US20150165670A1 - Method of making structured hybrid adhesive articles - Google Patents

Method of making structured hybrid adhesive articles Download PDF

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Publication number
US20150165670A1
US20150165670A1 US14/408,188 US201314408188A US2015165670A1 US 20150165670 A1 US20150165670 A1 US 20150165670A1 US 201314408188 A US201314408188 A US 201314408188A US 2015165670 A1 US2015165670 A1 US 2015165670A1
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Prior art keywords
epoxy
curative
article
epoxy curative
embossed
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US14/408,188
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English (en)
Inventor
Larry S. Hebert
Dmitriy Salnikov
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3M Innovative Properties Co
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3M Innovative Properties Co
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Priority to US14/408,188 priority Critical patent/US20150165670A1/en
Assigned to 3M INNOVATIVE PROPERTIES COMPANY reassignment 3M INNOVATIVE PROPERTIES COMPANY ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: HEBERT, LARRY S., SALNIKOV, DMITRIY
Publication of US20150165670A1 publication Critical patent/US20150165670A1/en
Abandoned legal-status Critical Current

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    • C—CHEMISTRY; METALLURGY
    • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08G—MACROMOLECULAR COMPOUNDS OBTAINED OTHERWISE THAN BY REACTIONS ONLY INVOLVING UNSATURATED CARBON-TO-CARBON BONDS
    • C08G59/00—Polycondensates containing more than one epoxy group per molecule; Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups
    • C08G59/18—Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups ; e.g. general methods of curing
    • C08G59/40—Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups ; e.g. general methods of curing characterised by the curing agents used
    • C08G59/50—Amines
    • C08G59/56—Amines together with other curing agents
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C59/00—Surface shaping of articles, e.g. embossing; Apparatus therefor
    • B29C59/005—Surface shaping of articles, e.g. embossing; Apparatus therefor characterised by the choice of material
    • C—CHEMISTRY; METALLURGY
    • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08G—MACROMOLECULAR COMPOUNDS OBTAINED OTHERWISE THAN BY REACTIONS ONLY INVOLVING UNSATURATED CARBON-TO-CARBON BONDS
    • C08G59/00—Polycondensates containing more than one epoxy group per molecule; Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups
    • C08G59/18—Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups ; e.g. general methods of curing
    • C08G59/40—Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups ; e.g. general methods of curing characterised by the curing agents used
    • C08G59/66—Mercaptans
    • C—CHEMISTRY; METALLURGY
    • C09—DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
    • C09D—COATING COMPOSITIONS, e.g. PAINTS, VARNISHES OR LACQUERS; FILLING PASTES; CHEMICAL PAINT OR INK REMOVERS; INKS; CORRECTING FLUIDS; WOODSTAINS; PASTES OR SOLIDS FOR COLOURING OR PRINTING; USE OF MATERIALS THEREFOR
    • C09D5/00—Coating compositions, e.g. paints, varnishes or lacquers, characterised by their physical nature or the effects produced; Filling pastes
    • C09D5/24—Electrically-conducting paints
    • C—CHEMISTRY; METALLURGY
    • C09—DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
    • C09J—ADHESIVES; NON-MECHANICAL ASPECTS OF ADHESIVE PROCESSES IN GENERAL; ADHESIVE PROCESSES NOT PROVIDED FOR ELSEWHERE; USE OF MATERIALS AS ADHESIVES
    • C09J163/00—Adhesives based on epoxy resins; Adhesives based on derivatives of epoxy resins
    • C09J7/02—
    • C—CHEMISTRY; METALLURGY
    • C09—DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
    • C09J—ADHESIVES; NON-MECHANICAL ASPECTS OF ADHESIVE PROCESSES IN GENERAL; ADHESIVE PROCESSES NOT PROVIDED FOR ELSEWHERE; USE OF MATERIALS AS ADHESIVES
    • C09J7/00—Adhesives in the form of films or foils
    • C09J7/20—Adhesives in the form of films or foils characterised by their carriers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2063/00—Use of EP, i.e. epoxy resins or derivatives thereof, as moulding material
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/0097—Glues or adhesives, e.g. hot melts or thermofusible adhesives
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2995/00—Properties of moulding materials, reinforcements, fillers, preformed parts or moulds
    • B29K2995/0003—Properties of moulding materials, reinforcements, fillers, preformed parts or moulds having particular electrical or magnetic properties, e.g. piezoelectric
    • B29K2995/0005—Conductive
    • C—CHEMISTRY; METALLURGY
    • C09—DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
    • C09J—ADHESIVES; NON-MECHANICAL ASPECTS OF ADHESIVE PROCESSES IN GENERAL; ADHESIVE PROCESSES NOT PROVIDED FOR ELSEWHERE; USE OF MATERIALS AS ADHESIVES
    • C09J2463/00—Presence of epoxy resin

Definitions

  • This disclosure relates to structured articles comprising adhesives and methods of their manufacture, including in some embodiments structured articles comprising curable epoxy adhesives.
