US3508874A - Production of carbon yarns - Google Patents
Production of carbon yarns Download PDFInfo
- Publication number
- US3508874A US3508874A US700672A US3508874DA US3508874A US 3508874 A US3508874 A US 3508874A US 700672 A US700672 A US 700672A US 3508874D A US3508874D A US 3508874DA US 3508874 A US3508874 A US 3508874A
- Authority
- US
- United States
- Prior art keywords
- yarn
- graphite
- acrylic
- yarns
- carbon
- 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.)
- Expired - Lifetime
Links
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 title description 48
- 229910052799 carbon Inorganic materials 0.000 title description 23
- 238000004519 manufacturing process Methods 0.000 title description 6
- 238000000034 method Methods 0.000 description 33
- 229910002804 graphite Inorganic materials 0.000 description 24
- 239000010439 graphite Substances 0.000 description 24
- NIXOWILDQLNWCW-UHFFFAOYSA-N acrylic acid group Chemical group C(C=C)(=O)O NIXOWILDQLNWCW-UHFFFAOYSA-N 0.000 description 19
- 239000002609 medium Substances 0.000 description 9
- 239000002243 precursor Substances 0.000 description 9
- 238000012545 processing Methods 0.000 description 9
- 238000000197 pyrolysis Methods 0.000 description 9
- 238000011282 treatment Methods 0.000 description 9
- 239000006185 dispersion Substances 0.000 description 8
- 239000007788 liquid Substances 0.000 description 8
- 238000001035 drying Methods 0.000 description 7
- 239000000835 fiber Substances 0.000 description 7
- BAPJBEWLBFYGME-UHFFFAOYSA-N Methyl acrylate Chemical compound COC(=O)C=C BAPJBEWLBFYGME-UHFFFAOYSA-N 0.000 description 6
- 238000005087 graphitization Methods 0.000 description 6
- NLHHRLWOUZZQLW-UHFFFAOYSA-N Acrylonitrile Chemical compound C=CC#N NLHHRLWOUZZQLW-UHFFFAOYSA-N 0.000 description 5
- 239000011162 core material Substances 0.000 description 5
- KFZMGEQAYNKOFK-UHFFFAOYSA-N Isopropanol Chemical group CC(C)O KFZMGEQAYNKOFK-UHFFFAOYSA-N 0.000 description 4
- 229920001577 copolymer Polymers 0.000 description 4
- 239000006229 carbon black Substances 0.000 description 3
- 238000001246 colloidal dispersion Methods 0.000 description 3
- 239000002131 composite material Substances 0.000 description 3
- 230000006378 damage Effects 0.000 description 3
- 229920002239 polyacrylonitrile Polymers 0.000 description 3
- 238000006116 polymerization reaction Methods 0.000 description 3
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 3
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 2
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 2
- 239000000919 ceramic Substances 0.000 description 2
- 239000011248 coating agent Substances 0.000 description 2
- 238000000576 coating method Methods 0.000 description 2
- 229930195733 hydrocarbon Natural products 0.000 description 2
- 150000002430 hydrocarbons Chemical class 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 239000011159 matrix material Substances 0.000 description 2
- 239000000178 monomer Substances 0.000 description 2
- 239000001301 oxygen Substances 0.000 description 2
- 229910052760 oxygen Inorganic materials 0.000 description 2
- 239000003870 refractory metal Substances 0.000 description 2
- 238000004804 winding Methods 0.000 description 2
- 239000004215 Carbon black (E152) Substances 0.000 description 1
- 229920013683 Celanese Polymers 0.000 description 1
- 229920006243 acrylic copolymer Polymers 0.000 description 1
- 150000001298 alcohols Chemical class 0.000 description 1
- AZDRQVAHHNSJOQ-UHFFFAOYSA-N alumane Chemical group [AlH3] AZDRQVAHHNSJOQ-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 239000012736 aqueous medium Substances 0.000 description 1
- 229910052786 argon Inorganic materials 0.000 description 1
- 235000015241 bacon Nutrition 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 238000012937 correction Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000003467 diminishing effect Effects 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 238000009730 filament winding Methods 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 230000035876 healing Effects 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 239000012761 high-performance material Substances 0.000 description 1
- 238000007654 immersion Methods 0.000 description 1
- 238000005470 impregnation Methods 0.000 description 1
- 229910052500 inorganic mineral Inorganic materials 0.000 description 1
- 238000011031 large-scale manufacturing process Methods 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 229910044991 metal oxide Inorganic materials 0.000 description 1
- 150000004706 metal oxides Chemical class 0.000 description 1
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 1
- 239000011707 mineral Substances 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 230000002265 prevention Effects 0.000 description 1
- 230000002787 reinforcement Effects 0.000 description 1
- 229920006395 saturated elastomer Polymers 0.000 description 1
- 230000035945 sensitivity Effects 0.000 description 1
- 230000009528 severe injury Effects 0.000 description 1
- 238000009987 spinning Methods 0.000 description 1
