Multi-layer insulation system for electrical conductors

Abstract
A multi-layer insulation system for electrical conductors, an insulated electrical conductor, a process for preparing an insulated conductor, and an insulated conductor prepared by such a process are provided. The insulated electrical conductors are lightweight, qualify for temperature ratings of up to approximately 230° C., and demonstrate mechanical durability and hydrolysis resistance. As such, these insulated conductors are particularly useful for aircraft wire and cable.
Description




TECHNICAL FIELD OF THE INVENTION




The present invention basically relates to a multi-layer insulation system for electrical conductors, an insulated electrical conductor, a process for preparing an insulated conductor, and an insulated conductor prepared by such a process. The insulated electrical conductors of the present invention are lightweight, qualify for temperature ratings of up to approximately 230° C., and demonstrate mechanical durability, and hydrolysis resistance. As such, these insulated conductors are particularly useful for aircraft wire and cable.




BACKGROUND OF THE INVENTION




Electrical insulation must meet a variety of construction and performance requirements. These requirements are particularly severe for electrical cable which is to be used in aircraft and similar equipment. Electrical cable useful for such applications must demonstrate a balance of electrical, thermal, and mechanical properties, with overall performance being evaluated by assessing properties such as abrasion and cut-through resistance, chemical and fluid resistance, dry and wet arc tracking, and flammability and smoke generation. At the same time, such cables must adhere to rigid weight limitations.




Aircraft wire constructions comprising a polyimide inner layer, and a polytetrafluoroethylene (PTFE) outer layer, are known. In such constructions, the polyimide inner layer is formed by spiral-wrapping an adhesive (e.g., PTFE, fluorinated ethylene-propylene (FEP), or perfluoroalkoxy (PFA))-coated polyimide tape, in an overlapping fashion, about a conductor. The spiral-wrapped polyimide tape is heat-sealed at the spiral-wrapped tape joints. The PTFE outer layer is formed by spiral-wrapping unsintered PTFE tape about the heat-sealed polyimide inner layer. The unsintered PTFE tape outer layer is also heat-sealed at the spiral-wrapped joints by sintering the wrapped tape.




The above-referenced aircraft wire constructions have a temperature rating of approximately 260° C., and while demonstrating good mechanical durability, these wire constructions provide only low-to-moderate long-term humidity resistance and laser markability properties. In addition, the PTFE outer layer is easily scrapped off, thereby exposing the inner layer and rendering it susceptible to hydrolysis in humid environments.




As will be readily apparent to those skilled in the art, the aircraft wire constructions described above do not employ a radiation crosslinked outer layer, where exposing perfluorinated polymers such as PTFE, FEP, and PFA to radiation would serve to degrade these materials.




Aircraft wire constructions comprising one or more layers of extruded ethylene tetrafluoroethylene (ETFE) copolymer, are also known. In such constructions, the ETFE copolymer layer(s) is generally crosslinked by irradiation to achieve use-temperature ratings of greater than 150° to 200° C. The reduction in use-temperature ratings is partially offset by the fact that these wire constructions demonstrate mechanical durability, long-term humidity resistance, and laser markability properties which are superior to those noted above for polyimide/PTFE wire constructions.




A need therefore exists for an aircraft wire construction which qualifies for higher use-temperatures, while demonstrating improved mechanical durability, long-term humidity resistance, and laser markabilty properties.




It is therefore an object of the present invention to provide such an insulated wire construction.




It is a more particular object to provide a multi-layer insulation system for electrical conductors.




It is another more particular object of the present invention, to provide a lightweight insulated electrical conductor prepared using the above-referenced multi-layer insulation system, which qualifies for a temperature rating of up to approximately 230° C., and which demonstrates improved mechanical durability, and hydrolysis resistance.




It is yet another more particular object to provide an insulated electrical conductor that further demonstrates flame resistance and laser markability.




It is a further object of the present invention to provide a process for preparing such an insulated conductor, and an insulated conductor prepared by such a process.




SUMMARY




The present invention therefore provides a multi-layer insulation system for electrical conductors, which comprises:




(a) a polyimide or fluoropolymer inner layer,




wherein, when the inner layer is a polyimide inner layer, the layer is formed by wrapping a polyimide film, which has been coated with a sealable component, in an overlapping fashion, along a portion or length of an electrical conductor, wherein the polyimide film is substantially uniformly sealed to itself in overlapping regions along the length of the conductor, thereby forming an effective seal against moisture, wherein the sealable component comprises a perfluoropolymer, a crosslinked fluoropolymer, or a polyimide adhesive,




wherein, when the inner layer is a fluoropolymer inner layer, the layer is formed by either extruding a fluoropolymer material along a portion or length of the electrical conductor, or by wrapping a fluoropolymer film, in an overlapping fashion, along a portion or length of the conductor,




(b) optionally, a polyimide middle layer, wherein the polyimide middle layer is formed by wrapping an optionally coated polyimide film, in an overlapping fashion, along a portion or length of the inner layer formed on the electrical conductor, and




(c) an extruded, crosslinked fluoropolymer outer layer, wherein the fluoropolymer is selected from the group consisting of copolymers and terpolymers of ethylene-tetrafluoroethylene, and mixtures thereof,




wherein, when the inner layer is a fluoropolymer inner layer, the multi-layer insulation system includes a polyimide middle layer.




The present invention also provides an insulated electrical conductor that comprises an electrical conductor insulated with the multi-layer insulation system described above.




The present invention further provides a process for preparing an insulated electrical conductor, which comprises:




(a) forming a polyimide or fluoropolymer inner layer on an electrical conductor,




wherein, when the inner layer is a polyimide inner layer, the layer is formed by wrapping a polyimide film, which has been coated with a sealable component, in an overlapping fashion, along a portion or length of the electrical conductor, wherein the sealable component comprises a perfluoropolymer, a crosslinked fluoropolymer, or a polyimide adhesive,




wherein, when the inner layer is a fluoropolymer inner layer, the layer is formed by either: i) extruding a fluoropolymer material along a portion or length of the electrical conductor, or ii) wrapping a fluoropolymer film, in an overlapping fashion, along a portion or length of the electrical conductor,




(b) optionally, forming a polyimide middle layer on the polyimide or fluoropolymer inner layer by wrapping an optionally coated polyimide film, in an overlapping fashion, along a portion or length of the inner layer,




(c) when the inner layer is a polyimide inner layer or when a middle layer is formed using a coated polyimide film, heating the polyimide film or films to a temperature ranging from about 240° to about 350° C. to cause overlapping regions of the coated film or films to bond, thereby forming an effective seal against moisture along the length of the conductor,




(d) forming a fluoropolymer outer layer on either the inner or middle layer by extruding a fluoropolymer material along a portion or length of that layer; and




(e) crosslinking the fluoropolymer outer layer, wherein, when the inner layer or the sealable component comprises a perfluoropolymer (e.g., polytetrafluoroethylene, fluorinated ethylene propylene copolymers, perfluoroalkoxy resins), the fluoropolymer outer layer is crosslinked by exposing it to less than 60 megarads of radiation, with applied voltages ranging from about 50 to about 120 kilo volts,




wherein, when the inner layer is a fluoropolymer inner layer, the process for preparing an insulated electrical conductor includes forming a polyimide middle layer on the fluoropolymer inner layer.




The present invention also provides an insulated electrical conductor prepared by the process described above.




The foregoing and other features and advantages of the present invention will become more apparent from the following description and accompanying drawings.











BRIEF DESCRIPTION OF THE DRAWINGS





FIG. 1

is an elevational side view of a stranded cable insulated with a preferred embodiment of the multi-layer insulation system of the present invention, having the outer insulating layer cut away for purposes of illustration;





FIG. 2

is an elevational side view of a stranded cable spiral-wrapped with a polyimide film or tape prior to undergoing a heat-sealing operation;





FIG. 3

is an elevational side view of a stranded cable axially-wrapped with a polyimide film or tape prior to undergoing a heat-sealing operation; and





FIG. 4

is an elevational side view of a stranded cable insulated with a more preferred embodiment of the multi-layer insulation system of the present invention, having middle and outer insulating layers cut away for purposes of illustration.











BEST MODE FOR CARRYING OUT THE INVENTION




The multi-layer insulation system of the present invention possesses or demonstrates a combination of characteristics or properties not found in conventional insulating materials. This unique combination of desirable properties make the inventive insulated conductor most valuable in applications such as aircraft, missiles, satellites, etc.




As will be described in more detail below, the high degree of high temperature adhesive bond strength demonstrated by the inner layer of a preferred embodiment of the present invention has been found to be particularly surprising.




Referring now to

FIG. 1

in detail, reference numeral


10


has been used to generally designate a preferred embodiment of the insulated electrical conductor of the present invention. Insulated electrical conductor


10


basically comprises an electrical conductor


12


, which is insulated with a multi-layer insulation system


14


comprising:




(1) a polyimide film inner layer


16


;




wherein the polyimide film inner layer


16


is formed by wrapping the film, which has been coated with a sealable component, in an overlapping fashion, along a portion or length of the electrical conductor


12


,




wherein the polyimide film is substantially uniformly sealed to itself in overlapping regions along the length of the conductor


12


, thereby forming an effective seal against moisture, and




wherein the sealable component comprises a perfluoropolymer, a crosslinked fluoropolymer, or a polyimide adhesive; and




(2) an extruded, crosslinked fluoropolymer outer layer


18


.




The electrical conductor


12


of the present invention may take various forms (e.g., metal wire, stranded cable), and may be prepared using any suitable conductive material including copper, copper alloys, nickel, nickel-clad copper, nickel-plated copper, tin, silver, and silver-plated copper. In a preferred embodiment, the electrical conductor is in the form of a stranded cable, and is prepared using copper or nickel-plated copper.