  • the present disclosure provides a method of making structured hybrid adhesive articles comprising the steps of: a) providing an adhesive article comprising: i) a base resin comprising an epoxy resin, ii) a first epoxy curative, and iii) a second epoxy curative, by reacting the base resin with the first epoxy curative such that the first epoxy curative is substantially reacted with epoxy resin in the article and the second epoxy curative is substantially unreacted in the article; b) embossing the adhesive article with a relief pattern; and c) curing the adhesive article such that the second epoxy curative is substantially reacted with epoxy in the article.
  • step a) is carried out prior to step b).
  • step a) is carried out simultaneously with step b).
  • the first and second epoxy curatives may be chosen such that the second epoxy curative may remain substantially unreacted in the composition under conditions of temperature and duration that render the first epoxy curative substantially reacted with epoxy resin in the composition. In some embodiments, the first and second epoxy curatives may be chosen such that the second epoxy curative remains substantially unreacted in the composition after 24 hours at 72° F. and the first epoxy curative becomes substantially reacted with epoxy resin in the composition after 24 hours at 72° F. In some embodiments, the first epoxy curative is a polymercaptan. In some embodiments, the second epoxy curative is a polyamine. In some embodiments, the base resin includes no acrylic resin.
  • the method additionally comprises the step of d) embedding a scrim in the adhesive layer prior to step b).
  • the method additionally comprises the step of e) depositing an electrically conductive layer such as a layer of metal onto the surface of the adhesive article embossed with a relief pattern prior to step c).
  • FIG. 1 is a photomicrograph of a cross section of a cured composite panel prepared from a curable embossed film as described below for Example 9.
  • the present disclosure provides structured articles comprising a high strength structural hybrid adhesive material.
  • two polymer networks are formed sequentially.
  • the first network provides structural integrity to the curable structural adhesive article.
  • the second network typically a thermosetting resin, can be cured after the adhesive article is formed into a structured article by embossing or any other type of patterning.
  • the resulting cured material can be an interpenetrating polymeric network or a single-phase polymeric network.
  • the present disclosure utilizes a high strength structural hybrid adhesive material and methods such as disclosed in PCT Patent App. US2011/067513 filed Dec. 28, 2011, claiming priority to U.S. Provisional Pat. App. 61/428,037, filed Dec. 29, 2010, the contents of which are incorporated herein by reference.
  • the adhesive used herein includes is a two step reactive system that includes a base resin component that reacts rapidly with a sufficient amount of a first component to provide an adhesive article which will retain an embossed relief pattern.
  • the invention includes a latent catalyst or curative for the remaining base resin that can be activated to provide a structural adhesive.
  • the first component reaction and chemistry are chosen to maintain the latency of the uncured resulting article.
  • the forming step can occur either on a web or on the substrate to be bonded.
  • the structural hybrid adhesive contains only one type of base resin, e.g., an epoxy resin.
  • the structural hybrid adhesive contains only epoxy resin as a base resin.
  • the structural hybrid adhesive contains only one resin as a base resin.
  • the structural hybrid adhesive contains only one epoxy resin as a base resin.
  • the base resin includes no acrylic resin.
