DE3307090A1 - Process for producing a laminated material of carbon - Google Patents
Process for producing a laminated material of carbonInfo
- Publication number
- DE3307090A1 DE3307090A1 DE19833307090 DE3307090A DE3307090A1 DE 3307090 A1 DE3307090 A1 DE 3307090A1 DE 19833307090 DE19833307090 DE 19833307090 DE 3307090 A DE3307090 A DE 3307090A DE 3307090 A1 DE3307090 A1 DE 3307090A1
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- Germany
- Prior art keywords
- carbon
- layers
- thermoplastic
- laminate
- laminated material
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/22—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
- B32B5/24—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
- B32B5/26—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B18/00—Layered products essentially comprising ceramics, e.g. refractory products
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/32—Layered products comprising a layer of synthetic resin comprising polyolefins
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B38/00—Ancillary operations in connection with laminating processes
- B32B38/0036—Heat treatment
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B9/00—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00
- B32B9/04—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising such particular substance as the main or only constituent of a layer, which is next to another layer of the same or of a different material
- B32B9/045—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising such particular substance as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin
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- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/71—Ceramic products containing macroscopic reinforcing agents
- C04B35/78—Ceramic products containing macroscopic reinforcing agents containing non-metallic materials
- C04B35/80—Fibres, filaments, whiskers, platelets, or the like
- C04B35/83—Carbon fibres in a carbon matrix
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- C—CHEMISTRY; METALLURGY
- C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
- C25B—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES FOR THE PRODUCTION OF COMPOUNDS OR NON-METALS; APPARATUS THEREFOR
- C25B11/00—Electrodes; Manufacture thereof not otherwise provided for
- C25B11/04—Electrodes; Manufacture thereof not otherwise provided for characterised by the material
- C25B11/042—Electrodes formed of a single material
- C25B11/043—Carbon, e.g. diamond or graphene
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M4/00—Electrodes
- H01M4/86—Inert electrodes with catalytic activity, e.g. for fuel cells
- H01M4/96—Carbon-based electrodes
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/10—Inorganic fibres
- B32B2262/106—Carbon fibres, e.g. graphite fibres
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2305/00—Condition, form or state of the layers or laminate
- B32B2305/10—Fibres of continuous length
- B32B2305/18—Fabrics, textiles
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2313/00—Elements other than metals
- B32B2313/04—Carbon
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2323/00—Polyalkenes
- B32B2323/04—Polyethylene
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- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
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- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/65—Aspects relating to heat treatments of ceramic bodies such as green ceramics or pre-sintered ceramics, e.g. burning, sintering or melting processes
- C04B2235/656—Aspects relating to heat treatments of ceramic bodies such as green ceramics or pre-sintered ceramics, e.g. burning, sintering or melting processes characterised by specific heating conditions during heat treatment
- C04B2235/6562—Heating rate
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- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/65—Aspects relating to heat treatments of ceramic bodies such as green ceramics or pre-sintered ceramics, e.g. burning, sintering or melting processes
- C04B2235/658—Atmosphere during thermal treatment
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- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
- C04B2237/30—Composition of layers of ceramic laminates or of ceramic or metallic articles to be joined by heating, e.g. Si substrates
- C04B2237/32—Ceramic
- C04B2237/36—Non-oxidic
- C04B2237/363—Carbon
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- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
- C04B2237/50—Processing aspects relating to ceramic laminates or to the joining of ceramic articles with other articles by heating
- C04B2237/58—Forming a gradient in composition or in properties across the laminate or the joined articles
