GB2319022A - Preparation of substantially polycrystalline silicon carbide fibres - Google Patents

Preparation of substantially polycrystalline silicon carbide fibres Download PDF

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GB2319022A
GB2319022A GB9226641A GB9226641A GB2319022A GB 2319022 A GB2319022 A GB 2319022A GB 9226641 A GB9226641 A GB 9226641A GB 9226641 A GB9226641 A GB 9226641A GB 2319022 A GB2319022 A GB 2319022A
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fibers
boron
weight
borosilazane
silicon carbide
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GB2319022B (en
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Duane Ray Bujalski
Gregg Alan Zank
Thomas Duncan Barnard
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Dow Silicones Corp
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Dow Corning Corp
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Priority to FR9300240A priority patent/FR2746417B1/en
Priority to DE4302211A priority patent/DE4302211C2/en
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    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B35/00Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/515Shaped 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
    • C04B35/56Shaped 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
    • C04B35/565Shaped 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 based on silicon carbide
    • C04B35/571Shaped 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 based on silicon carbide obtained from Si-containing polymer precursors or organosilicon monomers
    • CCHEMISTRY; METALLURGY
    • C01INORGANIC CHEMISTRY
    • C01BNON-METALLIC ELEMENTS; COMPOUNDS THEREOF; METALLOIDS OR COMPOUNDS THEREOF NOT COVERED BY SUBCLASS C01C
    • C01B32/00Carbon; Compounds thereof
    • C01B32/90Carbides
    • C01B32/914Carbides of single elements
    • C01B32/956Silicon carbide
    • CCHEMISTRY; METALLURGY
    • C01INORGANIC CHEMISTRY
    • C01BNON-METALLIC ELEMENTS; COMPOUNDS THEREOF; METALLOIDS OR COMPOUNDS THEREOF NOT COVERED BY SUBCLASS C01C
    • C01B32/00Carbon; Compounds thereof
    • C01B32/90Carbides
    • C01B32/914Carbides of single elements
    • C01B32/956Silicon carbide
    • C01B32/963Preparation from compounds containing silicon
    • C01B32/977Preparation from organic compounds containing silicon
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    • C01INORGANIC CHEMISTRY
    • C01PINDEXING SCHEME RELATING TO STRUCTURAL AND PHYSICAL ASPECTS OF SOLID INORGANIC COMPOUNDS
    • C01P2004/00Particle morphology
    • C01P2004/10Particle morphology extending in one dimension, e.g. needle-like
    • CCHEMISTRY; METALLURGY
    • C01INORGANIC CHEMISTRY
    • C01PINDEXING SCHEME RELATING TO STRUCTURAL AND PHYSICAL ASPECTS OF SOLID INORGANIC COMPOUNDS
    • C01P2004/00Particle morphology
    • C01P2004/60Particles characterised by their size
    • C01P2004/61Micrometer sized, i.e. from 1-100 micrometer
    • CCHEMISTRY; METALLURGY
    • C01INORGANIC CHEMISTRY
    • C01PINDEXING SCHEME RELATING TO STRUCTURAL AND PHYSICAL ASPECTS OF SOLID INORGANIC COMPOUNDS
    • C01P2006/00Physical properties of inorganic compounds
    • C01P2006/10Solid density
    • CCHEMISTRY; METALLURGY
    • C01INORGANIC CHEMISTRY
    • C01PINDEXING SCHEME RELATING TO STRUCTURAL AND PHYSICAL ASPECTS OF SOLID INORGANIC COMPOUNDS
    • C01P2006/00Physical properties of inorganic compounds
    • C01P2006/90Other properties not specified above

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Abstract

Thermally stable, substantially polycrystalline silicon carbide ceramic fibers are prepared using borosilazane resins. The method comprises spinning fibers from the resin, infusibilizing the spun fibers and pyrolyzing the spun fibers at a temperature greater than about 1700‹C. The high temperature pyrolysis reduces oxygen and nitrogen content of the fibres and compacts and re-strengthens the fibres.

