Search Images Maps Play YouTube News Gmail Drive More »
Sign in
Screen reader users: click this link for accessible mode. Accessible mode has the same essential features but works better with your reader.

Patents

  1. Advanced Patent Search
Publication numberUS2669646 A
Publication typeGrant
Publication dateFeb 16, 1954
Filing dateJan 20, 1950
Priority dateJan 20, 1950
Publication numberUS 2669646 A, US 2669646A, US-A-2669646, US2669646 A, US2669646A
InventorsFord Charles J
Original AssigneeGoodyear Tire & Rubber
Export CitationBiBTeX, EndNote, RefMan
External Links: USPTO, USPTO Assignment, Espacenet
Electrically conductive material
US 2669646 A
Abstract  available in
Images(2)
Previous page
Next page
Claims  available in
Description  (OCR text may contain errors)

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

Patent Citations
Cited PatentFiling datePublication dateApplicantTitle
US940151 *Oct 3, 1906Nov 16, 1909Gen ElectricResistance unit.
US1989282 *Aug 19, 1933Jan 29, 1935Gen Electric X Ray CorpElectrode
US2205543 *Nov 1, 1937Jun 25, 1940Maxime Ducret AndreHeating surface
US2274840 *Jun 7, 1941Mar 3, 1942Us Rubber CoElectrically conductive fabric
US2327756 *Oct 15, 1941Aug 24, 1943Us Rubber CoElectrically conductive fabric
US2386095 *Feb 18, 1944Oct 2, 1945Du PontHeating device
US2406367 *Nov 10, 1944Aug 27, 1946Honorary Advisory Council SciPrevention and removal of ice or frost on aircraft parts
US2473183 *Jul 16, 1947Jun 14, 1949Bates Mfg CoElectrically conductive fabric
US2503457 *Apr 4, 1947Apr 11, 1950Curtiss Wright CorpPropeller blade deicing shoe
US2559077 *Jul 1, 1946Jul 3, 1951Howard W JohnsonResistance element and method of preparing same
US2631219 *May 6, 1949Mar 10, 1953Charles T SuchyElectrical heating element
GB581212A * Title not available
Referenced by
Citing PatentFiling datePublication dateApplicantTitle
US2757273 *Dec 12, 1952Jul 31, 1956Goodyear Tire & RubberDe-icer
US2855495 *Sep 20, 1954Oct 7, 1958Statham Instrument IncTemperature control device
US3056005 *Aug 4, 1960Sep 25, 1962Larson Harry JMat switch and method of making the same
US3060303 *Jul 29, 1958Oct 23, 1962George A SkoglundHeating element
US3094452 *Jul 23, 1956Jun 18, 1963Sued West Chemie GmbhMethod of making interlocked welded connections between shaped thermoplastic articles
US3287684 *Feb 27, 1964Nov 22, 1966Motson Services IncElectrical heating device
US3359524 *Sep 2, 1964Dec 19, 1967Ioco LtdFlexible heating elements
US3364402 *May 27, 1966Jan 16, 1968Bunker RamoOrthogonal code transmitting array
US3594547 *Dec 17, 1968Jul 20, 1971Space Age Products Sales LtdElectrical heaters
US3940592 *Nov 29, 1973Feb 24, 1976Matsushita Electric Industrial Co., Ltd.Electrically heated alignment pad
US3973234 *Oct 8, 1974Aug 3, 1976Universal Oil Products CompanyPrecision type resistor
US4058704 *Dec 8, 1975Nov 15, 1977Taeo KimCoilable and severable heating element
US4296855 *Feb 27, 1980Oct 27, 1981The B. F. Goodrich CompanyElectrically conductive fabric
US4533821 *Sep 15, 1983Aug 6, 1985Ryoda SatoHeating sheet
US8441156Sep 2, 2009May 14, 2013T-Ink, Inc.Electrically conductive module
Classifications
U.S. Classification338/208, 338/323, 338/322, 338/254, 174/133.00R, 174/74.00R, 174/117.00R, 338/308, 338/275, 219/545, 338/331, 442/210, 338/203, 338/211
International ClassificationH05B3/06, D06Q1/04, H01B1/22, D06Q1/00, H05B3/68, H05B3/34
Cooperative ClassificationH05B3/06, H05B2203/013, H05B3/347, H05B2203/017, H01B1/22, H05B3/688, H05B2203/011, D06Q1/04, H05B2203/005, H05B2203/036
European ClassificationH05B3/34B4, H01B1/22, H05B3/68Z, D06Q1/04, H05B3/06