US2669646A - Electrically conductive material - Google Patents

Electrically conductive material Download PDF

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US2669646A
US2669646A US13955150A US2669646A US 2669646 A US2669646 A US 2669646A US 13955150 A US13955150 A US 13955150A US 2669646 A US2669646 A US 2669646A
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Prior art keywords
electrically conductive
fabric
conductive material
wires
composite
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Charles J Ford
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Goodyear Tire and Rubber Co
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Goodyear Tire and Rubber Co
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Priority to US13955150 priority Critical patent/US2669646A/en
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    • DTEXTILES; PAPER
    • D06TREATMENT OF TEXTILES OR THE LIKE; LAUNDERING; FLEXIBLE MATERIALS NOT OTHERWISE PROVIDED FOR
    • D06QDECORATING TEXTILES
    • D06Q1/00Decorating textiles
    • D06Q1/04Decorating textiles by metallising
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01BCABLES; CONDUCTORS; INSULATORS; SELECTION OF MATERIALS FOR THEIR CONDUCTIVE, INSULATING OR DIELECTRIC PROPERTIES
    • H01B1/00Conductors or conductive bodies characterised by the conductive materials; Selection of materials as conductors
    • H01B1/20Conductive material dispersed in non-conductive organic material
    • H01B1/22Conductive material dispersed in non-conductive organic material the conductive material comprising metals or alloys
    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05BELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
    • H05B3/00Ohmic-resistance heating
    • H05B3/02Details
    • H05B3/06Heater elements structurally combined with coupling elements or holders
    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05BELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
    • H05B3/00Ohmic-resistance heating
    • H05B3/20Heating elements having extended surface area substantially in a two-dimensional plane, e.g. plate-heater
    • H05B3/34Heating elements having extended surface area substantially in a two-dimensional plane, e.g. plate-heater flexible, e.g. heating nets or webs
    • H05B3/342Heating elements having extended surface area substantially in a two-dimensional plane, e.g. plate-heater flexible, e.g. heating nets or webs heaters used in textiles
    • H05B3/347Heating elements having extended surface area substantially in a two-dimensional plane, e.g. plate-heater flexible, e.g. heating nets or webs heaters used in textiles woven fabrics
    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05BELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
    • H05B3/00Ohmic-resistance heating
    • H05B3/68Heating arrangements specially adapted for cooking plates or analogous hot-plates
    • H05B3/688Fabrication of the plates
    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05BELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
    • H05B2203/00Aspects relating to Ohmic resistive heating covered by group H05B3/00
    • H05B2203/002Heaters using a particular layout for the resistive material or resistive elements
    • H05B2203/005Heaters using a particular layout for the resistive material or resistive elements using multiple resistive elements or resistive zones isolated from each other
    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05BELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
    • H05B2203/00Aspects relating to Ohmic resistive heating covered by group H05B3/00
    • H05B2203/011Heaters using laterally extending conductive material as connecting means
    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05BELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
    • H05B2203/00Aspects relating to Ohmic resistive heating covered by group H05B3/00
    • H05B2203/013Heaters using resistive films or coatings
    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05BELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
    • H05B2203/00Aspects relating to Ohmic resistive heating covered by group H05B3/00
    • H05B2203/017Manufacturing methods or apparatus for heaters
    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05BELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
    • H05B2203/00Aspects relating to Ohmic resistive heating covered by group H05B3/00
    • H05B2203/036Heaters specially adapted for garment heating
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T442/00Fabric [woven, knitted, or nonwoven textile or cloth, etc.]
    • Y10T442/30Woven fabric [i.e., woven strand or strip material]
    • Y10T442/3179Woven fabric is characterized by a particular or differential weave other than fabric in which the strand denier or warp/weft pick count is specified
    • Y10T442/322Warp differs from weft
    • Y10T442/3228Materials differ
    • Y10T442/3236Including inorganic strand material

Definitions

  • the present invention relates to an improved form of electrically conductive material and the method of making the same. More particularly, the invention is concerned with a composite form of electrically conductive material embodying integrally formed conductors therein.
  • An electrically conductive material of the type with which the teachings of the present invention are advantageously employed is any flexible material such, for example, as a thin plastic film or sheet, woven fabric, and the like on which a thin continuous deposit or coating has been formed rendering the normally non-conducting material capable of carrying an electrical current.