Any film-forming polyimide may be used in the practice of the present invention, with preferred polyimides being aromatic polyimide films. In a more preferred embodiment, the polyimide film is a polyimide copolymer film derived from the reaction of an aromatic tetracarboxylic acid dianhydride component comprising from 0 to 95 mole %, preferably from 10 to 95 mole %, of 3,3′,4,4′-biphenyltetracarboxylic dianhydride and from 5 to 100 mole %, preferably from 5 to 90 mole %, of pyromellitic dianhydride, and an aromatic diamine component comprising from 25 to 99 mole %, preferably from 40 to 98 mole %, of p-phenylene diamine and from 1 to 75 mole %, preferably from 2 to 60 mole %, of a diaminodiphenyl ether such as 4,4′-diaminodiphenyl ether, 3,3′-diaminodiphenyl ether or 3,4′-diaminodiphenyl ether. Such films are described in U.S. Pat. No. 5,731,088 to Philip R. La Court, which is incorporated herein by reference.




Polyimide films suitable for use in inner layer


16


of the present invention are films having a sealable component (i.e., a heat-sealable adhesive) coated or laminated on/to at least one surface. It is noted that such films are typically purchased with at least one surface coated with a heat-sealable adhesive, where the coating or lamination of such films constitutes a highly specialized area of practice undertaken by only a limited number of companies.




Heat-sealable adhesives which may be used in the present invention include perfluoropolymer, crosslinkable fluoropolymer, and polyimide adhesives.




Perfluoropolymer adhesives, suitable for use in the present invention, include PTFE, FEP, PFA, and copolymers of tetrafluoroethylene and perfluoromethylvinylether (MFA) adhesives, while suitable crosslinkable fluoropolymer adhesives include ETFE and chlorotrifluoroethylene (CTFE) copolymer and terpolymer adhesives which contain minor amounts of one or more fluorinated comonomers (e.g., HFP, HFIB, PFBE, VDF and VF).




Polyimide adhesives, suitable for use in the present invention, include thermoplastic polyimide adhesives, which soften and become fluid at or above 200° C.




Preferred heat-sealable films are polyimide films coated or laminated with a heat-sealable polyimide adhesive. Such materials are available from E.I. DuPont de Nemours and Company (“DuPont”), Wilmington, Del., under the trade designation KAPTON HKJ, KAPTON EKJ, and ELJ heat-sealable polyimide films.




The heat-sealable films are preferably applied to an electrical conductor


12


in tape form, by either spirally or axially wrapping the tape about the conductor


12


.




For spiral-wrap applications, the tape preferably has a width ranging from about 0.30 to about 0.95 centimeters (cm), and a thickness ranging from about 0.01 to about 0.04 millimeters (mm). As best shown in

FIG. 2

, which depicts electrical conductor


12


spiral-wrapped with a polyimide tape


20


prior to undergoing a heat-sealing operation, the tape


20


is preferably wrapped so as to achieve a degree of overlap ranging from about 10 to about 70%.




In regard to axial-wrap applications for typical aircraft wire, the tape


20


preferably has a width ranging from about 0.15 to about 0.50 cm, and a thickness ranging from about 0.01 to about 0.04 mm. For much larger conductors, such as main power lines in aircraft, the tape


20


preferably has a width of from about 115 to about 150% of the conductor circumference, and a thickness ranging from about 0.01 to about 0.04 mm. As best shown in

FIG. 3

, which depicts the conductor


12


axially-wrapped with the polyimide tape


20


prior to undergoing a heat-sealing operation, the tape


20


is preferably wrapped so as to achieve a degree of overlap ranging from about 15 to about 50%.




After the tape


20


is applied to the conductor


12


, the resulting assembly is heated to a temperature ranging from about 240 to about 350° C., preferably from about 260 to about 280° C. The purpose of the heating operation is to bond or fuse the overlapping regions of the polyimide tape


20


, thereby forming an effective seal against moisture along the length of the conductor


12


. As a result, the electrical integrity of the conductor


12


will be preserved.




The thickness of the inner layer


16


of the insulated electrical conductor


10


of the present invention preferably ranges from about 0.01 to about 0.08 mm, and more preferably ranges from about 0.02 to about 0.05 mm.




Inner layer


16


demonstrates a high temperature (i.e., 150° C.) adhesive bond strength ranging from about 100 to about 250 grams per inch-width (gm/inch-width). When inner layer


16


is prepared using a polyimide film coated or laminated with a heat-sealable polyimide adhesive, it demonstrates a high temperature (i.e., 150° C.) adhesive bond strength of greater than 1000 gm/inch-width, preferably greater than 1500 gm/inch-width. Such adhesive bond strengths are considerably higher than those demonstrated by prior art heat-sealed wire insulations. High temperature adhesive bond strength is measured in accordance with ASTM# 1876-00—Standard Test Method for Peel Resistance of Adhesives (T-Peel Test).




As referenced above, the high degree of high temperature adhesive bond strength demonstrated by inner layer


16


, when prepared using the preferred heat-sealable films, has been found to be particularly surprising.




Fluoropolymers which may advantageously be utilized in the outer layer


18


of the insulated electrical conductor


10


of the present invention include, for example, copolymers and terpolymers of ethylene-tetrafluoroethylene (ETFE), and mixtures thereof.




It is noted that extruded fluoropolymer outer layers change color as a result of thermal aging. Where polyimides demonstrate greater thermal stability than fluoropolymers, the noted color change in the outer layer can serve as an early warning signal that the insulated electrical conductor will need to be replaced. This feature is extremely valuable in aircraft wire and cable applications.




In a preferred embodiment, the fluoropolymer of outer layer


18


is an ETFE copolymer which comprises 35 to 60 mole % (preferably 40 to 50 mole %) of units derived from ethylene, 35 to 60 mole % (preferably 50 to 55 mole %) of units derived from tetrafluoroethylene and up to 10 mole % (preferably 2 mole %) of units derived from one or more fluorinated comonomers (e.g., HFP, HFIB, PFBE, VDF and VF). Such copolymers are available from DuPont under the trade designation TEFZEL HT 200, and from Daikin America, Inc. (“Daikin”), Orangeburg, N.Y., under the trade designation NEOFLON EP-541.




The fluoropolymer(s) preferably contains (as extruded) from about 4 to about 16% by weight of a crosslinking agent. Preferred crosslinking agents are radiation crosslinking agents that contain multiple carbon-carbon double bonds.




In a more preferred embodiment, crosslinking agents containing at least two allyl groups and more preferably, three or four allyl groups, are employed. Particularly preferred crosslinking agents are triallyl isocyanurate (TAIC), triallylcyanurate (TAC) and trimethallylisocyanurate (TMAIC).




In yet a more preferred embodiment, the fluoropolymer(s) contains a photosensitive substance (e.g., titanium dioxide), which renders the outer layer


18


receptive to laser marking. The term “laser marking,” as used herein, is intended to mean a method of marking an insulated conductor using an intense source of ultraviolet or visible radiation, preferably a laser source. In accordance with this method, exposure of the fluoropolymer outer layer


18


to such intense radiation will result in a darkening where the radiation was incident. By controlling the pattern of incidence, marks such as letters and numbers can be formed.




In yet a more preferred embodiment, the fluoropolymer(s) contains from about 1 to about 4% by weight, of titanium dioxide.




In addition to the above component(s), the fluoropolymer(s) may advantageously contain other additives such as pigments (e.g., titanium oxide), lubricants (e.g., PTFE powder), antioxidants, stabilizers, flame retardants (e.g., antimony oxide), fibers, mineral fibers, dyes, plasticizers and the like. However, some such additives may have an adverse effect on the desirable properties of the insulated electrical conductor of the present invention.




The components of the outer layer may be blended together by any conventional process until a uniform mix is obtained. In a preferred embodiment, a twin-screw extruder is used for compounding. The outer layer


18


is preferably formed by melt-extrusion, and then crosslinked using either known techniques, which include beta and gamma radiation crosslinking methods, or “skin irradiation” techniques. “Skin irradiation” techniques are described in more detail below.




The thickness of the outer layer


18


of the insulated electrical conductor


10


of the present invention preferably ranges from about 0.05 to about 0.25 mm, and more preferably ranges from about 0.10 to about 0.13 mm.




Referring now to

FIG. 4

in detail, reference numeral


110


has been used to generally designate a more preferred embodiment of the insulated electrical conductor of the present invention. In this more preferred embodiment, insulated electrical conductor


110


demonstrates improved flexibility, and comprises an electrical conductor


112


, which is insulated with a multi-layer insulation system


114


comprising:




(1) a fluoropolymer inner layer


116


,




wherein the fluoropolymer inner layer


116


is formed by either extruding a fluoropolymer material along a portion or length of the electrical conductor


112


, or wrapping a fluoropolymer film, in an overlapping fashion, along the length of the conductor


112


,




(2) a polyimide film middle layer


117


, wherein the polyimide middle layer


117


is formed by wrapping an optionally coated polyimide film, in an overlapping fashion, along a portion or length of the inner layer


116


; and




(3) an extruded, crosslinked fluoropolymer outer layer


118


.




Fluoropolymers which may advantageously be utilized in the inner layer


116


of the insulated electrical conductor


110


of the present invention include, for example, MFA, PFA, PTFE, ethylene-chlorotrifluoroethylene (ECTFE) copolymers, ethylene-tetrafluoroethylene (ETFE) copolymers, polyvinylidene fluoride (PVDF), tetrafluoroethylene-hexafluoropropylene-vinylidene fluoride (THV), polyvinylfluoride (PVF) resins, and mixtures thereof.




In a preferred embodiment, inner layer


116


is extruded and the fluoropolymer comprises a copolymer or terpolymer of ETFE. In a more preferred embodiment, the polymer is an ETFE terpolymer that has been compounded with a TAIC crosslinking agent. Such polymers are available from DuPont and Daikin, under the product designations TEFZEL HT200 fluoropolymer resin and NEOFLON EP-541 fluoropolymer resin, respectively.




In yet a more preferred embodiment, inner layer


116


is extruded and crosslinked and the extruded fluoropolymer material of inner layer


116


is substantially the same as the material used to prepare outer layer


118


, but contains less crosslinking agent.




In another preferred embodiment, inner layer


116


is wrapped and the fluoropolymer is PTFE tape. In a more preferred embodiment, the PTFE is in the form of a skived tape, with such tapes being available from Goodrich Corporation, Four Coliseum Centre, 2730 West Tyvola Road, Charlotte, N.C. 28217-4578, under the product designation PTFE Skived Tapes.




