DE1213334B - Foerm body made of carbonaceous material and a carbonaceous binder and process for their manufacture - Google Patents
Foerm body made of carbonaceous material and a carbonaceous binder and process for their manufactureInfo
- Publication number
- DE1213334B DE1213334B DEU9950A DEU0009950A DE1213334B DE 1213334 B DE1213334 B DE 1213334B DE U9950 A DEU9950 A DE U9950A DE U0009950 A DEU0009950 A DE U0009950A DE 1213334 B DE1213334 B DE 1213334B
- Authority
- DE
- Germany
- Prior art keywords
- binder
- graphite
- charred
- carbonaceous
- shaped body
- 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.)
- Pending
Links
- 238000000034 method Methods 0.000 title claims description 8
- 239000003575 carbonaceous material Substances 0.000 title claims description 6
- 238000004519 manufacturing process Methods 0.000 title claims description 5
- 239000011233 carbonaceous binding agent Substances 0.000 title claims description 4
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 25
- 229910002804 graphite Inorganic materials 0.000 claims description 20
- 239000010439 graphite Substances 0.000 claims description 20
- 239000011230 binding agent Substances 0.000 claims description 18
- 238000010438 heat treatment Methods 0.000 claims description 10
- 239000000203 mixture Substances 0.000 claims description 10
- 238000000465 moulding Methods 0.000 claims description 10
- HYBBIBNJHNGZAN-UHFFFAOYSA-N furfural Chemical compound O=CC1=CC=CO1 HYBBIBNJHNGZAN-UHFFFAOYSA-N 0.000 claims description 8
- 239000004744 fabric Substances 0.000 claims description 7
- 229920002678 cellulose Polymers 0.000 claims description 6
- 239000001913 cellulose Substances 0.000 claims description 6
- XPFVYQJUAUNWIW-UHFFFAOYSA-N furfuryl alcohol Chemical compound OCC1=CC=CO1 XPFVYQJUAUNWIW-UHFFFAOYSA-N 0.000 claims description 4
- 229920001568 phenolic resin Polymers 0.000 claims description 4
- 239000005011 phenolic resin Substances 0.000 claims description 4
- KXGFMDJXCMQABM-UHFFFAOYSA-N 2-methoxy-6-methylphenol Chemical compound [CH]OC1=CC=CC([CH])=C1O KXGFMDJXCMQABM-UHFFFAOYSA-N 0.000 claims description 3
- 239000000463 material Substances 0.000 claims description 3
- 239000003822 epoxy resin Substances 0.000 claims description 2
- 229920000647 polyepoxide Polymers 0.000 claims description 2
- 239000000835 fiber Substances 0.000 description 14
- 229910052799 carbon Inorganic materials 0.000 description 5
- 239000000126 substance Substances 0.000 description 4
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- 239000002296 pyrolytic carbon Substances 0.000 description 2
- 229920005989 resin Polymers 0.000 description 2
- 239000011347 resin Substances 0.000 description 2
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 2
- 229910052721 tungsten Inorganic materials 0.000 description 2
- 239000010937 tungsten Substances 0.000 description 2
- 229920000049 Carbon (fiber) Polymers 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 239000006229 carbon black Substances 0.000 description 1
- 239000003610 charcoal Substances 0.000 description 1
- 239000000571 coke Substances 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 230000003628 erosive effect Effects 0.000 description 1
- 238000005755 formation reaction Methods 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- LNEPOXFFQSENCJ-UHFFFAOYSA-N haloperidol Chemical compound C1CC(O)(C=2C=CC(Cl)=CC=2)CCN1CCCC(=O)C1=CC=C(F)C=C1 LNEPOXFFQSENCJ-UHFFFAOYSA-N 0.000 description 1
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- 239000002006 petroleum coke Substances 0.000 description 1
- 239000011295 pitch Substances 0.000 description 1
- 239000004576 sand Substances 0.000 description 1
- 239000007858 starting material Substances 0.000 description 1
- 238000003860 storage Methods 0.000 description 1
- 239000004753 textile Substances 0.000 description 1
- 239000003039 volatile agent Substances 0.000 description 1
Classifications
-
- 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
- C04B35/515—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics
- C04B35/52—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbon, e.g. graphite
- C04B35/522—Graphite
-
- 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
- C04B35/515—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics
- C04B35/52—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbon, e.g. graphite
-
- 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
- C04B35/515—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics
- C04B35/56—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbides or oxycarbides
-
- 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
-
- D—TEXTILES; PAPER
- D01—NATURAL OR MAN-MADE THREADS OR FIBRES; SPINNING
- D01F—CHEMICAL FEATURES IN THE MANUFACTURE OF ARTIFICIAL FILAMENTS, THREADS, FIBRES, BRISTLES OR RIBBONS; APPARATUS SPECIALLY ADAPTED FOR THE MANUFACTURE OF CARBON FILAMENTS
- D01F11/00—Chemical after-treatment of artificial filaments or the like during manufacture
- D01F11/10—Chemical after-treatment of artificial filaments or the like during manufacture of carbon
- D01F11/12—Chemical after-treatment of artificial filaments or the like during manufacture of carbon with inorganic substances ; Intercalation
-
- D—TEXTILES; PAPER
- D01—NATURAL OR MAN-MADE THREADS OR FIBRES; SPINNING
- D01F—CHEMICAL FEATURES IN THE MANUFACTURE OF ARTIFICIAL FILAMENTS, THREADS, FIBRES, BRISTLES OR RIBBONS; APPARATUS SPECIALLY ADAPTED FOR THE MANUFACTURE OF CARBON FILAMENTS
- D01F11/00—Chemical after-treatment of artificial filaments or the like during manufacture
- D01F11/10—Chemical after-treatment of artificial filaments or the like during manufacture of carbon
- D01F11/12—Chemical after-treatment of artificial filaments or the like during manufacture of carbon with inorganic substances ; Intercalation
- D01F11/125—Carbon
-
- D—TEXTILES; PAPER
- D01—NATURAL OR MAN-MADE THREADS OR FIBRES; SPINNING
- D01F—CHEMICAL FEATURES IN THE MANUFACTURE OF ARTIFICIAL FILAMENTS, THREADS, FIBRES, BRISTLES OR RIBBONS; APPARATUS SPECIALLY ADAPTED FOR THE MANUFACTURE OF CARBON FILAMENTS
- D01F11/00—Chemical after-treatment of artificial filaments or the like during manufacture
- D01F11/10—Chemical after-treatment of artificial filaments or the like during manufacture of carbon
- D01F11/14—Chemical after-treatment of artificial filaments or the like during manufacture of carbon with organic compounds, e.g. macromolecular compounds
-
- D—TEXTILES; PAPER
- D01—NATURAL OR MAN-MADE THREADS OR FIBRES; SPINNING
- D01F—CHEMICAL FEATURES IN THE MANUFACTURE OF ARTIFICIAL FILAMENTS, THREADS, FIBRES, BRISTLES OR RIBBONS; APPARATUS SPECIALLY ADAPTED FOR THE MANUFACTURE OF CARBON FILAMENTS
- D01F9/00—Artificial filaments or the like of other substances; Manufacture thereof; Apparatus specially adapted for the manufacture of carbon filaments
- D01F9/08—Artificial filaments or the like of other substances; Manufacture thereof; Apparatus specially adapted for the manufacture of carbon filaments of inorganic material
- D01F9/12—Carbon filaments; Apparatus specially adapted for the manufacture thereof
- D01F9/14—Carbon filaments; Apparatus specially adapted for the manufacture thereof by decomposition of organic filaments
- D01F9/16—Carbon filaments; Apparatus specially adapted for the manufacture thereof by decomposition of organic filaments from products of vegetable origin or derivatives thereof, e.g. from cellulose acetate
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01B—CABLES; CONDUCTORS; INSULATORS; SELECTION OF MATERIALS FOR THEIR CONDUCTIVE, INSULATING OR DIELECTRIC PROPERTIES
- H01B1/00—Conductors or conductive bodies characterised by the conductive materials; Selection of materials as conductors
- H01B1/04—Conductors or conductive bodies characterised by the conductive materials; Selection of materials as conductors mainly consisting of carbon-silicon compounds, carbon or silicon
-
- 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
- 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
-
- 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
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/70—Aspects relating to sintered or melt-casted ceramic products
- C04B2235/74—Physical characteristics
- C04B2235/77—Density
-
- 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
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/70—Aspects relating to sintered or melt-casted ceramic products
- C04B2235/96—Properties of ceramic products, e.g. mechanical properties such as strength, toughness, wear resistance
-
- 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
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/70—Aspects relating to sintered or melt-casted ceramic products
- C04B2235/96—Properties of ceramic products, e.g. mechanical properties such as strength, toughness, wear resistance
- C04B2235/9607—Thermal properties, e.g. thermal expansion coefficient