- C04B2237/582—Forming a gradient in composition or in properties across the laminate or the joined articles by joining layers or articles of the same composition but having different additives
- C04B2237/584—Forming a gradient in composition or in properties across the laminate or the joined articles by joining layers or articles of the same composition but having different additives the different additives being fibers or whiskers
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- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
- C04B2237/50—Processing aspects relating to ceramic laminates or to the joining of ceramic articles with other articles by heating
- C04B2237/70—Forming laminates or joined articles comprising layers of a specific, unusual thickness
- C04B2237/704—Forming laminates or joined articles comprising layers of a specific, unusual thickness of one or more of the ceramic layers or articles
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- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
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- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/622—Forming processes; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/626—Preparing or treating the powders individually or as batches ; preparing or treating macroscopic reinforcing agents for ceramic products, e.g. fibres; mechanical aspects section B
- C04B35/63—Preparing or treating the powders individually or as batches ; preparing or treating macroscopic reinforcing agents for ceramic products, e.g. fibres; mechanical aspects section B using additives specially adapted for forming the products, e.g.. binder binders
- C04B35/632—Organic additives
- C04B35/634—Polymers
- C04B35/63404—Polymers obtained by reactions only involving carbon-to-carbon unsaturated bonds
- C04B35/63408—Polyalkenes
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- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
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- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/622—Forming processes; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/626—Preparing or treating the powders individually or as batches ; preparing or treating macroscopic reinforcing agents for ceramic products, e.g. fibres; mechanical aspects section B
- C04B35/63—Preparing or treating the powders individually or as batches ; preparing or treating macroscopic reinforcing agents for ceramic products, e.g. fibres; mechanical aspects section B using additives specially adapted for forming the products, e.g.. binder binders
- C04B35/632—Organic additives
- C04B35/634—Polymers
- C04B35/63404—Polymers obtained by reactions only involving carbon-to-carbon unsaturated bonds
- C04B35/63432—Polystyrenes
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- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/622—Forming processes; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/626—Preparing or treating the powders individually or as batches ; preparing or treating macroscopic reinforcing agents for ceramic products, e.g. fibres; mechanical aspects section B
- C04B35/63—Preparing or treating the powders individually or as batches ; preparing or treating macroscopic reinforcing agents for ceramic products, e.g. fibres; mechanical aspects section B using additives specially adapted for forming the products, e.g.. binder binders
- C04B35/632—Organic additives
- C04B35/634—Polymers
- C04B35/63404—Polymers obtained by reactions only involving carbon-to-carbon unsaturated bonds
- C04B35/63444—Nitrogen-containing polymers, e.g. polyacrylamides, polyacrylonitriles, polyvinylpyrrolidone [PVP], polyethylenimine [PEI]
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02E60/30—Hydrogen technology
- Y02E60/50—Fuel cells
Abstract
Description
Verfahren zum Herstellen eines Schicht- Method for producing a layer
stoffs aus Kohlenstoff Die Erfindung betrifft ein Verfahren zur Herstellung eines Schichtstoffs, dessen Schichten durch einen carbonisierten Binder verbunden sind und wenigstens eine Schicht aus einer textilen Kohlenstofform enthält. Unter dem Begriff textile Kohlenstofform" werden im folgenden durch Carbonisieren textiler Flächengebilde aus Rayon, Polyacrylnitril und anderen Faserstoffen hergestellte flexible und poröse Kohlenstoffkörper verstanden. material made of carbon The invention relates to a method for production a laminate, the layers of which are connected by a carbonized binder and contains at least one layer made of a textile carbon form. Under The term “textile carbon form” will be made more textile by carbonization in the following Fabrics made from rayon, polyacrylonitrile and other fibers understood flexible and porous carbon bodies.
