US3689220A - Process for carbonizing fibrous cellulosic material - Google Patents

Process for carbonizing fibrous cellulosic material Download PDF

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Publication number
US3689220A
US3689220A US158355A US3689220DA US3689220A US 3689220 A US3689220 A US 3689220A US 158355 A US158355 A US 158355A US 3689220D A US3689220D A US 3689220DA US 3689220 A US3689220 A US 3689220A
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cellulosic material
silicon compound
carbon
cloth
silicon
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Paul A Smudski
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Stemcor Corp
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Carborundum Co
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Assigned to KENNECOTT CORPORATION reassignment KENNECOTT CORPORATION MERGER (SEE DOCUMENT FOR DETAILS). EFFECTIVE DEC. 31, 1980 NORTH DAKOTA Assignors: BEAR CREEK MINING COMPANY, BEAR TOOTH MINING COMPANY, CARBORUNDUM COMPANY THE, CHASE BRASS & COPPER CO. INCORPORATED, KENNECOTT EXPLORATION, INC., KENNECOTT REFINING CORPORATION, KENNECOTT SALES CORPORATION, OZARK LEAD COMPANY, PLAMBEAU MINING CORPORATION, RIDGE MINING CORPORATION (ALL MERGED INTO)
Assigned to STEMCOR CORPORATION, 200 PUBLIC SQUARE, CLEVELAND, OHIO 44114 A DE. CORP. reassignment STEMCOR CORPORATION, 200 PUBLIC SQUARE, CLEVELAND, OHIO 44114 A DE. CORP. ASSIGNMENT OF ASSIGNORS INTEREST. Assignors: KENNECOTT MINING CORPORATION
Assigned to KENNECOTT MINING CORPORATION reassignment KENNECOTT MINING CORPORATION CHANGE OF NAME (SEE DOCUMENT FOR DETAILS). EFFECTIVE DEC. 31, 1986. (SEE DOCUMENT FOR DETAILS) Assignors: KENNECOTT CORPORATION
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    • DTEXTILES; PAPER
    • D01NATURAL OR MAN-MADE THREADS OR FIBRES; SPINNING
    • D01FCHEMICAL FEATURES IN THE MANUFACTURE OF ARTIFICIAL FILAMENTS, THREADS, FIBRES, BRISTLES OR RIBBONS; APPARATUS SPECIALLY ADAPTED FOR THE MANUFACTURE OF CARBON FILAMENTS
    • D01F9/00Artificial filaments or the like of other substances; Manufacture thereof; Apparatus specially adapted for the manufacture of carbon filaments
    • D01F9/08Artificial filaments or the like of other substances; Manufacture thereof; Apparatus specially adapted for the manufacture of carbon filaments of inorganic material
    • D01F9/12Carbon filaments; Apparatus specially adapted for the manufacture thereof
    • D01F9/14Carbon filaments; Apparatus specially adapted for the manufacture thereof by decomposition of organic filaments
    • D01F9/16Carbon 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