The fluoropolymer film inner layer


116


may be a heat-sealed or a non-heat-sealed fluoropolymer film inner layer. It is noted that wrapped fluoropolymer tapes or films will fuse or bond to themselves in overlapping regions at temperatures at or above the melting point of the fluoropolymer, thereby obviating the need to employ a heat-sealable adhesive with such films.




The polyimide film of middle layer


117


is preferably applied to inner layer


116


in tape form, by spirally wrapping the tape about inner layer


116


, so as to achieve a degree of overlap ranging from about 10 to about 70%. In one embodiment, the polyimide film of middle layer


117


does not employ a heat-sealable adhesive and is not heat-sealed. In another embodiment, the polyimide film employs a heat-sealable adhesive and is substantially uniformly sealed to itself in over-lapping regions along the length of inner layer


116


. In one such embodiment, inner layer


116


is formed using a fluoropolymer tape and the fluoropolymer tape is heated together with the coated polyimide film, but is not sealed.




Preferred non-heat-sealable polyimide films have a thickness ranging from about 0.01 to about 0.04 mm, and are available from DuPont, under the trade designation KAPTON H and KAPTON E polyimide films. Preferred heat-sealable polyimide films are the same as those noted above for inner layer


16


.




The preferred insulated electrical conductor


110


described above, which employs a non-heat-sealed polyimide film middle layer, demonstrates a degree of flex which is substantially greater than prior art wire constructions. The degree of flex or wire flexibility is measured by: selecting a 0.9 meter section of insulated wire (i.e., an insulated stranded nickel plated copper conductor (20 American Wire Gage (AWG), 19 Strand, nickel plated copper) measuring 0.95 mm in diameter), which is substantially free of kinks and bends; attaching a ring connector to each end of the conductor; attaching a 100 gram weight to each ring connector; carefully suspending the insulated wire on a stationary mandrel having a diameter measuring 0.48 cm; waiting one minute; and measuring the width between parallel insulated wire segments at three different points along the length of the wire. The degree of flex or wire flexibility is an average of the three width measurements.




In a most preferred embodiment, insulated electrical conductor


110


comprises an electrical conductor


112


, which is insulated with a multi-layer insulation system


114


comprising: (1) an extruded, crosslinked ETFE inner layer


116


; (2) a non-heat-sealed polyimide film middle layer


117


; and (3) an extruded, crosslinked ETFE outer layer


118


.




In another most preferred embodiment, insulated electrical conductor


110


comprises an electrical conductor


112


, which is insulated with a multi-layer insulation system


114


comprising: (1) a non-heat-sealed PTFE inner layer


116


; (2) a heat-sealed polyimide film middle layer


117


; and (3) an extruded, crosslinked ETFE outer layer


118


.




It is noted that although the present inventive insulated electrical conductor


10


,


110


has been described hereinabove as an insulated stranded cable, it is not so limited. The insulated conductor


10


,


110


may comprise a single wire covered with the multi-layer insulation system


14


,


114


of the present invention, or may comprise a plurality of bunched, twisted, or bundled wires, with each wire separately covered with the multi-layer insulation system


14


,


114


. The insulated conductor


10


,


110


may also comprise a plurality of single or dual layer insulated wires which are coated with the polyimide or fluoropolymer inner layer


16


,


116


and optionally, with the polyimide film middle layer


117


. In this embodiment, the plurality of single or dual layer insulated wires are covered with a sheath consisting of the crosslinked fluoropolymer outer layer


18


,


118


.




The process for preparing the insulated electrical conductor


10


,


110


of the present invention basically comprises:




(a) forming a polyimide or fluoropolymer inner layer


16


,


116


on an electrical conductor


12


,


112


,




wherein, when the inner layer is a polyimide inner layer, the layer


16


,


116


is formed by wrapping a polyimide film, which has been coated with a sealable component, in an overlapping fashion, along a portion or length of the electrical conductor


12


,


112


, wherein the sealable component comprises a perfluoropolymer, a crosslinked fluoropolymer, or a polyimide adhesive,




wherein, when the inner layer is a fluoropolymer inner layer, the layer


16


,


116


is formed by either: i) extruding a fluoropolymer material along a portion or length of the electrical conductor


12


,


112


, or ii) wrapping a fluoropolymer film, in an overlapping fashion, along a portion or length of the electrical conductor


12


,


112


,




(b) optionally, forming a polyimide middle layer


117


on the polyimide or fluoropolymer inner layer


16


,


116


by wrapping an optionally coated polyimide film, in an overlapping fashion, along a portion or length of the inner layer


16


,


116


,




(c) when the inner layer


16


,


116


is a polyimide inner layer or when a middle layer


117


is formed using a coated polyimide film, heating the polyimide film or films to a temperature ranging from about 240° to about 350° C. to cause overlapping regions of the coated film or films to bond, thereby forming an effective seal against moisture along the length of the conductor


12


,


112


,




(d) forming a fluoropolymer outer layer


18


,


118


on either the inner or middle layer


16


,


116


,


117


by extruding a fluoropolymer material along a portion or length of that layer; and




(e) crosslinking the fluoropolymer outer layer


18


,


118


, wherein, when the inner layer


16


,


116


or the sealable component comprises a perfluoropolymer (e.g., polytetrafluoroethylene, fluorinated ethylene propylene copolymers, perfluoroalkoxy resins), the fluoropolymer outer layer


18


,


118


is crosslinked by exposing it to less than 60 megarads of radiation, with applied voltages ranging from about 50 to about 120 kilo volts,




wherein, when the inner layer


16


,


116


is a fluoropolymer inner layer, the process for preparing an insulated, electrical conductor includes forming a polyimide middle layer


117


on the polyimide or fluoropolymer inner layer


16


,


116


.




Insulated electrical conductors


10


,


110


that do not employ perfluoropolymers are preferably subjected to an irradiation step to effect crosslinking in the fluoropolymer outer layer


18


,


118


. In a more preferred embodiment, the dosage of ionizing radiation (e.g., accelerated electrons or gamma rays) employed in the irradiation step is below 50 megarads (Mrads), more preferably, between 5 and 25 Mrads and, most preferably, between 15 and 25 Mrads, while applied voltages range from about 0.25 to about 3.0 mega volts (MV), and preferably range from about 0.5 to about 1.0 MV. The irradiation step is preferably carried out at ambient temperature.




Insulated electrical conductors


10


,


110


, which employ an inner layer or sealable component comprising a perfluoropolymer are subjected to a so-called “skin irradiation” process to effect crosslinking in the fluoropolymer outer layer


18


,


118


. The subject process employs ionizing radiation in the form of accelerated electrons, and basically comprises using an accelerated voltage such that the maximum attained distance of accelerated charged particles is less than or equal to the thickness of the outer layer


18


,


118


. More specifically, with an applied voltage of 120 KV, most electrons will penetrate outer layer


18


,


118


to a maximum depth of approximately 0.13 mm.




Such a technique or process is briefly described in JP 4-52570 in regard to automotive low voltage wire coated with e.g. a soft vinyl chloride resin. JP 4-52570 is incorporated herein by reference.




In a preferred embodiment, the dosage of ionizing radiation (i.e., accelerated electrons) employed in the irradiation step is below 60 Mrads, more preferably, between 20 and 50 Mrads and, most preferably, between 30 and 40 Mrads, while applied voltages range from about 50 to about 120 kilo volts (KV), and preferably range from about 100 to about 120 KV. The “skin irradiation” technique or process is preferably carried out at ambient temperature.




It is noted that in the “skin irradiation” technique described above, where electrons do not reach the conductor during electron beam irradiation, electrons may accumulate in the insulation thereby increasing the possibility of flooding and/or channeling. As will be readily appreciated by those skilled in the art, electron flooding and channeling may damage the insulation by causing the formation of tiny pin-holes.




The present inventors have discovered that by exposing “skin irradiated” insulated electrical conductor


10


,


110


to elevated temperatures ranging from about 150 to about 220° C., accumulated electrons may be more effectively drained off without damaging the insulation.




The insulated electrical conductor


10


,


110


of the present invention is lightweight, and may be used in environments where temperatures may exceed 230° C. In addition, the inventive conductor


10


,


110


demonstrates mechanical durability and resistance to hydrolysis.




Preferably, insulated conductor


10


,


110


weighs from about 1.9 to about 2.0 kilograms (kg) per 305 meters (m), which serves to satisfy the maximum weight limits set forth in the following Military Specifications—M22759/92-20, M22759/86-20, M22759/32-20, and M22759/34-20.




The 230° C. temperature rating of insulated electrical conductor


10


,


110


was determined in accordance with Military Specification MIL-DTL-22759/87A—Accelerated Aging Test. This test, which requires aging wire samples for 500 hours in an air-circulating oven maintained at a temperature of 290° C., was modified to the extent that the oven temperature was reduced to 260° C.




Mechanical durability is evidenced by the ability of insulated electrical conductor


10


,


110


to pass the following tests: (1) Wire-to-Wire Abrasion Resistance—Boeing Specification Support Standard BSS 7324 entitled “Procedure for Testing Electrical Wire and Cable” dated Dec. 2, 1998 (“Boeing BSS 7324); (2) Dynamic Cut-Through Resistance (at elevated temperatures of up to 260° C.)—ASTM D 3032, Section 22, and Military Specification MIL-DTL-22759/87A; and (3) Sandpaper Abrasion Resistance—Society of Automotive Engineers (SAE) test method J1128 Section 5.10.




The resistance to hydrolysis demonstrated by insulated electrical conductor


10


,


110


was measured in accordance with SAE test method AS4373, Section 4.6.2, Method 602.




In a more preferred embodiment, the multi-layer insulation system and insulated electrical conductor


10


,


100


of the present invention demonstrate other desirable properties including excellent resistance to flame, the ability to be marked using ultraviolet or visible radiation, electrical resistance, humidity resistance, low smoke generation, notch propagation resistance, weathering resistance, wet and dry arc track resistance, and resistance to common solvents and other fluids used in the aircraft industry.




The subject invention will now be described by reference to the following illustrative examples. The examples are not, however, intended to limit the generally broad scope of the present invention.















