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US20030199947A1 - Thermoplastic laminate fabric heater and methods for making same - Google Patents

Thermoplastic laminate fabric heater and methods for making same Download PDF

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Publication number
US20030199947A1
US20030199947A1 US10/293,204 US29320402A US2003199947A1 US 20030199947 A1 US20030199947 A1 US 20030199947A1 US 29320402 A US29320402 A US 29320402A US 2003199947 A1 US2003199947 A1 US 2003199947A1
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United States
Prior art keywords
heater
layer
thermoplastic
bus bars
fabric
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Abandoned
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US10/293,204
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Alan Gardner
Andrew Miller
John Rolls
Jeff Parkin
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Individual
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Individual
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Priority to US10/293,204 priority Critical patent/US20030199947A1/en
Publication of US20030199947A1 publication Critical patent/US20030199947A1/en
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/22Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
    • B32B5/24Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
    • B32B5/26Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/68Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks
    • B29C70/82Forcing wires, nets or the like partially or completely into the surface of an article, e.g. by cutting and pressing
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/88Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts characterised primarily by possessing specific properties, e.g. electrically conductive or locally reinforced
    • B29C70/882Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts characterised primarily by possessing specific properties, e.g. electrically conductive or locally reinforced partly or totally electrically conductive, e.g. for EMI shielding
    • B29C70/885Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts characterised primarily by possessing specific properties, e.g. electrically conductive or locally reinforced partly or totally electrically conductive, e.g. for EMI shielding with incorporated metallic wires, nets, films or plates
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B17/00Layered products essentially comprising sheet glass, or glass, slag, or like fibres
    • B32B17/02Layered products essentially comprising sheet glass, or glass, slag, or like fibres in the form of fibres or filaments
    • B32B17/04Layered products essentially comprising sheet glass, or glass, slag, or like fibres in the form of fibres or filaments bonded with or embedded in a plastic substance
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D15/00De-icing or preventing icing on exterior surfaces of aircraft
    • B64D15/12De-icing or preventing icing on exterior surfaces of aircraft by electric heating
    • 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
    • H05B3/36Heating elements having extended surface area substantially in a two-dimensional plane, e.g. plate-heater flexible, e.g. heating nets or webs heating conductor embedded in insulating material
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B38/00Ancillary operations in connection with laminating processes
    • B32B38/04Punching, slitting or perforating
    • B32B2038/047Perforating
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2305/00Condition, form or state of the layers or laminate
    • B32B2305/10Fibres of continuous length
    • B32B2305/18Fabrics, textiles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2305/00Condition, form or state of the layers or laminate
    • B32B2305/10Fibres of continuous length
    • B32B2305/20Fibres of continuous length in the form of a non-woven mat
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00Properties of the layers or laminate
    • B32B2307/20Properties of the layers or laminate having particular electrical or magnetic properties, e.g. piezoelectric
    • B32B2307/202Conductive
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2315/00Other materials containing non-metallic inorganic compounds not provided for in groups B32B2311/00 - B32B2313/04
    • B32B2315/08Glass
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2398/00Unspecified macromolecular compounds
    • B32B2398/20Thermoplastics
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B37/00Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B32B37/14Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers
    • B32B37/16Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers with all layers existing as coherent layers before laminating
    • B32B37/20Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers with all layers existing as coherent layers before laminating involving the assembly of continuous webs only
    • B32B37/203One or more of the layers being plastic
    • 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
    • H05B2203/026Heaters specially adapted for floor heating
    • 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
    • H05B2203/029Heaters specially adapted for seat warmers
    • 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
    • H05B2203/033Heater including particular mechanical reinforcing 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
    • H05B2203/036Heaters specially adapted for garment heating