Definitions

  • Cellulosic material in fibrous form is converted to carbon by subjecting the cellulosic material to a silicon compound, such as silicon tetrachloride; subsequently, subjecting the silicon compound treated cellulosic material to a nitrogen compound, such as ammonia; and finally subjecting the silicon compound treated, nitrogen compound treated cellulosic material to thermal degradation in a nonoxidizing atmosphere.
  • This process can be utilized to yield carbon in fibrous form of quality comparable to that produced by other processes, to increase the yield of carbon produced from the cellulosic material, and most significantly to substantially reduce the time required for thermal degradation of the cellulosic material.
  • the material being processed possesses sufficient strength at all stages of processing to be self-supporting, permitting processing to occur in a semicontinuous fashion, with each step of processing being accomplished by passing the material to be processed from one roll through the processing apparatus, and onto a second roll.
  • carbon including graphitized carbon commonly called graphite
  • fibrous form such as yarns, fabrics and filaments
  • Carbon and graphite felts are used as insulation and heat shields in high temperature induction and resistance furnaces.
  • Graphite cloth heating elements are used for temperatures up to 2500 C. in vacuum and inert gas furnaces for metal working. At lower temperatures, graphite cloth is used in a variety of ways as an electric heat source. Aircraft de-icers, water heaters, and heaters for softening sheets of plastics are typical applications.
  • Carbon fiber reinforced plastic ablation materials for thermal protection in reentry and rocket propulsion systems constitute a most important use of these materials.
  • a presently developing application of immense commercial potential is the use of carbon fiber reinforced carbon bodies as brake linings for jet aircraft. For these purposes, the cost of carbon fiber and the time necessary to produce the carbon fiber, which is a major contributor to the cost of the carbon fiber, become of great importance.
  • Carbon fibers and fabrics can be made from any fibrous raw material which, upon being subjected to thermal degradation, pyrolizes without going through a fusion stage to yield a carbon residue, while maintaining the integrity of the fiber.
  • Cellulosic materials are well suited for this use, and one of the most commonly used raw materials is rayon. Methods for converting rayon and Patented Sept. 5, 1972 other cellulosic materials to carbon cloth are based on the carefully controlled thermal degradation of the cellulosic material. Two general approaches are employed. According to one method, cellulosic material is degraded in a nonoxidizing gaseous environment by raising the temperature of the cellulosic material very slowly.
  • Typical speeds of heating are as follows: 10 to 50 C./hour, up to about 400 or 500 0.; about C./hour up to about 1000 C.; and from 'l000 C. up to about 1800 C. (2800 C. if graphite cloth is desired) at a much faster rate, perhaps 3000 C./hour. Further details of such processes are given, for example, in W. T. Soltes, U.S. Pat. No. 3,011,981; and in C. E. Ford et al., US. Pat. No. 3,107,152.
  • a second approach comprises the low temperature degradation of cellulosic material in a liquid environment, typically at temperatures ranging from about to 400 0., followed by a second degradation at higher temperatures in a gaseous environment. Like the first approach, very low rates of heating are employed. Further details of the second process are described in M. T. Cory, US. Pat. No. 3,508,871.
  • fibrous cellulosic material (preferably dried of substantially all free water) is converted to carbon material by first subjecting the fibrous cellulosic material to an environment of a silicon compound selected from the group consisting of silicon tetrachloride (SiCl and organohalosilanes such as sili-' con tetrachloride substituted with from 1 to 3 lower alkyl groups; secondly subjecting the silicon compound treated material to an environment of a nitrogen compound selected from the group consisting of ammonia, and primary and secondary lower alkyl amines (i.e., ammonia substituted with 1 or 2 lower alkyl groups) in an amount at least suflicient to neutralize the unreacted chlorine in said material; and finally heating the cellulosic material which has been treated with both the silicon compound and the nitrogen compound to a temperature of at least about 1 600 C. in a nonoxidizing atmosphere, whereby to produce a carbon material from the cellulosic
  • FIG. 1 is a flow chart which illustrates the process of the present invention in its various steps, including the preferred preliminary drying step.
  • FIG. 2 is a schematic representation of an apparatus which can be utilized to subject the cellulosic material to successive environments of silicon and nitrogen compounds, prior to carbonization.
  • FIG. 3 is a schematic representation of a furnace which can be utilized to carbonize the treated cellulosic material.
  • Cellulosic fibers which can be utilized in the present invention include seed fibers, woody fibers, bast fibers, and
  • leaf fibers as well as regenerated cellulose, i.e., rayon.
  • Rayon is the preferred cellulosic material because it is essentially pure cellulose, and because it is readily available in continuous filament form.
  • the initial chemical treatment with the silicon compound is preferably accomplished with silicon tetrachloride.
  • Treatment can occur with the silicon tetrachloride in the vapor phase, or by passing the untreated cellulosic material through liquid silicon tetrachloride.
  • Various other chloro-silicon compounds can also be utilized, such as organohalosilanes, and in particular, lower alkyl substituted silicon tetrachloride. Lower alkyl as used herein indicates alkyl groups having from 1 to about 3 carbon atoms.
  • Silicon tetrachloride is the preferred silicon compound for use in the present invention, and the next favored compound is methyltrichlorosilane.
  • the cellulosic material it is not essential that the cellulosic material be dried prior to its chemical treatment, but it is usually preferred to remove substantially all free water from the cellulosic material prior to its treatment with the silicon compound. This can be accomplished, for example, by drying the cellulosic material at a temperature ranging from about 100 to 120 C. for about 1 to 7 days under an absolute pressure of less than about 150 mm. of mercury. Removal of water from the cellulosic material prior to treatment with the silicon compound is usually desirable since it reduces the amount of silicon compound which is consumed in the process, which in turn reduces the amount of silicon compounds left on the carbon cloth produced. Excessive water in the cellulosic material to be carbonized also results in decreased strength of the carbon cloth produced. If the amount of silicon compounds used or re maining in the cloth after carbonization and the strength of the carbon cloth are not matters of concern, the treatment of cellulosic material containing Water does have the positive effect of reducing weight loss and shrinkage during carbonization.