  • This method allows for the use of the epoxy resin in the forming and embossing steps as well as in thermosetting steps so strength is not compromised. Because of the low temperature processing, a variety of latent curative or catalysts become available for the second thermosetting step. Furthermore, thick, opaque and pigmented articles are possible to process.
  • the present disclosure makes use of a mixed curative that includes at least one rapid-reacting curative and at least one latent curative.
  • Any suitable epoxy resin may be used in the practice of the present disclosure.
  • any suitable rapid-reacting curative may be used in the practice of the present disclosure.
  • Any suitable latent curative may be used in the practice of the present disclosure.
  • the latent curative remains substantially unreacted with an epoxy resin under conditions of time and temperature sufficient to substantially react the rapid-reacting curative with the epoxy resin, and the latent curative will substantially react with the epoxy resin under more extensive conditions of time and temperature.
  • the present disclosure provides a method of blending an uncured epoxy resin with the mixed curative according to the present disclosure and substantially reacting (curing) the epoxy resin with the rapid-reacting curative while leaving the latent curative substantially unreacted (uncured) to form a structural hybrid adhesive material to form an article, which is thereafter embossed with a relief pattern to create an embossed adhesive article.
  • the present disclosure provides a method of blending an uncured epoxy resin with the mixed curative according to the present disclosure and substantially reacting (curing) the epoxy resin with the rapid-reacting curative while leaving the latent curative substantially unreacted (uncured) to form a structural hybrid adhesive material, while simultaneously embossing said material with a relief pattern to create an embossed adhesive article.
  • additional layers may be added to the embossed surface of the adhesive article.
  • an electrically conductive layer such as a metal layer may be applied to the embossed surface of the article.
  • the conductive layer may be added by any suitable method, including deposition methods such as chemical deposition, electrodeposition or vapor deposition.
  • the resulting article includes a patterned conductive layer. This method may be used to create articles described in PCT Patent App. US2010/031263, published Oct. 21, 2010, or PCT Patent App. US2010/031280, published Oct. 21, 2010, the disclosures of which are incorporated herein by reference.
  • the base resin is reacted with the first epoxy curative while in contact with an electrically conductive layer such as a metal layer, to form an article with attached conductive layer.
  • the article with attached conductive layer may be thereafter embossed to create an article which includes a patterned conductive layer.
  • the embossed surfaces of two layers of the embossed curable article may be brought together to create a bilayer with interstitial gaps.
  • the patterns of the embossed surfaces are brought together in registration, with gaps in one surface meeting gaps in the opposing surface.
  • the patterns of the embossed surfaces are brought together out of registration.
  • the pattern of an embossed surfaces is brought together with an unpatterned surface to create a bilayer with interstitial gaps.
  • the embossed adhesive article of the present disclosure is supplied on a liner. In some embodiments, the embossed adhesive article is supplied as a free-standing film without a liner. In some embodiments, the embossed adhesive article includes a barrier layer, such as a layer of fluoropolymer. In some embodiments, the embossed adhesive article includes a scrim. In some embodiments, the embossed adhesive article includes a non-woven scrim. In some embodiments, the embossed adhesive article includes a woven scrim.
  • the terms “substantially unreacted” or “substantially uncured” typically means at least 70% unreacted or uncured, but more typically means at least 80% unreacted or uncured and more typically means at least 90% unreacted or uncured.
  • the terms “substantially reacted” or “substantially cured” typically means at least 70% reacted or cured, but more typically means at least 80% reacted or cured and more typically means at least 90% reacted or cured.
  • to emboss As used herein, the terms “to emboss,” “embossing” or “embossed” refer to a process of producing a relief pattern on the surface of a material; typically accomplished by applying a tool or mold to the material with sufficient pressure to leave a durable impression after removal of the tool or mold.
  • CC3-800 A mercaptan-terminated liquid epoxy curing agent, available under the trade designation “CAPCURE 3-800” from BASF Corporation, Florham Park, N.J.
  • CC-40 A pre-catalyzed mercaptan based epoxy hardener, available under the trade designation “CAPCURE 40 SEC HV” from BASF Corporation.