Definitions

  • the invention relates to a heater element, a heater and a process for producing the heater element and heater.
  • the heater comprises an electrically conductive fabric layer laminated between two layers of glass fiber-reinforced thermoplastic films.
  • the heater further comprises bus bars and electrical leads, it is produced by consolidating the layers of film and fabrics into a single sheet heater.
  • the heater can be produced having variable geometry, electrical supply voltage and power.
  • the heater of the invention are more durable than prior art heater s because they are able to withstand more mechanical, chemical, ultraviolet radiation and other environmental stresses than prior art heaters.
  • Laminate or film heaters of the prior art have been made using metal foil, wires and electrically conductive fabrics laminated together using resins in between the layers to bond the integral layers together. Heaters manufactured from wire and foil have been used in industry for some time. In particular, such wire and foil heaters when used, for example, in the aerospace industry for deicing structures such as airplane wings and jet engine inlets, suffer from fatigue failure while in use, which considerably shortens their life when compared to fabrics. In addition, foil heaters, in particular, are expensive to produce and lack flexibility.
  • Laminate fabric heaters of the prior art have been made with woven or non-oven fabrics containing fibers, which are electrically conductive fibers such as carbon fibers, and nonconductive fibers such as polyester.
  • Non-conductive fibers for use in heaters are usually coated with a metal so that they can conduct the current via the metal coat, or the fibers are dispersed in a resin containing conductive particles, such as carbon black or iron particles.
  • Conductive fibers can also be coated with a metal to improve their conductive properties.
  • Carbon fibers consolidated into a random, non-woven fabric or veil have been used in the art for shielding against electromagnetic interference.
  • Conductive fabrics used in heaters for deicing and anti-icing aerospace structures are disclosed in, for example, U.S. Pat. No. 5,344,696 to Hastings et al. discloses an integrally bonded laminate that is used to thermally control a surface of an aircraft to which the laminate is bonded.
  • the patent describes that the use of fabrics have numerous advantages over prior methods for deicing and heating airplane wings; for example, the conductive fiber is of low weight, and or permits nominal intrusion in terms of aerodynamics; it is easy to handle compared to wire and foil, and most notably, it allows the even distribution of heat.
  • U.S. Pat. No. 4,534,886 to Kraus et al. discloses an electrically conductive web composed of a non-woven sheet of conductive fibers and non-conductive fibers. The sheet is saturated with a dispersion containing conductive particles and is then dried.
  • the Kraus et al. heater element is used primarily in heating pads.
  • the patent also discloses that the fabric heater layers are laminated together using an epoxy resin.
  • U.S. Pat. No. 5,925,275 to Lawson discloses an electrically conductive composite heating assembly.
  • the assembly has an electrically conductive non-woven fiber layer laminated between layers of fiberglass and other dielectric material.
  • the assembly further has an abrasion resistant outer layer.
  • the heater element is used on aerospace structures as an ice protection system to withstand the repeated mechanical stress and thermal cycles encountered in extremely harsh aerospace environments.
  • This patent also discloses that the fabric heater is manufactured using adhesive resins to bond the layers of the heater assembly.
  • Conductive fabric heaters disclosed in UK Patent Application No. 2,285,729 to Gerrard are manufactured by baking a woven polymeric fabric to extreme temperatures in a multi-step process.
  • the resultant fabric heater is limited by flexibility in resistance goals and furthermore lack variability of its Temperature Coefficients of Resistance.
  • the patent discloses that the fabric heaters are primary useful for low voltage source operation.
  • heater designs as mentioned in Kraus, Hastings and Lawson suffer from expensive production methods and low operating temperatures.
  • Machine setup is difficult to modify for different applications especially due to the use of epoxy and other resins, which have problems difficult to overcome; such as cost, shelf life, operating temperature and chemical limitations, long curing cycles and toxicity precautions.
  • the addition of carbon black particles, polyaramid fibers (1), conductive adhesives (3), and multistage layer processing (2) contribute to the complexity and therefore the heater cost while limiting service temperature, suitability for complex designs, and high volume—low cost production.
  • the invention is directed to a laminated fabric heater element, a heater and a process for manufacturing the heater element and heater.
  • the heater of the invention has many advantages over prior art heaters in that it is thin, flexible, produces more uniform temperature, has high fatigue life, and can be mass produced at less costs.
  • the heaters of the invention can be operated at voltages ranging from millivolts to about 600 volts from either alternating current or direct current power supplies.
  • the heater element comprises a consolidated electrically conductive fabric layer, two bus bars, and two thermoplastic layers; wherein each bus bar is contacting opposing edges of the conductive fabric layer and the consolidated electrically conductive fabric layer and the bus bars are sandwiched between the thermoplastic layers forming a single sheet.
  • the electrically conductive fabric layer of the laminated fabric heater of the invention may be selected from a variety of conductive fibers.
  • the electrically conductive fabric layer comprises nickel-coated carbon fibers.
  • the laminated fabric heater element can further be attached to electrical leads at bus bars to form the heater.
  • the bus bars of the laminated heater can be made of various material such as copper, brass or silver foils. In a preferred embodiment, however, the bus bars are made of copper foils.
  • the laminated fabric heater of the invention can further comprise a glass veil disposed on the outer surfaces of the thermoplastic layers for additional reinforcement depending on the requirements for the heater application before the heater is formed into a single sheet.
  • thermoplastic films can be obtained from commercially available sources. While any thermoplastic film can be used, the heaters of the invention are preferably manufactured with polyetherimide, polyetheretherketone, polyethersulfone, polysulfone polyvinylidine fluoride, acetobutylstyrene, polyphenylene oxide and polyamide.
  • the laminated fabric heater can further comprise cuts perpendicular to and through at least one of the bus bars in a zig-zag pattern for creating a circuit and to increase the resistance of the heater to a desired value depending on the application.
  • the laminated fabric heater of the invention further comprises an outer layer of thermoplastic or silicon rubber for increasing the dielectric strength of the heater.
  • the process for making the laminated fabric heater of the invention is as follows: A first thermoplastic layer on a surface where the heater is to be assembled. A layer of the electrically conductive fabric is disposed on the first thermoplastic layer. Bus bars, preferably made of copper foil are disposed on opposing edges of the electrically conductive fabric layer so that the bus bars are in contact with the electrically conductive fabric layer and are parallel to one another. Once the bus bars are in contact with the conductive fabric, they can be attached to the conductive fabric by piercing a hole through the bus bar and fabric using a piercing rivetor apparatus. The action of piercing causes the metal displaced to form a hole to curl and flatten under the fabric, thereby securing the bus bars to the fabric.
  • thermoplastic layer is disposed on the electrically conductive fabric layer and bus bars to form a heater assembly.
  • the heater assembly is heated at suitable temperatures to a set thickness to consolidate the conductive fabric layer sandwiched in the thermoplastic film layers, thereby forming a single sheet heater.
  • the heater is transferred to a cooling chamber to quench the heater at its maximum consolidation state.
  • a glass fiber reinforcement layer can be disposed on the outer surfaces of the thermoplastic layers prior to consolidation and depending on the heater output requirement.
  • the process described above can be performed at a small scale to produce a small number of small heaters using a hydraulic press
  • the process can be adapted for manufacturing heater elements and heaters in high volume using a roller laminating apparatuses.
  • the heater element In roller lamination, the heater element is produced in a single long sheet of indefinite length and width, which length and width are only limited by the length and width of the starting materials and machinery used.
  • the heater element made through roller lamination can be stored in rolls, and heaters can be made from segments of the heater element as required.
  • the process comprises combining a layer of electrically conductive fabric from a roll supply with two metal foil bus bars, wherein the bus bars are positioned parallel to one another at opposing edges of and contacting the conductive fabric in the direction of the roll.
  • the bus bars are secured to the conductive fabric by making a hole in the conductive fabric and bus bar by piercing both components in a piercing rivetor apparatus as described above.
  • the conductive fabric layer containing bus bars are drawn between two layers of thermoplastic films forming a sandwich type structure assembly.
  • the heater assembly sandwich is then fed through a pinch roller, which had been preheated at a predetermined temperature and set at a predetermined pressure to cause gelling of the thermoplastic layers.
  • thermoplastic layer causes some of the thermoplastic to flow through the conductive fabric, fusing the films and consolidating the conductive fibers into a single sheet heater element.
  • the resultant single sheet fabric heater is drawn over a cooling chamber so that maximal consolidation of the layers is maintained.
  • Individual heaters can be made by cutting a section from the heater sheet roll with a tooling die or a water jet cutter, attaching electrical leads by ultrasonic welding and laminating it once more with a layer of thermoplastic, thereby maintaining the gap cut by the die or water jet and providing a final dielectric layer.
  • FIG. 1 is a schematic diagram of the process for making the laminated fabric heaters of the invention in a roller laminating apparatus.
  • FIGS. 2A and 2B are cross-sections of the heater element of the invention showing the various layers prior to consolidation without and with glass fiber veil respectively.
  • FIG. 3 is a schematic representation of the heater at various stages of manufacturing through the roller laminating process.
  • FIG. 4 is a schematic drawing illustrating a cut away view of the heater of the invention showing the cuts through the heater in a zig-zag pattern.
  • FIG. 5 is a schematic diagram showing the various stages C, E, F, H and J of the process of manufacturing the heater of the invention.
  • FIG. 6 is a schematic drawing of the heater of the invention shown in cross-section.
  • FIG. 7 is a schematic diagram illustrating a heater of the invention in which holes are perforated through the laminate.
  • the heater element of the invention comprises a layer of conductive fabric, two bus bars position at opposing edges of the fabric sandwiched between two outer layers of thermoplastic.
  • the conductive fabric can be made from various materials, which are known in the art and comprises electrically conductive fibers.
  • the conductive fabric comprises electrically conductive fibers, and most preferred carbon fibers, in particular, nickel-coated carbon fibers.
  • the conductive fibers are chopped fibers and are converted into a non-woven conductive fabric using paper making techniques. An organic binder is used to hold the fibers together in the fabric. The thickness, density fiber coating and predominant fiber direction of the fabric all determine the final resistivity of the heater. Depending on the size of the heater and power output required, the appropriate length of fabric layer can be cut from a supply roll or an entire roll can be used for mass producing the heater elements.
  • the electrically conductive fabric layer is consolidated. A consolidated conductive fabric layer results from the consolidating step during the laminating process.
  • Consolidation is a process by which the thermoplastic layers of the heater are brought to a gelling state under pressure during bonding of the heater and to a predetermined thickness, this causes the electrically conductive fibers of the conductive fabric to be brought into intimate contact with one another through the laminating process.
  • Carbon filaments are manufactured from a polymer fiber under high temperature and pressure within an inert environment.
  • the fibers can be coated with a metal, such as nickel, brass, silver or other suitable metal or a combination thereof, by one of several processes, tailoring the Temperature Coefficient of Resistance (the rate at which the electrical resistance of a medium changes as a result of a change in temperature) and resistivity of the final fabric.
  • Fibers are combined into a tow and chopped to a desired length between about 3 millimeters and 12 millimeters or longer. Fiber length is a major factor in determining the fabric's resistance, flexibility, and structural conformity and heat uniformity.
  • thermoplastic films for use in the heater of the invention can be of various types and are commercially available.
  • the thermoplastic films are polyetherimide (Ultem®, Westlake Plastics, Inc., PA), polyetherketone (Victrex®, Westlake Plastics, Inc. PA), polyamide (Kapton®, E. I.
  • Thermoplastic films have different gelling temperatures. Therefore, in the process of the invention, the temperature at which the pinch rollers or hydraulic press is set is determined by the type of thermoplastic film used. In the process of manufacturing the heaters of the invention, Ultem® is used at a temperature of approximately 275 ° C., and Vitrex® is used at 350 ° C.
  • FIG. 1 illustrates the high volume production process useful for making the laminated fabric heaters of the invention.
  • the process involves a roller laminating apparatus.
  • the starting materials are all provided in rolls, i.e., the conductive fabric 10 , the bus bar strips 12 , 14 , the thermoplastic film 16 , 18 , and as needed, the glass fiber veil 20 , 22 .
  • the conductive fabric and copper foil, or other suitable metal are laminated in glass fiber-reinforced thermoplastic film, feed wires are attached and the whole heater finally encapsulated.
  • the process starts with a roll of conductive fabric 10 , two rolls of thermoplastic film 16 , 18 , two rolls of copper foil 12 , 14 , and two rolls of glass fiber veil 20 , 22 .
  • the conductive fabric 10 pulled from a roll, is combined with copper foil 12 , 14 , of 2 mils in thickness, separated by some predetermined distance and applied parallel to each other, contacting the conductive fabric, and in the same direction of the conductive fabric roll 10 , although other orientations are possible.
  • the copper foil bus bars near the free edges of the roll.
  • the copper foil bus bars 12 , 14 and conductive fabric 10 are drawn together through a piercing rivetor 24 , whereby perforated upper and lower support plates maintain fabric and copper foil bus bars 12 , 14 in proximity and a pin like tapered needle of small dimension, compared to the width of the copper, is pressed through the copper foil and conductive fabric.
  • the needle is withdrawn and the area around the pierced hole is compressed. Compression may take the form of a roller or pair of rollers or a press rod fixture clamping from both sides.
  • the action of piercing the copper splits the copper into several petals, much like a flower. As the taper of the needle continues into the opening the petals are curled over, moving away and entrapping local fibers. Once compressed the fibers are permanently held and the copper is securely attached to the fabric. This portion of the process is optional, but adds in locating the copper.
  • thermoplastic films 16 , 18 From the pierce/riveting action of the copper foil bus bars the final products are ready for the first lamination using the thermoplastic films 16 , 18 .
  • the conductive fabric 10 with the copper foil bus bars attached, are drawn between the two layers of thermoplastic film 16 , 18 which is slightly wider (by about 1 to 6 mm) than the conductive fabric 10 .
  • the top layer of thermoplastic film 16 may be perforated prior to the first lamination process.
  • glass fiber veil 20 , 22 are added to both sides of the laminate stack.
  • the conductive fiber layer with copper foil bus bars, sandwiched in the thermoplastic films with or without a fiberglass veil, as shown in the cross-section in FIG. 2, are drawn together through pinch rollers 15 , 17 , which have been preheated at a predetermined temperature and set at a predetermined distance depending on the type and thickness of thermoplastic film and fabric used.
  • the layers of dry materials are heated and fused together by pinch rollers into a consolidated sheet of exact thickness. Temperatures and pressures are such that the thermoplastic heats sufficiently to flow through the conductive fabric, pierced copper bus and glass fiber veil.
  • the pinch roller separation is set to achieve proper consolidation of the sheet and most importantly the conductive fabric. Once consolidated, the conductive fabric will achieve its final resistivity.
  • thermoplastic film For any given combination of conductive fabric, thermoplastic film, and glass fiber veil experimentation has shown that consolidation must always be compressed to at least 110% of the thermoplastic film thickness.
  • the product can be graded and stored for future use or further processed into cut heaters of predetermined design. Once consolidated, the sheet heater is transferred to a cooling chamber 19 to maintain maximal degree of consolidation.
  • perpendicular cuts 26 can be made through the laminate through at least one of the bus bars, as shown in FIG. 3. This can be done from stock or during the running process after cooling the sheet heater.
  • the continuous laminated sheet is pulled through a cutting or slitting device.
  • the device could be a die cutter made to the desired shape, or a dynamic cutter such as a water jet or laser cutter which are commercially available.
  • a circuit pattern such as a serpentine or zig-zag can be cut thereby further increasing the resistance to the desired value, by increasing the electrical path.
  • a first cut is made from outside copper edge to outside copper edge but within the maximum width of the thermoplastic layers. Cuts 26 such as this define a starting and stopping edge.
  • FIGS. 3 - 5 illustrate how circuits of even or odd number of strips can be created and thus affect wire placement.
  • wire attachment for each heater would be made on one side.
  • odd numbered-strip circuits the wires would be attached at opposite sides.
  • Electrical leads in the form of wires can be attached to the copper foil bus through the thermoplastic or perforations within the thermoplastic and at the location defining the beginning and end of the zig-zag pattern. Attachment would be accomplished by currently know methods such as solder, brazing, ultrasonic welding or crimping, and catered to the temperature, and electrical application requirements of the heater.
  • FIGS. 3 - 6 also show that once wires leads are attached, the heater is finally encapsulated to hold the element strips in place, increase the dielectric strength of the heater, and protect the circuit and wire attachment points.
  • the final encapsulating layer can either be additional thermoplastic layers, or other suitable dielectric materials, such as silicone rubber. If themoplastic films are used as the encapsulating layers, then the continuous, laminated heater sheet is drawn into another roll stack laminating machine where one additional layer of thermoplastic is fused to each side of the circuit, encapsulating the circuit and wire attachment points. An extra layer of thicker thermoplastic film may be added to the laminate stack at the same time to locally reinforce the heater around the wire attachment points.
  • the top roller should be coated with a layer of heat resisting rubber, e.g. silicone rubber, to enable the top thermoplastic film to be encapsulated over the top of the raised wire attachment points.
  • FIG. 5 illustrates also the final cutting stage of the process.
  • transverse cuts are made through the sheet product to separate the heaters from each other.
  • this can be achieved using die cutting techniques, water jet or laser cutting methods.
  • holes can be perforated at predetermined locations within the laminate as shown in FIG. 7. If perforations are provided in the laminate heater to facilitate encapsulation, additional layers of thermoplastic film or silicone rubber are added with perforations, or added after the second encapsulation is complete. Perforations of the second layers are of slightly smaller dimension, provided there is a need for a dielectric layer around the opening.
  • the heaters of the invention can be used in multiple applications depending on the heat requirements. Power can be delivered by means of single-use batteries, rechargeable batteries, power adapters, and generator derived systems such as wall supply, portable generators, solar energy and industrial transformers. Examples of the heaters of the invention in some low voltage applications, from millivolts to about 5 volts include, novelty gift items such as heated cards, coasters and eye mask; toys such as kitchen sets; electronic sensors for heating and deicing; personal rechargeable appliances such as hair curlers, and personal warmers such as ear muffs, gloves, socks, hats and the like.
  • Heater applications requiring medium voltage from about 6 to 28 volts include, for example, car parts and accessories such as floor mats, steering wheel, seats, door panel and mirror defrosters; motorcycle grips, mirrors, seat pad, tank and helmets; aircraft wings, propellers, floors, seats, instruments, controls, interior panels, galley and lavatory seats; in boats including ferry seats, deck, railings, galley and lavatory; warming counter and waste tanks in recreational vehicles; in other applications including, solar powered heating panel, pillows, electrical component/cabinet heaters, food preparation applications.
  • car parts and accessories such as floor mats, steering wheel, seats, door panel and mirror defrosters; motorcycle grips, mirrors, seat pad, tank and helmets; aircraft wings, propellers, floors, seats, instruments, controls, interior panels, galley and lavatory seats; in boats including ferry seats, deck, railings, galley and lavatory; warming counter and waste tanks in recreational vehicles; in other applications including, solar powered heating panel, pillows, electrical component/cabinet heaters,
  • Heater applications requiring high voltage from about 110 to about 250 volts single phase include, for example, aircraft wings, propellers, rotors, cowlings, inlets; household items such as appliances, room heaters (wall and floor), countertop warmers, firewood preheater/drier, walkways, driveways, steps, antenna pillows, food preparation; and commercial/industrial goods such as liquid drum heaters, ovens, shop space, machine processes, tools/dies, and the like.
  • Heater applications requiring the highest voltage, from about 208 to 600 volts multiphase include, commercial/industrial goods such as liquid drum (band) heaters, ovens, shop space, machine processes, tools/dies, transmitter/receiver of reflector antennas, electrical (signal) relay/component cabinets; large commercial and military aircrafts heaters for deicing parts, and the like.
  • commercial/industrial goods such as liquid drum (band) heaters, ovens, shop space, machine processes, tools/dies, transmitter/receiver of reflector antennas, electrical (signal) relay/component cabinets; large commercial and military aircrafts heaters for deicing parts, and the like.
  • the heater will have 4 strips of 11.38 mm width, produce 2.88 watts of power from 24 volts and deliver 0.08 watts per square centimeter at room temperature. Maximum temperature in air would be approximately 120° C. All the necessary materials are cut to the appropriate dimensions.
  • Four thermoplastic films, preferably Polyetherimide (PEI) of 75 microns thickness, and glass fiber veil of 20 grams per square meter are cut to 91 mm ⁇ 53 mm. Additionally, the glass fiber veil for the top is cut to 79 mm ⁇ 57 mm.
  • Two soft copper foil strips of 50 micron thickness to 3 mm ⁇ 57 mm are prepared, removing any sharp edge by smoothing with a hand-held roller.
  • PEI Polyetherimide
  • the smooth surface is treated with release agent such as dry Teflon lubricant to add in removal of the completed part once consolidation and cooling are achieved. After application of the release agent buff the surface to remove any excess material. The larger of the two glass fiber veils is placed on the treated surface, leaving sufficient clearance to the edges of the plate.
  • release agent such as dry Teflon lubricant
  • the conductive fabric is prepared by orienting the copper foil at opposite ends of the 85 mm length, overlaying the copper onto the fabric.
  • the copper foils are centered at the end allowing it to extend evenly beyond the width of and contacting the conductive fabric. This aids in maintaining the proper separation of the copper and eliminate the possibility of the copper shifting during assembly of the heater layers.
  • Over a small hole of 1 mm made in a flat plate such as plastic pierce through the copper foil and conductive fabric with a small needle at the four corners of the fabric; approximately 1 mm in from each corner. This is repeated for each corner.
  • the fabric is turned over onto a hard clean surface with the copper side down. With a short flat ended rod, the area is lightly compressed, thereby completing the piercing process. This compression will hold the copper to the fabric during consolidation.
  • the conductive fiber fabric is placed with the attached copper foil onto the layers of glass fiber veil and thermoplastic film already placed on the support plate.
  • the conductive fabric with copper side up is centered into the other layers.
  • the last 1 to 2 mm is gently and slightly bent upward by 30 to 45 degrees. This helps align the top layer of glass fiber.
  • the second thermoplastic film layer is disposed over the conductive fabric followed by the top glass fiber veil layer. The veil between the copper tips that were previously bent up is align and center.
  • a shim in the form of a frame can be fashioned to encompass the laminate.
  • a second laminate plate is placed which has been treated with release agent.
  • the stack is placed into a hydraulic press with platens preheated to 275° C. Compress the stack with 900 metric tons applied load for 3 minutes.
  • the laminate stack is cooled to 200° C. while maintaining the load. Once the temperature is reduced, the load and the stack are removed from the press. The plates are separated and the consolidated part is removed, allowing it to cool to room temperature.
  • the long edges of the consolidated part are trimmed square to the copper to 47 mm wide, removing the portions of the copper that were pierced. Additionally, the ends past the copper are trimmed to achieve a part dimension of 47 mm ⁇ 89 mm, leaving 2 mm of PEI beyond the copper.
  • the element gaps are cut to create the element strips.
  • Each gap is 0.5 mm wide running down the length of the conductive fabric and through the copper foil at one end stopping short of the part's edge.
  • the machine only cuts one copper foil bus per gap, alternating which bus (left or right) it cuts as the machine creates each strip. From the 47 mm wide laminate 3 cuts are made, resulting in strips of approximately 11.38 mm wide. This pattern creates an electrical path of 3 ⁇ 79 mm or 237 mm.
  • thermoplastic Using an ultrasonic wire welding device, one wire is attached through the thermoplastic to each of the two copper foil busses that measure 3 mm ⁇ 11.38 mm. Note that these are the two end strips where the electrical path starts and stops.
  • the consolidated and cut heater is placed over another layer of PEI film and onto the laminate plate. Again, another layer of PEI film is disposed over the part and cover with a high temperature silicone rubber sheet of approximately 1 to 5 mm.
  • the top laminate plate is replace inserted into the preheated press at 260° C. for an additional 5 minutes. The press is cooled to 200° C. and the part is removed. The edges are trimmed to 89 mm by 51 mm leaving 2 mm for dielectric and the consolidated heater is dressed or completed.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Surface Heating Bodies (AREA)
  • Laminated Bodies (AREA)
  • Resistance Heating (AREA)
  • Nonwoven Fabrics (AREA)

