US2266262A - Antenna system for wireless communication - Google Patents

Antenna system for wireless communication Download PDF

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Publication number
US2266262A
US2266262A US294723A US29472339A US2266262A US 2266262 A US2266262 A US 2266262A US 294723 A US294723 A US 294723A US 29472339 A US29472339 A US 29472339A US 2266262 A US2266262 A US 2266262A
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coil
core
antenna
loop
pick
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US294723A
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Wladimir J Polydoroff
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    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q7/00—Loop antennas with a substantially uniform current distribution around the loop and having a directional radiation pattern in a plane perpendicular to the plane of the loop
    • H01Q7/06—Loop antennas with a substantially uniform current distribution around the loop and having a directional radiation pattern in a plane perpendicular to the plane of the loop with core of ferromagnetic material
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01J—CHEMICAL OR PHYSICAL PROCESSES, e.g. CATALYSIS OR COLLOID CHEMISTRY; THEIR RELEVANT APPARATUS
    • B01J2/00—Processes or devices for granulating materials, e.g. fertilisers in general; Rendering particulate materials free flowing in general, e.g. making them hydrophobic
    • B01J2/02—Processes or devices for granulating materials, e.g. fertilisers in general; Rendering particulate materials free flowing in general, e.g. making them hydrophobic by dividing the liquid material into drops, e.g. by spraying, and solidifying the drops
    • B01J2/04—Processes or devices for granulating materials, e.g. fertilisers in general; Rendering particulate materials free flowing in general, e.g. making them hydrophobic by dividing the liquid material into drops, e.g. by spraying, and solidifying the drops in a gaseous medium
    • C—CHEMISTRY; METALLURGY
    • C05—FERTILISERS; MANUFACTURE THEREOF
    • C05C—NITROGENOUS FERTILISERS
    • C05C1/00—Ammonium nitrate fertilisers
    • C05C1/02—Granulation; Pelletisation; Stabilisation; Colouring
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04J—MULTIPLEX COMMUNICATION
    • H04J3/00—Time-division multiplex systems
    • H04J3/20—Time-division multiplex systems using resonant transfer
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04Q—SELECTING
    • H04Q11/00—Selecting arrangements for multiplex systems
    • H04Q11/04—Selecting arrangements for multiplex systems for time-division multiplexing

Definitions

  • This invention relates to a frame aerial", or
  • loop antenna which consists of several turns of wire wound on a frame.
  • Such an antenna is often connected with a capacitor and thus forms an oscillatory circuit capable, when properly adjusted. of being more responsive to a desired frequency than to other frequencies.
  • a similar oscillatory circuit may be used in the transmitting stations radiating an electromagnetic wave in which case a loop antenna may serve as a radiator.
  • this type of aerial possesses directional properties which are manifested by minimum or zero signal when the plane of the aerial is perpendicular to the direction of propagation of the received electromagnetic waves, 1. e. when the plane of the aerial is normal to the wavefront of electromagnetic waves.
  • This type of aerial although not as eificient as a straight antenna, finds its use in portable receivers, direction finders, transmitting beacons, airplane installations, etc. where a straight antenna. cannot be conveniently employed, but where the antenna should be responsive to waves whose wavelengths are relatively long compared with the linear dimensions of the antenna.
  • the coil of a frame aerial is designed to have a desired natural period of electrical oscillation or fundamental wave-length below the wave-length of the waves to be received, and from the viewpoint of efiiciency it is advantageous to employ a large turn-area, which, on the other hand, is limited by the distributed capacity of the coil.
  • This capacity is usually large in coils of large dimensions with small spacing between the turns.
  • the distributed capacity limits the tuning range unless very large and bulky tuning condensers are employed, and their use reduces the efiiciency of the system and increases the dimensions of the system.
  • the invention has for one of its objects the production of a frame aerial of high efliciency and in which distributed capacity is minimized.
  • the high elliciency and low distributed capacity are attained by the employment of ferromagnetic mass in the field of the loop antenna.