- 235000015096 spirit Nutrition 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
- 239000010935 stainless steel Substances 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
- 239000004753 textile Substances 0.000 description 1
- 238000007669 thermal treatment Methods 0.000 description 1
- 238000009827 uniform distribution Methods 0.000 description 1
Classifications
-
- 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
- D01F9/20—Carbon filaments; Apparatus specially adapted for the manufacture thereof by decomposition of organic filaments from polyaddition, polycondensation or polymerisation products
- D01F9/21—Carbon filaments; Apparatus specially adapted for the manufacture thereof by decomposition of organic filaments from polyaddition, polycondensation or polymerisation products from macromolecular compounds obtained by reactions only involving carbon-to-carbon unsaturated bonds
- D01F9/22—Carbon filaments; Apparatus specially adapted for the manufacture thereof by decomposition of organic filaments from polyaddition, polycondensation or polymerisation products from macromolecular compounds obtained by reactions only involving carbon-to-carbon unsaturated bonds from polyacrylonitriles
-
- 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
-
- 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
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S264/00—Plastic and nonmetallic article shaping or treating: processes
- Y10S264/19—Inorganic fiber
Definitions
- the general approach to the production of such carbonaceous yarns acrylic yarns comprises the sequence of preoxidizing the yarn at moderate temperatures to stabilize it against physical damage under the subsequent higher temperature treatments and then pyrolyzing the preoxidized yarn up to a temperature of about 1000- 1200 C. See, for example, U.S. Patent 3,285,696; French Patent 1,430,803 and Belgian Patent 678,679. If graphitized yarns are desired, the pyrolyzed yarn is then treated at about 2000-3 000 C.
- the preoxidized yarn highly susceptible to damage during subsequent processing.
- the preoxidation itself causes a marked loss of tensile strength in the yarn.
- the second factor arises from the economic consideration that this step be performed while the yarn is wound on a package or similar large batch in view of the time required for the preoxidation. Removal from this package for further processing is rendered difiicult by the tendency of the filaments between each layer to stick together.
- the yarn is subjected to severe stress which results in a high incidence of flaws and breakage.
- the acrylic precursor yarns suitable for use in the process of this invention can be formed in known manner from the polymerization product of from to by weight acrylonitrile and from 0 to 10% by weight of monomers copolymerizable therewith.
- acrylonitrile homopolymer or copolymer can be employed.
- a multitude of such acrylic copolymers and their preparation are known to the art.
- a preferred copolymer is that formed from 93-94% acrylonitrile and 6-7% methyl acrylate.
- These acrylic homoand copolymers can be formed into continuous filament yarn by various spinning procedures well known in the art.
- the acrylic yarn is highly molecularly oriented by drawing under suitable conditions.
- Such methods of orientation are disclosed, for example, in U.S. Patents Nos. 2,455,173; 2,948,581; and 3,122,412.
- Molecular orientation is a very difficult property to quantity of measure.
- Tenacity, an easily measurable property, is considered a related, thougth not exact measure, of molecular orientation. For the purposes of this specification it will be so measured.
- the tenacity of the precursor acrylic yarns of this invention should be at least 3 grams per denier, and preferebly, at least 4 grams per denier.
- particulate carbon Any form of particulate carbon can be used in the process of this invention.
- the two most preferred forms are powdered graphite and carbon black.
- the nature of the dispersing medium is not critical. For example water, lower alcohols, mineral spirits, and other low molecular weight liquid hydrocarbons can readily be employed.
- the preferred dispersing medium is isopropanol.
- the particulate carbon should be present in an amount from 2% to 8% by weight based on the total weight of the dispersion.
- the optimum amount depends on, inter alia, the nature of the dispersing medium. In water, the preferred weight is 4% particulate carbon.
- Other factors influencing the optimum content of particulate carbon are the specific acrylic precursor, the processing speed, and the nature of the subsequent processing conditions. In addition to the amount of particulate carbon on the yarn, the distribution is equally important in insuring the production of uniform yarn.
- Continuous drying, as compared to batch drying, of the dispersion-treated acrylic yarn increases the amount of residual particulate carbon on the yarn during and after preoxidation. Moreover, it promotes more uniform distribution of the particulate carbon.
