * 2008-09-11 2020-05-06 Wistron Neweb Corporation Elongated twin feed line rfid antenna with distributed radiation perturbations

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2551171A (en) * 1946-05-31 1951-05-01 Rca Corp Antenna system
US3500426A (en) * 1965-10-22 1970-03-10 Scott & Fetzer Co Magnetically driven antenna array
US6765530B1 (en) 2002-07-16 2004-07-20 Ball Aerospace & Technologies Corp. Array antenna having pairs of antenna elements
EP2332214B1 (en) * 2008-09-11 2020-05-06 Wistron Neweb Corporation Elongated twin feed line rfid antenna with distributed radiation perturbations

Also Published As

Publication number Publication date
BE363173A (en)
GB319267A (en) 1930-09-18
FR680502A (en) 1930-05-01

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