  • the efliciency of a frame aerial, having an area A and number of turns N may be expressed in terms-of pick-up factor", 1. e. the ratio of voltage developed across the coil terminals and the intensity of the electromagnetic wave at the receiver and may be expressed as follows:
  • the first term wL/R is commonly known as the Q of the coil and an increase in Q" results in greater pick-up and improved selectivity.
  • the second term 21rAN/x is known as the effective height of the antenna and while an increase in its value due to an increase in AN improves the pick-up of electromagnetic energy,,the electrostatic pick-up also simultaneously increases, a fact which is sometimes undesirable.
  • the same formula, a priori would apply to the transmitting station having a frame aerial as a radiator, in which case the power transmitted in the space will be proportional to the efliciency of the radiator loop and to the turn-area of the frame aerial.
  • both a: and x are expressed in terms of frequency, it will be observed that the received signal is proportional to the second power of the frequency, so that the aerial will not have the same performance when used at different frequencies.
  • Another object of the invention is to equalize the pick-up properties of a loop antenna by the employment of iron or ferromagnetic masses in the field of the coil of such antenna.
  • Still another object of the invention is to improve the directional properties of a loop antennawhich is accomplished by a properly shaped core composed of a ferro-magnetic mass in the field of the coil, said mass materially changing the con figuration of the magnetic fields of the coil and reducing the stray fields partly responsible to poor directional selectivity. Due tothe fact that the losses in the iron rapidly change with frequency it is possible by the use of the iron substantially to equalize the pick-up properties of the frame aerial for all frequencies within the tuning range.
  • the present invention materially improves the Q of the frame aerial and increases its pick-up, while at the same time rendering this latter more uniform throughout the frequency range.
  • Figs. 1 and 2 schematically represent two identical coil antennae, the one of Fig. 2 being equipped with an iron core.
  • Fig. 3 represents two identical air and iron cored loops of modified construction.
  • Fig. 4 represents the diagrams of signal strength and directional properties of the inven- Fig. represents a general layout of the sys tem.
  • Fig. 6 shows a grounding strip and its application to the invention
  • Fig. '7 shows another modification of the invention.
  • Figs. 1 and 2 there are shown two loop antennae of identical dimensions, both wound to the same inductance, the coil l of Fig. I being wound on a coil form 2 and the coil 3 of the loop antenna of Fig. 2 being wound on a 4 inch core 4 composed of finely divided particles of iron, whose dimensions are of the order of 3 microns and which are compressed and bound together in the well known manner.
  • Bakelite ribs 5 are cemented to the core in order to provide an adequate spacing of the turns from the iron core.
  • both loops have their axial length of 1 inch and for the same inductance, the air core loop of Fig. 1 had 52 turns of Litz cable made of 12 strands of No.
  • the effective permeability of the core in Fig. 2 can be computed from the ratio of square number of turns, 52 /40 which is equal to 1.7. The same was additionally verified by measuring the inductance of the second coil with and without the iron core. 1
  • the Q(wL/R) was then measured in the well known manner at a frequency of 300 kilocycles for which the above loop was designed and it was found to be 190 for the coil of Fig. 1 and 250 for the second coil. Thus an appreciable increase in Q was obtained due to the employment of iron in the coil.
  • the windings are made of Litz cable composed of 110 strands of No. 42 wire.
  • the effective permeability of .the core in the second example is 1.4, being smaller on account of less complete utilization of the iron.
  • the Q measured at 300 kilocycles was 390 for the air core loop and 470 for the iron core loop. This again yields a 20 percent increase in Q with a resultant increase of selectivity and signal to noise ratio.
  • the ratio of signal strength of both loops would be substantially unity.
  • the already existing air core loop antenna may be decreased in diameter (mean turn), this reduction being of the same order as the increase of permeability due to the core.
  • This application is of particular importance in an aircraft antenna where the reduction of the loop size and of the overall dimensions of its cover will reduce the drag or air resistance at high speeds.
  • a loop antenna equipped with a core is more directional and less affected by adjoining metal parts. Whilean air core loop should be mounted at least 6 inches from the metal surface of aireraft,the iron cored loop could be mounted as close as 2inches from the same surface without aifecting its Q.
  • Fig. 4 shows the measurements of directional properties of the two loops of Fig. 3, associated with radio frequency receiver, having a partial automatic volume control.