Abstract

The invention relates to a laminated fabric heater element, heater and a process for manufacturing the heater element and heater. The heater comprises an electrically conductive fabric layer attached to bus bars, is sandwiched between two thermoplastic films forming a heater assembly. In the process making the heater element or heater, the layers of the heater assembly by consolidating the layers of films and fabric into a single sheet heater without the use of adhesive resins. The heater can be made of variable geometry, electrical supply voltage and power, and can withstand more mechanical, chemical, ultraviolet radiation and other environmental stresses than prior art heaters.

Description

    TECHNICAL FIELD OF THE INVENTION
  • The invention relates to a heater element, a heater and a process for producing the heater element and heater. In particular, the heater comprises an electrically conductive fabric layer laminated between two layers of glass fiber-reinforced thermoplastic films. The heater further comprises bus bars and electrical leads, it is produced by consolidating the layers of film and fabrics into a single sheet heater. The heater can be produced having variable geometry, electrical supply voltage and power. The heater of the invention are more durable than prior art heater s because they are able to withstand more mechanical, chemical, ultraviolet radiation and other environmental stresses than prior art heaters. [0001]
  • BACKGROUND
  • Laminate or film heaters of the prior art have been made using metal foil, wires and electrically conductive fabrics laminated together using resins in between the layers to bond the integral layers together. Heaters manufactured from wire and foil have been used in industry for some time. In particular, such wire and foil heaters when used, for example, in the aerospace industry for deicing structures such as airplane wings and jet engine inlets, suffer from fatigue failure while in use, which considerably shortens their life when compared to fabrics. In addition, foil heaters, in particular, are expensive to produce and lack flexibility. [0002]
  • Because of their flexibility, light weight and even heat distribution characteristics, prior art laminate fabric heaters have been preferred in the art for many applications over metal foil heaters. In the aerospace industry, for example, fabric heaters are used for deicing structures such as airplane wings, jet engine inlets and antenna dishes, in the buildings industry for heating solid structures such as floors, countertops, pipes and tanks; in the food industry for heating food receptacles and in shipping industry and marine structures for preventing biofouling. See for example, U.S. Pat. Nos. 5,344,696; 5,925,275; 5,932,124; 5,942,140; 5,954,977; 5,966,501; 5,981,911. [0003]
  • Laminate fabric heaters of the prior art have been made with woven or non-oven fabrics containing fibers, which are electrically conductive fibers such as carbon fibers, and nonconductive fibers such as polyester. Non-conductive fibers for use in heaters are usually coated with a metal so that they can conduct the current via the metal coat, or the fibers are dispersed in a resin containing conductive particles, such as carbon black or iron particles. Conductive fibers can also be coated with a metal to improve their conductive properties. [0004]
  • Carbon fibers consolidated into a random, non-woven fabric or veil have been used in the art for shielding against electromagnetic interference. Conductive fabrics used in heaters for deicing and anti-icing aerospace structures are disclosed in, for example, U.S. Pat. No. 5,344,696 to Hastings et al. discloses an integrally bonded laminate that is used to thermally control a surface of an aircraft to which the laminate is bonded. The patent describes that the use of fabrics have numerous advantages over prior methods for deicing and heating airplane wings; for example, the conductive fiber is of low weight, and or permits nominal intrusion in terms of aerodynamics; it is easy to handle compared to wire and foil, and most notably, it allows the even distribution of heat. These factors contribute to a more efficient use of energy. Deicing and anti-icing aircraft applications necessitate an extreme in terms of product requirements. Because aircraft operate on very limited electrical resources and extreme atmospheric conditions, a system must be efficient as well as robust to provide protection. The patent also discloses, however, that the laminated fabric heater is manufactured using adhesive resins to bond the laminating layers together. [0005]
  • U.S. Pat. No. 4,534,886, to Kraus et al., discloses an electrically conductive web composed of a non-woven sheet of conductive fibers and non-conductive fibers. The sheet is saturated with a dispersion containing conductive particles and is then dried. The Kraus et al. heater element is used primarily in heating pads. The patent also discloses that the fabric heater layers are laminated together using an epoxy resin. [0006]
  • U.S. Pat. No. 5,925,275 to Lawson discloses an electrically conductive composite heating assembly. The assembly has an electrically conductive non-woven fiber layer laminated between layers of fiberglass and other dielectric material. The assembly further has an abrasion resistant outer layer. The heater element is used on aerospace structures as an ice protection system to withstand the repeated mechanical stress and thermal cycles encountered in extremely harsh aerospace environments. This patent also discloses that the fabric heater is manufactured using adhesive resins to bond the layers of the heater assembly. [0007]
  • Conductive fabric heaters disclosed in UK Patent Application No. 2,285,729 to Gerrard, are manufactured by baking a woven polymeric fabric to extreme temperatures in a multi-step process. The resultant fabric heater is limited by flexibility in resistance goals and furthermore lack variability of its Temperature Coefficients of Resistance. For example, the patent discloses that the fabric heaters are primary useful for low voltage source operation. [0008]
  • While laminated fabric heaters made using adhesive resins have been used with some success in the art, a disadvantage of using these type of heaters is due to the adhesive resins used. Adhesive resins used in making or bonding such laminated heaters must be cured and the process becomes time consuming and dangerous due to the toxicity of the materials involved. In addition, while adhesive resins are widely used to make laminated fabric heaters, the heat output from these type of heaters over a period of time dries the resin, leading to cracking of this layer and ultimate, the heater delaminates and loses fuction. Therefore, the art always seeks to develop new heaters or to improve the existing heaters. [0009]
  • In addition, heater designs as mentioned in Kraus, Hastings and Lawson suffer from expensive production methods and low operating temperatures. Machine setup is difficult to modify for different applications especially due to the use of epoxy and other resins, which have problems difficult to overcome; such as cost, shelf life, operating temperature and chemical limitations, long curing cycles and toxicity precautions. The addition of carbon black particles, polyaramid fibers (1), conductive adhesives (3), and multistage layer processing (2) contribute to the complexity and therefore the heater cost while limiting service temperature, suitability for complex designs, and high volume—low cost production. [0010]
  • SUMMARY OF THE INVENTION
  • The invention is directed to a laminated fabric heater element, a heater and a process for manufacturing the heater element and heater. The heater of the invention has many advantages over prior art heaters in that it is thin, flexible, produces more uniform temperature, has high fatigue life, and can be mass produced at less costs. In addition, the heaters of the invention can be operated at voltages ranging from millivolts to about 600 volts from either alternating current or direct current power supplies. [0011]
  • Specifically, the heater element comprises a consolidated electrically conductive fabric layer, two bus bars, and two thermoplastic layers; wherein each bus bar is contacting opposing edges of the conductive fabric layer and the consolidated electrically conductive fabric layer and the bus bars are sandwiched between the thermoplastic layers forming a single sheet. [0012]
  • The electrically conductive fabric layer of the laminated fabric heater of the invention may be selected from a variety of conductive fibers. However, in a preferred embodiment of the invention, the electrically conductive fabric layer comprises nickel-coated carbon fibers. [0013]
  • The laminated fabric heater element can further be attached to electrical leads at bus bars to form the heater. The bus bars of the laminated heater can be made of various material such as copper, brass or silver foils. In a preferred embodiment, however, the bus bars are made of copper foils. [0014]
  • In another embodiment, the laminated fabric heater of the invention can further comprise a glass veil disposed on the outer surfaces of the thermoplastic layers for additional reinforcement depending on the requirements for the heater application before the heater is formed into a single sheet. [0015]
  • In the heater of the invention, the thermoplastic films can be obtained from commercially available sources. While any thermoplastic film can be used, the heaters of the invention are preferably manufactured with polyetherimide, polyetheretherketone, polyethersulfone, polysulfone polyvinylidine fluoride, acetobutylstyrene, polyphenylene oxide and polyamide. [0016]
  • The laminated fabric heater can further comprise cuts perpendicular to and through at least one of the bus bars in a zig-zag pattern for creating a circuit and to increase the resistance of the heater to a desired value depending on the application. [0017]
  • In another embodiment, the laminated fabric heater of the invention further comprises an outer layer of thermoplastic or silicon rubber for increasing the dielectric strength of the heater. [0018]
  • The process for making the laminated fabric heater of the invention is as follows: A first thermoplastic layer on a surface where the heater is to be assembled. A layer of the electrically conductive fabric is disposed on the first thermoplastic layer. Bus bars, preferably made of copper foil are disposed on opposing edges of the electrically conductive fabric layer so that the bus bars are in contact with the electrically conductive fabric layer and are parallel to one another. Once the bus bars are in contact with the conductive fabric, they can be attached to the conductive fabric by piercing a hole through the bus bar and fabric using a piercing rivetor apparatus. The action of piercing causes the metal displaced to form a hole to curl and flatten under the fabric, thereby securing the bus bars to the fabric. Thereafter, a second thermoplastic layer is disposed on the electrically conductive fabric layer and bus bars to form a heater assembly. Once the heater layers are assembled, the heater assembly is heated at suitable temperatures to a set thickness to consolidate the conductive fabric layer sandwiched in the thermoplastic film layers, thereby forming a single sheet heater. After consolidation of the layers, and specially of the conductive fabric layer, the heater is transferred to a cooling chamber to quench the heater at its maximum consolidation state. A glass fiber reinforcement layer can be disposed on the outer surfaces of the thermoplastic layers prior to consolidation and depending on the heater output requirement. [0019]
  • While the process described above can be performed at a small scale to produce a small number of small heaters using a hydraulic press, the process can be adapted for manufacturing heater elements and heaters in high volume using a roller laminating apparatuses. In roller lamination, the heater element is produced in a single long sheet of indefinite length and width, which length and width are only limited by the length and width of the starting materials and machinery used. The heater element made through roller lamination can be stored in rolls, and heaters can be made from segments of the heater element as required. In this embodiment of the invention, the process comprises combining a layer of electrically conductive fabric from a roll supply with two metal foil bus bars, wherein the bus bars are positioned parallel to one another at opposing edges of and contacting the conductive fabric in the direction of the roll. The bus bars are secured to the conductive fabric by making a hole in the conductive fabric and bus bar by piercing both components in a piercing rivetor apparatus as described above. Once the bus bars are secured to the fabric, the conductive fabric layer containing bus bars are drawn between two layers of thermoplastic films forming a sandwich type structure assembly. The heater assembly sandwich is then fed through a pinch roller, which had been preheated at a predetermined temperature and set at a predetermined pressure to cause gelling of the thermoplastic layers. The gelling of the thermoplastic layer causes some of the thermoplastic to flow through the conductive fabric, fusing the films and consolidating the conductive fibers into a single sheet heater element. Once consolidation occurs, the resultant single sheet fabric heater is drawn over a cooling chamber so that maximal consolidation of the layers is maintained. Individual heaters can be made by cutting a section from the heater sheet roll with a tooling die or a water jet cutter, attaching electrical leads by ultrasonic welding and laminating it once more with a layer of thermoplastic, thereby maintaining the gap cut by the die or water jet and providing a final dielectric layer.[0020]
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • FIG. 1 is a schematic diagram of the process for making the laminated fabric heaters of the invention in a roller laminating apparatus. [0021]
  • FIGS. 2A and 2B are cross-sections of the heater element of the invention showing the various layers prior to consolidation without and with glass fiber veil respectively. [0022]
  • FIG. 3 is a schematic representation of the heater at various stages of manufacturing through the roller laminating process. [0023]
  • FIG. 4 is a schematic drawing illustrating a cut away view of the heater of the invention showing the cuts through the heater in a zig-zag pattern. [0024]
  • FIG. 5 is a schematic diagram showing the various stages C, E, F, H and J of the process of manufacturing the heater of the invention. [0025]
  • FIG. 6 is a schematic drawing of the heater of the invention shown in cross-section. [0026]
  • FIG. 7 is a schematic diagram illustrating a heater of the invention in which holes are perforated through the laminate.[0027]
  • DETAILED DESCRIPTION OF THE INVENTION
  • The heater element of the invention comprises a layer of conductive fabric, two bus bars position at opposing edges of the fabric sandwiched between two outer layers of thermoplastic. [0028]
  • The conductive fabric can be made from various materials, which are known in the art and comprises electrically conductive fibers. In a preferred embodiment, the conductive fabric comprises electrically conductive fibers, and most preferred carbon fibers, in particular, nickel-coated carbon fibers. In this embodiment, the conductive fibers are chopped fibers and are converted into a non-woven conductive fabric using paper making techniques. An organic binder is used to hold the fibers together in the fabric. The thickness, density fiber coating and predominant fiber direction of the fabric all determine the final resistivity of the heater. Depending on the size of the heater and power output required, the appropriate length of fabric layer can be cut from a supply roll or an entire roll can be used for mass producing the heater elements. In a preferred embodiment of the invention, the electrically conductive fabric layer is consolidated. A consolidated conductive fabric layer results from the consolidating step during the laminating process. [0029]
  • Consolidation is a process by which the thermoplastic layers of the heater are brought to a gelling state under pressure during bonding of the heater and to a predetermined thickness, this causes the electrically conductive fibers of the conductive fabric to be brought into intimate contact with one another through the laminating process. [0030]
  • Carbon filaments are manufactured from a polymer fiber under high temperature and pressure within an inert environment. The fibers can be coated with a metal, such as nickel, brass, silver or other suitable metal or a combination thereof, by one of several processes, tailoring the Temperature Coefficient of Resistance (the rate at which the electrical resistance of a medium changes as a result of a change in temperature) and resistivity of the final fabric. Fibers are combined into a tow and chopped to a desired length between about 3 millimeters and 12 millimeters or longer. Fiber length is a major factor in determining the fabric's resistance, flexibility, and structural conformity and heat uniformity. [0031]