  • CG-1400 A micronized dicyandiamide, having an approximate amine equivalent weight of 21 grams/equivalent, available under the trade designation “AMICURE CG-1400”, from Air Products and Chemicals, Inc.
  • DEH-85 An unmodified bis-phenol-A hardener having an active hydrogen equivalent weight of approximately 265 grams/equivalent, available under the trade designation “DEH-85”, from Dow Chemical Company, Midland, Mich.
  • DER-6508 An isocyanate-modified 2-functional epoxy resin, obtained under the trade designation “DER-6508” from Dow Chemical, Midland, Mich.
  • DF-1 A polymeric, non-silicone, flow additive, available under the trade designation “DYNOADD F-1” from Dynea Oy, Helsinki, Finland.
  • EPON 826 A medium molecular weight diglycidyl ether of bisphenol A resin having an epoxide equivalent weight of from 178 to 186 grams/equivalent, available under the trade designation “EPON 826” from Momentive Performance Materials, Houston, Tex.
  • EPON 828 A bisphenol-A polyepoxide resin having an approximate epoxy equivalent weight of 188 grams/equivalent, available under the trade designation “EPON 828”, from Momentive Specialty Chemicals.
  • EPON SU-8 An epoxy novolac resin having an average epoxide group functionality of approximately eight, available under the trade designation “EPON SU-8” from Momentive Specialty Chemicals.
  • MX-120 A diglycidyl ether of bisphenol-A epoxy resin containing 25 weight percent butadiene-acrylic co-polymer core shell rubber having an approximate epoxy equivalent weight of 243 grams/equivalent, available under the trade designation “KANE ACE MX-120”, from Kaneka Texas Corporation, Pasadena, Tex.
  • MX-257 A diglycidyl ether of bisphenol-A epoxy resin containing 37.5 weight percent butadiene-acrylic co-polymer core shell rubber having an approximate epoxy equivalent weight of 294 grams/equivalent, available under the trade designation “KANE ACE MX-257”, from Kaneka Texas Corporation.
  • MY-720 A multifunctional epoxy resin, available under the trade designation “ARALDITE MY-720” from Huntsman Corporation, Woodlands, Tex.
  • PG-7 A copper-phthaocyanine pigment, available under the trade designation “VYNAMON GREEN 600734” from Heucotech Ltd., Fairless Hills, Pa.
  • QX-11 A mercaptan curing agent, available under the trade designation “EPOMATE QX-11”, from Japan Epoxy Resins, Inc., Tokyo, Japan.
  • R-960 A rutile titanium dioxide pigment, available under the trade designation “TI-PURE R-960” from E.I. du Dupont de Nemours and Company, Wilmington, Del.
  • RA-95 A bisphenol-A epoxy resin modified carboxyl terminated butadiene acrylonitrile elastomer, available under the trade designation “HYPDX RA-95” from CVC Specialty Chemicals Inc., Moorestown, N.J. SD-3: A modified hectorite clay, available under the trade designation “BENTONE SD-3” from Elementis Specialities, Hightown, N.J.
  • TDI-CDI A 40% by weight solution in toluene of a phenyl isocyanate capped toluene diisocyanate polycarbodiimide, having a 2:1 by weight ratio of toluene diisocyanate:phenyl isocyanate.
  • TMMP Trimethylolpropane tris(3-mercaptoproprionate), available from Wako Chemical USA, Inc., Richmond, Va.
  • U-52 An aromatic substituted urea (4,4′-methylene bis(phenyl dimethyl urea), having an approximate amine equivalent weight of 170 grams/equivalent, available under the trade designation “OMICURE U-52”, from CVC Specialty Chemicals Inc., Moorestown, N.J.
  • UR2T An epoxy resin hardener, available under the trade designation “AMICURE UR2T” from Air Products and Chemicals Inc.