  • the ordinates indicate the signal strength received under identical conditions and the abscissae reprwent thedegree of rotation of the loops from the null point, i. e. when the loops plane is perpendicular to the source of radiation.
  • Curve a represents the part of a polar diagram of an-air core loop, while curve b shows the same for an iron core loop.
  • Fig. 5 shows a-schematic arrangement of a wireless transmitting-receiving system in which two closed circuits are employed for transmission TR andreception RC respectively. Both coils are equipped with iron cores so that double advantage is to be expected.
  • the transmitter may of course be in the form of a straight radiator,
  • Fig. 2 shows a solid pellet of iron inserted .n the coils, in the case of larger loops, from 6 inches to 12 inches in diameter, the core itself takes the shape of a toroidal ring so that its weight is materially reduced, as compared with a solid cylindrical core. It was found that the toroidal ring core produces improved Q of the coil owing to the particular distribution of magnetic fields. Core 4 of Fig. 3 shows such ring.
  • the frame aerial coil may also be wound in the form of a fiat spiral or in the form of a short solenoid or in the form of multi-layer windings.
  • the open-type iron core may consistof a toroidal ring, its thickness being greater than the axial length of the winding. While in the first example the core may approach the inner turn of the coil very closely, in the second and third examples the spacing of about inch should be allotted between the'coil and core and the axial length of the coil should be smaller than the coil diameter so as to not to increase the distributed capacity.
  • the effective permeability of the iron is not greater than 2 but a marked improvement in Q is attributed not so much to the reduction of copper but rather to the particular distribution of the coil field and to a consequent reduction of losses in the surrounding medium.
  • a groove may be provided in the outer surface of the ring and the whole Winding placed over the groove.
  • the construction according to a feature of the present invention allows simple means for balancing out electrostatic influences.
  • the core itself has a certain conductivity and may be considered as a poor antenna.
  • the core may then be connected to earth potential of the circuit, thus reducing to zero the effective height of the electrostatic factor of the antenna.
  • Fig. 5 shows such an arrangement where the core of the receiver is shown grounded.
  • a metal strip may be employed on the inner surface of the core ring without detriment to the efliciency of the coil, in which case the strip should be split.
  • Fig. 6 shows this construction.
  • a core 4 similar to one shown on Fig. 5 is used in connection with coil I to form an antenna.
  • a metal conductive strip I is placed on the inner surface of the hollow core.
  • This strip may be made of copper or other highly conductive metal or may be deposited on the surface of the core, for example by spraying. To avoid the short circuiting effects this strip is discontinued or left open at the top. At the bottom the strip is connected to the ground or other points of the circuit.
  • the shaft 9 and the supporting bracket 8 are used for rotating the loop.
  • Coil winding I is made in two sections. The employment of a ring core produces the beneficial effect of improving the efiiciency of the coil even in the case when the coil is completely surrounded by an electrostatic screen. In such a case the core may be placed between the screen and the coil.
  • the frame aerial is made rotatable in order that its directional properties may be utilized (minimum signal when the plane of the loop is perpendicular to the direction of the transmitter). It is then convenient to rotate the core together with the loop for which purpose both coil and core are assembled together.
  • either or both elements may be rotated separately in which case a certain inductance variation may occur depending on the shape of the core so that the coil may be set at the minimum signal position with the plane of the core parallel to the plane of the coil and the system tuned to the transmitter. The subsequent rotation of the coil will produce de-tuning so that the signal strength diminishes when the plane of the coil points toward the station.
  • a study of the polar diagram obtained when the receiver was tuned to the frequency at the minimum position shows two pronounced peaks on each side of the minima. It is obvious that in such an arrangement a rotatable frame aerial permits periodic pick-up of two or more signals of different frequencies, or operation through a certain band is possible.
  • Fig. 7 shows an arrangement where a coil antenna I may rotate around the core 4.
  • Coil winding is placed on a coil-former 2 made of insulating material.
  • a bushing II attached to the former 2 allows a free rotation of the loop coil around its shaft 8, fixed to a supporting stand 8.