  • the preferred rate of utilization of the silicon compound is less than 1 liter, preferably from about 0.1 to about 0.5 liter, of liquid silicon compound per 100 kg. of uncarbonized cellulosic material. If a gaseous silicon compound is used, an equivalent amount should be used.
  • the rate of silicon compound utilization can be varied by maintaining a pool of the liquid material for evapora tion. The rate of evaporation, and therefore of utiliZation, is proportional to the surface area on the top of the liquid pool. Silicon compound use can therefore be controlled by varying this surface area.
  • the amount of the nitrogen compound utilized is not highly critical, but at least enough should be used to neutralize the unreacted chlorine in the cellulosic material. This can be determined by the cessation of noticeable white cloud formation or by the change of odor from that characteristic of the silicon compound used, or of hydrochloric acid, to that characteristic of the nitrogen compound used.
  • FIG. 1 is a flow chart which illustrates the various steps of the process of the present invention.
  • the first drying step is optional, although highly preferred, and can be accomplished with existing conventional machinery.
  • the second and third steps of subjecting the cellulosic starting material to a silicon compound and subsequently to a nitrogen compound can conveniently be accomplished in apparatus such as that illustrated in FIG. 2.
  • FIG. 2 illustrates a chemical treatment apparatus divided into siX chambers 1116.
  • Chamber 11 contains feed roll 17 which is the source of cellulosic starting material 18.
  • Cellulosic material 18 is fed from feed chamber 11 through first purge chamber 12, silicon compound treatment chamber 13, second purge chamber 14, nitrogen compound treatment chamber 15, to collection chamber 16.
  • Each two adjacent chambers are separated by walls 1923, each wall containing a narrow slit which allows the passage of cellulosic material 18.
  • the cellulosic material which is to be treated in the apparatus of FIG. 2 is preferably in the form of a bolt of cellulosic cloth, such as rayon cloth, but the apparatus can also be used to treat cellulosic material in fiber form.
  • purge chambers 12 and 14 and collection chamber 16 are provided with purge gas inlets 12A, 14A and 16A, respectively. Through these purge gas inlets, 12A, 14A and 16A there is provided a suitable purge gas, preferably nitrogen, which prevents the silicon compound and nitrogen compound from getting into the wrong locations within the apparatus. This purge gas, together with vapors from chambers 13 and 15, is exhausted from the apparatus through exhaust outlet 26.
  • Silicon compound treatment chamber 13 is provided with silicon compound reservoir 28 containing pool 29 of the silicon compound to be utilized for treating the cellulosic material 18.
  • a reservoir 28 which has a wedge-shaped cross section, such as that shown in FIG. 2, the surface area of the silicon compound available for evaporation can be varied by merely varying the depth to which silicon compound reservoir 28 is filled. This is desirable in order to vary the amount of silicon compound which is available for treating cellulosic ma terial 18 so that excessive amounts of silicon compound is not utilized to treat the cellulosic material.
  • the pool 29 in reservoir 28 is maintained at a constant level by replenishment from silicon compound source 30.
  • silicon compound treatment chamber 13 can be outfitted with a silicon compound inlet analogous to nitrogen compound inlet 31, to be described below.
  • the cellulosic material 18 traveling through silicon compound treatment chamber 13 can be passed through a pool of the liquid silicon compound itself.
  • Nitrogen compound treatment chamber 15 is provided with a nitrogen compound inlet 31, through which a gaseous nitrogen compound such as ammonia is fed. If it is desired to utilize a liquid nitrogen compound, apparatus analogous to that utilized in silicon compound treatment chamber 13 can be provided in nitrogen compound treatment chamber 15. As mentioned above, the amount of nitrogen compound utilized is not highly critical; it is only necessary to utilize sufiicient nitrogen compound to neutralize any unreacted chlorine in cellulosic material 18.
  • the cellulosic material After passage through silicon compound treatment chamber 13 and nitrogen compound treatment chamber 15, the cellulosic material is wound up on take-up roll 24, to await the next step of processing, carbonization. Alternatively, the treated cloth can be fed directly into the carbonization furnace.
  • FIG. 3 illustrates a carbonization furnace which can be utilized to carry out the thermal degradation necessary for carbonizing the treated cellulosic material obtained from the apparatus of FIG. 2.
  • Feed roll 35 which in reality can be the same roll as take-up roll 24 of the apparatus of FIG. 2, provides treated cellulosic material 36 which is fed through furnace 37 to take-up roll 38.
  • Furnace 37 is provided with a number of heating elements 39, which are maintained at differing temperatures in order to provide a temperature gradient within furnace 37. By correlating the temperature gradient maintained within furnace 37 and the feed rate of treated cellulosic material 36 through furnace 37, the rate of heating of treated cellulosic material 36 can be closely controlled.
  • furnace 37 Since it is desired to carry out the carbonization in a non-oxidizing atmosphere, furnace 37 is provided with inlets 40 and 41 for nonoxidizing gas, such as nitrogen. Since the carbonization process yields a number of volatile materials, including the degradation products of the cellulosic material as well as the products from the treatment process carried out in the apparatus of FIG. 2, the nonoxidizing gas together with these degradation products is carried off through exhaust outlet 43. Since a temperature gradient is maintained within furnace 37, it is possible that volatile materials which are driven off from the cellulosic material 36 at the hotter (right hand as illustrated in 'FIG. 3) end of furnace 37 can be condensed in the cooler (left hand) end of the furnace 37.
  • nonoxidizing gas such as nitrogen
  • cellulosic material 36 is provided with protective means, such as protective cloth 48, to protect the cellulosic material from condensed vapors produced from the carbonization process.