Zur Herstellung eines im wesentlichen aus Kohlenstoff bestehenden Schichtstoffs ist es bekannt, Schichten oder Bahnen aus Kohlenstoffilz, -vlies oder -gewebe mit einem carbonisierbaren Binder zu beschichten, die beschichteten Bahnen aufeinanderzustapeln und den Stapel zur Carbonisierung des Binders, gegebenenfalls unter Druck, zu erhitzen (DE-PS 12 87 499). Als Binder sind duroplastische Kunstharze vorgeschlagen worden, deren Koksrückstand bei der Wärmebehandlung besonders groß ist, z.B. Phenolformaldehydharze, Epoxidharze und Furanharze, und die feste Schichtkörper mit vergleichsweise großer Biegesteifigkeit ergeben. Ähnliche Ergebnisse erzielt man mit Steinkohlenteerpech, das beim Erwärmen des Schichtstapels zunächst erweicht (DE-PS 15 71 390). Der Binder wird auf die Oberflächen der einzelnen Kohlenstoffschichten gesprüht, gepinselt oder auch durch Tauchen aufgebracht. Ein Teil des Binders diffundiert bei dieser Behandlung und der Erwärmung des Schicht stapels in den Kern der einzelnen Schichten und es ist offensichtlich, daß die Eigenschaften des fertigen Schichtstoffs von der Menge des innerhalb der Schichten gebildeten sekundären Kokses mitbestimmt werden. Bestimmende Größen für die Koksmenge sind u.a.To produce one consisting essentially of carbon Laminate, it is known, layers or webs of carbon felt, fleece or -to coat the coated webs with a carbonizable binder stack on top of each other and the stack for carbonization of the binder, if necessary under pressure to be heated (DE-PS 12 87 499). Thermosetting synthetic resins are used as binders have been proposed whose coke residue is particularly large in the heat treatment such as phenol-formaldehyde resins, epoxy resins and furan resins, and the solid laminated body with a comparatively high flexural strength. Achieved similar results one with coal tar pitch, which initially softens when the stack of layers is heated (DE-PS 15 71 390). The binder gets onto the surfaces of each carbon layer sprayed, brushed or applied by dipping. A part the binder diffuses during this treatment and the heating of the layer stack in the core of each layer and it is obvious that the properties of the finished laminate depends on the amount of that formed within the layers secondary coke are also determined. Determining variables for the amount of coke are i.a.
die Viskosität des Binders, die Porosität der Kohlenstoffschicht und das zum Auftragen des Binders verwendete Verfahren. Da die Parameter nur bis zu einem gewissen Grade konstant sind, ist die Streuung der Produkteigenschaften verhältnismäßig groß. Zur Verbesserung des Produkts ist deshalb vorgeschlagen worden, die Kohlenstoff schichten vollständig mit einem Binder, der gegebenenfalls mit einem Lösungsmittel verdünnt ist, zu imprägnieren und den Binder dann zu einem größeren Teil zu entfernen, so daß nur kleine besser reproduzierbare und über den gesamten Querschnitt gleichmäßig verteilte Mengen in der Kohlenstoffschicht verbleiben (DE-PS 27'00 866). Der Binderüberschuß wird zu diesem Zweck durch Walzen, Pressen, Schleudern usw. extrahiert und man erhält eine Faserschicht, deren einzelne Fasern mit einer Binderschicht von im wesentlichen gleichmäßiger Dicke überzogen sind. Die Schichten werden dann in bekannter Weise übereinandergestapelt und zur Carbonisierung des Binders unter Druck einer Wärmebehandlung unterworfen. Der Kohlenstoffschichtkörper ist von gleichmäßiger Beschaffenheit und weist eine vergleichsweise kleine Biegesteifigkeit auf. Die Schichtstoffe sind allein oder in Verbindung mit anderen temperaturbeständigen Stoffen, wie z.B. Graphitfolie, hervorragende Isolationsmittel für hohe Temperaturen. Andere Verwendungszwecke sind poröse Durchflußelektroden und Träger für Katalysatoren.the viscosity of the binder, the porosity of the carbon layer and the method used to apply the binder. Since the parameters are only up to are constant to a certain extent, the spread of the product properties is proportional great. In order to improve the product it has therefore been proposed that the carbon layer completely with a binder, optionally with a solvent is diluted, to impregnate and then to remove a larger part of the binder, so that only small ones are more reproducible and uniform over the entire cross-section distributed amounts remain in the carbon layer (DE-PS 27'00 866). The excess binder is extracted for this purpose by rolling, pressing, spinning, etc. and is obtained a fiber layer, the individual fibers of which with a binder layer of substantially are coated with a uniform thickness. The layers are then made in a known manner stacked one on top of the other and a heat treatment for carbonization of the binder under pressure subject. The carbon composite is of uniform texture and has a comparatively low flexural rigidity. The laminates are alone or in connection with other temperature-resistant materials, such as graphite foil, excellent insulation for high temperatures. Other uses are porous flow electrodes and supports for catalysts.