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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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/29—Coated or structually defined flake, particle, cell, strand, strand portion, rod, filament, macroscopic fiber or mass thereof
- Y10T428/2913—Rod, strand, filament or fiber
- Y10T428/2918—Rod, strand, filament or fiber including free carbon or carbide or therewith [not as steel]
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Ceramic Engineering (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Textile Engineering (AREA)
- General Chemical & Material Sciences (AREA)
- Structural Engineering (AREA)
- Organic Chemistry (AREA)
- Materials Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Inorganic Chemistry (AREA)
- Composite Materials (AREA)
- Ceramic Products (AREA)
Description
DEUTSCHESGERMAN
PATENTAMTPATENT OFFICE
AUSLEGESCHRIFTEDITORIAL
Int. α.:Int. α .:
C04bC04b
Deutsche Kl.: 80 b-8/12 German class: 80 b -8/12
Nummer: 1213 334Number: 1213 334
Aktenzeichen: U9950VIb/80bFile number: U9950VIb / 80b
Anmeldetag: 9. Juli 1963 Filing date: July 9, 1963
Auslegetag: 24. März 1966Opening day: March 24, 1966
Es ist bekannt, Fasern, Gewebe oder andere Textilgebilde aus Cellulose zu verkohlen und sie gegebenenfalls durch weiteres Erhitzen in Graphit überzuführen. Man erhält auf diese Art Gebilde von einer gewissen Elastizität und Biegsamkeit.It is known to carbonize fibers, fabrics or other textile structures made of cellulose and, if necessary, to use them converted into graphite by further heating. In this way one receives formations from a certain Elasticity and flexibility.
Es ist ferner bekannt, poröse Formkörper aus Kohlenstoff oder Graphit mit einem in der Wärme härtbaren Harz zu tränken und das Harz dann durch Erwärmen auszuhärten.It is also known to have porous molded bodies made of carbon or graphite with one in the heat to impregnate curable resin and then cure the resin by heating.
Es ist schließlich vorgeschlagen worden, Bahnen aus durch Erhitzen in Graphit übergeführtem Cellulosegewebe mit einem kohlenstoffhaltigen Bindemittel zu überziehen oder zu tränken, die so behandelten Bahnen zu stapeln, das gestapelte Gebilde zur Aushärtung des Bindemittels zu erwärmen und das Ganze dann schließlich bis zu etwa 900° C zu erhitzen, um das Bindemittel zu verkohlen. So hergestellte Schichtstoffe und Formkörper haben sich in vielen Beziehungen als wertvoll und brauchbar erwiesen. In manchen Fällen zeigen sich aber Nachteile, und zwar wegen der Anisotropie der Schichtstoffe oder Formkörper. So ist z. B. die Biegefestigkeit in Richtung gegen die Faserlage nicht immer genügend, und der thermische Ausdehnungskoeffizient ist besonders bei erhöhter Temperatur nicht in allen Richtungen der gleiche.Finally, it has been proposed to use sheets of cellulosic fabric converted into graphite by heating to coat or soak with a carbonaceous binder those treated in this way Stacking sheets, heating the stacked structure to harden the binding agent and the whole thing then finally to heat up to about 900 ° C in order to char the binder. Laminates made in this way and moldings have proven valuable and useful in many respects. In some In some cases, however, there are disadvantages due to the anisotropy of the laminates or moldings. So is z. B. the flexural strength in the direction towards the fiber layer is not always sufficient, and the thermal The coefficient of expansion is not the same in all directions, especially at elevated temperatures.
Diese Nachteile werden bei der Erfindung vermieden. These disadvantages are avoided in the invention.
Die Erfindung betrifft Formkörper aus kohlenstoffhaltigem Material und einem kohlenstoffhaltigen Bindemittel. Die Formkörper sind dadurch gekennzeichnet, daß sie als kohlenstoffhaltiges Material ein zerfasertes ungeordnetes verkohltes, vorzugsweise durch Erhitzen in Graphit übergeführtes Gewebe aus Cellulose enthalten.The invention relates to molded bodies made of carbon-containing material and a carbon-containing material Binder. The shaped bodies are characterized in that they are used as a carbonaceous material fiberized, disordered charred tissue, preferably converted into graphite by heating Contain cellulose.
In einer bevorzugten Ausführungsform enthalten die erfindungsgemäßen Formkörper auch das Bindemittel in verkohlter, zweckmäßigerweise durch Erhitzen in Graphit übergeführter Form.In a preferred embodiment, the moldings according to the invention also contain the binder in charred form, expediently converted into graphite by heating.