  • a millbase was prepared as follows. At a temperature of 70° F. (21.1° C.), 66.66 grams EPON 826, 168.36 grams MX-120, 3.7 grams PG-7, 18.44 grams R-960, 6.18 grams SD-3, 34.83 grams CG-1400 and 1.83 grams U-52 were charged into plastic cup designed for use in a planetary mill, model “SPEED MIXER DA 400 FV”, available from Synergy Devices Limited, Buckinghamshire, United Kingdom. The cup was placed into a planetary mixer and mixed at 2200 rpm for 2 minutes. The mixture was milled in a three-roll mill for three passes and then set aside.
  • Reactive compositions as listed in Table 1 were prepared according to the procedure generally described in A-1.
  • Part-A and Part-B compositions were added, according to the parts by weight ratios listed in Table 2, to a 20 gram capacity planetary mill type cup and mixed at 2,750 rpm and 72° F. (22.2° C.) on the planetary mill for 20 seconds.
  • the one-part epoxy reactive mixture was applied on the silicone coated side of a 5 mil (127 ⁇ m) bleached paper liner having an opposing polyethylene coating, product number “23210 76# BL KFT H/HP 4D/6MH” Loparex, Inc., Iowa City, Iowa, by means of a knife-over-bed coating station at 72° F. (22° C.) and a bar gap of 8 mils (203.2 ⁇ m).
  • Each liner-film construction measuring approximately 11.5 by 6 inches (29.2 by 15.2 cm), was dried at 135° F. (57.2° C.), cooled and held for 24 hours at 72° F. (22.2° C.), then stored at ⁇ 20° F. ( ⁇ 28.9° C.) until used for subsequent processing.
  • the blended two-part epoxy reactive mixture was applied between the silicone coated sides of two 5 mil (127 ⁇ m) bleached paper liners having an opposing polyethylene coating, product number “23210 76# BL KFT H/HP 4D/6MH” Loparex, Inc., Iowa City, Iowa.
  • the liner/curable epoxy film/liner sandwich was made by means of a knife-over-bed coating station at 72° F. (22° C.) and a bar gap of 13 mils (203.2 ⁇ m). Each liner/film/liner sandwich, measuring approximately 11.5 by 6 inches (29.2 by 15.2 cm), was held for 24 hours at 72° F. (22.2° C.), then stored at ⁇ 20° F. ( ⁇ 28.9° C.) until used for subsequent processing.
  • a liner/curable epoxy film construction was made according to the method generally described in Method A, wherein the one-part epoxy reactive mixture was substituted with a two-part epoxy reactive mixture, after which it was stored at approximately 72° F. (22° C.) for 24 hours.
  • One liner of a liner-curable film-liner sandwich was removed and replaced with a similar size section of 0.125 oz/yd 2 (4 g/m 2 ) nonwoven polyester fabric, obtained from Technical Fiber Products, Inc., New York.
  • a polypropylene liner was placed over the nonwoven polyester fabric and the lay-up passed between two rubber-coated nip rollers at approximately 72° F. (22° C.) and 80 psi (551.6 kPa) in order to embed the polyester fabric.
  • the curable embossed film was subjected to a partial cure cycle, as listed in Table 3 then allowed to cool to 72° F. (22.2° C.).
  • a 0.5 inch (12.7 millimeters) thick aluminum tool having an approximately 40 mil (1 mm) high truncated pyramidal (frustum) pattern at densities between 50 and 150 pyramids/sq. inch was fabricated.
  • One face of the curable film was exposed and laid on the aluminum tool.
  • the film was covered by a sheet of 0.005 inch (0.13 millimeters) thick paper liner having a silicone coating on one side and a polyethylene coating on the opposite side, such that the curable epoxy contacted the silicone-coated side of the liner.
  • a 0.5 inch (12.7 millimeters) thick aluminum plate was laid over the release liner and the assembly placed in a hydraulic press operating at about 100 psi (689 kPa).
  • the assembly was preheated according to the time and temperature listed in Table 2, after which the film was removed from the sandwich and allowed to cool to 72° F. (22.2° C.).
  • the one-part reactive composition was applied to the embossed surface of the embossed curable film and manually wetted out and filled into each depression in the surface using a spreader.
  • the film was then oven dried for 20 minutes at 135° F. (57.2° C.) and allowed to cool back to 72° F. (22.2° C.).