WORKING EXAMPLES






Components Used











In the Working Examples set forth below, the following components and






materials were used:















CONDUCTOR:




a stranded nickel plated copper conductor (20







American Wire Gage (AWG), 19 Strand, nickel







plated copper) measuring 0.95 mm in diameter.






POLYIMIDE




heat-sealable polyimide film coated or laminated






FILM I:




on both sides with a heat-activated, high







temperature polyimide adhesive, marketed under the







trade designation KAPTON HKJ heat-sealable







polyimide film, by DuPont.






POLYIMIDE




heat-sealable polyimide film coated or laminated on






FILM II:




both sides with a heat-activated, high temperature







polyimide adhesive, marketed under the trade







designation KAPTON EKJ heat-sealable polyimide







film, by DuPont.






POLYIMIDE




heat-sealable polyimide film coated or laminated on






FILM III:




both sides with a heat-activated, medium







temperature polyimide adhesive, marketed under the







trade designation KAPTON ELJ heat-sealable







polyimide film, by DuPont.






POLYIMIDE




heat-sealable polyimide film coated or laminated on






FILM IV:




both sides with a heat-activated perfluoropolymer







adhesive, marketed under the trade designation







KAPTON XP heat-sealable polyimide film, by







DuPont.






POLYIMIDE




heat-sealable polyimide film coated or laminated on






FILM V:




both sides with a heat-activated perfluoropolymer







adhesive, marketed under the trade designation







OASIS TWT561 heat-sealable polyimide film, by







DuPont.






ETFE:




a copolymer comprising 35 to 60 mole % of







ethylene; 60 to 35 mole % of tetrafluoroethylene;







and up to 10 mole % of a fluorinated termonomer,







marketed under the trade designation TEFZEL HT







200 fluoropolymer resin, by DuPont. Melting point







of fluoropolymer resin is approximately 270° C.






ETFE(I):




a copolymer comprising 30 to 50 mole % of







ethylene; 70 to 50 mole % of tetrafluoroethylene;







and up to 10 mole % of a fluorinated termonomer,







marketed under the trade designation TEFZEL







HT 2127 fluoropolymer resin, by DuPont. Melting







point of fluoropolymer resin is approximately







243° C.






PTFE:




a skived polytetrafluoroethylene film, marketed







under the trade designation TEFLON TFE fluoro-







polymer resin, by DuPont.






TAIC:




a triallyl isocyanurate crosslinking agent, marketed







under the designation TAIC triallyl isocyanurate, by







Nippon Kasei Chemical Co., Ltd., Tokyo, Japan.






TiO


2


:




titanium dioxide pigment in powder form (≧96%







in purity), marketed under the trade designation







TIPURE titanium dioxide pigment, by DuPont.














Sample Preparation




EXAMPLES 1A TO 1E




A continuous strip of POLYIMIDE FILM I, measuring 0.64 cm in width and 0.03 mm in thickness, was spiral-wrapped, at a 53% overlap, about a CONDUCTOR. The spiral-wrapped CONDUCTOR was then heated in a continuous process to a temperature in excess of 300° C. for approximately 5 seconds to heat-seal the overlapping portions of the POLYIMIDE FILM I strip, and was then allowed to cool. The thickness of the heat-sealed, spiral-wrapped POLYIMIDE FILM I inner layer was 0.05 mm.




A quantity of ETFE was compounded with 8% by wt. TAIC and 2% by wt. TiO


2


and was then extruded over the POLYIMIDE FILM I inner layer using a single-screw extruder having four heating zones which were set at 200°, 240°, 275°, and 290° C., respectively. The thickness of the extruded ETFE layer was 0.13 mm.




Test samples were then irradiated using electron-beam radiation, with air-cooling. Total beam dosages were 10, 15, 20, or 30 megarads, while applied voltages were either 120 KV, 150 KV, or 0.5 MEV.




The subject wire construction is described in Table 1, hereinbelow.




EXAMPLES 2, 3A TO 3C, 4A AND 4B




Four test samples of the wire construction labeled Example 2, ten test samples of Example 3, and six test samples of Example 4, were prepared substantially in accordance with the method identified above for Example 1, except that test samples for each Example were prepared using a different polyimide film. As above, total beam dosages were 10, 15, 20, or 30 megarads, while applied voltages were either 120 KV, 150 KV, or 0.5 MEV.




The subject wire constructions are more fully described in Table 1, hereinbelow.




EXAMPLE 5




One thousand feet of the wire construction labeled Example 5 were repared substantially in accordance with the method identified above for Examples 1A to 1E, except that total beam dosage was 18 megarads, while applied voltages were 0.5 mega electron volts.




The subject wire construction is more fully described in Table 1, hereinbelow.




EXAMPLES 6 TO 9




A continuous strip of PTFE, measuring 0.63 cm in width and 0.025 mm in thickness, was spiral-wrapped, at either a 54% overlap (Example 6) or a 15% overlap (Examples 7 to 9), about a CONDUCTOR. A continuous strip of either POLYIMIDE FILM III (Examples 6 and 7), measuring 0.63 cm in width and 0.025 mm in thickness or POLYIMIDE FILM II (Examples 8 and 9), measuring 0.63 cm in width and 0.018 mm in thickness, was then spiral-wrapped, at a 54% overlap, about the spiral-wrapped PTFE inner layer. The spiral-wrapped CONDUCTOR was then heated in a continuous process to a temperature in excess of 300° C. for approximately 5 seconds to heat-seal the overlapping portions of the POLYIMIDE FILM layer, and was then allowed to cool. The thickness of the inner and middle layers was 0.076 mm (Examples 6 and 7) and 0.061 mm (Examples 8 and 9).




A quantity of ETFE or ETFE(I) was compounded with 8% by wt. TAIC and 2% by wt. TiO


2


and was then extruded over the POLYIMIDE FILM middle layer using a single-screw extruder having four heating zones which were set at 200°, 240°, 275°, and 290° C., respectively. The thickness of the extruded ETFE or ETFE(I) layers was 0.13 mm (Examples 6 and 7) and 0.14 mm (Examples 8 and 9).




Five hundred feet of each test sample wire construction were then irradiated using electron-beam radiation, with air-cooling. Total beam dosages were 18 megarads for Examples 6 and 7, and 36 megarads for Examples 8 and 9, while applied voltages were 0.5 MEV.




The subject wire constructions are more fully described in Table 1, hereinbelow.




EXAMPLES C-1 AND C-2




Four test samples each of prior art wire constructions C-1 and C-2 were prepared as set forth below.




C-1 was prepared substantially in accordance with the method identified above for Example 1, except that 0.06 mm thick PTFE tape was spiral-wrapped, with a 53% overlap, over a spiral-wrapped POLYIMIDE FILM IV inner layer prior to heat-sealing. The resulting wire construction was then exposed to a temperature in excess of 330° C. to effect heat-sealing in both layers.




C-2 was prepared by compounding ETFE with 1.5% by wt. TAIC, and then by extruding the compounded material over the CONDUCTOR using a single-screw extruder, as described above. A quantity of compounded ETFE material, which had been compounded with 8% by wt. TAIC, was then extruded over the ETFE inner layer, and the resulting wire construction irradiated using electron-beam radiation, with air cooling. Total beam dosage was 30 megarads, with an applied voltage of 0.5 MEV.




The subject prior art wire constructions are more fully described in Table 1, hereinbelow.












TABLE 1











Summary of Examples 1A to 1E, 2, 3A to 3C, 4A, 4B, 5 to 9, C-1 and C-2























1A, 1B, 1C,
















EXAMPLE




1D, 1E




2




3A, 3B, 3C




4A, 4B




5




6




7




8




9




C-1




C-2









Inner Layer




Polyimide




Polyimide




Polyimide




Polyimide




Polyimide




PTFE




PTFE




PTFE




PTFE




Polyimide




ETFE







Film I




Film II




Film IV




Film V




Film I








Film V






Adhesive




PI


1






PI




FP


2






FP




PI
























FP




N/A






Thickness of




0 05




0.08




0 08




0 06




0 05




0 03




0 03




0 03




0 03




0 06




0 09






Inner Layer






(mm)






Middle





























Polyimide




Polyimide




Polyimide




Polyimide
















Layer









Film III




Film III




Film II




Film II






Adhesive





























PI




PI




PI




PI
















Thickness of





























0 05




0 05




0 04




0 04
















Middle






Layer (mm)






Outer Layer




ETFE




ETFE




ETFE




ETFE




ETFE




ETFE




ETFE




ETFE (I)




ETFE




PTFE




ETFE






Thickness of




0.13




0 13




0 13




0 13




0 13




0.13




0 13




0 13




0.13




0 13




0 13






Outer Layer






(mm)






Total




0 20




0.20




0 20




0 20




0 20




0 21




0 20




0 20




0 21




0 20




0 20






Insulation






Thickness






(mm)






Total Weight




6 50




6 69




6 37




6 40




6 50




6 69




6 62




6 46




6 71




6 89




6 60






of Insulated






Wire






(gms/m)













1


PI = polyimide adhesive












2


FP = perfluoropolymer adhesive













The prepared test samples were then subjected to the test procedures identified below. Test procedures, with the exception of ease of peel, are fully described in the following publications: (1) Boeing Specification Support Standard BSS 7324 entitled “Procedure for Testing Electrical Wire and Cable” dated Dec. 2, 1998 (“Boeing BSS 7324”); (2) Military Specification MIL-DTL-22759/87A entitled “Wire, Electrical, Polytetrafluoroethylene/Polyimide Insulated, Normal Weight, Nickel Coated Copper Conductor, 260° C., 600 Volts,” and dated Feb. 23, 1998; (3) Military Specification MIL-STD-2223 entitled “Test Methods for Insulated Electrical Wire,” and dated Aug. 31, 1992; (4) Society of Automotive Engineers (SAE) test method AS4374 entitled “Test Methods for Insulated Electrical Wire,” and dated August, 1994; and (5) SAE test method J1128 entitled “Surface Vehicle Standard, Low Tension Primary Cable,” and dated May, 2000, all of which are incorporated herein by reference.















Test Methods
























Accelerated Aging or




Boeing BSS 7324, paragraph no. 7.1a, pp. 12 to 14, conducted






Shrinkage Resistance (P, F):




at 280° C.