Die Erfindung betrifft ferner ein Verfahren zur Herstellung der beschriebenen Formkörper. Dieses Verfahren ist dadurch gekennzeichnet, daß man ein verkohltes Gewebe aus Cellulose zerfasert, die zerfaserten Stücke ungeordnet mit einem verkohlbaren Bindemittel mischt, das Gemisch unter Druck formt und schließlich bis zur Verkohlung des Bindemittels erhitzt. Gegebenenfalls kann man das Gemisch auf eine solche Temperatur erhitzen, daß das Bindemittel in Graphit übergeführt wird.The invention also relates to a method for producing the shaped bodies described. This The method is characterized in that a charred tissue made of cellulose is fiberized, the fiberized Mixing pieces randomly with a charring binder, forming the mixture under pressure and finally heated until the binder is charred. If necessary, the mixture can be added heat to such a temperature that the binder is converted into graphite.
Als verkohlbare Bindemittel kommen beispielsweise Phenolharze, Peche, Epoxyharze, Furfurol, Furfuralkohol
oder Gemische dieser Stoffe in Betracht. Bewährt hat sich als Bindemittel ein Gemisch aus etwa
Formkörper aus kohlenstoffhaltigem Material
und einem kohlenstoffhaltigen Bindemittel und
Verfahren zu ihrer HerstellungFor example, phenolic resins, pitch, epoxy resins, furfural, furfural alcohol or mixtures of these substances come into consideration as carbonizable binders. A mixture of, for example, shaped bodies made of carbonaceous material has proven useful as a binder
and a carbonaceous binder and
Process for their manufacture
Anmelder:Applicant:
Union Carbide Corporation, New York, N. Y.
(V. St. A.)Union Carbide Corporation, New York, NY
(V. St. A.)
Vertreter:Representative:
Dipl.-Ing. H. Görtz, Patentanwalt,
Frankfurt/M., Schneckenhofstr. 27Dipl.-Ing. H. Görtz, patent attorney,
Frankfurt / M., Schneckenhofstr. 27
Als Erfinder benannt:Named as inventor:
William Clay Beasley, Lawrenceburg, Term.William Clay Beasley, Lawrenceburg, Term.
(V. St. A.)(V. St. A.)
Beanspruchte Priorität:Claimed priority:
V. St. v. Amerika vom 9. JuH 1962 (208 510)V. St. v. America from June 9, 1962 (208 510)
Gewichtsprozent Phenolharz, etwa 25 Gewichtsprozent Furfuralkohol und etwa 25 Gewichtsprozent Furfurol.Weight percent phenolic resin, about 25 weight percent furfural alcohol and about 25 weight percent Furfural.
Gute Formkörper werden erhalten, wenn man bei ihrer Herstellung auf 1 Teil des Bindemittels 2 bis Teile des verkohlten Gewebes verwendet.Good moldings are obtained if 1 part of the binder is used for 2 bis Parts of the charred tissue used.
Bei der Herstellung der Formkörper können das Formen und Erhitzen gegebenenfalls gleichzeitig durchgeführt werden. Die erfindungsgemäßen Formkörper zeichnen sich durch hohe Festigkeit und geringe Dichte aus.In the production of the moldings, the molding and heating can optionally be carried out at the same time be performed. The moldings according to the invention are distinguished by high and low strength Density.
2 Teile eines zerfaserten Kohlenstoffgewebes wurden mit 1 Teil eines Gemisches aus 50 Gewichtsprozent Phenolharz, 25 Gewichtsprozent Furfuralkohol und Gewichtsprozent Furfurol gemischt. Das Gemisch. wurde unter einem Druck von 0,50 kg/mm2 zu einer Scheibe mit 25 cm Durchmesser und 7,5 cm Dicke2 parts of a fiberized carbon fabric were mixed with 1 part of a mixture of 50 percent by weight phenolic resin, 25 percent by weight furfural alcohol and percent by weight furfural. The mixture. became a disk 25 cm in diameter and 7.5 cm in thickness under a pressure of 0.50 kg / mm 2
609 539/395609 539/395
verformt und 6 Stunden bei etwa 130° C ausgehärtet. Die so hergestellte Scheibe wurde in einem Behälter in Koks eingebettet, wobei der Zutritt der Luft mittels einer 7,5 cm dicken Holzkohleschicht und einer 5 cm dicken Sandschicht verhindert wurde. Dann wurde die Temperatur um 10° C stündlich auf 600° C, um 60° C stündlich auf 800° C gesteigert und 2 Stunden lang bei 8000C gehalten. : deformed and cured for 6 hours at about 130 ° C. The disk produced in this way was embedded in coke in a container, the air being prevented from entering by means of a 7.5 cm thick layer of charcoal and a 5 cm thick layer of sand. Then, the temperature was 10 ° C per hour to 600 ° C, per hour increased by 60 ° C to 800 ° C and kept at 800 0 C for 2 hours. :
Einige Eigenschaften des so hergestellten Formkörpers bei Raumtemperatur sind:Some properties of the molded body produced in this way at room temperature are:
Schüttgewieht 0,94 g/cm3 Bulk weight 0.94 g / cm 3
Biegefestigkeit . ... Flexural strength. ...