  • the curable embossed film composite was then vacuum bagged with a vacuum of approximately 28 inches mercury (94.8 kPa) in an autoclave, model number “ECONOCLAVE 3 ⁇ 5”, from ASC Process Systems, Sylmar, Calif. Autoclave pressure was increased to 60 psi (413.7 kPa) and the temperature was increased at a rate of 4.5° F. (2.5° C.) per minute to 350° F. (176.7° C.), held for 90 minutes at this temperature, then cooled at a rate of 5° F. (2.8° C.) per minute to 72° F. (22.2° C.) before releasing the pressure and vacuum.
  • Autoclave pressure was increased to 60 psi (413.7 kPa) and the temperature was increased at a rate of 4.5° F. (2.5° C.) per minute to 350° F. (176.7° C.), held for 90 minutes at this temperature, then cooled at a rate of 5° F. (2.8° C.) per minute to 72° F. (22.2° C.)
  • the curable embossed film composite was then vacuum bagged with a vacuum of approximately 28 inches mercury (94.8 kPa) in an autoclave, model number “ECONOCLAVE 3 ⁇ 5”, from ASC Process Systems, Sylmar, Calif.
  • Autoclave pressure was increased to 45 psi (310.3 kPa), during which the vacuum bag was vented to the atmosphere once the autoclave pressure surpassed 15 psi (103.4 kPa).
  • Autoclave temperature was then increased at a rate of 4.5° F. (2.5° C.) per minute to 250° F. (121.1° C.), held for 90 minutes at this temperature, then cooled at a rate of 5° F. (2.8° C.) per minute to 72° F. (22.2° C.) before releasing the pressure and vacuum.
  • the curable embossed film was cured, open faced, in an oven at 270° F. (132.2° C.) for the duration in Table 3. After curing, the film was removed from the oven and allowed to cool to 72° F. (22.2° C.).
  • a conductive interlayer is applied to the embossed surface of the embossed curable film prior to application of the one-part reactive composition described above in “Curable Composite Panel Preparation.”
  • the conductive layer is added by a deposition method, such as chemical deposition, electrodeposition or vapor deposition.
  • the resulting panel contains a patterned interior conductive interlayer.
  • This method may be used to create articles described in PCT Patent App. US2010/031263, published Oct. 21, 2010, or PCT Patent App. US2010/031280, published Oct. 21, 2010, the disclosures of which are incorporated herein by reference.
  • the embossed surfaces of two layers of the embossed curable film are brought together prior to final cure to create a bilayer with interstitial gaps.
  • the patterns of the embossed surfaces are brought together in registration, with gaps in one surface meeting gaps in the opposing surface.
  • the patterns of the embossed surfaces are brought together out of registration.
  • the embossed surface of one layer of the embossed curable film is brought together with an unembossed second layer prior to final cure to create a bilayer with interstitial gaps.

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  • Chemical Kinetics & Catalysis (AREA)
  • Medicinal Chemistry (AREA)
  • Polymers & Plastics (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Wood Science & Technology (AREA)
  • Laminated Bodies (AREA)
  • Adhesives Or Adhesive Processes (AREA)
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PCT/US2013/045623 WO2014007963A1 (en) 2012-07-03 2013-06-13 Method of making structured hybrid adhesive articles
US14/408,188 US20150165670A1 (en) 2012-07-03 2013-06-13 Method of making structured hybrid adhesive articles

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US (2) US20150165670A1 (enrdf_load_stackoverflow)
EP (1) EP2870190B1 (enrdf_load_stackoverflow)
JP (1) JP6130502B2 (enrdf_load_stackoverflow)
KR (1) KR20150036272A (enrdf_load_stackoverflow)
CN (1) CN104619742B (enrdf_load_stackoverflow)
BR (1) BR112015000114A2 (enrdf_load_stackoverflow)
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WO2014007963A1 (en) 2014-01-09
CN104619742A (zh) 2015-05-13
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KR20150036272A (ko) 2015-04-07
BR112015000114A2 (pt) 2017-06-27
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US10625463B2 (en) 2020-04-21
CN104619742B (zh) 2016-08-17

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