  • a cloth fabric woven from threads of natural or synthetic origin or from a mixture of both is particularly well suited to such use and electrically conductive properties can be readily imparted to it in the manner suggested above.
  • connections While they can be accomplished by soldering or brazing, are exceedingly bulky and susceptible to parting or breaking, especially where the connections are subjected in the normal use of the electrically conductive flexible material to vibrations of high frequency. Conditions of this nature are found, for example, in the use of such treated material in the fabrication of de-icing equipment for aircraft and the like. This represents only one of many such uses for the material possessing comparable conditions affecting the security of electrical connections thereto.
  • Fig. 1 represents a partial plan view of a segment of a composite cloth fabric of the type 2 employed to advantage in the practice of the present invention.
  • Fig. 2 illustrates the composite fabric of Fig. l to which a coating of an electrically conductive material and a dressing has been applied with an electrical circuit shown diagrammatically.
  • Fig. 3 is a fragmentary enlarged cross section of an article, for example, a heating element comprising a core of material such as that shown in Fig. 2 and exposed laminae .Q insulating material.
  • Fig. 4 shows a plastic film having metallic conductors attached and coated with an electrically conductive material.
  • Fig. 5 is an enlarged cross section of the article shown in Fig. 4 and taken along the line 55 therein.
  • Fig. 6 is a diagrammatic representation of an electrical circuit especially adapted to use with the article illustrated in Fig. 4.
  • the reference numeral I identifies a composite structure or fabric.
  • the composite fabric I is made up of a plurality of weft or woof threads 2 extending transversely of the material and a plurality of warp threads 3 extending in a longitudinal direction or normal to the woof.
  • a plurality of metal wires or strands of electrically conductive material such, for example, as the metal Wires 4 are substituted for certain of the warp threads so as to provide a distinct area, strip, or selvage 5 in the body of the fabric.
  • the metal wires 4 may extend in either direction and, moreover, may be arranged together in spaced groups or areas, each advantageously including a plurality of strands, throughout the body of the material depending upon the use to which the composite fabric I is to be put. Moreover, the metal strands or wires 4 can be sewn or otherwise secured to the fabric in restricted areas thereof. In any event, it should be understood that the use of the strip or selvage' 5 adjacent the edge of the composite fabric I is found to be advantageous for certain specific uses to which the material is to be put, but is by no means restrictive of the invention.
  • the core 5 illustrated in Fig. 2 represents the composite fabric I to which a sheath or coating 1 has been applied.
  • This sheath or coating embodies an electrically conductive substance which is intimately bonded to the woof and warp threads 2 and 3, as well as to the metal wires 4 so as to form a homogeneous covering over the entire width of the composite fabric, but not necessarily filling the voids in the fabric.
  • the wires 4 forming the selvage portion 5 of the composite fabric 3 I are adapted to be compacted, twisted, or gathered together in the manner indicated by the reference numeral 8 so as to provide a satisfactory connection for the electrical conductors 9 and I6 between which is disposed a source of electrical energy such, for example, as the battery I.
  • 5 may advantageously be employed to vfacilitate the connection of the conductors 9 and to the ends of the individual groups or gathers 8 of the wires at the ends of the selvage portions 5.
  • the electrically conductive substance used in the coating 1 applied to the composite tab'ric I may take any of several forms. ,It may take the form of a chemically deposited metallic sub"- stance, such as metallic silver deposited frcr'n a silver nitrate solution. A coating'i of copper er other suitable electrically conductive 'r'netals may be formed on the components of the composite fabric by an electrochemical or plating process. It is essential that a substantially continuous sheath or coating be formed ever the composite fabric I so as to insure a uniform particle-toparticle contact over the entire surface "of the fabric. Other external dressings maybe applied over the coating 1. I I I
  • the completed core 6 is particularly well suited to incor oration in a laminated structure in which the cure is completely enclosed in sheaths of suitable insulating and moisture resistant .-l-flt terial l2 and -
  • These sheaths of insulating material i2 and i3 may advantageously be relatively thin layers or vulcanized or unvulcanize'd rubber v'vh'i'ch, in the latter instance, are subsequently vulcanized.
  • This construction is particularly well adapted to be afix'ed by 'a suitable bonding agent to a surface, such, for example, as that of a propeller or the wing surfaces of an airplane. Electrical current then suppliedL to the core 8 or the completed structure It serves to facilitate the removal cf ice collecting upon exposed surface.