  • protective cloth 48 to protect the cellulosic material from condensed vapors produced from the carbonization process.
  • the protective cloth approach if used, preferably utilizes a carbon cloth which will not undergo any further degradation throughout the carbonization process.
  • Other heat resistant materials can also be utilized, however.
  • cellulosic material 36 can be protected by a permanent cover (not shown) which is provided within furnace 37 immediately over cellulosic material 36.
  • Support table 51 within furnace 37, as well as rollers 52-55, are utilized in order to maintain cellulosic material 36 in a fiat position as it is traveling through furnace 37. Rollers 56 and 57 supplement rollers 52-55 in supporting protective cloth 48, if it is used.
  • Both of the above operations i.e., chemical treatment with the silicon compound and the nitrogen compound, as well as the carbonization operation, can be performed in a batch operation if desired.
  • Batch processing is preferred if the piece of cellulosic material to be converted to carbon material is relatively small, and semicontinuous processing, such as that illustrated in FIGS. 2 and 3, is preferred if the piece of cellulosic material to be converted into carbon is relatively large.
  • semicontinuous processing such as that illustrated in FIGS. 2 and 3
  • the second carbonization can proceed under conditions of temperature gradient and speed of travel such that the rate of increase of temperature in the carbon cloth is much greater, for example, from about 5000 to about 6000 C./hour, culminating in a maximum temperature of about 1650 C., in the event that ordinary carbon cloth is desired, or on the order of about 2800 C. in the event that graphite cloth is desired.
  • EXAMPLE 1 Six pieces of rayon about 4 feet long and 5 inches wide were exposed to a silicon compound, as set forth in Table 1. Four different methods of exposure were utilized, as follows:
  • Method 1 The rayon cloth was pulled through a beaker containing vapor of the silicon compound. About 8 inches of the cloth could be contained conveniently in the beaker at one time. This section of cloth was allowed to sit in the vapor for the indicated time period, and a new 8-inch section was drawn in and the treated section was moved to a beaker containing ammonia vapor where the cloth was accumulated until the whole strip was treated.
  • Method 2 Strips were treated by folding them up end over end so that the whole strip could be contained in the beaker. Otherwise, method 2 was similar to method 1.
  • Method 3 The strip was processed according to method 2, and then the strip was removed and refolded in the opposite direction for additional exposure to the silicon compound.
  • Method 4 Strips were drawn quickly through the liquid silicon compound, the exposure time being just long enough to wet the cloth. The strips were then placed in a beaker containing ammonia vapor, prior to carbonization.
  • Strips processed as above were then subjected to a carbonization operation, by placing the strips in graphite boats 3 feet long and 5 inches in internal diameter. It was necessary to fold the strips once, end over end, to get them into the boats.
  • the boats were then pushed through a furnace under an atmosphere of nitrogen at a rate of about 1 inch per minute.
  • the furnace contained a hot zone at a temperature of about 1600 C., which extended for about 3 feet in length.
  • the rayon Prior to reaching the hot zone, the rayon passed through a temperature gradient wherein the rayon was gradually increased from room temperature to the 1600 C. temperature of the hot zone.
  • the length of the temperature gradient was about 12 feet, so that the increase in temperature for the carbon cloth was about 650 to 675 C./hour.
  • the percent warp shrinkage and carbon yield were measured for each sample, as was the average strength of the carbon cloth produced. The results are set out in Table 1.
  • EXAMPLE 2 Pieces of rayon cloth about 20 cm. x 35 cm. were carbonized according to the present example.
  • the rayon samples were exposed to silicon tetrachloride vapor for various lengths of time as set out in Table 2.
  • the silicon tetrachloride treated rayon was then exposed to ammonia.
  • the pieces of treated rayon were then carbonized in two steps, the first step having varying conditions as set out in Table 2.
  • the initial heating conditions listed are the time required for the initial heating, and the maximum temperature attained during that heating process.
  • the treated rayon samples were subjected to a baking at 1650 C., the heating taking place at a much more rapid rate than the first step.
  • the percentage of shrinkage, carbon yield and average strength were measured for all of the samples; and five of the samples were analyzed for carbon content, silicon content, nitrogen content, and chlorine content. The results of these tests are set out in Table 2.
  • EXAMPLE 3 rolls of rayon cloth were converted to carbon in a semicontinuous manner, i.e., the rayon was fed from one roll to another in a continuous fashion until the rayon material was used up.
  • the first step of this example was drying the rayon cloth.
  • a charge of approximately 60 lbs. (just under 60 sq. yards) was placed in an oven maintained at a temperature of 100 C. for 7 days.
  • the pressure maintained within this oven varied from about to about 125 mm. of mercury absolute.
  • Successive charges of rayon subjected to this vacuum-heating technique showed weight losses ranging from about 8 to about 10%.
  • a process for producing carbonized fibrous cellulosic material comprising the steps of (1) subjecting the fibrous cellulosic material to be carbonized to an environment of a silicon compound selected from the group consisting of silicon tetrachloride and silicon tetrachloride substituted with from 1 to 3 lower alkyl groups, whereby to form a silicon compound treated material;
  • a process according to claim 1, comprising in addition the step of drying the cellulosic material to remove substantially all free water, prior to the step of subjecting the cellulosic material to an environment of a silicon compound.
  • a process according to claim 3, wherein the drying is accomplished by subjecting the cellulosic material to a temperature ranging from about to about C., for a period of from about 1 to about 7 days, under an absolute pressure of less than about mm. of mercury.
  • silicon compound is selected from the group consisting of silicon tetrachloride and methyltrichlorosilane.
  • gaseous silicon tetrachloride is utilized at a rate equivalent to from about 0.1 to about 0.5 liter of liquid silicon tetrachloride per 100 kg. of dried cellulosic material.

