US20030199947A1 - Thermoplastic laminate fabric heater and methods for making same - Google Patents
Thermoplastic laminate fabric heater and methods for making same Download PDFInfo
- 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
- Authority
- US
- United States
- Prior art keywords
- heater
- layer
- thermoplastic
- bus bars
- fabric
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Abandoned
Links
- 239000004744 fabric Substances 0.000 title claims abstract description 119
- 239000004416 thermosoftening plastic Substances 0.000 title claims abstract description 66
- 229920001169 thermoplastic Polymers 0.000 title claims abstract description 63
- 238000000034 method Methods 0.000 title claims abstract description 46
- 238000004519 manufacturing process Methods 0.000 claims abstract description 10
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 46
- 239000000835 fiber Substances 0.000 claims description 30
- 239000011889 copper foil Substances 0.000 claims description 23
- 238000007596 consolidation process Methods 0.000 claims description 13
- 239000002184 metal Substances 0.000 claims description 12
- 229910052751 metal Inorganic materials 0.000 claims description 12
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims description 10
- 238000010030 laminating Methods 0.000 claims description 10
- 239000004697 Polyetherimide Substances 0.000 claims description 9
- 239000011888 foil Substances 0.000 claims description 9
- 229920001601 polyetherimide Polymers 0.000 claims description 9
- 238000001816 cooling Methods 0.000 claims description 8
- 238000005520 cutting process Methods 0.000 claims description 8
- 238000010438 heat treatment Methods 0.000 claims description 8
- 238000003475 lamination Methods 0.000 claims description 7
- 229920002379 silicone rubber Polymers 0.000 claims description 7
- 229920000049 Carbon (fiber) Polymers 0.000 claims description 6
- 239000004917 carbon fiber Substances 0.000 claims description 6
- 239000011521 glass Substances 0.000 claims description 6
- 229910052759 nickel Inorganic materials 0.000 claims description 5
- 239000004945 silicone rubber Substances 0.000 claims description 5
- KRHYYFGTRYWZRS-UHFFFAOYSA-M Fluoride anion Chemical compound [F-] KRHYYFGTRYWZRS-UHFFFAOYSA-M 0.000 claims description 3
- 239000004952 Polyamide Substances 0.000 claims description 3
- 239000004721 Polyphenylene oxide Substances 0.000 claims description 3
- 229920002647 polyamide Polymers 0.000 claims description 3
- 229920006380 polyphenylene oxide Polymers 0.000 claims description 3
- 229920002725 thermoplastic elastomer Polymers 0.000 claims description 3
- 239000004696 Poly ether ether ketone Substances 0.000 claims description 2
- 229920002530 polyetherether ketone Polymers 0.000 claims description 2
- 150000003457 sulfones Chemical class 0.000 claims 1
- 239000004840 adhesive resin Substances 0.000 abstract description 7
- 229920006223 adhesive resin Polymers 0.000 abstract description 7
- 239000000126 substance Substances 0.000 abstract description 3
- 230000006353 environmental stress Effects 0.000 abstract description 2
- 230000005855 radiation Effects 0.000 abstract description 2
- 229910052802 copper Inorganic materials 0.000 description 23
- 239000010949 copper Substances 0.000 description 23
- 239000003365 glass fiber Substances 0.000 description 14
- 239000000463 material Substances 0.000 description 6
- 229920003023 plastic Polymers 0.000 description 6
- 239000004033 plastic Substances 0.000 description 6
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 5
- 239000002245 particle Substances 0.000 description 4
- 229920005989 resin Polymers 0.000 description 4
- 239000011347 resin Substances 0.000 description 4
- 239000003795 chemical substances by application Substances 0.000 description 3
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- 229910001369 Brass Inorganic materials 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 2
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 239000004695 Polyether sulfone Substances 0.000 description 2
- BQCADISMDOOEFD-UHFFFAOYSA-N Silver Chemical compound [Ag] BQCADISMDOOEFD-UHFFFAOYSA-N 0.000 description 2
- 229920004738 ULTEM® Polymers 0.000 description 2
- 239000010951 brass Substances 0.000 description 2
- 229910052799 carbon Inorganic materials 0.000 description 2
- 239000006229 carbon black Substances 0.000 description 2
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 239000003989 dielectric material Substances 0.000 description 2
- 238000009826 distribution Methods 0.000 description 2
- 206010016256 fatigue Diseases 0.000 description 2
- 239000011152 fibreglass Substances 0.000 description 2
- 239000007788 liquid Substances 0.000 description 2
- 229920006393 polyether sulfone Polymers 0.000 description 2
- 238000002360 preparation method Methods 0.000 description 2
- 230000002787 reinforcement Effects 0.000 description 2
- 238000000926 separation method Methods 0.000 description 2
- 229910052709 silver Inorganic materials 0.000 description 2
- 239000004332 silver Substances 0.000 description 2
- 239000007858 starting material Substances 0.000 description 2