Description

PREPARATION OF SUBSTANTIALLY CRYSTALLINE SILICON CARBIDE FIBERS FRQM BOROSILAZANES This invention relates to the preparation of thermally stable, substantially polycrystalline silicon carbide ceramic fibers using borosilazane resins. The method described herein provides a simple yet effective method of preparing desirable fiber at a relatively low cost.
Silicon carbide ceramic fibers are known in the art for their mechanical strength at high temperatures. Because of this property, they have found utility in numerous areas such as reinforcement for plastic, ceramic or metal matrices to produce high performance composite materials or the formation of fibrous products such as high temperature insulation, belting, gaskets and curtains.
Several methods have been developed to manufacture such fibers. For instance, it is known that organosilicon polymers may be spun into fibers, infusibilized (cured) and pyrolyzed at elevated temperatures to form a ceramified fiber. Unfortunately, this method suffers from the disadvantage that substantial amounts of oxygen and/or nitrogen are often incorporated into the fibers either directly through the polymer or indirectly by incorporation during spinning, infusibilization or ceramification. When these fibers are heated to temperatures above 1400 C., the oxygen and nitrogen is lost causing weight loss, porosity and decreased tensile strength.
Recently, polycarbosilane preceramic polymers having a Si-C skeletal structure have been used to minimize the incorporation of nitrogen and oxygen. Yajima et al. in U.S. Patents 4,052,430 and 4,100,233, for example, teach a method of producing silicon carbide fibers by spinning, infusibilizing and pyrolyzing various polycarbosilanes.
Nippon Carbon Co., moreover, utilizes this technology to produce a SiC ceramic fiber sold under the trade name NICALONtm. These fibers too, however, are known to contain about 9-15% oxygen and, thus, degrade at temperatures as low as 12000C. (see Mah et al., J. Mat. Sci. 19, 1191-1201 (1984) Borosilazanes are also known in the art. For instance, Japanese Kokai Patent No. Hei 2-84437 describes the formation of borosilazanes by reacting a silazane with a boron compound. The reference describes the resultant materials as useful in the formation of ceramics. In "International Symposium on Organosilicon Chemistry Directed Towards Material Science", Abstracts, P. 95-96, Sendai, Japan, 25-29 March (1990), the same inventors describe the use of these materials in the formation of fibers. However, since the fibers contained insufficient carbon and were only pyrolyzed up to 17000C., the resultant product is described as an amorphous silicon boron nitride fiber. The fibers claimed in the present application, on the other hand, are predominantly crystalline, silicon carbide.
European Patent No. 364,323 describes a method of forming polymers based on boron and nitrogen comprising reacting a silazane with a trihalogen borane. The resultant materials are taught therein as being useful in the formation of boron nitride ceramics, including fibers.
Takamizawa et al. in U.S. Patent 4,604,367 teach the preparation of an organoborosilicon polymer by mixing an organopolysilane with an organoborazine compound, spinning fibers and then ceramifying the fibers by heating to temperatures in the range of 900-18000C. The organoborosilicon polymer therein, however, is described as having a skeletal structure comprising Si, C, N and B compared to the Si, B and N chains of the present invention. Moreover, this reference teaches that the tensile strength of the fibers drops off dramatically when heated above 15000C. (note the graph on the cover of the reference).
U.S. Patent No. 4,910,173 granted to Niebylski describes the formation of organoborosilazane polymers by the reaction of a polysilazane with a boroxine. The reference states that the resultant materials are useful in the formation of ceramic fibers but fails to teach the methodology.
Seyferth et al., J. Am. Ceram. Soc. 73, 2131-2133 (1990) likewise teach the formation of borosilazane polymers by the reaction of silazanes with boranes. The reference teaches that the resultant materials are useful in the production of borosilicon nitride ceramic fibers.
The present inventors have now unexpectedly found that thermally stable, substantially polycrystalline SiC fibers can be formed by firing borosilazane fibers having greater than about 0.2% boron and greater than about 0.1 % free carbon incorporated therein to a temperature greater than about 17000C.