  • The thermoplastic films for use in the heater of the invention can be of various types and are commercially available. In a preferred embodiment, the thermoplastic films are polyetherimide (Ultem®, Westlake Plastics, Inc., PA), polyetherketone (Victrex®, Westlake Plastics, Inc. PA), polyamide (Kapton®, E. I. Dupont de Nemours, DE), polyethersulfone, sulfonr, polyvinylidine fluoride (Kynar®, PVDF, Westlake Plastics, Inc., PA), acetobutylstyrene (Cycolac, ABS, Westlake Plastics, Inc., PA), polyphenylene oxide (Noryl®, Westlake Plastics, Inc., PA) and the like. Thermoplastic films have different gelling temperatures. Therefore, in the process of the invention, the temperature at which the pinch rollers or hydraulic press is set is determined by the type of thermoplastic film used. In the process of manufacturing the heaters of the invention, Ultem® is used at a temperature of approximately [0032] 275° C., and Vitrex® is used at 350° C.
  • The process and the heater element and heater of the invention can be described with references to the figures. FIG. 1 illustrates the high volume production process useful for making the laminated fabric heaters of the invention. As seen in FIG. 1, the process involves a roller laminating apparatus. The starting materials are all provided in rolls, i.e., the [0033] conductive fabric 10, the bus bar strips 12, 14, the thermoplastic film 16, 18, and as needed, the glass fiber veil 20, 22.
  • As shown in FIG. 1 in a roll stack operation, the conductive fabric and copper foil, or other suitable metal, are laminated in glass fiber-reinforced thermoplastic film, feed wires are attached and the whole heater finally encapsulated. In a preferred embodiment, the process starts with a roll of [0034] conductive fabric 10, two rolls of thermoplastic film 16, 18, two rolls of copper foil 12, 14, and two rolls of glass fiber veil 20, 22. The conductive fabric 10, pulled from a roll, is combined with copper foil 12, 14, of 2 mils in thickness, separated by some predetermined distance and applied parallel to each other, contacting the conductive fabric, and in the same direction of the conductive fabric roll 10, although other orientations are possible. Preferably the copper foil bus bars near the free edges of the roll.
  • The copper foil bus bars [0035] 12, 14 and conductive fabric 10 are drawn together through a piercing rivetor 24, whereby perforated upper and lower support plates maintain fabric and copper foil bus bars 12, 14 in proximity and a pin like tapered needle of small dimension, compared to the width of the copper, is pressed through the copper foil and conductive fabric. The needle is withdrawn and the area around the pierced hole is compressed. Compression may take the form of a roller or pair of rollers or a press rod fixture clamping from both sides. The action of piercing the copper splits the copper into several petals, much like a flower. As the taper of the needle continues into the opening the petals are curled over, moving away and entrapping local fibers. Once compressed the fibers are permanently held and the copper is securely attached to the fabric. This portion of the process is optional, but adds in locating the copper.
  • From the pierce/riveting action of the copper foil bus bars the final products are ready for the first lamination using the [0036] thermoplastic films 16, 18. The conductive fabric 10, with the copper foil bus bars attached, are drawn between the two layers of thermoplastic film 16, 18 which is slightly wider (by about 1 to 6 mm) than the conductive fabric 10. To facilitate wire attachment to the copper foil bus-bar the top layer of thermoplastic film 16 may be perforated prior to the first lamination process. Over and outside the thermoplastic film, glass fiber veil 20, 22 are added to both sides of the laminate stack.
  • The conductive fiber layer with copper foil bus bars, sandwiched in the thermoplastic films with or without a fiberglass veil, as shown in the cross-section in FIG. 2, are drawn together through [0037] pinch rollers 15, 17, which have been preheated at a predetermined temperature and set at a predetermined distance depending on the type and thickness of thermoplastic film and fabric used. The layers of dry materials are heated and fused together by pinch rollers into a consolidated sheet of exact thickness. Temperatures and pressures are such that the thermoplastic heats sufficiently to flow through the conductive fabric, pierced copper bus and glass fiber veil. The pinch roller separation is set to achieve proper consolidation of the sheet and most importantly the conductive fabric. Once consolidated, the conductive fabric will achieve its final resistivity. For any given combination of conductive fabric, thermoplastic film, and glass fiber veil experimentation has shown that consolidation must always be compressed to at least 110% of the thermoplastic film thickness. When the first lamination process is complete the product can be graded and stored for future use or further processed into cut heaters of predetermined design. Once consolidated, the sheet heater is transferred to a cooling chamber 19 to maintain maximal degree of consolidation.
  • To increase the resistance of the heater, [0038] perpendicular cuts 26 can be made through the laminate through at least one of the bus bars, as shown in FIG. 3. This can be done from stock or during the running process after cooling the sheet heater. The continuous laminated sheet is pulled through a cutting or slitting device. The device could be a die cutter made to the desired shape, or a dynamic cutter such as a water jet or laser cutter which are commercially available. With the necessary cutting tool a circuit pattern such as a serpentine or zig-zag can be cut thereby further increasing the resistance to the desired value, by increasing the electrical path. A first cut is made from outside copper edge to outside copper edge but within the maximum width of the thermoplastic layers. Cuts 26 such as this define a starting and stopping edge. Additional cuts in an alternating fashion across the roll from inside copper edge to outside copper edge, and at specified distances from each other down the roll form a circuit by which electrical current can be made to travel in this zig-zag pattern (see FIG. 4). These cuts also terminate short of the thermoplastic layer edge. Lastly a cut, in a similar manner to the first cut, is made which defines the final width of that circuit. Using the last cut as the first cut for the next series, the pattern process can continue for the entire laminated heater roll. To vary the circuit design, the intermediate cuts, those that alternate, can be made at different spacing, as narrow a 4 mils or as wide as the design requires. Varying the spacing within one design allows the designer to vary the heat output for each strip within the circuit. Cuts short of the thermoplastic edge essentially frame the circuit, holding the strips in place while wires are attached and final lamination is completed.
  • FIGS. [0039] 3-5 illustrate how circuits of even or odd number of strips can be created and thus affect wire placement. For even numbered-strip circuits wire attachment for each heater would be made on one side. For odd numbered-strip circuits the wires would be attached at opposite sides. Electrical leads in the form of wires can be attached to the copper foil bus through the thermoplastic or perforations within the thermoplastic and at the location defining the beginning and end of the zig-zag pattern. Attachment would be accomplished by currently know methods such as solder, brazing, ultrasonic welding or crimping, and catered to the temperature, and electrical application requirements of the heater.
  • FIGS. [0040] 3-6 also show that once wires leads are attached, the heater is finally encapsulated to hold the element strips in place, increase the dielectric strength of the heater, and protect the circuit and wire attachment points. In a preferred method, the final encapsulating layer can either be additional thermoplastic layers, or other suitable dielectric materials, such as silicone rubber. If themoplastic films are used as the encapsulating layers, then the continuous, laminated heater sheet is drawn into another roll stack laminating machine where one additional layer of thermoplastic is fused to each side of the circuit, encapsulating the circuit and wire attachment points. An extra layer of thicker thermoplastic film may be added to the laminate stack at the same time to locally reinforce the heater around the wire attachment points. The top roller should be coated with a layer of heat resisting rubber, e.g. silicone rubber, to enable the top thermoplastic film to be encapsulated over the top of the raised wire attachment points.
  • FIG. 5 illustrates also the final cutting stage of the process. Depending on the application and size of heater required, transverse cuts are made through the sheet product to separate the heaters from each other. As in the circuit cutting stage, this can be achieved using die cutting techniques, water jet or laser cutting methods. [0041]
  • To further increase the resistance and/or facilitate encapsulation into another medium, holes can be perforated at predetermined locations within the laminate as shown in FIG. 7. If perforations are provided in the laminate heater to facilitate encapsulation, additional layers of thermoplastic film or silicone rubber are added with perforations, or added after the second encapsulation is complete. Perforations of the second layers are of slightly smaller dimension, provided there is a need for a dielectric layer around the opening. [0042]
  • The heaters of the invention can be used in multiple applications depending on the heat requirements. Power can be delivered by means of single-use batteries, rechargeable batteries, power adapters, and generator derived systems such as wall supply, portable generators, solar energy and industrial transformers. Examples of the heaters of the invention in some low voltage applications, from millivolts to about 5 volts include, novelty gift items such as heated cards, coasters and eye mask; toys such as kitchen sets; electronic sensors for heating and deicing; personal rechargeable appliances such as hair curlers, and personal warmers such as ear muffs, gloves, socks, hats and the like. [0043]
  • Heater applications requiring medium voltage from about 6 to 28 volts include, for example, car parts and accessories such as floor mats, steering wheel, seats, door panel and mirror defrosters; motorcycle grips, mirrors, seat pad, tank and helmets; aircraft wings, propellers, floors, seats, instruments, controls, interior panels, galley and lavatory seats; in boats including ferry seats, deck, railings, galley and lavatory; warming counter and waste tanks in recreational vehicles; in other applications including, solar powered heating panel, pillows, electrical component/cabinet heaters, food preparation applications. [0044]
  • Heater applications requiring high voltage from about 110 to about 250 volts single phase, include, for example, aircraft wings, propellers, rotors, cowlings, inlets; household items such as appliances, room heaters (wall and floor), countertop warmers, firewood preheater/drier, walkways, driveways, steps, antenna pillows, food preparation; and commercial/industrial goods such as liquid drum heaters, ovens, shop space, machine processes, tools/dies, and the like. Heater applications requiring the highest voltage, from about 208 to 600 volts multiphase, include, commercial/industrial goods such as liquid drum (band) heaters, ovens, shop space, machine processes, tools/dies, transmitter/receiver of reflector antennas, electrical (signal) relay/component cabinets; large commercial and military aircrafts heaters for deicing parts, and the like. [0045]
  • EXAMPLE I
  • Construction of a Business Card Sized Novelty Heater by Batch Processing for Small Quantities. [0046]
  • The heater will have 4 strips of 11.38 mm width, produce 2.88 watts of power from 24 volts and deliver 0.08 watts per square centimeter at room temperature. Maximum temperature in air would be approximately 120° C. All the necessary materials are cut to the appropriate dimensions. Four thermoplastic films, preferably Polyetherimide (PEI) of 75 microns thickness, and glass fiber veil of 20 grams per square meter are cut to 91 mm×53 mm. Additionally, the glass fiber veil for the top is cut to 79 mm×57 mm. Two soft copper foil strips of 50 micron thickness to [0047] 3 mm×57 mm are prepared, removing any sharp edge by smoothing with a hand-held roller.
  • From a roll of conductive veil with the following properties (5% nickel coated carbon, 6 mm fiber and 8 grams per square meter, having a surface resistivity of 6.7 ohms/sq, such as that provided by Thermion Systems International, Stratford, Conn. and known as THERMION) a piece is cut off the end of the roll 53 mm wide, assuring the cut is made as parallel to the axis of the roll as possible. One end is trimmed off square and a piece 85 mm long is cut from the strip. [0048]
  • On a suitable metal support plate of 4 times the part's size and of smoothness to 2 microns, such as laminate press plate, the smooth surface is treated with release agent such as dry Teflon lubricant to add in removal of the completed part once consolidation and cooling are achieved. After application of the release agent buff the surface to remove any excess material. The larger of the two glass fiber veils is placed on the treated surface, leaving sufficient clearance to the edges of the plate. One of the cut PEI films is disposed on top of the glass fiber veil in a similar orientation. [0049]
  • The conductive fabric is prepared by orienting the copper foil at opposite ends of the 85 mm length, overlaying the copper onto the fabric. The copper foils are centered at the end allowing it to extend evenly beyond the width of and contacting the conductive fabric. This aids in maintaining the proper separation of the copper and eliminate the possibility of the copper shifting during assembly of the heater layers. Over a small hole of 1 mm made in a flat plate such as plastic, pierce through the copper foil and conductive fabric with a small needle at the four corners of the fabric; approximately 1 mm in from each corner. This is repeated for each corner. The fabric is turned over onto a hard clean surface with the copper side down. With a short flat ended rod, the area is lightly compressed, thereby completing the piercing process. This compression will hold the copper to the fabric during consolidation. [0050]
  • The conductive fiber fabric is placed with the attached copper foil onto the layers of glass fiber veil and thermoplastic film already placed on the support plate. The conductive fabric with copper side up is centered into the other layers. At the extreme ends of the copper strips, the last 1 to 2 mm is gently and slightly bent upward by 30 to 45 degrees. This helps align the top layer of glass fiber. The second thermoplastic film layer is disposed over the conductive fabric followed by the top glass fiber veil layer. The veil between the copper tips that were previously bent up is align and center. [0051]
  • At opposite side of the laminate or preferably around the laminate, several 150 micron shims are placed. Alternatively a shim in the form of a frame can be fashioned to encompass the laminate. Over the laminate and shims, a second laminate plate is placed which has been treated with release agent. The stack is placed into a hydraulic press with platens preheated to 275° C. Compress the stack with 900 metric tons applied load for 3 minutes. The laminate stack is cooled to 200° C. while maintaining the load. Once the temperature is reduced, the load and the stack are removed from the press. The plates are separated and the consolidated part is removed, allowing it to cool to room temperature. The long edges of the consolidated part (heater) are trimmed square to the copper to 47 mm wide, removing the portions of the copper that were pierced. Additionally, the ends past the copper are trimmed to achieve a part dimension of 47 mm×89 mm, leaving 2 mm of PEI beyond the copper. [0052]
  • Using a die cutter set to the correct dimensions or a water jet cutting machine, the element gaps are cut to create the element strips. Each gap is 0.5 mm wide running down the length of the conductive fabric and through the copper foil at one end stopping short of the part's edge. The machine only cuts one copper foil bus per gap, alternating which bus (left or right) it cuts as the machine creates each strip. From the 47 mm wide laminate 3 cuts are made, resulting in strips of approximately 11.38 mm wide. This pattern creates an electrical path of 3×79 mm or 237 mm. [0053]
  • Using an ultrasonic wire welding device, one wire is attached through the thermoplastic to each of the two copper foil busses that measure 3 mm×11.38 mm. Note that these are the two end strips where the electrical path starts and stops. The consolidated and cut heater is placed over another layer of PEI film and onto the laminate plate. Again, another layer of PEI film is disposed over the part and cover with a high temperature silicone rubber sheet of approximately 1 to 5 mm. The top laminate plate is replace inserted into the preheated press at 260° C. for an additional 5 minutes. The press is cooled to 200° C. and the part is removed. The edges are trimmed to 89 mm by 51 mm leaving 2 mm for dielectric and the consolidated heater is dressed or completed. [0054]