Ein Nachteil des Extraktionsverfahrens ist der große technische Aufwand. Man benötigt besondere Walzwerke, Zentrifugen und dgl. und besonders bei der Verwendung verdünnter Binder, wirkungsvolle Einrichtungen zum Auffangen der freiwerdenden Lösungsmittel. Es sind schließlich Verfahren bekannt geworden, bei welchen textile Flächengebilde, wie Gewebe und unidirektionale Faserbänder mit einer Folie aus einem thermoplastischen Kunststoff, vorzugsweise einem Kunststoff mit hohem Erweichungspunkt, belegt und unter Einwirkung von Temperatur und Druck miteinander verbunden werden (EP-A 0 040 967).A disadvantage of the extraction process is the great technical effort. Special rolling mills are required Centrifuges and the like. And especially when using dilute binders, effective means of collecting the released solvents. Finally, procedures have become known in which textile fabrics, such as fabrics and unidirectional fiber ribbons with a film made of a thermoplastic plastic, preferably a plastic with a high softening point, covered and exposed to temperature and pressure are connected to one another (EP-A 0 040 967).
Man erhält einen schichtförmigen faserverstärkten Thermoplasten, dessen thermische und chemische Beständigkeit sehr begrenzt ist. Der Erfindung liegt nun die Aufgabe zugrunde, ein verbessertes Verfahren zur Herstellung eines ausschließlich aus Kohlenstoff bestehenden Schichtstoffs zu schaffen, der wenigstens eine Schicht aus einer textilen Kohlenstofform enthält. Der Schichtstoff soll eine große Porosität haben, eine hohe Gleichförmigkeit und eine begrenzte Biegesteifigkeit aufweisen.A layered fiber-reinforced thermoplastic is obtained, its thermal and chemical resistance is very limited. The invention now lies the object of an improved method for producing an exclusively to create a carbon laminate that has at least one layer contains from a textile carbon form. The laminate should have a large porosity have high uniformity and limited flexural rigidity.
Die Aufgabe wird dadurch gelöst, daß die den Schichtstoff bildenden Schichten gestapelt werden, zwischen je zwei Schichten eine Folie aus einem thermoplastischen Kunststoff angeordnet und der Stapel unter Druck zur Carbonisierung des Kunststoffs einer Wärmebehandlung unterworfen wird. Nach einer bevorzugten Ausbildung des Verfahrens werden thermoplastische Kunststoffolien verwendet, deren Verkokungsrückstand 10 bis 20 % beträgt.The object is achieved in that the forming the laminate Layers are stacked with a thermoplastic film between each two layers Plastic arranged and the stack under pressure to carbonize the plastic is subjected to a heat treatment. According to a preferred embodiment of the method thermoplastic plastic films are used, the coking residue of which is 10 up to 20%.
Der Vorteil des erfindungsgemäßen Verfahrens besteht darin, daß in die porösen Schichten des Schichtstoffs beim Erwärmen der Anordnung nur geringe durch die Verfahrensbedingungen genau bestimmbare Mengen des thermoplastischen Kunststoffs fließen, dessen Verkokungsrückstand verglichen mit den bekannten Bindern zudem klein ist. Die Versprödung des Schichtstoffs durch die Koks- bildung ist entsprechend gering, ohne daß die Verbindungsfestigkeit beeinträchtigt wird. Der Schichtstoff ist aufgrund seiner Biegesteifigkeit selbsttragend, er ist andererseits aber so flexibel, daß er durch Biegen gekrümmten Konturen angepaßt werden kann.The advantage of the method according to the invention is that in the porous layers of the laminate only slightly when the arrangement is heated Quantities of the thermoplastic material that can be precisely determined by the process conditions flow, whose coking residue is also small compared to the known binders is. The embrittlement of the laminate due to the coke education is correspondingly low without impairing the connection strength. Of the Laminate is self-supporting due to its flexural strength, on the other hand it is but so flexible that it can be adapted to curved contours by bending.