  • a pulley I4 attached to the bushing with a cable I2 provides the means of manual control for rotation of the loop.
  • the core 4 is provided with a tubular shaft I3 which is placed around the shaft 9 and another pulley I4 at the bottom is used for the rotation of the core. Both coil and core may be rotated independently or simultaneously by the operator.
  • the invention is not limited to the employment in periodic or tunable aerials but may be equally well applied to aperiodic loops in which the energy is transferred to selective circuit through a current transformer, having primary and secondary windings, the primary being connected across the loop coil.
  • the invention is applicable to all cases of transmission of electromagnetic waves where it is now possible to improve, direct or condense the energy of radiations by means of the employment of suitable magnetic material, in substantially the same manner as has been recently developed for the propagation of electrostatic waves through dielectrics.
  • An antenna system for the reception of radiated electromagnetic waves including a coil said coil in order to obtain directional hearings on a plurality of sources of said radiations.
  • a system for the reception of electromagnetic radiations comprising a loop coil-antenna the diameter of which is greater than its axial length, and a ferromagnetic mass in the fields of said radiations, said mass being in the form of an open type core for said coil and composed of finely divided and insulated magnetic particles.
  • a ferromagnetic open-type cylindrical core inside of said coil and spaced therefrom to reduce the efiective permeability of said core in said coil, said core comprising finely divided particles insulated from each other and of a size of the order of three microns, whereby the efiective height and directional properties of said system are improved.
  • An antenna system for the reception of radiated electromagnetic waves including a lowcost high-inductance coil having a diameter greater than its axial length, a ferromagnetic cylindrical core of the open-type inside of said coil and spaced therefrom, said core comprising finely divided magnetic particles insulated from each other, the size of said particles being of the order of several microns to preserve the low loss characteristics of said antenna system whereby the pick-up factorand directional properties of said system are improved.
  • An antenna system for the reception of electromagnetic waves including a pick-up coil, having a diameter greater than its axial length, an open-type ferromagnetic core in the field of said coil for improving the electromagnetic pick-up properties of said system, and means for suppressing the electrostatic pick-up, said means comprising a layer of conductive material placed around said core and connected to the ground of said system.
  • An antenna system for the reception of electromagnetic radiations said system having a pick-up coil whose diameter is greater than its axial length, an open-type ferromagnetic core in the field of said radiations for improving the efficiency of said system, and means for rotating said coil around said core in order toobtain directional bearings of the source of said radiations.
  • An antenna system for the reception of electromagnetic radiations said system having a pick-up coil whose diameter is greater than its axial length, an open-type ferromagnetic core in the field of said radiations for improving the efliciency of the system, means for simultaneously rotating and varying the inductance of the maximum dimension of said core transverse to the coil axis notexceeding the minimum coil diameter.
  • a system for the reception of electromagnetic radiations comprising a coil antenna whose axial length is less than its maximum dimension transverse to its axis, and a ferromagnetic open type core the dimension of said core in any direction transverse to said axis being less than the dimension of the coil in the same direction, said core being composed of compressed insulated magnetic particles of the order of three microns and being exposed to the field of said radiations.
  • An antenna system for the reception of electromagnetic radiations including a pick-up coil wound with spaced sections, said sections having axial length not exceeding the inner diameter of said coil, and an open type cylindrical ferromagnetic core inside of said coil, said core being composed of finely divided and insulated magnetic particles and being exposed to the field of said radiations.
  • An antenna system for the reception of electromagnetic radiations comprising a coil and a ferromagnetic core, said coil having a high Q value and spacedly wound with a multi-stranded cable, the length of said coil not exceeding the diameter thereof, said core being composed of insulated magnetic particles of the order of three microns, the maximum dimension of said core transverse to the coil axis not exceeding the minimum coil diameter, said core being of toroidal shape of the length greater than that of said coil, whereby the directional selectivity of said system is improved.
  • An antenna system for the reception of electromagnetic radiations comprising a coil and a ferromagnetic core, said coil being composed of spaced sections having axial length not exceeding the minimum diameter of the coil, said core being composed of insulated magnetic particles of the order of several microns, the maximum dimension of said core transverse to the coil axis not exceeding the said minimum diameter, said core being of toroidal shape of the length greater than the total length of the coil, whereby the directional selectivity of said system is improved.