Current Overload




Boeing BSS 7324, paragraph no. 7.16, pp. 48 to 50, conducted






Capacity:




at room temperature.







The insulated wire test samples were evaluated for current







overload capacity by removing 13 mm of insulation from wire







samples measuring 1.5 m in length. The samples were then







suspended horizontally in a test set-up with no visible sag.







Then, 33 amperes (amps) of current was applied to each test







sample for a period of 5 minutes and the samples cooled to







room temperature. Each test sample was visually inspected







during current application and after the samples were returned







to room temperature. The test samples were then subjected to







the dry dielectric test that is described in the Boeing BSS 7324







Specification. The test, which was repeated six times, was







deemed passed if at least five out of the six samples passed the







test.






Cut-Through




MIL-DTL-22759/87






Resistance (lbs):




Boeing BSS 7324, paragraph no. 7.23, p. 58, Dynamic Cut-







Through







The insulated wire samples were tested for cut-through







resistance using the method described below. The cut-through







test measured the resistance of the wire insulation to the







penetration of a cutting surface and simulated the type of







damage that can occur when a wire is forced by mechanical







loading against a sharp edge. The test was performed at room







temperature (23° C.), at 150° C., at 200° C., and at 260° C., to







evaluate the effect of the elevated temperature on insulation







performance. The standard cutting edge used was stainless steel







and had a radius of 0.406 mm.







For each test, a 600 mm (in length) test sample was clamped in







place between a blade and a flat plate within an INSTRON







compression tester, and the ends of the conductor connected to







an 18 VDC electrical circuit. The cutting edge of the blade was







oriented perpendicularly to the axis of the sample. The cutting







edge was then forced through the insulation at a constant rate of







1.27 mm per minute until contact with the conductor occurred.







A detection circuit sensed contact of the cutting edge with the







conductor and recorded the maximum force, encountered during







the test. The test was then repeated four times rotating the







sample between tests to offset the effect of eccentric insulation.







The reported cut-through resistance was the arithmetic mean of







five tests performed on each sample.






Dry Arc Propagation




MIL-STD-2223 Method 3007.






Resistance (P, F, or




Boeing BSS 7324, paragraph no. 7.4, pp. 16 to 30, conducted at






number of wires passed):




room temperature.







The insulated wire samples were tested for dry arc propagation







resistance using the method described below. Each test sample







was cut into 7 pieces, with each piece measuring 35 cm in







length. The insulation from five of the seven pieces was







stripped from the ends of each piece exposing about 5 mm of







conductor and the pieces designated “active wires.” The







insulation from the remaining two wires was left intact and the







pieces designated “passive wires.”







The seven wire pieces were then bundled such that one active







wire was located in the center of the bundle while the







remaining six wire pieces surrounded the central active wire.







The two passive wires were located side-by-side within the







bundle. The seven-wire bundle was laced together at four







locations so as to keep all seven wires tightly held together







throughout the length of the bundle. The distance between the







two central laces was about 2.5 cm, while the distance between







the central two laces and the outer two laces was about 1.25







cm.







The wire bundle was then placed in a jig similar to that shown







in the Boeing BSS 7324 Specification. The two passive wires







were located at the bottom of the jig, while the stripped wires







were individually connected to an electrical circuit. More







specifically, the five active wires were connected to a three







phase 400 Hz power source. Then, a knife blade with a 250 gm







load was placed on top of the wire bundle perpendicular to







each wire and the blade movement initiated. The blade moved







back and forth at a speed of 0.75 cycles/second. When the top







two wires were shorted out, the system was de-energized. Each







wire was exposed to a 1000 volt wet dielectric withstand test to







check whether the remaining insulation could withstand such







voltage. When the insulation withstood 1000 volts, the voltage







was increased to 2500 volts. When the wire withstood 1000







volts, it is considered to have passed the test.







This test was deemed passed if: (1) a minimum of 64 wires







passed the dielectric test; (2) three wires or less failed the







dielectric test in any one bundle; and (3) actual damage to the







wire was not more than 3 inches in any test bundle.






Ease of Peel:




Test samples employing a dual layer insulation system and







measuring 0.9 meter in length were tested for ease of peel by







(1) removing the outer insulation layer, (2) manually seizing a







leading edge of the inner insulation layer (i.e., polyimide tape),







and (3) slowly peeling the tape off of the conductor or wire.







The inner insulation layer was deemed “continuously peelable”







if the entire width of the tape could be continuously peeled







from at least five revolutions of the wire without tearing.






Hydrolysis Resistance (P, F):




MIL-DTL-22759/87A and SAE AS4373, Method 602 Test







(Unconditioned Wire: AS4373, Section 4.6.2.4.2)







Test samples having an insulation thickness of approximately







0.20 mm and measuring approximately 762 mm in length were







separately fixed and wound on an 8 mm mandrel and placed in







salt solution [5% (m/m) of NaCl in water] contained in a 2 liter







beaker. The ends of each wound test sample were positioned







outside or above the salt solution in the beaker. The test







samples were then allowed to age in the salt solution for from







672 to >10,000 hours at 70° C. ± 2° C. Starting at 672 hours, the







test samples were visually inspected and then periodically







subjected to the Withstand Voltage Test as described below.







The Hydrolysis Test was deemed “passed” if the sample, upon







being subjected to the Withstand Voltage Test, did not







demonstrate any electrical breakdown.







Withstand Voltage Test (P, F): For this test, the ends of each







test sample were twisted together to form a loop. The looped







test sample was then immersed in the salt solution contained in







the beaker. The ends of each test sample were located above







the solution. A test voltage of 2.5 kV (rms) was then applied







through an electrode between the conductor and the solution for







five (5) minutes.






Life Cycle (P, F):




MIL-DTL-22759/87A. Five (5) hours at 230 to 290° C. ± 2° C.







Dielectric test, 2.5 kV (rms) for five (5) minutes.







Test samples were tested for life cycle by aging the samples







and then by subjecting the aged samples to the Withstand







Voltage Test noted above. The samples were aged by







separately fixing the samples on a mandrel having a one-half







inch diameter and then placing the mandrel and test samples in







an air circulation oven set at 30° C. above the intended







temperature rating for the product, for a period of 500 hours.






Laser Markability:




Boeing BSS 7324, paragraph no. 7.36, pp. 82 to 83, conducted







at room temperature.







Test conducted by Spectrum Technologies PLC, Western







Avenue, Bridgend CF31 3RT, UK, using a CMS II Contrast







Meter.






Sandpaper Abrasion (mm):




SAE J1128, Section 6.10







Test samples having an insulation thickness of approximately







0.20 mm and measuring 1,000 mm in length were tested for







sandpaper abrasion resistance by removing 25 mm of insulation







from one end of each test sample and by horizontally mounting







each test sample (taut and without stretching) on a continuous







strip of abrasion tape in an apparatus that was built by Glowe-







Smith Industrial, Inc. (G.S.I. Model No. CAT-3) in accordance







with Military Specification MIL-T-5438 and that was capable







of exerting a force on the sample while drawing the abrasion







tape under the sample at a fixed rate. For each test, 150J garnet







sandpaper (with 10 mm conductive strips perpendicular to the







edge of the sandpaper spaced a maximum of every 75 mm) was







drawn under the sample at a rate of 1500 ± 75 mm/min while a







total force of 2.16 ± 0.05 N was exerted on the test sample.







The sandpaper approached and exited each test sample from







below at an angle of 29 ± 2° to the axis of the test sample and







was supported by a rod 6.9 mm in diameter. The length of







sandpaper necessary to expose the core or wire was recorded







and the test sample moved approximately 50 mm and rotated







clockwise 90°. The above-referenced procedure was repeated







for a total of four readings. The mean of the four readings







constituted the sandpaper abrasion resistance for the subject test







sample.







It is noted that since the test samples had very thin insulation,







this test had to be stopped frequently to observe failure points.






Strippability:




ASTM D3032 Section 27.







Boeing BSS 7324, paragraph no. 7.48, pp. 96 to 97, conducted







at room temperature.







Test samples were tested for strippability by carefully removing







70 mm of insulation from test samples measuring 76 mm in







length. The bare conductor portion of the test specimen was







then threaded through a loosely fitted hole of a jig so that the







unstripped insulation stayed at one side of the jig and the







stripped wire at the other. Using an INSTRON Tensile Tester,







the bare conductor was pulled while the jig was fixed in place.







The force required to pull the remaining 6 mm slug of insulation







from the test sample was reported as strip force.







This test was deemed passed if the strip force fell within the







range of from ¼ to 6 pounds (lbs).






Wet Arc Propagation




MIL-STD-2223, Method 3006.






Resistance (P, F, or




Boeing BSS 7324, paragraph no. 7.4.6 & 7, pp. 26 to 29,






number of wires passed):




conducted at room temperature







Test samples were tested for wet arc propagation resistance by







preparing seven test samples measuring 35 cm in length from a







3 m long insulated wire sample. Five of the seven wire







segments were stripped at both ends exposing about 5 mm of







conductor. These stripped wire segments were designated







“active wires.” The remaining two wire segments that were not







stripped were called “passive wires.”







The seven wire pieces were then bundled such that one active







wire was located in the center of the bundle while the







remaining six wire pieces surrounded the central active wire.







The two passive wires were located side-by-side within the







bundle. The seven-wire bundle was laced together at four







locations so as to keep all seven wires tightly held together







throughout the length of the bundle. The distance between the







two central laces was about 2.5 cm, while the distance between







the central two laces and the outer two laces was about 1.25







cm.







Two wires located on top of the seven-wire bundle had slits







measuring 0.5 to 1.0 mm in width that were perpendicular to the







wire axis. The slits were positioned 6 mm apart. The stripped







wires were connected to a three phase power source according







to the scheme set forth in the Boeing BSS 73244 Specification.







The wire bundle was energized and a 5% aqueous salt solution







was dripped onto the wire bundle where the two exposed slits







were located. The rate of application of the salt solution was 8







to 10 drops per minute. This condition was continued for 8







hours unless the bundle failed by tripping a circuit breaker.