Claims (17)

We claim:
1. A laminated fabric heater, comprising a consolidated electrically conductive fabric layer, two bus bars, and two thermoplastic layers; wherein each bus bar is contacting opposing edges of the conductive fabric layer and the consolidated electrically conductive fabric layer and the bus bars are sandwiched between the thermoplastic layers forming a single sheet.
2. The laminated fabric heater according to claim 1, wherein the consolidated electrically conductive fabric layer comprises nickel-coated carbon fibers.
3. The laminated heater according to claim 1, further comprising electrical leads attached to the bus bars.
4. The laminated heater according to claim 3, wherein the bus bars are made of copper foil.
5. The laminated fabric heater according to claim 1, further comprising disposing a first glass veil on the outer surface of the first thermoplastic layer and a second glass veil on the outer surface of the second thermoplastic layer prior to forming the heater into a single sheet.
6. The laminated fabric heater according to claim 1, wherein the thermoplastic layers are thermoplastic films selected from the group consisting of polyetherimide, polyetheretherketone, polyethersuldone, sulfone, polyvinylidine fluoride, acetobutylsyrene, polyphenylene oxide and polyamide.
7. The laminated fabric heater according to claim 1, further comprising cuts perpendicular to and through at least one of the bus bars in a zig-zag pattern for creating a circuit and to increase the resistance of the heater to a desired value.
8. The laminated fabric heater according to claim 3 or 7, further comprising an outer layer of thermoplastic or silicon rubber for increasing dielectric strength of the heater.
9. The laminated fabric heater according to claim 1, further having perforations through the laminate.
10. A process for making the laminated fabric heater of claim 1, comprising:
disposing a first thermoplastic layer on a surface;
disposing a layer of electrically conductive fabric on the first thermoplastic layer;
disposing bus bars at opposing edges of the electrically conductive fabric layer so that the bus bars are in contact with the electrically conductive fabric layer;
disposing a second thermoplastic layer on the electrically conductive fabric layer and bus bars;
heating the heater at suitable temperatures under pressure to consolidate the conductive fabric; and
transferring the heater to a cooling chamber so that maximum consolidation is maintained.
11. A process for manufacturing the heater according to claim 1 in a roller lamination apparatus, comprising:
combining a layer of electrically conductive fabric from a roll supply with two metal foil bus bars, wherein the bus bars are parallel to one another and are placed at opposing edges of and contacting the conductive fabric in the direction of the roll;
securing the bus bars to the conductive fabric by making a hole in the conductive fabric and bus bar in a piercing rivetor;
drawing the conductive fabric layer containing bus bars between two layers of thermoplastic film forming a sandwich structure;
feeding the sandwich structure through a pinch roller preheated at a predetermined temperature and thickness to cause gelling of the thermoplastic layers;
consolidating the conductive fiber layer to form a single sheet heater; and
cooling the single sheet heater in a cooling chamber.
12. The process according to claim 10 or 11, further comprising providing a glass fiber-reinforcement layer on the thermoplastic layers prior to feeding the sandwich structure through the pinch roller.
13. The process according to claim 10 or 11, further comprising attaching electrical leads to bus bars.
14. The process according to claim 10 or 11, further comprising cutting the heater perpendicular to and through at least one of the bus bars to create circuit of variable power output.
15. The process according to claim 10 or 11, further comprising laminating at least one thermoplastic layer on opposing surfaces of the heater.
16. The process according to claim 10 or 11, further comprising perforating the laminate to create holes.
17. The process according to claim 16, further comprising attaching an additional layer of thermoplastic or silicone rubber to the laminate.
US10/293,204 1999-12-10 2002-11-13 Thermoplastic laminate fabric heater and methods for making same Abandoned US20030199947A1 (en)