- 230000001988 toxicity Effects 0.000 description 2
- 231100000419 toxicity Toxicity 0.000 description 2
- 239000004593 Epoxy Substances 0.000 description 1
- -1 Inc. PA) Polymers 0.000 description 1
- 229920006370 Kynar Polymers 0.000 description 1
- 239000004727 Noryl Substances 0.000 description 1
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- 239000002033 PVDF binder Substances 0.000 description 1
- 239000004809 Teflon Substances 0.000 description 1
- 229920006362 Teflon® Polymers 0.000 description 1
- 229920004695 VICTREX™ PEEK Polymers 0.000 description 1
- 238000005299 abrasion Methods 0.000 description 1
- 239000000853 adhesive Substances 0.000 description 1
- 230000001070 adhesive effect Effects 0.000 description 1
- WYTGDNHDOZPMIW-RCBQFDQVSA-N alstonine Natural products C1=CC2=C3C=CC=CC3=NC2=C2N1C[C@H]1[C@H](C)OC=C(C(=O)OC)[C@H]1C2 WYTGDNHDOZPMIW-RCBQFDQVSA-N 0.000 description 1
- 229920003235 aromatic polyamide Polymers 0.000 description 1
- 239000011230 binding agent Substances 0.000 description 1
- 238000005219 brazing Methods 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 238000002788 crimping Methods 0.000 description 1
- 239000006185 dispersion Substances 0.000 description 1
- 229920001971 elastomer Polymers 0.000 description 1
- 239000003822 epoxy resin Substances 0.000 description 1
- 238000009499 grossing Methods 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 238000003698 laser cutting Methods 0.000 description 1
- 239000000314 lubricant Substances 0.000 description 1
- 239000004745 nonwoven fabric Substances 0.000 description 1
- LCCNCVORNKJIRZ-UHFFFAOYSA-N parathion Chemical compound CCOP(=S)(OCC)OC1=CC=C([N+]([O-])=O)C=C1 LCCNCVORNKJIRZ-UHFFFAOYSA-N 0.000 description 1
- 229920001643 poly(ether ketone) Polymers 0.000 description 1
- 229920003223 poly(pyromellitimide-1,4-diphenyl ether) Polymers 0.000 description 1
- 229920002492 poly(sulfone) Polymers 0.000 description 1
- 229920000647 polyepoxide Polymers 0.000 description 1
- 229920000728 polyester Polymers 0.000 description 1
- 229920005594 polymer fiber Polymers 0.000 description 1
- 229920002981 polyvinylidene fluoride Polymers 0.000 description 1
- 238000010791 quenching Methods 0.000 description 1
- 239000005060 rubber Substances 0.000 description 1
- 229920006395 saturated elastomer Polymers 0.000 description 1
- 229910000679 solder Inorganic materials 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 230000035882 stress Effects 0.000 description 1
- 238000010792 warming Methods 0.000 description 1
- 239000002699 waste material Substances 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered 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
- B32B5/22—Layered 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
- B32B5/24—Layered 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
- B32B5/26—Layered 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/68—Shaping 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
- B29C70/82—Forcing wires, nets or the like partially or completely into the surface of an article, e.g. by cutting and pressing
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/88—Shaping 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
- B29C70/882—Shaping 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
- B29C70/885—Shaping 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B17/00—Layered products essentially comprising sheet glass, or glass, slag, or like fibres
- B32B17/02—Layered products essentially comprising sheet glass, or glass, slag, or like fibres in the form of fibres or filaments
- B32B17/04—Layered 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
- B64D15/12—De-icing or preventing icing on exterior surfaces of aircraft by electric heating
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
- H05B3/00—Ohmic-resistance heating
- H05B3/20—Heating elements having extended surface area substantially in a two-dimensional plane, e.g. plate-heater
- H05B3/34—Heating elements having extended surface area substantially in a two-dimensional plane, e.g. plate-heater flexible, e.g. heating nets or webs
- H05B3/36—Heating 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B38/00—Ancillary operations in connection with laminating processes
- B32B38/04—Punching, slitting or perforating
- B32B2038/047—Perforating
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2305/00—Condition, form or state of the layers or laminate
- B32B2305/10—Fibres of continuous length
- B32B2305/18—Fabrics, textiles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2305/00—Condition, form or state of the layers or laminate
- B32B2305/10—Fibres of continuous length
- B32B2305/20—Fibres of continuous length in the form of a non-woven mat
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/20—Properties of the layers or laminate having particular electrical or magnetic properties, e.g. piezoelectric
- B32B2307/202—Conductive
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2315/00—Other materials containing non-metallic inorganic compounds not provided for in groups B32B2311/00 - B32B2313/04