in Faserrichtung 0,984 kg/τητη2 1S in the grain direction 0.984 kg / τητη 2 1S
gegen die Faserrichtung .. 0,633 kg/mm2 against the grain direction .. 0.633 kg / mm 2
Young-ModulYoung module
in. Faserrichtung 0,70 kg/mm2 · 103 in. fiber direction 0.70 kg / mm 2 · 10 3
gegen die Faserrichtung .. 0,35 kg/mm2 · 103 against the grain direction .. 0.35 kg / mm 2 · 10 3
Elektrischer WiderstandElectrical resistance
in Faserrichtung 0,022 Mikroohm/cm0.022 microohm / cm in the fiber direction
gegen die Faserrichtung .. 0,031 Mikroohm/cmagainst the fiber direction .. 0.031 microohms / cm
Als Ausgangsstoff wurde ein Graphitgewebe verwendet. Bis zum Verkohlen der Scheibe wurde so verfahren, wie es im Beispiel 1 beschrieben ist. Dann wurde die Temperatur um 15°C stündlich auf 500°C, um 60° C stündlich auf 800° C gesteigert und 2 Stunden bei 800° C gehalten.A graphite fabric was used as the starting material. This was done until the disk was charred, as described in Example 1. Then the temperature increased by 15 ° C every hour to 500 ° C, increased by 60 ° C hourly to 800 ° C and held at 800 ° C for 2 hours.
Anschließend ließ man den Formkörper im Behälter auf 300°C abkühlen.The shaped body was then allowed to cool to 300 ° C. in the container.
Einige Eigenschaften des so hergestellten Formkörpers bei Raumtemperatur sind:Some properties of the molded body produced in this way at room temperature are:
4040
Schüttgewieht 1,10 g/cm3 Bulk weight 1.10 g / cm 3
GragMtierung wurde ,der Ofen stündlich mit'0,15 bis 0,30 m3 Stickstoff zur Entfernung der sich entwickelnden flüchtigen Stoffe gespült. Nach Abkühlen auf etwa 500° C wurden die Gegenstände aus dem Ofen entfernt. ,-The furnace was flushed every hour with 0.15 to 0.30 m 3 of nitrogen to remove the volatile substances that developed. After cooling to about 500 ° C, the items were removed from the oven. , -
Einige Eigenschaften der so hergestellten Formkörper bei Raumtemperatur sind: Some properties of the moldings produced in this way at room temperature are:
Schüttgewieht , 1,00 g/cm3 Bulk weight, 1.00 g / cm 3
IO Biegefestigkeit IO flexural strength
in Faserrichtung ^. 1,195 kg/mm2 in grain direction ^. 1.195 kg / mm 2
gegen die Faserrichtung .. 0,352 kg/mm2 against the grain direction .. 0.352 kg / mm 2
t_' Young-Modul t _ 'Young module
in Faserrichtung i 0,5484 kg/mm2 · 103 in the direction of the grain i 0.5484 kg / mm 2 · 10 3
gegen die Faserrichtung .. 0,1687 kg/mm2 · 103 against the grain direction .. 0.1687 kg / mm 2 · 10 3
Elektrischer WiderstandElectrical resistance
in Faserrichtung 0,003 Mikroohm/cm0.003 microohm / cm in the fiber direction
gegen die Faserrichtung .. 0,007 Mikroohm/cmagainst the grain direction .. 0.007 microohms / cm
BiegefestigkeitFlexural strength
in Faserrichtung 0,773 kg/mm2'in grain direction 0.773 kg / mm 2 '
gegen die Fäserrichtung .. 0,211 kg/mm2 against the direction of the grain .. 0.211 kg / mm 2
4545
Young-ModulYoung module
in Faserrichtung 0,795 kg/mm2 · 103 in the direction of the grain 0.795 kg / mm 2 · 10 3
gegen die Faserrichtung .. 0,225 kg/mm2 · ΙΟ3 against the grain direction .. 0.225 kg / mm 2 · ΙΟ 3
Elektrischer WiderstandElectrical resistance
in Faserrichtung 0^010 Mikroohm/cmin the fiber direction 0 ^ 010 microohms / cm
gegen die Faserrichtung .. 0,024 Mikroohm/cmagainst the fiber direction .. 0.024 microohm / cm
Gemäß- Beispiel 2 hergestellte Scheiben wurden zerkleinert und die Stücke in einen 50 cm langen Graphitbehälter mit einem Innendurchmesser von 23 cm gepackt. Discs produced according to Example 2 were comminuted and the pieces packed in a 50 cm long graphite container with an inner diameter of 23 cm.