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  • Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • General Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Textile Engineering (AREA)
  • Inorganic Fibers (AREA)
  • Treatment Of Fiber Materials (AREA)
  • Ceramic Products (AREA)
US158355A 1971-06-30 1971-06-30 Process for carbonizing fibrous cellulosic material Expired - Lifetime US3689220A (en)

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JP (1) JPS5545646B1 (enrdf_load_stackoverflow)
CA (1) CA978714A (enrdf_load_stackoverflow)
DE (1) DE2232096A1 (enrdf_load_stackoverflow)
FR (1) FR2143892A1 (enrdf_load_stackoverflow)
GB (1) GB1375634A (enrdf_load_stackoverflow)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3935301A (en) * 1972-08-07 1976-01-27 Toray Industries, Inc. Process for producing carbon fibers from organic fibrous material
US4009248A (en) * 1975-04-04 1977-02-22 Japan Exlan Company Limited Process for producing carbon fibers
US20090277772A1 (en) * 2006-04-15 2009-11-12 Toho Tenax Co., Ltd. Process for Continous Production of Carbon Fibres
US20110104489A1 (en) * 2007-10-11 2011-05-05 Toho Tenax Co., Ltd. Hollow carbon fibres and process for their production

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3935301A (en) * 1972-08-07 1976-01-27 Toray Industries, Inc. Process for producing carbon fibers from organic fibrous material
US4009248A (en) * 1975-04-04 1977-02-22 Japan Exlan Company Limited Process for producing carbon fibers
US20090277772A1 (en) * 2006-04-15 2009-11-12 Toho Tenax Co., Ltd. Process for Continous Production of Carbon Fibres
US20110104489A1 (en) * 2007-10-11 2011-05-05 Toho Tenax Co., Ltd. Hollow carbon fibres and process for their production

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FR2143892A1 (enrdf_load_stackoverflow) 1973-02-09
DE2232096A1 (de) 1973-01-11
JPS5545646B1 (enrdf_load_stackoverflow) 1980-11-19
CA978714A (en) 1975-12-02
GB1375634A (enrdf_load_stackoverflow) 1974-11-27

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