- B32B2315/08—Glass
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2398/00—Unspecified macromolecular compounds
- B32B2398/20—Thermoplastics
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
- B32B37/14—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers
- B32B37/16—Methods 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
- B32B37/20—Methods 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
- B32B37/203—One or more of the layers being plastic
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
- H05B2203/00—Aspects relating to Ohmic resistive heating covered by group H05B3/00
- H05B2203/002—Heaters using a particular layout for the resistive material or resistive elements
- H05B2203/005—Heaters using a particular layout for the resistive material or resistive elements using multiple resistive elements or resistive zones isolated from each other
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
- H05B2203/00—Aspects relating to Ohmic resistive heating covered by group H05B3/00
- H05B2203/011—Heaters using laterally extending conductive material as connecting means
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
- H05B2203/00—Aspects relating to Ohmic resistive heating covered by group H05B3/00
- H05B2203/013—Heaters using resistive films or coatings
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
- H05B2203/00—Aspects relating to Ohmic resistive heating covered by group H05B3/00
- H05B2203/017—Manufacturing methods or apparatus for heaters
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
- H05B2203/00—Aspects relating to Ohmic resistive heating covered by group H05B3/00
- H05B2203/026—Heaters specially adapted for floor heating
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
- H05B2203/00—Aspects relating to Ohmic resistive heating covered by group H05B3/00
- H05B2203/029—Heaters specially adapted for seat warmers
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
- H05B2203/00—Aspects relating to Ohmic resistive heating covered by group H05B3/00
- H05B2203/033—Heater including particular mechanical reinforcing means
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
- H05B2203/00—Aspects relating to Ohmic resistive heating covered by group H05B3/00
- H05B2203/036—Heaters 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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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
- 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.
- 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.
- 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.
- 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. 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.
- 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. For example, the patent discloses that the fabric heaters are primary useful for low voltage source operation.
- 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.
- 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.
- 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.
- 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.
- 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.
- 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.
- 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.
- 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.
- 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.
- 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.
- 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.
- 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.
- 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. 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.
- 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.
- 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 approximately275° 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
conductive fabric 10, the bus bar strips 12, 14, thethermoplastic film glass fiber veil - 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
conductive fabric 10, two rolls ofthermoplastic film copper foil 12, 14, and two rolls ofglass fiber veil conductive fabric 10, pulled from a roll, is combined withcopper 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 theconductive 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 bars12, 14 and
conductive fabric 10 are drawn together through a piercingrivetor 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
thermoplastic films conductive fabric 10, with the copper foil bus bars attached, are drawn between the two layers ofthermoplastic film conductive fabric 10. To facilitate wire attachment to the copper foil bus-bar the top layer ofthermoplastic film 16 may be perforated prior to the first lamination process. Over and outside the thermoplastic film,glass fiber veil - 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 cooling chamber 19 to maintain maximal degree of consolidation. - To increase the resistance of the heater,
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.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.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.