Der Deckel und der Boden des Behälters hatten kleine Öffnungen für den Austritt flüchtiger Stoffe,, die sich während der G'raphitierung entwickeln. Der Behälter wurde in die heiße Zone eines Rohrofens mit einem Durchmesser von 25 cm eingebracht und 4 Stunden lang· auf 2800° C erhitzt. Während derThe lid and the bottom of the container had small openings for the escape of volatile substances. which develop during the graphing. The container was placed in the hot zone of a tube furnace with a diameter of 25 cm and heated to 2800 ° C. for 4 hours. During the
Eine gemäß Beispiel 1 hergestellte und bearbeitete Scheibe wurde; gemäß Beispiel 3 graphitiert mit der Abweichung, daß sie annähernd 8 Stunden lang auf 2800° C erhitzt wurde.A disk produced and machined according to Example 1 was; graphitized according to Example 3 with the The difference is that it was heated to 2800 ° C for approximately 8 hours.
Diese verlängerte Erhitzungsdauer verhindert Rißbildung durch Schrumpfen und läßt den flüchtigen Stoffen mehr Zeit zum Entweichen.This extended heating time prevents cracking by shrinking and allowing more time for volatiles to escape.
Einige Eigenschaften der so hergestellten Formkörper bei Raumtemperatur sind:Some properties of the moldings produced in this way at room temperature are:
Schüttgewieht 0,96 g/cm2·Bulk weight 0.96 g / cm 2
Biegefestigkeit·Flexural strength
in Faserrichtung ,. 1,410 kg/mm2 in grain direction,. 1.410 kg / mm 2
gegen die Faserrichtung .. 0,492 kg/mm2 against the grain direction .. 0.492 kg / mm 2
Young-ModulYoung module
in Faserrichtung 0,654 kg/mm2 in the direction of the grain 0.654 kg / mm 2
gegen die Faserrichtung .. 0,281 kg/mm2 against the grain direction .. 0.281 kg / mm 2
Elektrischer WiderstandElectrical resistance
in Faserrichtung 0,005 Mikroohm/cm0.005 microohm / cm in the fiber direction
gegen die Faserrichtung. .. 0,009 Mikroohm/cmagainst the grain. .. 0.009 microohms / cm
Die erfindungsgemäßen Gegenstände aus reinem Graphit unterscheiden sich von den bekannten Laminaten durch die geringere Ausrichtung der Fasern. Diese ungeordnete Faserlagerung ist in der Mikrophotographie erkennbar.The objects according to the invention made of pure graphite differ from the known ones Laminates due to the lower alignment of the fibers. This disordered fiber storage is in the Photomicrograph recognizable.
Die ganz aus Graphit bestehenden erfindungsrgemäßen Gegenstände sind als Träger für pyrolytischen Kohlenstoff für aus Dampf abgeschiedenes Wolfram und andere hochtemperaturfeste Schichten sowie als Unterlagen für freistehende Einsätze aus Wolfram,, pyrolytischem Kohlenstoff und Graphit geeignet. Die neuen Stoffe können auch in Bereichen geringer Erosion,, beispielsweise für Teile von Geschossen und Raketen, verwendet werden.The entirely made of graphite according to the invention Articles are used as a support for pyrolytic carbon for vapor deposited Tungsten and other high-temperature-resistant layers and as a base for free-standing applications Tungsten, pyrolytic carbon and graphite are suitable. The new substances can also be used in areas of low erosion, for example for parts of projectiles and missiles.