Die zur Herstellung des Schichtstoffes verwendeten Schichten bestehen vorzugsweise aus Kohlenstoffilz mit 2 einer Rohdichte von 0,07 bis 0,10 g/cm , was etwa einer Porosität von 95 % entspricht. Andere geeignete Schichten sind Kohlenstoffgewebe oder -vlies und Graphitfolie, die wegen ihrer geringen Permeabilität besonders als äußere Schicht des Schichtstoffs von Vorteil ist. Besonders günstig ist die Verwendung von thermoplastischen Kunststoffolien, die ganz oder zu einem Teil aus Polyethylen bestehen. Das Verhältnis der Schichtdicken der porösen Kohlenstoffschichten und der Folien sollte zweckmäßig 10 : 1 bis 10 : 2 betragen, der erste Grenzwert gilt im allgemeinen für thermoplastische Kunststoffolien mit einem großen Verkokungsrückstand, der zweite Grenzwert für Folien mit einem kleinen Verkokungsrückstand. Die alternierend übereinandergestapelten porösen Kohlenstoffschichten und Folien werden unter einem Druck von ca.The layers used to manufacture the laminate exist preferably made of carbon felt with a bulk density of 0.07 to 0.10 g / cm, what corresponds approximately to a porosity of 95%. Other suitable layers are carbon cloth or fleece and graphite foil, which because of their low permeability especially as outer layer of the laminate is advantageous. The use is particularly favorable of thermoplastic plastic films that are wholly or partly made of polyethylene exist. The ratio of the layer thicknesses of the porous carbon layers and of the foils should expediently be 10: 1 to 10: 2, the first limit value applies generally for thermoplastic plastic films with a large coking residue, the second limit value for foils with a small amount of coking residue. The alternating Stacked porous carbon layers and foils are under one Pressure of approx.
0,05 bis 0,2 N/mm2 zum Verkoken des thermoplastischen Kunstharz es in einer inerten oder reduzierenden Atmosphäre auf etwa 700 bis 1000 0C erhitzt. Die Erhitzungsgeschwindigkeit beträgt unter 250 bis 300 0C ca.0.05 to 0.2 N / mm2 for coking the thermoplastic synthetic resin heated to about 700 to 1000 0C in an inert or reducing atmosphere. The heating rate is below 250 to 300 0C approx.
30 bis 100 K/h, oberhalb dieser Temperaturen etwa 120 bis 200 K/h.30 to 100 K / h, above these temperatures about 120 to 200 K / h.
Die Erfindung wird im folgenden anhand von Beispielen erläutert: Beispiel 1 Zwei Kohlenstoffilz-Schichten mit einer Dicke von je 10 mm, deren Rohdichte 0,09 g/cm³ betrug, und eine 2,1 mm dicke Polyethylenfolie, entsprechend einem Flä- chengewicht von 180 g/m², wurden alternierend übereinandergestapelt und der Stapel unter einem Druck von 0,1 N/mm2 mit einem Gradienten von 50 K/h auf 260 °C und von 150 K/h in Argon auf 1000 °C erhitzt. Der durch Erhitzen der Folie in Helium auf 1000 °C mit einem Gradienten von 10 K/min bestimmte Verkokungsrückstand betrug 14,5 %.The invention is illustrated below with the aid of examples: Example 1 Two layers of carbon felt, each 10 mm thick, with a bulk density of 0.09 g / cm³, and a 2.1 mm thick polyethylene film, corresponding to an area weight of 180 g / m², were alternately stacked one on top of the other and the stack under one Pressure of 0.1 N / mm2 with a gradient of 50 K / h to 260 ° C and 150 K / h in Argon heated to 1000 ° C. The by heating the foil in helium to 1000 ° C with Coking residue determined using a gradient of 10 K / min was 14.5%.