After an 8-hour exposure to the dripping salt solution under the







energized condition, the wire bundles were taken out. Each







wire was initially exposed to a 1000 volt wet dielectric







withstand test initially, then 2500 volts. When a wire







withstood a 1000 volt wet dielectric withstand test, it passed







the test.







This test was deemed passed if: (1) a minimum of 64 wires







passed the dielectric test; (2) three wires or less failed the







dielectric test in any one bundle; and (3) actual damage to the







wire was not more than 3 inches in any test bundle.






Wire-to-wire abrasion




Boeing BSS 7324, paragraph no. 7.57, p. 108.






resistance (cycles to failure,




Test samples were tested for wire-to-wire abrasion resistance in






6,150,000 cycles minimum):




accordance with the following method. One wire test sample







measuring approximately 28 cm in length was crossed with







another wire sample measuring approximately 40 cm in length







at the center of the shorter wire as shown in the Boeing BSS







7324 Specification. One end of one wire specimen was fixed







on an upper plate while the other end of the same wire was







fixed on a lower plate. One end of the other wire was fixed on







the lower plate while the other end of the same wire was loaded







with a 1.13 Kg weight. The upper and lower plates were 45 mm







apart.







The lower plate moved back and forth with a 6.35 mm double







amplitude at 10 cycles per second. The fixed member of the







wire was connected to a power source so that the cycle counter







stopped when the two wire specimens made an electrical







contact by wearing out the insulation layer. If the cycle count at







the stopping point was greater than 6,150,000, the result was







considered passing.














WORKING EXAMPLE 1A




In this example, the prepared wire constructions or test samples were tested for shrinkage resistance, mechanical durability, hydrolysis resistance, and wet arc track resistance, while confirming the temperature rating of 230° C. The results are set forth in Table 2, hereinbelow.












TABLE 2











Summary of Example 1A



















TOTAL




ELECTRON







WET ARC




WIRE-TO-WIRE







BEAM




BEAM




LIFE




ACCELERATED




HYDROLYSIS




PROPAGATION




ABRASION







DOSAGE




VOLTAGE




CYCLE




AGING




RESISTANCE


1






RESISTANCE




(6,150,000 cycles






EXAMPLE




(Mrad)




(MV)




(P, F)




(P, F)




(P, F)




(P, F)




minimum)









1A




30




0.5




P




P




P




P




42,885,600













1


2000 hour requirement met, test continuing.













As shown in Table 2, the insulated conductor of the present invention may be used at temperatures of up to 230° C., and demonstrates a balance of properties including shrinkage resistance, mechanical durability, hydrolysis resistance, and wet arc propagation resistance.




WORKING EXAMPLES 1B, 2, 3A, C-1 AND C-2




In these examples, the prepared wire constructions or test samples were tested for sandpaper abrasion resistance. The results are reported in Table 3, hereinbelow.












TABLE 3











Summary of Examples 1B, 2, 3A, C-1 and C-2















TOTAL









BEAM




ELECTRON







DOSAGE




BEAM




SANDPAPER ABRASION (mm)

















EXAMPLE




(Mrad)




VOLTAGE (MV)




OUTER LAYER




AVG




BOTH LAYERS




AVG









1B




30




0.5




40




42




117




124









14





153









41





151









46





  75






2 




30




0.5




38




43




229




172









41





158









43





153









48





146






3A




30




0.5




37




41




114




142









40





148









41





153









46





151






C-1




N/A




N/A




 9




12




117




109









11





153









13





 79









16





 85






C-2




30




0.5




40




53




164




157









53





151









56





153









62





158














As shown by Examples 1B, 2, and 3A in Table 3, the insulated conductor of the present invention demonstrated a resistance to sandpaper abrasion which was greatly improved over that demonstrated by the prior art wire construction Example C-1, which employed a PTFE outer layer.




WORKING EXAMPLES 1C, 1D, 1E, 3B, 3C, 4A AND 4B




In these examples, the prepared wire constructions or test samples were tested for ease of peel. The results are shown in Table 4, hereinbelow.












TABLE 4











Summary of Examples 1C, 1D, 1E, 3B, 3C, 4A and 4B
















BEAM








TOTAL BEAM




VOLTAGE






EXAMPLE




DOSAGE (Mrad)




(KV)




EASE OF PEEL









1C




10




120




not continuously peelable







15





not continuously peelable







20





not continuously peelable






1D




10




150




not continuously peelable







15





not continuously peelable







20





not continuously peelable






1E




30




500




not continuously peelable






3B




10




120




not continuously peelable







15





not continuously peelable







20





not continuously peelable






3C




10




150




continuously peelable







15





continuously peelable







20





continuously peelable






4A




10




120




not continuously peelable







15





not continuously peelable







20





not continuously peelable






4B




10




150




continuously peelable







15





continuously peelable







20





continuously peelable














Examples 3B and 4A demonstrate that insulated conductors employing irradiation degradable perfluoropolymer adhesives may be successfully prepared using a “skin irradiation” technique which effects crosslinking of the outer layer using low electron beam voltages of less than or equal to 120 KV. As shown in Examples 3C and 4B, exposing these samples to electron voltages of 150 KV appears to degrade the adhesive resulting in a sample where the outer layer is continuously peelable along the length of the test sample.




Examples 1C, 1D and 1E, which employed a polyimide adhesive, were not easily peelable regardless of whether the sample was irradiated at 120, 150 or 500 KV, which indicated that higher electron beam voltages do not serve to degrade the polyimide adhesive.




WORKING EXAMPLES 5 TO 9, C-1 AND C-2




In these examples, the prepared wire constructions or test samples were tested for hydrolysis, sandpaper abrasion, cut-through, wet and dry arc propagation and wire-to-wire abrasion resistance, laser markability, strippability, life cycle and current overload capability. The results are set forth in Table 5, hereinbelow.












TABLE 5











Summary of Examples 5 to 9, C-1 and C-2


















Sandpaper Abrasion








Total





Resistance (mm)

















Insulation




Hydrolysis




Outer









Thickness




Resistance




Layer




Whole




Cut-Through Resistance (lbs)



















Example




(mm)




(P, F)




Only




Insulation




23° C.




150° C.




200° C.




260° C.









5




0 200




P




40




172




89.0




73 9




53 9




66 2






6




0 210




P




45




182




95 7




64 0




54.0




51 3






7




0 198




P




41




192




89 6




52.7




50 2




46 7






8




0 198




 P


1






28




 77




80 0




75 0




64 0




54 0






9




0 210




 P


1






22




 74




79 0




67 0




60 0




52 0






C-1




0 203




P




 5




116




45  




54  




42  




30  






C-2




0 203




P




55




156




35  




 5 5





























Wet Arc Propagation Resistance




Dry Arc Propagation Resistance







Total




(# of bundles, # of wires passed)




(# of bundles, # of wires passed)





















Insulation




# of




# of




# of




# of




# of




# of




# of




# of







Thickness




bundles




bundles




wires




wires




bundles




bundles




wires




wires






Example




(mm)




tested




passed




tested




passed




tested




passed




tested




passed









5




0 200




15




12




75




60














25




21






6




0 210




15




15




75




75




15




15




75




71






7




0 198




15




15




75




75




15




15




75




69






8




0 198
























15




15




75




68






9




0 210




15




15




75




75


























C-1




0 203




15




15




75




73




15




15




75




74






C-2




0 203




15




15




75




74




15




15




71




71




















Laser











Mark-







ability





Wire-To-







or




Strip-




Wire




Life Cycle (# of wires passed)




















Total




Mark-




pability




Abrasion




Aging






Current






Ex-




Insulation




ing




(lbs. of




Resistance




Temper-




# of




# of




Overload






am-




Thickness




Contrast




strip




(6,150,000




ature




Wires




Wires




Capacity






ple




(mm)




(%)




force)




minimum)




° C.




Tested




Passed




(P, F)









5




0.200









3.76




42,885,600




230




3




3




P











260




3




3






6




0.210









0.63









230




3




3




P











260




3




0






7




0.198









1.15




23,600,000




230




3




3




P











260




3




0






8




0.198




74




0.38




22,775,000




230




3




3




P











260




3




2






9




0.210




74




0.39









230




3




3




P











260




3




0






C-1




0.203




63









>6,150,000




230




3




3




P






C-2




0.203














>6,150,000




290




3




3




P













1


test continuing, expect to pass













As shown in Table 5, the insulated conductors of the present invention demonstrate a balance of properties including mechanical durability and hydrolysis resistance. More specifically, Examples 5 to 7 demonstrated good hydrolysis resistance, with Examples 8 and 9 noted as currently being tested but expected to demonstrate the same level of resistance. With regard to sandpaper abrasion resistance, Examples 5 to 7 performed similar to Comparative Example C-2. Examples 8 to 9 showed a slight drop-off in this property, while Comparative Example C-1 performed poorly presumably due to the nature of the PTFE outer layer. In terms of cut-through and wire-to-wire abrasion resistance properties, the insulated conductors of the present invention demonstrated greatly improved cut-through resistance over Comparative Examples C-1 and C-2, at all of the temperatures tested, while Examples 5, 7 and 8 demonstrated remarkable levels of wire-to-wire abrasion resistance. With regard to wet arc propagation resistance, Examples 6, 7 and 9 passed each test, while Example 5 passed a majority of the tests. Similar results were obtained for dry arc propagation resistance, with each Example passing all, or a majority of, the tests. In addition, Examples 8 and 9 both demonstrated improved laser markability over Comparative Example C-1, while all of the inventive insulated conductors successfully passed the industry standard for strippability, namely—a strip force of from ¼ to 6 lbs. With regard to life cycle and temperature ratings, Example 8 qualified for a temperature rating of 230° C. Finally, all of the test samples satisfied the requirements for threshold current overload capacity.




Although the present invention has been shown and described with respect to detailed embodiments thereof, it will be understood by those skilled in the art that various changes in form and detail thereof may be made without departing from the spirit and scope of the claimed invention.