In der folgenden Tabelle sind einige Eigenschaften von Formkörpern gemäß der Erfindung und vom Formkörpern aus Graphit und aus gebundenen geschichteten Graphitgeweben zusammengestellt.In the following table are some properties of shaped bodies according to the invention and of shaped bodies made of graphite and of bonded layered ones Graphite fabrics put together.
Eigenschaftcharacteristic
Üblicher Graphit aus RußCommon graphite made from carbon black
austhe end
Petroleumkoks Petroleum coke
GraphitgewebeschichtenGraphite fabric layers
mit Kohlenstoff gebundenbound with carbon
Graphit gebunden Erfindungsgemäße FormkörperGraphite bonded moldings according to the invention
Fasern mit
Kohlenstoff
gebundencharred
Fibers with
carbon
bound
mit Koh
lenstoff
gebundengraph
with Koh
fuel
bound
mit
Graphit
gebundenit fibers
with
graphite
bound
0,6330.984
0.633
0,2111.195
0.211
6,3521.195
6.352
0,0310.022
0.031
0,0250.042
0.025
0,0070.003
0.007
36,528.7
36.5
34,4 '29.2
34.4 '
1,83.7
1.8
2,75.6
2.7
9 bis 1825 to 31
9 to 18
Fasern und Bindemittel gleichzeitig graphitiertFibers and binders graphitized at the same time
Schüttgewicht,
g/cm3 Bulk weight,
g / cm 3
Biegefestigkeit,
kg/mmFlexural strength,
kg / mm
i. F i. F.
g.F g.F
Spezifischer Widerstand, Ohm/cmSpecific resistance, ohms / cm
i. F i. F.
ε. F ε. F.
1,531.53
1,687
1,2661.687
1.266
0,0063
0,00630.0063
0.0063
Wärmeausdehnungskoeffizient· io-7/°cThermal expansion coefficient io- 7 / ° c
i. F i. F.
g-F g-F
Wärmeleitfähigkeit
kcal/h -Hi-0CThermal conductivity
kcal / h -Hi- 0 C
i. F i. F.
g-F g-F
. F. = in Faserrichtung
g. F. = gegen Faserrichtung. F. = in the direction of the grain
G. F. = against grain direction
45 bis 50
45 bis 5045 to 50
45 to 50
22,2 bis 29,6
22,2 bis 29,622.2 to 29.6
22.2 to 29.6
1,581.58
1,828 0,7001.828 0.700
0,0080 0,00130.0080 0.0013
25,0 35,025.0 35.0
119 bis 178 74 bis 104119 to 178 74 to 104
1,191.19
1,547 0,0351.547 0.035
0,010 0,0720.010 0.072
24,8 41,824.8 41.8
1,161.16
2,25 0,072.25 0.07
0,0025 0,01300.0025 0.0130
28,3 34,728.3 34.7
21 bis 7,4 bis 0,9621 to 7.4 to 0.96
1,410 0,4921.410 0.492
0,005 0,0090.005 0.009
26,026.0
Claims (9)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US208510A US3407038A (en) | 1962-07-09 | 1962-07-09 | Shredded carbonaceous fiber compactions and method of making the same |
Publications (1)
Publication Number | Publication Date |
---|---|
DE1213334B true DE1213334B (en) | 1966-03-24 |
Family
ID=22774852
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DEU9950A Pending DE1213334B (en) | 1962-07-09 | 1963-07-09 | Foerm body made of carbonaceous material and a carbonaceous binder and process for their manufacture |
Country Status (4)
Country | Link |
---|---|
US (1) | US3407038A (en) |
DE (1) | DE1213334B (en) |
FR (1) | FR1361676A (en) |
GB (1) | GB1049661A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1646576B1 (en) * | 1967-03-08 | 1972-04-27 | Hoechst Ag | RAMPING MASS FOR METALLURGICAL OVENS |
Families Citing this family (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3927157A (en) * | 1969-08-21 | 1975-12-16 | Hitco | High temperature resistant products and methods for making the same |
US3943213A (en) * | 1970-04-06 | 1976-03-09 | Great Lakes Carbon Corporation | Method for manufacturing high temperature graphite fiber-graphite composites |
US3908061A (en) * | 1972-03-10 | 1975-09-23 | Dow Chemical Co | Composite materials comprising resin matrix and carbon fibers |
US3914395A (en) * | 1972-04-03 | 1975-10-21 | Avco Corp | Process for the manufacture of high strength carbon/carbon graphitic composites |
US3993738A (en) * | 1973-11-08 | 1976-11-23 | The United States Of America As Represented By The United States Energy Research And Development Administration | High strength graphite and method for preparing same |