Der Schichtstoff war von gleichmäßiger Beschaffenheit, die Rohdichte 0,13 g/cm3 und die Biegeb#uchfestigkeit 0,4 N/mm2.The laminate was of uniform consistency, the bulk density 0.13 g / cm3 and the flexural strength 0.4 N / mm2.
Beispiel 2 Es wurde ein Stapel aus vier Kohlenstoffilz-Schichten der in Beispiel 1 beschriebenen Beschaffenheit und drei zwischen je zwei Schichten angeordneten Folien auf der Basis Polyethylen-Vinylacetat- und Styrol-Butadien-Copolymer, Flächengewicht 190 g/m2, Dicke 2,1 mm, Verkokungsrückstand 11,5 %, gebildet und der Stapel unter einem Druck von ca. 0,08 N/mm wie in Beispiel 1 auf 1000 0C erhitzt. Bei gleicher Rohdichte von 0,13 g/cm3 betrug die Biegefestigkeit 0,6 N/mm2.Example 2 A stack of four carbon felt layers was produced from in Example 1 described nature and three arranged between two layers Films based on polyethylene-vinyl acetate and styrene-butadiene copolymers, weight per unit area 190 g / m2, thickness 2.1 mm, coking residue 11.5%, formed and the stack below heated to a pressure of approx. 0.08 N / mm as in Example 1 to 1000 ° C. With the same Density of 0.13 g / cm3, the flexural strength was 0.6 N / mm2.
Beispiel 3 Es wurde ein Stapel mit der Folge Graphitfilz, Folie, Graphitgewebe, Folie, Graphitfolie gebildet. Die Eigenschaften der Komponenten waren: Graphitfilz - Rohdichte 0,07 g/cm³, Dicke 9 mm, Graphitgewebe - Flächengewicht 350 g/cm2, Graphitfolie - Rohdichte 1,0 g/cm3, Dicke 0,35 mm, Polyamidfolie - Flächengewicht 180 g/m2, Dicke 1,6 mm, Verkokungsrückstand 11,0 %. Der Schichtstapel wurde in Stickstoff unter einem Druck von 0,12 N/mm² mit einem Gradienten von 30 K/h auf 250 0C und mit einem Gradienten von 200 K/h auf 950 K erhitzt. Der als Hitzeschild verwendete Schichtstoff hatte eine Rohdichte von etwa 0,15 g/cm³ und eine Biegefestigkeit von etwa 1,0 N/mm².Example 3 A stack with the sequence graphite felt, foil, graphite fabric, Foil, graphite foil formed. The properties of the components were: graphite felt - Density 0.07 g / cm³, thickness 9 mm, graphite fabric - weight per unit area 350 g / cm2, graphite foil - gross density 1.0 g / cm3, thickness 0.35 mm, polyamide film - weight per unit area 180 g / m2, thickness 1.6 mm, coking residue 11.0%. The layer stack was taken in nitrogen a pressure of 0.12 N / mm² with a gradient of 30 K / h to 250 0C and with a Gradients from 200 K / h to 950 K heated. The laminate used as a heat shield had an apparent density of about 0.15 g / cm³ and a flexural strength of about 1.0 N / mm².