  • An antenna system for wireless communication comprising a coil the diameter of which is greater than its length, and a ferromagnetic core composed of finely divided and insulated magnetic particles in the field of said coil, said core being of the open type and having its maximum dimension transverse to the coil axis not exceeding the minimum diameter of said coil and its length being greater than that of said coil.

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  • Chemical & Material Sciences (AREA)
  • Organic Chemistry (AREA)
  • Engineering & Computer Science (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Signal Processing (AREA)
  • Near-Field Transmission Systems (AREA)
  • Details Of Aerials (AREA)
US294723A 1938-12-13 1939-09-13 Antenna system for wireless communication Expired - Lifetime US2266262A (en)

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Cited By (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2438680A (en) * 1943-03-11 1948-03-30 Wladimir J Polydoroff Loop antenna apparatus
US2442310A (en) * 1943-06-14 1948-05-25 Wladimir J Polydoroff Directional antenna system
US2460492A (en) * 1946-10-30 1949-02-01 Hoffman Radio Corp Loop inductance compensator
US2581348A (en) * 1948-04-10 1952-01-08 Int Standard Electric Corp Antenna
US2824306A (en) * 1950-10-04 1958-02-18 Admiral Corp Antenna
US2915752A (en) * 1953-12-29 1959-12-01 Raytheon Co Directional antenna
US2953785A (en) * 1956-08-02 1960-09-20 Gasaccumulator Svenska Ab Arrangement for radio direction finding
US3078462A (en) * 1958-07-18 1963-02-19 Julius Herman One-turn loop antenna
US4441498A (en) * 1982-05-10 1984-04-10 Cardio-Pace Medical, Inc. Planar receiver antenna coil for programmable electromedical pulse generator
US4703278A (en) * 1984-10-09 1987-10-27 Texaco Inc. Well logging disc coil receiving means and method
EP1193793A2 (de) * 2000-09-28 2002-04-03 Hitachi Kokusai Electric Inc. Antenne
EP1902505A2 (de) 2005-07-12 2008-03-26 Massachusetts Institute of Technology (MIT) Drahtlose strahlungslose energieübertragung
WO2009009559A1 (en) 2007-07-09 2009-01-15 Nigelpower, Llc Wireless energy transfer using coupled antennas
US20100277387A1 (en) * 2004-12-21 2010-11-04 Q-Track Corporation Space Efficient Magnetic Antenna Method
US8436780B2 (en) 2010-07-12 2013-05-07 Q-Track Corporation Planar loop antenna system
US9444265B2 (en) 2005-07-12 2016-09-13 Massachusetts Institute Of Technology Wireless energy transfer
US9831682B2 (en) 2008-10-01 2017-11-28 Massachusetts Institute Of Technology Efficient near-field wireless energy transfer using adiabatic system variations
US9997845B2 (en) 2004-12-21 2018-06-12 Q-Track Corporation Embedded symmetric multiple axis antenna system with isolation among the multiple axes

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE914984C (de) * 1950-08-05 1954-07-12 Max Grundig Drehbare magnetische Richtantenne

Cited By (38)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2438680A (en) * 1943-03-11 1948-03-30 Wladimir J Polydoroff Loop antenna apparatus
US2442310A (en) * 1943-06-14 1948-05-25 Wladimir J Polydoroff Directional antenna system
US2460492A (en) * 1946-10-30 1949-02-01 Hoffman Radio Corp Loop inductance compensator
US2581348A (en) * 1948-04-10 1952-01-08 Int Standard Electric Corp Antenna
US2824306A (en) * 1950-10-04 1958-02-18 Admiral Corp Antenna
US2915752A (en) * 1953-12-29 1959-12-01 Raytheon Co Directional antenna
US2953785A (en) * 1956-08-02 1960-09-20 Gasaccumulator Svenska Ab Arrangement for radio direction finding