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Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL1027053C2 (en) * 2004-09-16 2006-03-20 Robert Oosterling Rollable floor heating.
US20100185078A1 (en) * 2009-01-20 2010-07-22 Leonh.Lang Bioelectrode
CN102555238A (en) * 2010-12-23 2012-07-11 上海杰事杰新材料(集团)股份有限公司 Manufacturing method of fiber cloth reinforced thermoplastic resin composite material
US20130186884A1 (en) * 2012-01-20 2013-07-25 W.E.T. Automotive Systems, Ltd. Felt heater and method of making
EP2599738A3 (en) * 2004-01-19 2014-06-18 Winstore Europe B.V. Method for producing container parts, container parts, method for producing a multilayer foil, multilayer foil.
US20140190957A1 (en) * 2008-04-25 2014-07-10 Innovative Heating Technologies Inc. Planar Heating Element for Underfloor Heating
US11376811B2 (en) 2018-07-03 2022-07-05 Goodrich Corporation Impact and knife cut resistant pre-impregnated woven fabric for aircraft heated floor panels

Families Citing this family (177)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
TW457137B (en) * 1999-04-28 2001-10-01 Sharp Kk Washer having a partial washing apparatus
US20050205551A1 (en) * 2001-02-15 2005-09-22 Integral Technologies, Inc. Low cost heated clothing manufactured from conductive loaded resin-based materials
US20050172950A1 (en) * 2001-02-15 2005-08-11 Integral Technologies, Inc. Low cost heated clothing manufactured from conductive loaded resin-based materials
US7372006B2 (en) * 2001-02-15 2008-05-13 Integral Technologies, Inc Low cost heating devices manufactured from conductive loaded resin-based materials
ITMI20011454A1 (en) * 2001-07-09 2003-01-09 Cadif Srl POLYMER BITUME BASED PLANT AND TAPE PROCEDURE FOR SURFACE AND ENVIRONMENTAL HEATING OF STRUCTURES AND INFRASTRUCTURES
US7777156B2 (en) * 2002-01-14 2010-08-17 Mmi-Ipco, Llc Electric heating/warming fabric articles
US20080047955A1 (en) * 2002-01-14 2008-02-28 Malden Mills Industries, Inc. Electric Heating/Warming Fabric Articles
US20040045955A1 (en) * 2002-01-14 2004-03-11 Moshe Rock Electric heating/warming fabric articles
US7202443B2 (en) * 2002-01-14 2007-04-10 Malden Mills Industries, Inc. Electric heating/warming fabric articles
US7268320B2 (en) * 2002-01-14 2007-09-11 Mmi-Ipco, Llc Electric heating/warming fabric articles
US6893086B2 (en) * 2002-07-03 2005-05-17 W.E.T. Automotive Systems Ltd. Automotive vehicle seat insert
US20040262294A1 (en) * 2003-06-24 2004-12-30 Horey Leonard I. Serpentine conductive path for woven substrates
ATE370842T1 (en) * 2003-06-26 2007-09-15 Key Tech Inc METHOD FOR THERMALLY PRINTING A DYE IMAGE ON A THREE-DIMENSIONAL OBJECT BY USING FLEXIBLE HEATING ELEMENTS
ATE551780T1 (en) 2003-07-23 2012-04-15 Lg Electronics Inc INTERNAL ANTENNA AND A MOBILE DEVICE WITH THIS INTERNAL ANTENNA
US6946628B2 (en) * 2003-09-09 2005-09-20 Klai Enterprises, Inc. Heating elements deposited on a substrate and related method
US7274007B2 (en) 2003-09-25 2007-09-25 W.E.T. Automotive Systems Ltd. Control system for operating automotive vehicle components
US7461892B2 (en) 2003-12-01 2008-12-09 W.E.T. Automotive Systems, A.C. Valve layer for a seat
US8288693B2 (en) * 2004-03-08 2012-10-16 W.E.T. Automotive Systems Ag Flat heating element
US7763833B2 (en) * 2004-03-12 2010-07-27 Goodrich Corp. Foil heating element for an electrothermal deicer
US20060027555A1 (en) * 2004-06-25 2006-02-09 Integral Technologies, Inc. Low cost heating elements for cooking applications manufactured from conductive loaded resin-based materials
US7622695B2 (en) * 2004-11-04 2009-11-24 Dipucchio Jay Multi-layered carrier
US8258443B2 (en) * 2005-02-17 2012-09-04 417 And 7/8, Llc Heating unit for warming pallets
US20090107972A1 (en) * 2005-02-17 2009-04-30 David Naylor Heating unit for warming propane tanks
US10920379B2 (en) 2005-02-17 2021-02-16 Greenheat Ip Holdings Llc Grounded modular heated cover
US8633425B2 (en) 2005-02-17 2014-01-21 417 And 7/8, Llc Systems, methods, and devices for storing, heating, and dispensing fluid
US20090114634A1 (en) 2005-02-17 2009-05-07 David Naylor Heating unit for warming fluid conduits
US9945080B2 (en) 2005-02-17 2018-04-17 Greenheat Ip Holdings, Llc Grounded modular heated cover
US20090107975A1 (en) * 2005-02-17 2009-04-30 Thomas Caterina Heating unit for warming pallets
US9392646B2 (en) 2005-02-17 2016-07-12 417 And 7/8, Llc Pallet warmer heating unit
US7183524B2 (en) * 2005-02-17 2007-02-27 David Naylor Modular heated cover
US7230213B2 (en) * 2005-02-17 2007-06-12 David Naylor Modular heated cover
US7880121B2 (en) * 2005-02-17 2011-02-01 David Naylor Modular radiant heating apparatus
US20080272106A1 (en) * 2007-05-03 2008-11-06 David Naylor Grounded modular heated cover
US20090101632A1 (en) 2005-02-17 2009-04-23 David Naylor Heating unit for direct current applications
US20090107986A1 (en) * 2005-02-17 2009-04-30 David Naylor Three layer glued laminate heating unit
US20090114633A1 (en) * 2005-02-17 2009-05-07 David Naylor Portable Pouch Heating Unit
KR20060100568A (en) * 2005-03-17 2006-09-21 삼성전자주식회사 Information recording medium and apparatus for recording/reproducing the same
DE102005015050A1 (en) * 2005-03-31 2006-10-12 Ewald Dörken Ag panel heating
EP1866202B1 (en) * 2005-04-04 2012-11-21 Goodrich Corporation Electrothermal deicing apparatus and a dual function heater conductor for use therein
US20060278631A1 (en) * 2005-06-10 2006-12-14 Challenge Carbon Technology Co., Ltd. Of Taiwan Laminate fabric heater and method of making
CA2611656C (en) * 2005-06-22 2014-01-07 Airbus France Anti-icing and deicing system for aircraft engine pod with resistive mat
JP2009507330A (en) 2005-07-12 2009-02-19 カーボニック・ヒート・コーポレイション Plate type heater and manufacturing method thereof
US20070017395A1 (en) * 2005-07-22 2007-01-25 Neri Joel D Method and apparatus for uniformly heating a substrate
US7478869B2 (en) 2005-08-19 2009-01-20 W.E.T. Automotive Systems, Ag Automotive vehicle seat insert
US7543344B2 (en) * 2005-09-29 2009-06-09 Augustine Biomedical And Design Llc Cover for a heating blanket
US20070068931A1 (en) * 2005-09-29 2007-03-29 Augustine Scott D Novel designs for an electric warming blanket including a flexible heater
US7851729B2 (en) * 2005-09-29 2010-12-14 Augustine Temperature Management LLC Electric warming blanket having optimized temperature zones
US20070068916A1 (en) * 2005-09-29 2007-03-29 Augustine Scott D Heating blanket cover construction and methods of manufacture
US7633450B2 (en) 2005-11-18 2009-12-15 Goodrich Corporation Radar altering structure using specular patterns of conductive material
EP1796432A1 (en) * 2005-12-09 2007-06-13 Roth Werke GmbH Heating sheet
US7340933B2 (en) 2006-02-16 2008-03-11 Rohr, Inc. Stretch forming method for a sheet metal skin segment having compound curvatures
US7291815B2 (en) * 2006-02-24 2007-11-06 Goodrich Corporation Composite ice protection heater and method of producing same
US7923668B2 (en) * 2006-02-24 2011-04-12 Rohr, Inc. Acoustic nacelle inlet lip having composite construction and an integral electric ice protection heater disposed therein
US7308193B2 (en) * 2006-02-28 2007-12-11 Richard Halsall Non-metallic heating element for use in a fluid heater
EP1996465A2 (en) 2006-03-10 2008-12-03 Goodrich Corporation Low density lightning strike protection for use in airplanes
GB2436194A (en) * 2006-03-17 2007-09-19 Gkn Aerospace Transparency Sys A method of making an impregnated heater structure and an impregnated heater structure
WO2007130979A2 (en) 2006-05-02 2007-11-15 Rohr, Inc. Modification of reinforcing fiber tows used in composite materials by using nanoreinforcements
US7784283B2 (en) * 2006-05-03 2010-08-31 Rohr, Inc. Sound-absorbing exhaust nozzle center plug
US8197621B2 (en) * 2006-06-27 2012-06-12 Naos Co. Ltd. Method for manufacturing planar heating element using carbon micro-fibers
KR101005733B1 (en) * 2006-07-20 2011-01-06 와틀로 일렉트릭 매뉴팩츄어링 컴파니 Layered Heater System Having Conductive Overlays
US7621882B2 (en) * 2006-08-07 2009-11-24 Phillips Anthony G Medical device for a user's limb
US8062343B2 (en) * 2006-10-13 2011-11-22 Augustine Temperature Management LLC Heating blanket
DE102006049210B3 (en) * 2006-10-18 2008-04-10 Linkwin Technology Co., Ltd. Flexible strip heater fabrication method for e.g. earmuff, involves fixing protective sheet to surface of heating element opposite to film, retracting film, and fixing another protective sheet to surface of element opposite to former sheet
US7268325B1 (en) 2006-10-23 2007-09-11 Linkwin Technology Co., Ltd. Method of making flexible sheet heater
DE102006058198C5 (en) * 2006-12-07 2018-01-18 Fibretemp Gmbh & Co. Kg Electrically heated mold in plastic construction
US20080156786A1 (en) * 2006-12-29 2008-07-03 Seung Mo Choi Direct current powered heating pad for bed
US20080166563A1 (en) 2007-01-04 2008-07-10 Goodrich Corporation Electrothermal heater made from thermally conducting electrically insulating polymer material
WO2008089412A1 (en) * 2007-01-18 2008-07-24 Augustine Biomedical And Design Llc Shut-off timer for a heating blanket
US10201935B2 (en) 2007-03-19 2019-02-12 Augustine Temperature Management LLC Electric heating pad
US8283602B2 (en) * 2007-03-19 2012-10-09 Augustine Temperature Management LLC Heating blanket
US20150366367A1 (en) 2007-03-19 2015-12-24 Augustine Temperature Management LLC Electric heating pad with electrosurgical grounding
DE102007019843B3 (en) * 2007-03-26 2008-05-08 I.G. Bauerhin Gmbh Electrical seat heater for heating surface of seat i.e. passenger car-seat, has plastic-foil strip running between segments along electrical conductor, where strip is made of polyimide or PET and is in heat conducting contact with conductor
ATE461601T1 (en) 2007-08-03 2010-04-15 Frenzelit Werke Gmbh & Co Kg SURFACE HEATING SYSTEM
US20090099630A1 (en) * 2007-10-12 2009-04-16 Augustine Biomedical And Design Llc Tuckable electric warming blanket for patient warming
KR101168601B1 (en) 2007-10-18 2012-07-30 베.에.테. 오토모티브 시스템스 아게 Electrical control device
GB2453934B (en) * 2007-10-18 2012-09-05 Gkn Aerospace Services Ltd Aircraft leading edge component with thermoplastic heater
GB2453769B (en) * 2007-10-18 2012-09-05 Gkn Aerospace Services Ltd An aircraft leading edge thermoplastic heating mat
GB2453933A (en) * 2007-10-18 2009-04-29 Gkn Aerospace Services Ltd Aircraft leading edge ice protection system comprising a thermoplastic heater mat
US7837150B2 (en) * 2007-12-21 2010-11-23 Rohr, Inc. Ice protection system for a multi-segment aircraft component
DE102008006523A1 (en) 2008-01-29 2009-07-30 Airbus Deutschland Gmbh Fiber composite component for an aircraft or spacecraft
US7876195B2 (en) * 2008-03-27 2011-01-25 Jack Chen Fan resistor
WO2009129615A1 (en) * 2008-04-22 2009-10-29 Datec Coating Corporation Thick film high temperature thermoplastic insulated heating element
US20100065686A1 (en) * 2008-04-28 2010-03-18 Tauscher Kurt M Aircraft heated floor panel
US9095005B2 (en) * 2008-05-20 2015-07-28 Kenyon International, Inc. Induction cook-top apparatus