  • the referencenumeral l'l generally identifies the composite structure.
  • the composite structure embodies a plastic sheet 18 which carries a plurality "of continuous electrically conducting strands or wires t9 arranged in a plurality of spaced mutually parallel :gr'o'ups 2
  • the individual 'wires H which must be exposed, are advantageously secured to the plastic "sheet 18 as by means of a thin :layer of an --elem'ent -or other type of electrical unit.
  • , 22, and 23 set up a complex electrical circuit diagrammatically illustrated in Fig. 6.
  • the plastic sheet H! of the composite structure I! with the coating 24 comprises a plate resistor in cooperation with the several groups 20, 2
  • a series of mutually parallel circuits is formed rm/owing the several groups 26, 2
  • and 22, 22 and 23 represent individual mutually parallel resistances.
  • the resistance circuit 29 represents that set up on the coated plastic sheet 18 between the jc'ooperating groups 29 and 2
  • the resistance 30 represents the completed circuit across the coated plastic sheet l8 between the groups 2
  • the resistance 3! represents the completed circuit across the coated plastic sheet between groups 22 and 23 of Wires l9.
  • a n electrically conductive material ccmpri'sin'g a woven fabric of normally ncn-conductix e warp and woof threads with'certa-in of the warp threads at least two -'spaced mutually parallel areas of the fabri'e adjac'ent the edges thereof being replaced by substantially continuous line wires having electrically conductive properties to form a composite fabric with integrally formed strips of metal thereingand a uniform coating of an electrically conductive metal extending over both the non-conductive threads and the conductive wires in the composite fabri'c.

Description

Feb. 16, 1954 c. J. FORD ELECTRICAL-LY CONDUCTIVE MATERIAL 2 SheefLs-Sheet 1 Filed Jan. 20, 1950 Charles J Ford ATTORNEY Feb. 16, 1954 c. J. FORD 2,669,646
ELECTRICAL-LY CONDUCTIVE MATERIAL Filed Jan. 20., 1950 2 Sheets-Sheet 2 FIG. 4
7 FIG. 6 W
- Charles J. Ford 25 'III/IIIIIIII/IIIIIIII.
FlG. 5 Ki ATTO R N EY Patented Feb. 16, 1954 ELECTRICALLY CONDUCTIVE IVIATERIAL Charles J. Ford, Akron, Ohio, assignor, by mesne assignments, to The Goodyear Tire & Rubber Company, a corporation of Ohio Application January 20, 1950, Serial No. 139,551
1 Claim. 1
The present invention relates to an improved form of electrically conductive material and the method of making the same. More particularly, the invention is concerned with a composite form of electrically conductive material embodying integrally formed conductors therein. v
An electrically conductive material of the type with which the teachings of the present invention are advantageously employed is any flexible material such, for example, as a thin plastic film or sheet, woven fabric, and the like on which a thin continuous deposit or coating has been formed rendering the normally non-conducting material capable of carrying an electrical current. A cloth fabric woven from threads of natural or synthetic origin or from a mixture of both is particularly well suited to such use and electrically conductive properties can be readily imparted to it in the manner suggested above.
One of the problems frequently encountered in the use of such electrically conductive flexible material, however, has been the difliculty experienced in satisfactorily securing electrical conductors or connections to the electrically conductive material itself.
Such connections, while they can be accomplished by soldering or brazing, are exceedingly bulky and susceptible to parting or breaking, especially where the connections are subjected in the normal use of the electrically conductive flexible material to vibrations of high frequency. Conditions of this nature are found, for example, in the use of such treated material in the fabrication of de-icing equipment for aircraft and the like. This represents only one of many such uses for the material possessing comparable conditions affecting the security of electrical connections thereto.
It is, therefore, an object of the present invention to obviate any and all such difficulties as are encountered in the provision of a secure electrical connection to the fabric by an improved method of forming the flexible material itself.
It is a further object of the present invention to provide an electrically conductive material in which the strands comprising the electrical conductors are intimately secured to or formed integrally with the material itself, thereby producing a completely homogeneous product.
Other objects and advantages of the invention will become apparent as the following description of one specific application of the inventive concept proceeds.