US3078462A (en) * 1958-07-18 1963-02-19 Julius Herman One-turn loop antenna
US4441498A (en) * 1982-05-10 1984-04-10 Cardio-Pace Medical, Inc. Planar receiver antenna coil for programmable electromedical pulse generator
US4703278A (en) * 1984-10-09 1987-10-27 Texaco Inc. Well logging disc coil receiving means and method
EP1193793A2 (de) * 2000-09-28 2002-04-03 Hitachi Kokusai Electric Inc. Antenne
US20020053992A1 (en) * 2000-09-28 2002-05-09 Hitachi Kokusai Electric Inc. Antenna
EP1193793A3 (de) * 2000-09-28 2004-03-03 Hitachi Kokusai Electric Inc. Antenne
US6861992B2 (en) 2000-09-28 2005-03-01 Hitachi Kokusai Electric Inc. Antenna
US20100277387A1 (en) * 2004-12-21 2010-11-04 Q-Track Corporation Space Efficient Magnetic Antenna Method
US8922440B2 (en) 2004-12-21 2014-12-30 Q-Track Corporation Space efficient magnetic antenna method
US9997845B2 (en) 2004-12-21 2018-06-12 Q-Track Corporation Embedded symmetric multiple axis antenna system with isolation among the multiple axes
US9450421B2 (en) 2005-07-12 2016-09-20 Massachusetts Institute Of Technology Wireless non-radiative energy transfer
US9831722B2 (en) 2005-07-12 2017-11-28 Massachusetts Institute Of Technology Wireless non-radiative energy transfer
US11685271B2 (en) 2005-07-12 2023-06-27 Massachusetts Institute Of Technology Wireless non-radiative energy transfer
US11685270B2 (en) 2005-07-12 2023-06-27 Mit Wireless energy transfer
EP2306616B1 (de) 2005-07-12 2020-09-02 Massachusetts Institute of Technology (MIT) Drahtlose strahlungslose Energieübertragung
US9065286B2 (en) 2005-07-12 2015-06-23 Massachusetts Institute Of Technology Wireless non-radiative energy transfer
US9444265B2 (en) 2005-07-12 2016-09-13 Massachusetts Institute Of Technology Wireless energy transfer
US9450422B2 (en) 2005-07-12 2016-09-20 Massachusetts Institute Of Technology Wireless energy transfer
EP2306615B1 (de) 2005-07-12 2020-05-27 Massachusetts Institute of Technology (MIT) Drahtlose strahlungslose Energieübertragung
US9509147B2 (en) 2005-07-12 2016-11-29 Massachusetts Institute Of Technology Wireless energy transfer
US10666091B2 (en) 2005-07-12 2020-05-26 Massachusetts Institute Of Technology Wireless non-radiative energy transfer
EP1902505A2 (de) 2005-07-12 2008-03-26 Massachusetts Institute of Technology (MIT) Drahtlose strahlungslose energieübertragung
US10141790B2 (en) 2005-07-12 2018-11-27 Massachusetts Institute Of Technology Wireless non-radiative energy transfer
US10097044B2 (en) 2005-07-12 2018-10-09 Massachusetts Institute Of Technology Wireless energy transfer
US20090015075A1 (en) * 2007-07-09 2009-01-15 Nigel Power, Llc Wireless Energy Transfer Using Coupled Antennas
US9634730B2 (en) * 2007-07-09 2017-04-25 Qualcomm Incorporated Wireless energy transfer using coupled antennas
WO2009009559A1 (en) 2007-07-09 2009-01-15 Nigelpower, Llc Wireless energy transfer using coupled antennas
EP2168252A1 (de) * 2007-07-09 2010-03-31 Qualcomm Incorporated Drahtlose energieübertragung anhand gekoppelter antennen
EP2168252A4 (de) * 2007-07-09 2014-01-22 Qualcomm Inc Drahtlose energieübertragung anhand gekoppelter antennen
US9831682B2 (en) 2008-10-01 2017-11-28 Massachusetts Institute Of Technology Efficient near-field wireless energy transfer using adiabatic system variations
US8436780B2 (en) 2010-07-12 2013-05-07 Q-Track Corporation Planar loop antenna system

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BE482157A (de)
CH260212A (de) 1949-02-28
GB522492A (en) 1940-06-19

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