Claims
  • 1. A multi-layer insulation system for electrical conductors, which comprises:(a) a polyimide inner layer, wherein, the polyimide inner layer is formed by wrapping a polyimide film, which has been coated with a sealable component, in an overlapping fashion, along a portion or length of an electrical conductor, wherein, the polyimide film is substantially uniformly sealed to itself in overlapping regions along the length of the conductor, thereby forming an effective seal against moisture, wherein, the sealable component is selected from the group of perfluoropolymer, crosslinked fluoropolymer and polyimide adhesives, (b) a polyimide middle layer, wherein the polyimide middle layer is formed by wrapping an optionally coated polyimide film, in an overlapping fashion, along a portion or length of the inner layer formed on the electrical conductor, and (c) an extruded, crosslinked fluoropolymer outer layer, wherein the fluoropolymer is selected from the group of copolymers and terpolymers of ethylene-tetrafluoroethylene, and mixtures thereof.
  • 2. The multi-layer insulation system of claim 1 wherein the sealable component coated onto the polyimide film is a polyimide sealable component selected from the group of thermoplastic polyimides which soften and become fluid at greater than or equal to 200° C.
  • 3. The multi-layer insulation system of claim 2, wherein the polyimide inner layer demonstrates a high temperature (greater than or eaual to 150° C.) adhesive bond strength (ASTM# 1876-00) of greater than 1000 grams per inch-width.
  • 4. The multi-layer insulation system of claim 1 wherein the sealable component coated onto the polyimide film is a perfluoropolymer sealable component selected from the group of polytetrafluoroethylene, fluorinated ethylene-propylene, perfluoroalkoxy, copolymers of tetrafluoroethylene and perfluoromethylvinylether, and mixtures thereof.
  • 5. The multi-layer insulation system of claim 1 wherein the sealable component coated onto the polyimide film is a crosslinked fluoropolymer sealable component selected from the group of ethylene-tetrafluoroethylene copolymers, chlorotrifluoroethylene copolymers and terpolymers containing minor amounts of one or more fluorinated comonomers, and mixtures thereof.
  • 6. The multi-layer insulation system of claim 1 wherein the polyimide inner layer demonstrates a high temperature (greater than or equal to 150° C.) adhesive bond strength (ASTM# 1876-00) ranging from about 100 to about 250 grams per inch-width.
  • 7. A multi-layer insulation system for electrical conductors, which comprises:(a) a fluoropolymer inner layer, wherein, the inner layer is formed by wrapping a fluoropolymer film, in an overlapping fashion, along a portion or length of an electrical conductor, (b) a polyimide middle layer, wherein the polyimide middle layer has a polyimide film, which has been coated with a sealable component and which is formed by wrapping the coated polyimide film, in an overlapping fashion, along a portion or length of the inner layer formed on the electrical conductor, and (c) an extruded, crosslinked fluoropolymer outer layer, wherein the fluoropolymer is selected from the group of copolymers and terpolymers of ethylene-tetrafluoroethylene, and mixtures thereof.
  • 8. The multi-layer insulation system of claim 7, wherein the polyimide film of the polyimide film middle layer is coated with a sealable component and is substantially uniformly sealed to itself in overlapping regions along the length of the inner layer, thereby forming an effective seal against moisture and wherein the sealable component is selected from the group of perfluoropolymer, crosslinked fluoropolymer and polyimide adhesives.
  • 9. The multi-layer insulation system of claim 7, wherein the fluoropolymer inner layer is a non-heat-sealed fluoropolymer film inner layer.
  • 10. The multi-layer insulation system of claim 9, wherein the fluoropolymer film is a polytetrafluoroethylene film.
  • 11. The multi-layer insulation system of claim 10, wherein the polytetrafluoroethylene film is in the form of a skived tape.
  • 12. The multi-layer insulation system of claim 7, wherein the fluoropolymer inner layer is a heat-sealed fluoropolymer film inner layer, wherein the fluoropolymer film is substantially uniformly sealed to itself in overlapping regions along the length of the conductor, thereby forming an effective seal against moisture.
  • 13. A multi-layer insulation system for electrical conductors, which comprises:(a) a fluoropolymer inner layer, wherein, the inner layer is formed by extruding a fluoropolymer material along a portion or length of an electrical conductor, (b) a polyimide middle layer, wherein the polyimide middle layer has polyimide film, which has been coated with a sealable component and which is formed by wrapping the coated polyimide film, in an overlapping fashion, along a portion or length of the inner layer formed on the electrical conductor, and (c) an extruded, crosslinked fluoropolymer outer layer, wherein the fluoropolymer is selected from the group of copolymers and terpolymers of ethylene-tetrafluoroethylene, and mixtures thereof.
  • 14. The multi-layer insulation system of claims 7 or 13, wherein the fluoropolymer of the fluoropolymer outer layer contains a photosensitive substance rendering the outer layer receptive to laser marking.
  • 15. The multi-layer insulation system of claims 7 or 13, wherein the fluoropolymer of the fluoropolymer inner layer is selected from the group of copolymers of tetrafluoroethylene and perfluoromethylvinylether, perfluoroalkoxy, polytetrafluoroethylene, ethylene-chlorotnfluoroethylene copolymers, ethylene tetrafluoroethylene copolymers, polyvinylidene fluoride, tetrafluoroethylene-hexafluoropropylene-vinylidene fluoride, polyvinyifluoride resins, and mixtures thereof.
  • 16. The multi-layer insulation system of claims 7 or 13, wherein the polyimide middle layer is a non-heat-sealed polyimide middle layer.
  • 17. The multi-layer insulation system of claim 13, wherein the fluoropolymer inner layer is a non-heat-sealed fluoropolymer film inner layer.
  • 18. The multi-layer insulation system of claim 13, wherein the fluoropolymer inner layer is a heat-sealed fluoropolymer film inner layer, wherein the fluoropolymer film is substantially uniformly sealed to itself in overlapping regions along the length of the conductor, thereby forming an effective seal against moisture.
  • 19. The multi-layer insulation system of claim 13, wherein the polyimide middle layer is formed by a polyimide film coated with a sealable component, wherein the polyimide film is substantially uniformly sealed to itself in overlapping regions along the length of the inner layer, thereby forming an effective seal against moisture and wherein the sealable component is selected from the group of perfluoropolymer, crosslinked fluoropolymer and polyimide adhesives.
  • 20. The multi-layer insulation system of claim 1, wherein the extruded fluoropolymer inner layer is a crosslinked extruded fluoropolymer inner layer.
  • 21. The multi-layer insulation system of claims 7 or 13, wherein the fluoropolymer of the fluoropolymer outer layer is an ethylene-tetrafluoroethylene copolymer which comprises 35 to 60% by weight of units derived from ethylene, 35 to 60% by weight of units derived from tetrafluoroethylene and up to 10% by weight of units derived from one or more fluorinated comonomers.
  • 22. A multi-layer insulation system for electrical conductors, which comprises:(a) a polyimide inner layer, wherein the polyimide inner layer is formed by wrapping a polyimide film, which has been coated with a heat-sealable polyimide adhesive, in an overlapping fashion, along a portion or length of an electrical conductor, wherein, the polyimide film is substantially uniformly sealed to itself in overlapping regions along the length of the conductor, thereby forming an effective seal against moisture, and wherein, the polyimide inner layer demonstrates a high temperature (greater than or equal to 150° C.) adhesive bond strength (ASTM# 1876-00) of greater than 1000 grams per inch-width; and (b) an extruded, crosslinked fluoropolymer outer layer, wherein the fluoropolymer is selected from the group of copolymers and terpolymers of ethylene-tetrafluoroethylene, and mixtures thereof.
  • 23. The multi-layer insulation system of claim 22, wherein the heat-sealable polyimide adhesive is a thermoplastic polyimide that softens and becomes fluid at greater than or equal to 200° C.
  • 24. The multi-layer insulation system of claim 22, wherein the polyimide inner layer demonstrates a high temperature adhesive bond strength of greater than 1500 grams per inch-width.
  • 25. An insulated electrical conductor that comprises an electrical conductor and a multi-layer insulation system, wherein the multi-layer insulation system comprises:(a) a fluoropolymer inner layer, wherein, the inner layer is formed by wrapping a fluoropolymer film, in an overlapping fashion, along a portion or length of the conductor, (b) a polyimide middle layer, wherein the polyimide middle layer has a polyimide film, which has been coated with a sealable component and which is formed by wrapping the coated polyimide film, in an overlapping fashion, along a portion or length of the inner layer formed on the electrical conductor, and (c) an extruded, crosslinked fluoropolymer outer layer, wherein the fluoropolymer is selected from the group of copolymers and terpolymers of ethylene-tetrafluoroethylene, and mixtures thereof.
  • 26. A process for preparing an insulated electrical conductor, which comprises:(a) forming a polvimide inner layer on an electrical conductor, wherein, the polyimide inner layer is formed by wrapping a polyimide film, which has been coated with a sealable component, in an overlapping fashion, along a portion or length of the electrical conductor, wherein the sealable component is selected from the group of perfluoropolymer, crosslinkable fluoropolymer and polyimide adhesives, (b) heating the polyimide film to a temperature ranging from about 240° to about 350° C. to cause overlapping regions of the coated film to bond, thereby forming an effective seal against moisture along the length of the conductor, wherein, the polyimide inner layer demonstrates a hiah temperature (greater than or equal to 150° C.) adhesive bond strength (ASTM# 1876-00) ranging from about 100 to about 250 grams per inch-width: and (c) forming a fluoropolyrner outer layer on the inner layer by extruding a fluoropolymer material along a portion or length of that layer; and (d) crosslinking the fluoropolymer outer layer, wherein, if the sealable component comprises a perfiuoropolymer, the fluoropolymer outer layer is crosslinked by exposing it to less than 60 megarads of radiation, with applied voltages ranging from about 50 to about 120 kilo volts.
  • 27. A process for preparing an insulated electrical conductor, which comprises:(a) forming a fluoropolymer inner layer on an electrical conductor by wrapping a fluoropolymer film, in an overlapping fashion, along a portion or length of the electrical conductor, (b) forming a polyimide middle layer on the fluoropolymer inner layer by wrapping a polyimide film, which has been coated with a sealable component, in an overlapping fashion, along a portion or length of the fluoropolymer inner layer, wherein the sealable component is selected from the group of perfluoropolymer, crosslinked fluoropolymer and polyimide adhesives, (c) heating the polyimide film to a temperature ranging from about 240° to about 350° C. to cause overlapping regions of the film to bond, thereby forming an effective seal against moisture along the length of the conductor, (d) forming a fluoropolymer outer layer on the polyimide middle layer by extruding a fluoropolymer material along a portion or length of that layer, and (e) crosslinking the fluoropolymer outer layer, wherein, when the inner layer or the sealable component comprises a perfluoropolymer, the fluoropolymer outer layer is crosslinked by exposing it to less than 60 megarads of radiation, with applied voltages ranging from about 50 to about 120 kilo volts.
  • 28. An insulated electrical conductor that comprises an electrical conductor and a multi-layer insulation system, wherein the multi-layer insulation system comprises:(a) a fluoropolymer inner layer, (b) a polyimide middle layer, and (c) an extruded, crosslinked fluoropolymer outer layer, wherein the fluoropolymer is selected from the group of copolymers and terpolymers of ethylene-tetrafluoroethylene, and mixtures thereof, wherein, the insulated electrical conductor is prepared by a process that comprises: (i) forming a fluoropolymer inner layer on an electrical conductor by wrapping a fluoropolymer film, in an overlapping fashion, along a portion or length of the conductor, (ii) forming a polyimide middle layer on the fluoropolymer inner layer by wrapping a polyimide film, which has been coated with a sealable component, in an overlapping fashion, along a portion or length of the fluoropolymer inner layer, wherein the sealable component is selected from the group of perfluoropolymer, crosslinked fluoropolymer and polyimide adhesives, (iii) heating the polyimide film to a temperature ranging from about 240° to about 350° C. to cause overlapping regions of the coated film to bond, thereby forming an effective seal against moisture along the length of the conductor, (iv) forming a fluoropolymer outer layer on the polyimide middle layer by extruding a fluoropolymer material along a portion or length of the middle layer, and (v) crosslinking the fluoropolymer outer layer, wherein, when the inner layer or the sealable component comprises a perfluoropolymer, the fluoropolymer outer layer is crosslinked by exposing it to less than 60 megarads of radiation, with applied voltages ranging from about 50 to about 120 kilo volts.
  • 29. A multi-layer insulation system for electrical conductors, which comprises:(a) a polyimide inner layer, wherein the polyimide inner layer is formed by wrapping a polyimide film, which has been coated with a sealable component, in an overlapping fashion, along a portion or length of an electrical conductor, wherein, the polyimide film is substantially uniformly sealed to itself in overlapping regions along the length of the conductor, thereby forming an effective seal against moisture, wherein, the sealable component is selected from the group of perfluoropolymer, crosslinked fluoropolymer and polyimide adhesives, and wherein, the polyimide inner layer demonstrates a high temperature (greater than or egual to 150° C.) adhesive bond strength (ASTM# 1876-00) ranging from about 100 to about 250 grams per inch-width: and (b) an extruded, crosslinked fluoropolymer outer layer, wherein the fluoropolymer is selected from the group of copolymers and terpolymers of ethylene-tetrafluoroethylene, and mixtures thereof.
  • 30. A process for preparing an insulated electrical conductor, which comprises:(a) forming a fluoropolymer inner layer on an electrical conductor by extruding a fluoropolymer material along a portion or length of the conductor, (b) forming a polyimide middle layer on the fluoropolymer inner layer by wrapping a polyimide film, which has been coated with a sealable component, in an overlapping fashion, along a portion or length of the fluoropolymer inner layer, wherein the sealable component is selected from the group, of perfluoropolymer, crosslinked fluoropolymer and polyimide adhesives, (c) heating the polyimide film to a temperature ranging from about 240° to about 350° C. to cause overlapping regions of the coated film to bond, thereby forming an effective seal against moisture along the length of the conductor, (d) forming a fluoropolymer outer layer on the polyimide middle layer by extruding a fluoropolymer material along a portion or length of that layer; and (e) crosslinking the fluoropolymer outer layer, wherein, if the inner layer or the sealable component comprises a perfluoropolymer, the fluoropolymer outer layer is crosslinked by exposing it to less than 60 megarads of radiation, with applied voltages ranging from about 50 to about 120 kilo volts.
  • 31. A process for preparing an insulated electrical conductor, which comprises:(a) forming a polyirnide inner layer on an electrical conductor, wherein, the polyimide inner layer is formed by wrapping a polyimide film, which has been coated with a sealable component, in an overlapping fashion, along a portion or length of the electrical conductor, wherein the sealable component is selected from the group of perfluoropolymer, crosslinkable fluoropolymer and polyimide adhesives, (b) forming a polyimide middle layer on the inner layer by wrapping a coated polyimide film, in an overlapping fashion, along a portion or length of the inner layer, (c) heating the polyimide film or films to a temperature ranging from about 240° to about 350° C. to cause overlapping regions of the coated film or films to bond, thereby forming an effective seal against moisture along the length of the conductor, (d) forming a fluoropolymer outer layer on the middle layer by extruding a fluoropolymer material along a portion or length of that layer; and (e) crosslinking the fluoropolymer outer layer, wherein, if the sealable component comprises a perfluoropolymer, the fluoropolymer outer layer is crosslinked by exposing it to less than 60 megarads of radiation, with applied voltages ranging from about 50 to about 120 kilo volts.
  • 32. An insulated electrical conductor that comprises an electrical conductor and a multi-layer insulation system, wherein the multi-layer insulation system comprises:(a) a polyimide inner layer, wherein, the polyimide inner layer is formed by wrapping a polyimide film, which has been coated with a sealable component, in an overlapping fashion, along a portion or length of an electrical conductor, wherein, the polyimide film is substantially uniformly sealed to itself in overlapping regions along the length of the conductor, thereby forming an effective seal against moisture, wherein, the sealable component is selected from the group of perfluoropolymer, crosslinked fluoropolymer and polyimide adhesives, (b) a polyimide middle layer, wherein the polyimide middle layer is formed by wrapping an optionally coated polyimide film, in an overlapping fashion, along a portion or length of the inner layer formed on the electrical conductor, and (c) an extruded, crosslinked fluoropolymer outer layer, wherein the fluoropolymer is selected from the group of copolymers and terpolymers of ethylene-tetrafluoroethylene, and mixtures thereof.
  • 33. An insulated electrical conductor that comprises an electrical conductor and a multi-layer insulation system, wherein the multi-layer insulation system comprises:(a) a fluoropolymer inner layer, wherein, the inner layer is formed by extruding a fluoropolymer material along a portion or length of an electrical conductor, (b) a polyimide middle layer, wherein the polyimide middle layer has apolyimide film, which has been coated with a sealable component and which is formed by wrapping the coated polyimide film, in an overlapping fashion, along a portion or length of the inner layer formed on the electrical conductor, and (c) an extruded, crosslinked fluoropolymer outer layer, wherein the fluoropolymer is selected from the group of copolymers and terpolymers of ethylene-tetrafluoroethylene, and mixtures thereof.
  • 34. An insulated electrical conductor that comprises an electrical conductor and a multi-layer insulation system, wherein the multi-layer insulation system comprises:(a) a polyimide inner layer, wherein, the polyimide inner layer is formed by wrapping a polyimide film, which has been coated with a sealable component, in an overlapping fashion, along a portion or length of the electrical conductor, wherein, the polyimide film is substantially uniformly sealed to itself in overlapping regions along the length of the conductor, thereby forming an effective seal against moisture, wherein, the sealable component is selected from the group of perfluoropolymer, crosslinked fluoropolymer and polyimide adhesives, and wherein, the polyimide inner layer demonstrates a high temperature (greater than or equal to 150° C.) adhesive bond strength (ASTM # 1876-00) ranging from about 100 to about 250 grams per inch-width , and (b) an extruded, crosslinked fluoropolymer outer layer, wherein the fluoropolymer is selected from the group of copolymers and terpolymers of ethylene-tetrafluoroethylene, and mixtures thereof.
RELATED APPLICATION