Fig. 1 represents a partial plan view of a segment of a composite cloth fabric of the type 2 employed to advantage in the practice of the present invention. Fig. 2 illustrates the composite fabric of Fig. l to which a coating of an electrically conductive material and a dressing has been applied with an electrical circuit shown diagrammatically. Fig. 3 is a fragmentary enlarged cross section of an article, for example, a heating element comprising a core of material such as that shown in Fig. 2 and exposed laminae .Q insulating material. Fig. 4 shows a plastic film having metallic conductors attached and coated with an electrically conductive material. Fig. 5 is an enlarged cross section of the article shown in Fig. 4 and taken along the line 55 therein. Fig. 6 is a diagrammatic representation of an electrical circuit especially adapted to use with the article illustrated in Fig. 4.
In Fig. 1 of the drawings, the reference numeral I identifies a composite structure or fabric. The composite fabric I is made up of a plurality of weft or woof threads 2 extending transversely of the material and a plurality of warp threads 3 extending in a longitudinal direction or normal to the woof. At or adjacent the edges of the composite fabric I, a plurality of metal wires or strands of electrically conductive material such, for example, as the metal Wires 4 are substituted for certain of the warp threads so as to provide a distinct area, strip, or selvage 5 in the body of the fabric.
It will be readily understood that the metal wires 4 may extend in either direction and, moreover, may be arranged together in spaced groups or areas, each advantageously including a plurality of strands, throughout the body of the material depending upon the use to which the composite fabric I is to be put. Moreover, the metal strands or wires 4 can be sewn or otherwise secured to the fabric in restricted areas thereof. In any event, it should be understood that the use of the strip or selvage' 5 adjacent the edge of the composite fabric I is found to be advantageous for certain specific uses to which the material is to be put, but is by no means restrictive of the invention.
The core 5 illustrated in Fig. 2 represents the composite fabric I to which a sheath or coating 1 has been applied. This sheath or coating embodies an electrically conductive substance which is intimately bonded to the woof and warp threads 2 and 3, as well as to the metal wires 4 so as to form a homogeneous covering over the entire width of the composite fabric, but not necessarily filling the voids in the fabric. The wires 4 forming the selvage portion 5 of the composite fabric 3 I are adapted to be compacted, twisted, or gathered together in the manner indicated by the reference numeral 8 so as to provide a satisfactory connection for the electrical conductors 9 and I6 between which is disposed a source of electrical energy such, for example, as the battery I. The clips I4 and |5 may advantageously be employed to vfacilitate the connection of the conductors 9 and to the ends of the individual groups or gathers 8 of the wires at the ends of the selvage portions 5.
The electrically conductive substance used in the coating 1 applied to the composite tab'ric I may take any of several forms. ,It may take the form of a chemically deposited metallic sub"- stance, such as metallic silver deposited frcr'n a silver nitrate solution. A coating'i of copper er other suitable electrically conductive 'r'netals may be formed on the components of the composite fabric by an electrochemical or plating process. It is essential that a substantially continuous sheath or coating be formed ever the composite fabric I so as to insure a uniform particle-toparticle contact over the entire surface "of the fabric. Other external dressings maybe applied over the coating 1. I I
The completed core 6 is particularly well suited to incor oration in a laminated structure in which the cure is completely enclosed in sheaths of suitable insulating and moisture resistant .-l-flt terial l2 and -|3 as indicated in Fig. 3. These sheaths of insulating material i2 and i3 may advantageously be relatively thin layers or vulcanized or unvulcanize'd rubber v'vh'i'ch, in the latter instance, are subsequently vulcanized. This construction is particularly well adapted to be afix'ed by 'a suitable bonding agent to a surface, such, for example, as that of a propeller or the wing surfaces of an airplane. Electrical current then suppliedL to the core 8 or the completed structure It serves to facilitate the removal cf ice collecting upon exposed surface.
-In Figs. 4, '5, and *6 is shown another type of "flexible material, in this instance, a thin plastic film or sheet. The referencenumeral l'l generally identifies the composite structure. The composite structure embodies a plastic sheet 18 which carries a plurality "of continuous electrically conducting strands or wires t9 arranged in a plurality of spaced mutually parallel :gr'o'ups 2|), 2|, 22, 23, the whole being covered with a uniform coating 24 of an electrically conductive substance such, .for example, as 'a metal of the ;class including silver, gold, copper, and the like ortheir alloys. The individual 'wires H), which must be exposed, are advantageously secured to the plastic "sheet 18 as by means of a thin :layer of an --elem'ent -or other type of electrical unit.