- This continuous drying treatment can be performed in numerous ways, most conveniently by passing over a steam-heated roll or through a heated tube. The residence time should be about 5 seconds to 1 minute, depending on total yarn denier, the liquid used and the temperature.
- the yarn is wound around a core constructed of a material that will not be destroyed or compressed by the heat exposure or by the stress developed by the highly oriented yarn upon heating.
- An aluminum core has been especially well suited for this purpose.
- suitable core materials include carbon, graphite, stainless steel, ceramics and the like.
- the preoxidation should preferably be in air at a temperature of between 240- 300C. for a time sufficient to attain a level of combined oxygen between 417% by weight and preferably 6 to 17% by weight.
- the pyrolysis can be conducted in any of several known methods. See for example US. Patent 3,285,696, Belgian Patent 678,679 and French Patent 1,430,803.
- the pyrolyzed fibers of my invention can be graphitized in several ways. They can be passed through a graphite tube furnace at 2000 3000 C. which can conveniently be arranged in series with the pyrolysis tube. Other methods include resistance graphitization as described in U.S. Patent 3,313,597, or flame graphitization according to the method of copending application S.N. 614,811 filed Feb. 9, 1967, now abandoned.
- Example I illustrates a preferred embodiment of this invention.
- Example II illustrates the importance of the graphite treatment of this invention.
- Example III illustrates the criticality of the yarn being impregnated with an aqueous colloidal dispersion of graphite as opposed to dry powdered graphite.
- Example IV illustrates the criticality of first drying the graphite-impregnated yarn before preoxidation.
- EXAMPLE I A 100 meter length of a 750' filament yarn of a copolymer of acrylonitrile and methyl acrylate in the proportions of approximately 93/7 respectively, is employed as the precursor yarn. This yarn is passed continuously under about grams tension through an aqueous colloidal dispersion of graphite (4% by weight) for an immersion time of about 0.1 second. Excess dispersion is wiped off by passing the saturated yarn upwardly through a series of five ceramic pins. Thereafter, the wet impregnated yarn is continuously passed to a drying roll heated to within the range of 105-ll0 C. The dried yarn is then wound on to a 3 inch diameter aluminum tube under 150 grams tension and the tube is placed in a heated 4 air oven for the preoxidation treatment. The preoxidation schedule consists of 16 hours at 200 C., 1 hour rise to 270 C. and two hours at 270 C. The tube of yarn is then removed from the oven and allowed to cool.
- the stabilized yarn is then pyrolyzed by passing it continuously through a resistance-heated metal tube which is /2 inch in diamter and is 48 inches long.
- the yarn enters and leaves the tube chamber through 1 mm. diameter orifices to keep out air and the tube is flushed constantly in the top end by the flow of 300 cc./min. of argon.
- Tension on the yarn is maintained at grams.
- the tube wall temperature is about 600 C. over the upper 12 inch of length and about 1200 C. over the lower 36 inches.
- the resulting pyrolyzed yarn is graphitized in nitrogen by passing it continuously under 100 grams tension through a graphite tube heated to 3000 C. for an exposure time of /2 minute.
- the yarns are flexible and non-sticky. This is reflected in trouble-free winding and unwinding and handling over rolls without yarn breakage. Moreover the treated yarn could sustain very high tensions in processing, as high as 700 grams during the above pyrolysis treatment and 500 grams during the above graphitization treatment, indicating low mechanical sensitivity to processing.
- Example I The process of Example I is repeated except that the graphite treatment is omitted. Following the preoxidation step, no more than a few inches of the yarn could be unwound from the spool without severe damage due to sticking between yarn wraps.
- Example III The process of Example I is repeated except that a very fine commercial graphite powder in a dry form is substituted for the aqueous colloidal graphite dispersion in the precursor yarn dip.
- the dry impregnation of powdered graphite resulted in only about 0.5% pick-up of graphite on the yarn.
- the preoxidation step it was difiicult to unwind the preoxidized yarn from the spool without damage due to sticking between yarn wraps.
- the yarn was quite stiff and could not be subjected successfully to the graphitization step due to frequent breakage of the yarn under the standard tension of 100 grams.
- the filament of the pyrolyzed yarn cannot be separated from the yarn bundle for testing due to excess sticking between filaments,
- EXAMPLE IV An acrylonitrile homopolymer arn is passed through a solution containing 4% by weight graphite dispersed in Water. One portion of this yarn is directly wound on a core, over-dried and preoxidized. The resulting yarn has an average residual graphite content of 3% and this graphite is poorly distributed. A second portion of the yarn passed through this solution is first dried on a steamheated roll. It is then Wound on the same core and subjected to the same preoxidation conditions. The resultant yarn has a residual graphite content of 7% by weight and this graphite is well distributed. Processing of the latter yarn proceeds much better than that of the former yarn.