This application claims the benefit of U.S. Provisional Patent Application Serial No. 60/284,302, filed Apr. 17, 2001.

US Referenced Citations (25)
Number Name Date Kind
3269862 Lanza et al. Aug 1966 A
3408453 Shelton, Jr. Oct 1968 A
3422215 Humes Jan 1969 A
3488537 Beddows Jan 1970 A
3763222 Aronoff et al. Oct 1973 A
3852518 Wargotz et al. Dec 1974 A
3894118 Aronoff et al. Jul 1975 A
3911192 Aronoff et al. Oct 1975 A
3970770 Dhami Jul 1976 A
3995091 Dhami Nov 1976 A
4031167 Aronoff et al. Jun 1977 A
4155823 Gotcher et al. May 1979 A
4184001 Hildreth Jan 1980 A
4310597 Checkland et al. Jan 1982 A
4353961 Gotcher et al. Oct 1982 A
4401845 Odhner et al. Aug 1983 A
4430385 Dillow et al. Feb 1984 A
4451306 Verne May 1984 A
4628003 Katz Dec 1986 A
4791966 Eilentropp Dec 1988 A
4801501 Harlow Jan 1989 A
5059483 Lunk et al. Oct 1991 A
5220133 Sutherland et al. Jun 1993 A
5399434 Katz et al. Mar 1995 A
5731088 La Court Mar 1998 A
Foreign Referenced Citations (4)
Number Date Country
1066817 Dec 1992 CN
2053960 May 1972 DE
4052570 Feb 1992 JP
PCTUS9000981 Sep 1990 WO
Non-Patent Literature Citations (2)
Entry
Solomon et al., New Insulation Constructions for Aerospace Wiring Applications, vol. I: Testing and Evaluation, at 1.0 Introduction, 2.0 Description of Test Article, 11.0 Overall Summary, 12.0 Observations, 13.0 Conclusions and Recommendations, McDonnel Douglas Corporation/Wright Laboratory (Jun. 1991).
Solomon et al., New Insulation Constructions for Aerospace Wiring Applications, vol. II: 270 VDC Arc Tracking Testing with Power Controllers at 1.0 Introduction, 5.0 Conclusions, McDonnel Douglas Corporation/Wright Laboratory (Jun. 1991).
Provisional Applications (1)
Number Date Country
60/284302 Apr 2001 US