With a composite structure of the type illustrated in Fig. 4 of the drawings, the several groups 20, 2|, 22, and 23 set up a complex electrical circuit diagrammatically illustrated in Fig. 6. In other words, the plastic sheet H! of the composite structure I! with the coating 24 comprises a plate resistor in cooperation with the several groups 20, 2|, 22, and 23 of wires |9. Thus, a series of mutually parallel circuits is formed rm/owing the several groups 26, 2|, 22, and 23, as shown in Fi 6.
The several cooperating groups 20 and 2|, 2| and 22, 22 and 23 represent individual mutually parallel resistances. The resistance circuit 29 represents that set up on the coated plastic sheet 18 between the jc'ooperating groups 29 and 2| of the wires l9. "The resistance 30 represents the completed circuit across the coated plastic sheet l8 between the groups 2| and 22. Similarly, the resistance 3! represents the completed circuit across the coated plastic sheet between groups 22 and 23 of Wires l9.
'Ma-ny other highly advantageous uses of the material will readily suggest themselves to those skilled in the art such, for example, as heating wall panels, enclosures for oil tanks to insure elevated temperatures of the contents, heated clothing, and 'm-any other similar uses. It will be understood that while certain representative embodiments and details have been shown for the purpose of illustrating the invention, it will be apparent to those skilled in this art that various changes and modifications may be made therein without departing from the spirit or scope or the invention.
1 claim:
A n electrically conductive material ccmpri'sin'g a woven fabric of normally ncn-conductix e warp and woof threads with'certa-in of the warp threads at least two -'spaced mutually parallel areas of the fabri'e adjac'ent the edges thereof being replaced by substantially continuous line wires having electrically conductive properties to form a composite fabric with integrally formed strips of metal thereingand a uniform coating of an electrically conductive metal extending over both the non-conductive threads and the conductive wires in the composite fabri'c.
. CHARLES J.
References Cited. in the file of this patent UNITED STATES PATENTS Nu -nicer Name Date Modal. l leath Nov. '16, I909 inseam nimble Jan. 29, 19st 2305,54; Rideau et al. June 25, T9 11) -2r,27 l,;8fltl lviarick et a1. a Mar. '3, 1942 2,327,756 Adamson Aug. 24, 1943 2,386,095 Edgar et all. 00 13. 2, 1 945 anodes? Griffith et-al. Aug. 27,1946 2, 4;7' 3,l. 33 Watson June 14,1949 2, i' 0i, l 5 '7 $pe ir e't-al. Apr. 11, I950 2,5594) Johnson et a1. July 3-, :1 2,631,219 Suchy Mar. 1O, I953 FGREZEGN PATENTS l luziiber "Country Date 581,212 Great "Britain Oct. 4, T946
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Cited By (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2757273A (en) * 1952-12-12 1956-07-31 Goodyear Tire & Rubber De-icer
US2855495A (en) * 1954-09-20 1958-10-07 Statham Instrument Inc Temperature control device
US3056005A (en) * 1960-08-04 1962-09-25 Harry J Larson Mat switch and method of making the same
US3060303A (en) * 1958-07-29 1962-10-23 George A Skoglund Heating element
US3094452A (en) * 1955-07-23 1963-06-18 Sued West Chemie Gmbh Method of making interlocked welded connections between shaped thermoplastic articles
US3287684A (en) * 1964-02-27 1966-11-22 Motson Services Inc Electrical heating device
US3359524A (en) * 1963-11-11 1967-12-19 Ioco Ltd Flexible heating elements
US3364402A (en) * 1966-05-27 1968-01-16 Bunker Ramo Orthogonal code transmitting array
US3594547A (en) * 1967-12-23 1971-07-20 Space Age Products Sales Ltd Electrical heaters
US3940592A (en) * 1972-12-13 1976-02-24 Matsushita Electric Industrial Co., Ltd. Electrically heated alignment pad
JPS5150038A (en) * 1974-10-28 1976-05-01 Nippon Nonetsu Kk
US3973234A (en) * 1974-10-08 1976-08-03 Universal Oil Products Company Precision type resistor
US4058704A (en) * 1974-12-27 1977-11-15 Taeo Kim Coilable and severable heating element
US4296855A (en) * 1978-09-13 1981-10-27 The B. F. Goodrich Company Electrically conductive fabric
US4533821A (en) * 1982-12-11 1985-08-06 Ryoda Sato Heating sheet
US20100156196A1 (en) * 2008-09-03 2010-06-24 Usg Interiors, Inc. Electrically conductive element, system, and method of manufacturing
US20100170616A1 (en) * 2008-09-03 2010-07-08 Usg Interiors, Inc. Electrically conductive tape for walls and ceilings
US20100170702A1 (en) * 2008-09-03 2010-07-08 Usg Interiors, Inc. Electrically conductive module
CN102644137A (en) * 2011-02-21 2012-08-22 李查启学 Conductive yarn and cloth structure applying same
US20210307163A1 (en) * 2018-08-03 2021-09-30 Electroninks Incorporated Conductive materials and their methods of preparation by metallization with metal complex conductive ink compositions

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US940151A (en) * 1906-10-03 1909-11-16 Gen Electric Resistance unit.