- a process according to claim 1 wherein said acrylic yarn is formed from the polymerization product of from 90 to 100% by weight acrylonitrile and from 0 to by weight of a monomer copolymerizable therewith.
- said acrylic yarn is formed from the polymerization product of 93- 94% acrylonitrile and 67% methyl acrylate.
Landscapes
- Chemical & Material Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- General Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Textile Engineering (AREA)
- Inorganic Chemistry (AREA)
- Inorganic Fibers (AREA)
Description
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US70067268A | 1968-01-12 | 1968-01-12 |
Publications (1)
Publication Number | Publication Date |
---|---|
US3508874A true US3508874A (en) | 1970-04-28 |
Family
ID=24814440
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US700672A Expired - Lifetime US3508874A (en) | 1968-01-12 | 1968-01-12 | Production of carbon yarns |
Country Status (1)
Country | Link |
---|---|
US (1) | US3508874A (en) |
Cited By (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3648452A (en) * | 1968-08-03 | 1972-03-14 | Dunlop Holdings Ltd | Method of forming reinforcing yarns or cords |
US3660018A (en) * | 1969-08-04 | 1972-05-02 | Rolls Royce | Method of manufacturing carbon fibre |
US3779789A (en) * | 1971-04-20 | 1973-12-18 | Celanese Corp | Production of pervious low density carbon fiber reinforced composite articles |
US3900556A (en) * | 1968-11-20 | 1975-08-19 | Celanese Corp | Process for the continuous carbonization and graphitization of a stabilized acrylic fibrous material |
US3935301A (en) * | 1972-08-07 | 1976-01-27 | Toray Industries, Inc. | Process for producing carbon fibers from organic fibrous material |
US3975482A (en) * | 1972-06-21 | 1976-08-17 | Celanese Corporation | Process for drawing acrylic fibrous materials to form a product which particularly is suited for thermal stabilization and carbonization |
JPS51137694A (en) * | 1975-05-23 | 1976-11-27 | Toho Rayon Co Ltd | Method of producing activated carbon fiber |
US3997654A (en) * | 1974-04-24 | 1976-12-14 | Bergwerksverband Gmbh | Method for the production of carbonaceous articles, particularly strands |
US4029955A (en) * | 1974-02-08 | 1977-06-14 | General Electric Company | Luminaire filter material |
US4055583A (en) * | 1974-04-24 | 1977-10-25 | Bergwerksverband Gmbh | Method for the production of carbonaceous articles, particularly strands |
US4112059A (en) * | 1974-11-14 | 1978-09-05 | Celanese Corporation | Process for the production of carbon filaments utilizing an acrylic precursor |
US4275051A (en) * | 1979-01-29 | 1981-06-23 | Union Carbide Corporation | Spin size and thermosetting aid for pitch fibers |
US4276278A (en) * | 1979-01-29 | 1981-06-30 | Union Carbide Corporation | Spin size and thermosetting aid for pitch fibers |
US4534919A (en) * | 1983-08-30 | 1985-08-13 | Celanese Corporation | Production of a carbon fiber multifilamentary tow which is particularly suited for resin impregnation |
US4714642A (en) * | 1983-08-30 | 1987-12-22 | Basf Aktiengesellschaft | Carbon fiber multifilamentary tow which is particularly suited for weaving and/or resin impregnation |
US4781223A (en) * | 1985-06-27 | 1988-11-01 | Basf Aktiengesellschaft | Weaving process utilizing multifilamentary carbonaceous yarn bundles |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2799915A (en) * | 1953-03-30 | 1957-07-23 | Johns Manville | Thermal modification of acrylonitrile polymers |
US3235323A (en) * | 1960-04-14 | 1966-02-15 | Minnesota Mining & Mfg | Heat-resistant black fibers and fabrics derived from rayon |
US3242000A (en) * | 1963-08-30 | 1966-03-22 | Deering Milliken Res Corp | Impregnated carbonized acrylic textile product and method for producing same |
US3281261A (en) * | 1963-08-30 | 1966-10-25 | Deering Milliken Res Corp | Method of preparing refractory metal oxide coated carbonized acrylic textile fibers |
US3285696A (en) * | 1960-08-25 | 1966-11-15 | Tokai Denkyoku Seizo Kabushiki | Method for the preparation of flexible carbon fibre |
US3305315A (en) * | 1962-09-20 | 1967-02-21 | Union Carbide Corp | Process for manufacturing flexible carbonaceous textile material |