US8431866B2 (en) * 2008-07-23 2013-04-30 The Boeing Company Method of installing and removing a bracket on a mounting surface
US20110233183A1 (en) * 2008-09-03 2011-09-29 North American Rescue, LLC. Steering wheel heater assembly
US7827675B2 (en) * 2008-09-11 2010-11-09 Ching-Ling Pan Method of manufacturing an activated carbon fiber soft electric heating product
US20110290775A1 (en) * 2008-12-03 2011-12-01 Illinois Tool Works Inc. Combination seat heater and occupant sensor antenna
US20100161016A1 (en) * 2008-12-19 2010-06-24 Augustine Biomedical And Design, Llc Apparatus and method for effectively warming a patient
DE202009017049U1 (en) 2008-12-21 2010-05-12 W.E.T. Automotive Systems Ag aerator
DE202010002050U1 (en) 2009-02-18 2010-07-15 W.E.T. Automotive Systems Ag Air conditioning device for vehicle seats
DE102009030491A1 (en) 2009-03-18 2010-09-23 W.E.T. Automotive Systems Ag Air conditioning device for an air-conditioned object in a vehicle interior
US8561934B2 (en) 2009-08-28 2013-10-22 Teresa M. Kruckenberg Lightning strike protection
CN102012061B (en) * 2009-09-08 2012-11-21 清华大学 Electric warmer
US20110056924A1 (en) * 2009-09-10 2011-03-10 Benjamin Park Townsend Solar defrost panels
EP2496889B1 (en) * 2009-11-05 2017-06-28 Winstone Wallboards Limited Heating panel and method therefor
CN102056353A (en) * 2009-11-10 2011-05-11 清华大学 Heating device and manufacturing method thereof
FR2953090B1 (en) * 2009-11-25 2012-12-14 Dynabat DEVICE FOR PRODUCING AN ELECTRIC HEATING FLOOR
DE102009059995A1 (en) * 2009-12-21 2011-06-22 W.E.T. Automotive Systems AG, 85235 Electric heater
DE102011014516A1 (en) 2010-04-06 2012-05-10 W.E.T. Automotive Systems Ag MFP
US8263906B2 (en) 2010-05-11 2012-09-11 Cambro Manufacturing Company Food warming system
US10293947B2 (en) * 2010-05-27 2019-05-21 Goodrich Corporation Aircraft heating system
DE102011105675A1 (en) 2010-07-15 2012-01-19 W.E.T. Automotive Systems Ag Electrical cable for resistance device in e.g. contacting device for keeping e.g. airplane wing at moderate temperature in interior component of e.g. vehicle, has substrate support arranged in limiting substrate
US9326498B2 (en) * 2010-09-14 2016-05-03 JAB Distributors, LLC Heatable enclosure for pest eradication
US9191997B2 (en) 2010-10-19 2015-11-17 Gentherm Gmbh Electrical conductor
GB2484980A (en) * 2010-11-01 2012-05-02 Bill John Finch Low voltage heating sheet
RU2474981C2 (en) * 2010-12-15 2013-02-10 Вячеслав Александрович Богулин Device to heat flat electric heaters (versions)
EP2684740B1 (en) * 2011-03-07 2016-10-26 Panasonic Intellectual Property Management Co., Ltd. Vehicle seat heater
WO2012125919A1 (en) * 2011-03-16 2012-09-20 GKN Aerospace Services Structures, Corp. Composite laminate having a flexible circuit bridge and method of manufacture thereof
DE102012000977A1 (en) 2011-04-06 2012-10-11 W.E.T. Automotive Systems Ag Heating device for complex shaped surfaces
FI20115536L (en) * 2011-05-31 2013-03-25 Teknologian Tutkimuskeskus Vtt Oy Wind turbine blades and associated manufacturing method
ES2942856T3 (en) 2011-07-13 2023-06-07 Fisher & Paykel Healthcare Ltd Impeller and motor assembly
LU91913B1 (en) * 2011-12-15 2013-06-17 Iee Sarl Sheet-type ohmic heating element
US8998144B2 (en) * 2012-02-06 2015-04-07 Textron Innovations Inc. Thermal insulation barrier for an aircraft de-icing heater
US20150083709A1 (en) * 2012-03-23 2015-03-26 Soleno Textiles Techniques Inc. Shapeable heating panel system
EA028795B1 (en) * 2012-08-01 2017-12-29 Сэн-Гобэн Гласс Франс Composite pane with electrical contact-making means
DE102012015215B3 (en) * 2012-08-03 2014-02-20 Carl Freudenberg Kg Arrangement with busbars
DE102012017047A1 (en) 2012-08-29 2014-03-06 W.E.T. Automotive Systems Ag Electric heater
US10471225B2 (en) 2012-12-18 2019-11-12 Fisher & Paykel Healthcare Limited Impeller and motor assembly
DE102012024903A1 (en) 2012-12-20 2014-06-26 W.E.T. Automotive Systems Ag Flat structure with electrical functional elements
EP2779784A1 (en) * 2013-03-14 2014-09-17 Shui-Po Lee Heating plate
GB201304691D0 (en) * 2013-03-15 2013-05-01 Smiths Medical Int Ltd Heating means and methods of manufacture
DE102013215522A1 (en) * 2013-08-07 2015-02-12 Robert Bosch Gmbh Sensor device for determining at least one parameter of a fluid flowing through a channel
ITBI20130013A1 (en) * 2013-11-05 2015-05-06 Cofilea Srl Uninominale TEXTILE ARTICLE OF THE MULTILAYER TYPE WITH INTERNAL LAYER OF ELECTRIFIED FABRIC AND RELATIVE PROCESS OF MANUFACTURE
DE102014204773A1 (en) * 2014-03-14 2015-09-17 Takraf Gmbh Heating device for chutes and baffles
WO2015157674A2 (en) 2014-04-10 2015-10-15 Augustine Biomedical And Design, Llc Underbody warming systems
EP3174705B1 (en) 2014-07-30 2019-11-27 General Nano LLC Carbon nanotube sheet structure and method for its making
CN104244474B (en) * 2014-09-15 2016-05-25 王宇 A kind of far-infrared electrothermal film
DE102014222297B4 (en) * 2014-10-31 2024-06-20 Bayerische Motoren Werke Aktiengesellschaft Single-track motor-driven vehicle with load-bearing fairing
US10206248B2 (en) 2014-11-13 2019-02-12 Augustine Temperature Management LLC Heated underbody warming systems with electrosurgical grounding
FI10797U1 (en) * 2014-12-04 2015-03-10 Wicetec Oy A conductor joint for connecting a copper conductor
CN107409442B (en) * 2015-01-12 2020-11-27 拉米纳热能控股有限公司 Fabric heating element
DE102015114163B4 (en) * 2015-08-26 2024-10-17 Deutsches Zentrum für Luft- und Raumfahrt e.V. Method for producing a flow body
EP3366080A1 (en) * 2015-10-19 2018-08-29 LaminaHeat Holding Ltd. Laminar heating elements with customized or non-uniform resistance and/or irregular shapes, and processes for manufacture
CA2912509A1 (en) * 2015-11-20 2017-05-20 John Forzani Hand warmer
US10758936B2 (en) 2015-12-08 2020-09-01 The Boeing Company Carbon nanomaterial composite sheet and method for making the same
US11021369B2 (en) 2016-02-04 2021-06-01 General Nano Llc Carbon nanotube sheet structure and method for its making
US20170238369A1 (en) * 2016-02-12 2017-08-17 Goodrich Corporation Heated aircraft floor panels
JP6832658B2 (en) * 2016-09-23 2021-02-24 スタンレー電気株式会社 Light transmission board, display device, signal device, and lighting device
DE102016119678A1 (en) * 2016-10-14 2018-04-19 Hotlineglass Gmbh Method and device for laying collecting strips in foils
WO2018098005A2 (en) * 2016-11-22 2018-05-31 Gentherm Gmbh Film heater and method of making
US10323556B2 (en) 2016-12-16 2019-06-18 Gates Corporation Electric immersion heater for diesel exhaust fluid reservoir
CN106626440B (en) * 2017-01-20 2018-07-06 中国商用飞机有限责任公司 Machining and forming method for multi-layer electric heating unit
US10457404B2 (en) * 2017-01-31 2019-10-29 Wan Tony Chee Carbon nanotube anti-icing and de-icing means for aircraft
DE102017001097A1 (en) 2017-02-07 2018-08-09 Gentherm Gmbh Electrically conductive foil
US20200113357A1 (en) * 2017-12-13 2020-04-16 Encompass Group, Llc Metalized fabric heating blanket
US10805988B2 (en) * 2017-03-14 2020-10-13 Encompass Group, Llc Metalized fabric heating blanket and method of manufacturing such
US10274436B2 (en) * 2017-03-15 2019-04-30 Baylor University Radiometric system and method for detecting ice accumulation inside an operating jet engine
CN107117319B (en) * 2017-03-22 2019-12-03 武汉航空仪表有限责任公司 One kind preventing/deicing composite material by multilayer structure
US11401974B2 (en) 2017-04-23 2022-08-02 Fisher & Paykel Healthcare Limited Breathing assistance apparatus
US10993557B2 (en) 2018-08-03 2021-05-04 American Sterilizer Company Pressure management warming headrest
KR101865825B1 (en) * 2017-09-27 2018-06-08 에버웰테크놀로지 주식회사 Heater including carbon felt and method for manufacturing the same
US11091856B2 (en) * 2017-10-27 2021-08-17 Bumblebee Tech Co., Ltd. Electric heating cloth having gaps and connection structure thereof
DE102017130463A1 (en) * 2017-12-19 2019-06-19 Digel Sticktech GmbH u. Co. KG panel heating
US11124161B2 (en) * 2018-01-26 2021-09-21 Robert Anthony Orazem Heated license plate system
GB2572616B (en) 2018-04-05 2022-11-30 Gkn Aerospace Services Ltd Heater Mat
DE202018102013U1 (en) * 2018-04-13 2018-05-09 Webasto SE Electric heater for mobile applications
US11084593B2 (en) * 2018-10-11 2021-08-10 Goodrich Corporation Additive manufactured heater elements for propeller ice protection
DE102019104635A1 (en) * 2019-02-25 2020-08-27 Deutsches Zentrum für Luft- und Raumfahrt e.V. Method of manufacturing a multilayer electrical resistance welding element, resistance welding element, plastic component and plastic component group
LU101201B1 (en) * 2019-04-30 2020-10-30 Iee Sa Flexible and Stretchable Electric Heater based on Electrically Conductive Textile Material and Method of Manufacturing Same
WO2020174000A1 (en) * 2019-02-26 2020-09-03 Iee International Electronics & Engineering S.A. Flexible and stretchable electric heater based on electrically conductive textile material and method of manufacturing same
US10765580B1 (en) 2019-03-27 2020-09-08 Augustine Biomedical And Design, Llc Patient securement system for the surgical trendelenburg position
US12108512B2 (en) 2019-06-06 2024-10-01 Kenyon International, Inc. Cooktop mat with control window
CN110482307A (en) * 2019-08-29 2019-11-22 江苏闳业机械股份有限公司 A kind of graphene heating film flat rubber belting complex machine unreeling device
CN110421952A (en) * 2019-08-30 2019-11-08 江苏闳业机械股份有限公司 A kind of graphene heating film flat rubber belting compounding machine and its processing method
USD911038S1 (en) 2019-10-11 2021-02-23 Laminaheat Holding Ltd. Heating element sheet having perforations
US11207866B2 (en) * 2020-01-03 2021-12-28 The Boeing Company Method to embed an antenna within a composite panel
WO2021155160A2 (en) 2020-01-31 2021-08-05 American Sterilizer Company Patient warming system
WO2021155146A1 (en) 2020-01-31 2021-08-05 American Sterilizer Company Ptc heating element and warming device including same for use in a patient warming system
US11952130B2 (en) 2020-03-27 2024-04-09 Airbus Operations Gmbh Structural component for an aircraft with integrated heating layer and structural battery
TWI821573B (en) * 2020-06-15 2023-11-11 財團法人紡織產業綜合研究所 Electrothermal fabric
CN111823685A (en) * 2020-06-19 2020-10-27 盐城市协和机械有限公司 Hot melting bonder for graphene floor heating material
KR102554876B1 (en) * 2021-04-13 2023-07-12 현대자동차주식회사 Car seat heater improving energy efficiency
EP4124174A1 (en) * 2021-07-19 2023-01-25 B/E Aerospace, Inc. Thin-lightweight-smart heater for freeze protection of aircraft waste fluid systems
CN113894983A (en) * 2021-11-11 2022-01-07 苏州矽美科导热科技有限公司 Automatic production line for heat-conducting silica gel gaskets and using method of automatic production line
EP4228376A1 (en) * 2022-02-15 2023-08-16 Nimesis Technology Method for manufacturing an assembly comprising a body and a device for thermal regulation of said body and assembly obtained
US11844733B1 (en) 2022-06-23 2023-12-19 Augustine Biomedical And Design, Llc Patient securement system for the surgical Trendelenburg position