Claims (5)
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DE19833307090 DE3307090A1 (en) | 1983-03-01 | 1983-03-01 | Process for producing a laminated material of carbon |
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DE19833307090 DE3307090A1 (en) | 1983-03-01 | 1983-03-01 | Process for producing a laminated material of carbon |
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Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0175878A2 (en) * | 1984-09-24 | 1986-04-02 | C. CONRADTY NÜRNBERG GmbH & Co. KG | Self-supporting, dimensionally stable carbon composite and process for its production |
EP0248918A1 (en) * | 1986-06-07 | 1987-12-16 | SIGRI GmbH | Thermal insulation |
EP0389634A1 (en) * | 1988-08-19 | 1990-10-03 | Osaka Gas Co., Ltd. | Molded heat insulator and process for its production |
US5242723A (en) * | 1988-08-19 | 1993-09-07 | Osaka Gas Company, Ltd. | Formed thermal insulator and process for preparation of same |
US5599603A (en) * | 1989-07-25 | 1997-02-04 | Dunlop Limited, A British Company | Manufacture of carbon fibre preform |
DE19544323A1 (en) * | 1995-11-28 | 1997-06-05 | Magnet Motor Gmbh | Gas diffusion electrode for polymer electrolyte membrane fuel cells |
DE10209199A1 (en) * | 2002-03-04 | 2003-10-02 | Schunk Kohlenstofftechnik Gmbh | Process for producing a multi-layer carbon brush |
DE102005013106B4 (en) * | 2005-03-18 | 2012-02-02 | Gerhard Präzisionspresstechnik GmbH | Carbon brush assembly |
EP3018772A1 (en) | 2014-11-05 | 2016-05-11 | Schunk Kohlenstofftechnik GmbH | Multi-layer carbon brush and method for producing same |
US20210086474A1 (en) * | 2018-05-03 | 2021-03-25 | Skc Co., Ltd. | Multilayer graphite sheet with excellent electromagnetic shielding capability and thermal conductivity and manufacturing method therefor |
-
1983
- 1983-03-01 DE DE19833307090 patent/DE3307090A1/en not_active Withdrawn
Cited By (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0175878A2 (en) * | 1984-09-24 | 1986-04-02 | C. CONRADTY NÜRNBERG GmbH & Co. KG | Self-supporting, dimensionally stable carbon composite and process for its production |
EP0175878A3 (en) * | 1984-09-24 | 1988-01-20 | C. CONRADTY NÜRNBERG GmbH & Co. KG | Self-supporting, dimensionally stable carbon composite and process for its production |
EP0248918A1 (en) * | 1986-06-07 | 1987-12-16 | SIGRI GmbH | Thermal insulation |
EP0389634A1 (en) * | 1988-08-19 | 1990-10-03 | Osaka Gas Co., Ltd. | Molded heat insulator and process for its production |
EP0389634A4 (en) * | 1988-08-19 | 1992-03-11 | Osaka Gas Company, Limited | Molded heat insulator and process for its production |
US5242723A (en) * | 1988-08-19 | 1993-09-07 | Osaka Gas Company, Ltd. | Formed thermal insulator and process for preparation of same |
US5599603A (en) * | 1989-07-25 | 1997-02-04 | Dunlop Limited, A British Company | Manufacture of carbon fibre preform |
DE19544323A1 (en) * | 1995-11-28 | 1997-06-05 | Magnet Motor Gmbh | Gas diffusion electrode for polymer electrolyte membrane fuel cells |
DE10209199A1 (en) * | 2002-03-04 | 2003-10-02 | Schunk Kohlenstofftechnik Gmbh | Process for producing a multi-layer carbon brush |
US7308759B2 (en) | 2002-03-04 | 2007-12-18 | Schunk Kohlenstofftechnik Gmbh | Method for production of a multi-layer carbon brush |
DE102005013106B4 (en) * | 2005-03-18 | 2012-02-02 | Gerhard Präzisionspresstechnik GmbH | Carbon brush assembly |
EP3018772A1 (en) | 2014-11-05 | 2016-05-11 | Schunk Kohlenstofftechnik GmbH | Multi-layer carbon brush and method for producing same |
DE102014116114A1 (en) | 2014-11-05 | 2016-05-12 | Schunk Kohlenstofftechnik Gmbh | Multi-layer carbon brush and production of such |
US20210086474A1 (en) * | 2018-05-03 | 2021-03-25 | Skc Co., Ltd. | Multilayer graphite sheet with excellent electromagnetic shielding capability and thermal conductivity and manufacturing method therefor |
US11745463B2 (en) * | 2018-05-03 | 2023-09-05 | Skc Co., Ltd. | Multilayer graphite sheet with excellent electromagnetic shielding capability and thermal conductivity and manufacturing method therefor |
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