US1989282A (en) * 1933-08-19 1935-01-29 Gen Electric X Ray Corp Electrode
US2205543A (en) * 1936-11-06 1940-06-25 Rideau Jean Robert Heating surface
US2274840A (en) * 1941-06-07 1942-03-03 Us Rubber Co Electrically conductive fabric
US2327756A (en) * 1941-10-15 1943-08-24 Us Rubber Co Electrically conductive fabric
US2386095A (en) * 1944-02-18 1945-10-02 Du Pont Heating device
US2406367A (en) * 1944-11-10 1946-08-27 Honorary Advisory Council Sci Prevention and removal of ice or frost on aircraft parts
GB581212A (en) * 1944-05-18 1946-10-04 Callender Suchy Developments L Improvements in electrically heated clothing, blankets and the like
US2473183A (en) * 1947-07-16 1949-06-14 Bates Mfg Co Electrically conductive fabric
US2503457A (en) * 1947-04-04 1950-04-11 Curtiss Wright Corp Propeller blade deicing shoe
US2559077A (en) * 1946-07-01 1951-07-03 Carl G Westerberg Resistance element and method of preparing same
US2631219A (en) * 1949-05-06 1953-03-10 Charles T Suchy Electrical heating element

Patent Citations (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US940151A (en) * 1906-10-03 1909-11-16 Gen Electric Resistance unit.
US1989282A (en) * 1933-08-19 1935-01-29 Gen Electric X Ray Corp Electrode
US2205543A (en) * 1936-11-06 1940-06-25 Rideau Jean Robert Heating surface
US2274840A (en) * 1941-06-07 1942-03-03 Us Rubber Co Electrically conductive fabric
US2327756A (en) * 1941-10-15 1943-08-24 Us Rubber Co Electrically conductive fabric
US2386095A (en) * 1944-02-18 1945-10-02 Du Pont Heating device
GB581212A (en) * 1944-05-18 1946-10-04 Callender Suchy Developments L Improvements in electrically heated clothing, blankets and the like
US2406367A (en) * 1944-11-10 1946-08-27 Honorary Advisory Council Sci Prevention and removal of ice or frost on aircraft parts
US2559077A (en) * 1946-07-01 1951-07-03 Carl G Westerberg Resistance element and method of preparing same
US2503457A (en) * 1947-04-04 1950-04-11 Curtiss Wright Corp Propeller blade deicing shoe
US2473183A (en) * 1947-07-16 1949-06-14 Bates Mfg Co Electrically conductive fabric
US2631219A (en) * 1949-05-06 1953-03-10 Charles T Suchy Electrical heating element

Cited By (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2757273A (en) * 1952-12-12 1956-07-31 Goodyear Tire & Rubber De-icer
US2855495A (en) * 1954-09-20 1958-10-07 Statham Instrument Inc Temperature control device
US3094452A (en) * 1955-07-23 1963-06-18 Sued West Chemie Gmbh Method of making interlocked welded connections between shaped thermoplastic articles
US3060303A (en) * 1958-07-29 1962-10-23 George A Skoglund Heating element
US3056005A (en) * 1960-08-04 1962-09-25 Harry J Larson Mat switch and method of making the same
US3359524A (en) * 1963-11-11 1967-12-19 Ioco Ltd Flexible heating elements
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