-
1968
- 1968-01-12 US US700672A patent/US3508874A/en not_active Expired - Lifetime
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2799915A (en) * | 1953-03-30 | 1957-07-23 | Johns Manville | Thermal modification of acrylonitrile polymers |
US3235323A (en) * | 1960-04-14 | 1966-02-15 | Minnesota Mining & Mfg | Heat-resistant black fibers and fabrics derived from rayon |
US3285696A (en) * | 1960-08-25 | 1966-11-15 | Tokai Denkyoku Seizo Kabushiki | Method for the preparation of flexible carbon fibre |
US3305315A (en) * | 1962-09-20 | 1967-02-21 | Union Carbide Corp | Process for manufacturing flexible carbonaceous textile material |
US3242000A (en) * | 1963-08-30 | 1966-03-22 | Deering Milliken Res Corp | Impregnated carbonized acrylic textile product and method for producing same |
US3281261A (en) * | 1963-08-30 | 1966-10-25 | Deering Milliken Res Corp | Method of preparing refractory metal oxide coated carbonized acrylic textile fibers |
Cited By (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3648452A (en) * | 1968-08-03 | 1972-03-14 | Dunlop Holdings Ltd | Method of forming reinforcing yarns or cords |
US3900556A (en) * | 1968-11-20 | 1975-08-19 | Celanese Corp | Process for the continuous carbonization and graphitization of a stabilized acrylic fibrous material |
US3660018A (en) * | 1969-08-04 | 1972-05-02 | Rolls Royce | Method of manufacturing carbon fibre |
US3779789A (en) * | 1971-04-20 | 1973-12-18 | Celanese Corp | Production of pervious low density carbon fiber reinforced composite articles |
US3975482A (en) * | 1972-06-21 | 1976-08-17 | Celanese Corporation | Process for drawing acrylic fibrous materials to form a product which particularly is suited for thermal stabilization and carbonization |
US3935301A (en) * | 1972-08-07 | 1976-01-27 | Toray Industries, Inc. | Process for producing carbon fibers from organic fibrous material |
US4029955A (en) * | 1974-02-08 | 1977-06-14 | General Electric Company | Luminaire filter material |
US3997654A (en) * | 1974-04-24 | 1976-12-14 | Bergwerksverband Gmbh | Method for the production of carbonaceous articles, particularly strands |
US4055583A (en) * | 1974-04-24 | 1977-10-25 | Bergwerksverband Gmbh | Method for the production of carbonaceous articles, particularly strands |
US4112059A (en) * | 1974-11-14 | 1978-09-05 | Celanese Corporation | Process for the production of carbon filaments utilizing an acrylic precursor |
JPS51137694A (en) * | 1975-05-23 | 1976-11-27 | Toho Rayon Co Ltd | Method of producing activated carbon fiber |
JPS5820883B2 (en) * | 1975-05-23 | 1983-04-26 | トウホウベスロン カブシキガイシヤ | Activated carbon fiber manufacturing method |
US4275051A (en) * | 1979-01-29 | 1981-06-23 | Union Carbide Corporation | Spin size and thermosetting aid for pitch fibers |
US4276278A (en) * | 1979-01-29 | 1981-06-30 | Union Carbide Corporation | Spin size and thermosetting aid for pitch fibers |
US4534919A (en) * | 1983-08-30 | 1985-08-13 | Celanese Corporation | Production of a carbon fiber multifilamentary tow which is particularly suited for resin impregnation |
US4714642A (en) * | 1983-08-30 | 1987-12-22 | Basf Aktiengesellschaft | Carbon fiber multifilamentary tow which is particularly suited for weaving and/or resin impregnation |
US4781223A (en) * | 1985-06-27 | 1988-11-01 | Basf Aktiengesellschaft | Weaving process utilizing multifilamentary carbonaceous yarn bundles |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
AS | Assignment |
Owner name: CCF, INC., Free format text: ASSIGNMENT OF ASSIGNORS INTEREST.;ASSIGNOR:CELANESE CORPORATION;REEL/FRAME:004413/0650 Effective date: 19850510 |
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AS | Assignment |
Owner name: BASF STRUCTURAL MATERIALS, INC., 1501 STEELE CREEK Free format text: ASSIGNMENT OF ASSIGNORS INTEREST.;ASSIGNOR:INMONT CORPORATION, A CORP. OF DE.;REEL/FRAME:004540/0948 Effective date: 19851231 |
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AS | Assignment |
Owner name: INMONT CORPORATION Free format text: MERGER;ASSIGNORS:NARMCO MATERIALS, INC.;QUANTUM, INCORPORATED;CCF, INC.;REEL/FRAME:004580/0870 Effective date: 19860417 |
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