JPS5817319B2 (en) * | 1974-03-13 | 1983-04-06 | 呉羽化学工業株式会社 | TAKOSHITSU CARBON SEAT NO SEIZOU HOU |
GB1460876A (en) * | 1975-01-03 | 1977-01-06 | Coal Ind | Carbon artefacts |
DE2554606C2 (en) * | 1975-12-04 | 1983-12-22 | C. Conradty Nürnberg GmbH & Co KG, 8505 Röthenbach | Carbon electrode |
US4350672A (en) * | 1976-02-25 | 1982-09-21 | United Technologies Corporation | Binderless carbon or graphite articles |
US4115528A (en) * | 1977-08-15 | 1978-09-19 | United Technologies Corporation | Method for fabricating a carbon electrode substrate |
US4297307A (en) * | 1979-06-29 | 1981-10-27 | Union Carbide Corporation | Process for producing carbon-carbon fiber composites suitable for use as aircraft brake discs |
JPS58117649A (en) * | 1981-12-29 | 1983-07-13 | Kureha Chem Ind Co Ltd | Manufacture of electrode substrate of fuel cell |
US4664988A (en) * | 1984-04-06 | 1987-05-12 | Kureha Kagaku Kogyo Kabushiki Kaisha | Fuel cell electrode substrate incorporating separator as an intercooler and process for preparation thereof |
EP0297695B1 (en) * | 1987-04-03 | 1993-07-21 | Nippon Oil Co. Ltd. | Process for fabricating carbon/carbon fibre composite |
KR100970319B1 (en) * | 2007-07-24 | 2010-07-15 | 신에쓰 가가꾸 고교 가부시끼가이샤 | Furnace for fabricating a glass preform or an optical fiber |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2796331A (en) * | 1954-06-09 | 1957-06-18 | Pittsburgh Coke & Chemical Co | Process for making fibrous carbon |
GB810509A (en) * | 1955-07-22 | 1959-03-18 | Siemens Planiawerke Ag | Improvements in or relating to the production of impregnated porous bodies |
FR1236007A (en) * | 1959-06-01 | 1960-07-15 | Lorraine Carbone | Manufacturing process for dense and impermeable graphite parts |
US2997739A (en) * | 1959-08-17 | 1961-08-29 | Owens Corning Fiberglass Corp | Binder curing of fibrous masses |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1896070A (en) * | 1931-06-17 | 1933-02-07 | Economy Fuse And Mfg Company | Molded gear |
US2003232A (en) * | 1933-05-15 | 1935-05-28 | Continental Diamond Fibre Co | Hollow articles, such as pipe fittings and the like, and method of making the same |
US3238054A (en) * | 1959-07-02 | 1966-03-01 | Atomic Energy Authority Uk | Method for producing a composite carbon article and articles produced thereby |
US3053775A (en) * | 1959-11-12 | 1962-09-11 | Carbon Wool Corp | Method for carbonizing fibers |
-
1962
- 1962-07-09 US US208510A patent/US3407038A/en not_active Expired - Lifetime
-
1963
- 1963-06-10 GB GB22987/63A patent/GB1049661A/en not_active Expired
- 1963-06-27 FR FR939638A patent/FR1361676A/en not_active Expired
- 1963-07-09 DE DEU9950A patent/DE1213334B/en active Pending
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2796331A (en) * | 1954-06-09 | 1957-06-18 | Pittsburgh Coke & Chemical Co | Process for making fibrous carbon |
GB810509A (en) * | 1955-07-22 | 1959-03-18 | Siemens Planiawerke Ag | Improvements in or relating to the production of impregnated porous bodies |
FR1236007A (en) * | 1959-06-01 | 1960-07-15 | Lorraine Carbone | Manufacturing process for dense and impermeable graphite parts |
US2997739A (en) * | 1959-08-17 | 1961-08-29 | Owens Corning Fiberglass Corp | Binder curing of fibrous masses |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1646576B1 (en) * | 1967-03-08 | 1972-04-27 | Hoechst Ag | RAMPING MASS FOR METALLURGICAL OVENS |
Also Published As
Publication number | Publication date |
---|---|
FR1361676A (en) | 1964-05-22 |
US3407038A (en) | 1968-10-22 |
GB1049661A (en) | 1966-11-30 |
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