- 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.
- 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.
- 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.
- Construction of a Business Card Sized Novelty Heater by Batch Processing for Small Quantities.
- 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 to3 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.
- 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.
- 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. 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.
- 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.
- 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.
- 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.
Claims (17)
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.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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US10/293,204 US20030199947A1 (en) | 1999-12-10 | 2002-11-13 | Thermoplastic laminate fabric heater and methods for making same |
Applications Claiming Priority (3)
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US17001699P | 1999-12-10 | 1999-12-10 | |
US09/733,729 US6483087B2 (en) | 1999-12-10 | 2000-12-08 | Thermoplastic laminate fabric heater and methods for making same |
US10/293,204 US20030199947A1 (en) | 1999-12-10 | 2002-11-13 | Thermoplastic laminate fabric heater and methods for making same |
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US09/733,729 Continuation US6483087B2 (en) | 1999-12-10 | 2000-12-08 | Thermoplastic laminate fabric heater and methods for making same |
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US20030199947A1 true US20030199947A1 (en) | 2003-10-23 |
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US10/293,204 Abandoned US20030199947A1 (en) | 1999-12-10 | 2002-11-13 | Thermoplastic laminate fabric heater and methods for making same |
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US09/733,729 Expired - Fee Related US6483087B2 (en) | 1999-12-10 | 2000-12-08 | Thermoplastic laminate fabric heater and methods for making same |
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Cited By (7)
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)
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 |
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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 |
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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 |
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US10274436B2 (en) * | 2017-03-15 | 2019-04-30 | Baylor University | Radiometric system and method for detecting ice accumulation inside an operating jet engine |
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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 |
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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 |
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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 |
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EP4124174A1 (en) * | 2021-07-19 | 2023-01-25 | B/E Aerospace, Inc. | Thin-lightweight-smart heater for freeze protection of aircraft waste fluid systems |
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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)
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)
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 |
-
2000
- 2000-12-08 AU AU20717/01A patent/AU2071701A/en not_active Abandoned
- 2000-12-08 DE DE60033425T patent/DE60033425D1/en not_active Expired - Lifetime
- 2000-12-08 CA CA002393970A patent/CA2393970C/en not_active Expired - Fee Related
- 2000-12-08 CN CNB008169810A patent/CN1183805C/en not_active Expired - Fee Related
- 2000-12-08 AT AT00984037T patent/ATE354266T1/en not_active IP Right Cessation
- 2000-12-08 WO PCT/US2000/033261 patent/WO2001043507A1/en active IP Right Grant
- 2000-12-08 JP JP2001543076A patent/JP2003516609A/en active Pending
- 2000-12-08 EP EP00984037A patent/EP1238572B1/en not_active Expired - Lifetime
- 2000-12-08 US US09/733,729 patent/US6483087B2/en not_active Expired - Fee Related
-
2002
- 2002-11-13 US US10/293,204 patent/US20030199947A1/en not_active Abandoned
Patent Citations (23)
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)
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 |
Also Published As
Publication number | Publication date |
---|---|
JP2003516609A (en) | 2003-05-13 |
US20020153368A1 (en) | 2002-10-24 |
CN1183805C (en) | 2005-01-05 |
CA2393970C (en) | 2004-07-20 |
CA2393970A1 (en) | 2001-06-14 |
WO2001043507A1 (en) | 2001-06-14 |
EP1238572B1 (en) | 2007-02-14 |
AU2071701A (en) | 2001-06-18 |
DE60033425D1 (en) | 2007-03-29 |
EP1238572A1 (en) | 2002-09-11 |
US6483087B2 (en) | 2002-11-19 |
CN1409941A (en) | 2003-04-09 |
ATE354266T1 (en) | 2007-03-15 |
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