Citations (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3657516A (en) * 1969-11-10 1972-04-18 Kansai Hoon Kogyo Kk Flexible panel-type heating unit
US3774299A (en) * 1970-09-21 1973-11-27 Kureha Chemical Ind Co Ltd Method for production of panel heater
US3859504A (en) * 1972-04-06 1975-01-07 Kureha Chemical Ind Co Ltd Moisture resistant panel heater
US3898427A (en) * 1973-06-29 1975-08-05 Sierracin Corp Flexible warming structure
US4245149A (en) * 1979-04-10 1981-01-13 Fairlie Ian F Heating system for chairs
US4250397A (en) * 1977-06-01 1981-02-10 International Paper Company Heating element and methods of manufacturing therefor
US4534886A (en) * 1981-01-15 1985-08-13 International Paper Company Non-woven heating element
US4734231A (en) * 1985-12-23 1988-03-29 Gunei Kagaku Kogyo Kabushiki Kaisha Process for the preparation of fiberboards
US4737618A (en) * 1984-12-26 1988-04-12 Aerospatiale Societe Nationale Industrielle Heating element for a defrosting device for a wing structure, such a device and a process for obtaining same
US5250228A (en) * 1991-11-06 1993-10-05 Raychem Corporation Conductive polymer composition
US5344696A (en) * 1990-01-24 1994-09-06 Hastings Otis Electrically conductive laminate for temperature control of aircraft surface
US5824996A (en) * 1997-05-13 1998-10-20 Thermosoft International Corp Electroconductive textile heating element and method of manufacture
US5932124A (en) * 1996-04-19 1999-08-03 Thermion Systems International Method for heating a solid surface such as a floor, wall, or countertop surface
US5954977A (en) * 1996-04-19 1999-09-21 Thermion Systems International Method for preventing biofouling in aquatic environments
US5966501A (en) * 1996-04-19 1999-10-12 Themion Systems International Method for controlling the viscosity of a fluid in a defined volume
US5981911A (en) * 1996-04-19 1999-11-09 Thermicon Systems International Method for heating the surface of a food receptacle
US6018141A (en) * 1996-04-19 2000-01-25 Thermion Systems International Method for heating a tooling die
US6057530A (en) * 1996-08-29 2000-05-02 Thermosoft International Corporation Fabric heating element and method of manufacture
US6145787A (en) * 1997-05-20 2000-11-14 Thermion Systems International Device and method for heating and deicing wind energy turbine blades
US6172344B1 (en) * 1993-12-24 2001-01-09 Gorix Limited Electrically conductive materials

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2934046B2 (en) 1991-03-22 1999-08-16 帝人株式会社 Tire warmer
EP0732038B1 (en) 1993-11-30 1999-10-06 AlliedSignal Inc. An electrically conductive composite heater and method of manufacture

Patent Citations (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3657516A (en) * 1969-11-10 1972-04-18 Kansai Hoon Kogyo Kk Flexible panel-type heating unit
US3774299A (en) * 1970-09-21 1973-11-27 Kureha Chemical Ind Co Ltd Method for production of panel heater
US3859504A (en) * 1972-04-06 1975-01-07 Kureha Chemical Ind Co Ltd Moisture resistant panel heater
US3898427A (en) * 1973-06-29 1975-08-05 Sierracin Corp Flexible warming structure
US4250397A (en) * 1977-06-01 1981-02-10 International Paper Company Heating element and methods of manufacturing therefor
US4245149A (en) * 1979-04-10 1981-01-13 Fairlie Ian F Heating system for chairs
US4534886A (en) * 1981-01-15 1985-08-13 International Paper Company Non-woven heating element
US4737618A (en) * 1984-12-26 1988-04-12 Aerospatiale Societe Nationale Industrielle Heating element for a defrosting device for a wing structure, such a device and a process for obtaining same
US4734231A (en) * 1985-12-23 1988-03-29 Gunei Kagaku Kogyo Kabushiki Kaisha Process for the preparation of fiberboards
US5344696A (en) * 1990-01-24 1994-09-06 Hastings Otis Electrically conductive laminate for temperature control of aircraft surface
US5250228A (en) * 1991-11-06 1993-10-05 Raychem Corporation Conductive polymer composition
US6172344B1 (en) * 1993-12-24 2001-01-09 Gorix Limited Electrically conductive materials
US5981911A (en) * 1996-04-19 1999-11-09 Thermicon Systems International Method for heating the surface of a food receptacle
US5942140A (en) * 1996-04-19 1999-08-24 Thermion Systems International Method for heating the surface of an antenna dish
US5954977A (en) * 1996-04-19 1999-09-21 Thermion Systems International Method for preventing biofouling in aquatic environments
US5966501A (en) * 1996-04-19 1999-10-12 Themion Systems International Method for controlling the viscosity of a fluid in a defined volume
US5932124A (en) * 1996-04-19 1999-08-03 Thermion Systems International Method for heating a solid surface such as a floor, wall, or countertop surface
US6015965A (en) * 1996-04-19 2000-01-18 Thermion Systems International Method for heating a solid surface such as a floor, wall, roof, or countertop surface
US6018141A (en) * 1996-04-19 2000-01-25 Thermion Systems International Method for heating a tooling die
US6087630A (en) * 1996-04-19 2000-07-11 Thermion Systems International Method for heating a solid surface such as a floor, wall, roof, or countertop surface
US6057530A (en) * 1996-08-29 2000-05-02 Thermosoft International Corporation Fabric heating element and method of manufacture
US5824996A (en) * 1997-05-13 1998-10-20 Thermosoft International Corp Electroconductive textile heating element and method of manufacture
US6145787A (en) * 1997-05-20 2000-11-14 Thermion Systems International Device and method for heating and deicing wind energy turbine blades

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2599738A3 (en) * 2004-01-19 2014-06-18 Winstore Europe B.V. Method for producing container parts, container parts, method for producing a multilayer foil, multilayer foil.
US20060086717A1 (en) * 2004-09-16 2006-04-27 Robert Oosterling Roll-up heating for a floor, or wall
US7589298B2 (en) 2004-09-16 2009-09-15 Devi A/S Roll-up heating for a floor, or wall
NL1027053C2 (en) * 2004-09-16 2006-03-20 Robert Oosterling Rollable floor heating.
US7862375B2 (en) 2004-09-16 2011-01-04 Devi A/S Electrical connector for a roll-up heating
US20140190957A1 (en) * 2008-04-25 2014-07-10 Innovative Heating Technologies Inc. Planar Heating Element for Underfloor Heating
US8989874B2 (en) * 2009-01-20 2015-03-24 Leonh.Lang Bioelectrode
US20100185078A1 (en) * 2009-01-20 2010-07-22 Leonh.Lang Bioelectrode
CN102555238A (en) * 2010-12-23 2012-07-11 上海杰事杰新材料(集团)股份有限公司 Manufacturing method of fiber cloth reinforced thermoplastic resin composite material
US20130186884A1 (en) * 2012-01-20 2013-07-25 W.E.T. Automotive Systems, Ltd. Felt heater and method of making
US10201039B2 (en) * 2012-01-20 2019-02-05 Gentherm Gmbh Felt heater and method of making
US11376811B2 (en) 2018-07-03 2022-07-05 Goodrich Corporation Impact and knife cut resistant pre-impregnated woven fabric for aircraft heated floor panels
US11878500B2 (en) 2018-07-03 2024-01-23 Goodrich Corporation Impact and knife cut resistant pre-impregnated woven fabric for aircraft heated floor panels

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