The present invention relates to a method for the preparation of thermally stable, substantially polycrystalline silicon carbide fibers. The method comprises forming a fiber from a preceramic borosilazane resin characterized by containing at least about 0.2% by weight boron and by its ceramic char containing at least about 0.1% free carbon. The fiber is infusibilized to render it non-melting and then pyrolyzed at a temperature greater than about 17000C. in a non-oxidizing environment.
The present invention also relates to silicon carbide fibers which have at least 75% crystallinity, a density of at least about 2.9 gm/cc, a very low residual oxygen content and which contain greater than 1 weight percent nitrogen.
The present invention is based on the discovery that borosilazane polymers which have at least about 0.2% by weight boron and at least about 0.1% by weight free carbon incorporated therein can be used to form substantially polycrystalline SiC fibers which retain their strength at high temperatures. These fibers have at least 75% crystallinity, a density of at least about 2.9 gm/cc and a very low residual oxygen content.
The borosilazanes used in the present invention are especially valuable precursors for such fibers since they are relatively simple and inexpensive to manufacture and can be modified to produce a char with nearly any desired stoichiometry. In addition, the use of these polymers assures a uniform distribution of boron throughout the fibers. Such uniformity avoids the boron agglomeration flaws which may occur when boron is incorporated into the fibers by other methods.
The borosilazanes useful herein are generally well known in the art and can comprise any which provide sufficient boron and carbon on pyrolysis. These can include, for instance, those described in US Patent Number 4,910,173 granted to Niebylski, those described by Funayama et al., International Symposium on Organosilicon Chemistry Directed Towards Material Science, Abstracts, P. 95-96, Sendai, Japan, 25-29 March (1990), those described by Seyferth et al., J.
Am. Ceram. Soc. 73, 2131-2133 (1990), those described by Noth, B. Anorg. Chem. Org.. Chem., 16(9), 618-21, (1961), those described by Araud et al. in European Patent No. 364,323 and those described by Funayama et al. in Japanese Kokai Patent No. 2-84437.
The method for preparing such compounds is likewise known in the art and described in the above references. The preferred method, however, comprises reacting a boron trihalide with a silazane oligomer such as (RSi(NH)l 5)x or ((CH3)3Si)2NH, wherein R is selected from the croup consisting of hydrogen, a hydrocarbon radical and a substituted hydrocarbon radical and x is an integer of 2-20.
Examples of the R groups include alkyls such as methyl, ethyl, propyl, butyl, etc., alkenyls such as allyl, vinyl, etc. and saturated or unsaturated cyclic groups such a cyclopentane, cyclohexane, cycloheptane, phenyl, etc.
Especially preferred are hydrocarbons with 1-6 carbon atoms with methyl being most preferred.
If boron tribromide is to be used in this process, the amount of the silazane oligomer should be greater than 2.7 equivalents to avoid gelation. Since such gelation may be a potential problem with the use of boron tribromide, it is more preferred to use boron trichloride. Other equivalent methods, however, are also contemplated herein. Specific methods for preparation of suitable borosilazanes are also illustrated in the examples.
The specific polymer chosen should be one which contains at least about 0.2 weight percent boron based on the total weight of the polymer. This amount of boron is necessary for the fibers to undergo a densification process which decreases porosity and strengthens the fiber. Polymers containing at least about 0.6% by weight are more preferred for this effect.
The specific polymer chosen should also yield a ceramic char in which at least about 0.1% free carbon is generated. Preferably, the polymer should yield a char having between about 0.1 and about 5 weight percent free carbon. What is meant by free carbon in this invention is the amount of free or excess carbon derived from the borosilazane during pyrolysis. The total amount of carbon in the ceramic char equals the amount of free or excess carbon plus the amount of carbon combined with silicon in the form of silicon carbide.
The amount of free carbon derived from the borosilazane is determined by pyrolysis of the borosilazane to an elevated temperature under an inert atmosphere until a stable ceramic char is obtained. For purposes of this invention, a "stable ceramic char" is defined as the ceramic char produced under an inert atmosphere at an elevated temperature which will not significantly decrease in weight upon further exposure at the elevated temperature. Normally, a stable ceramic char is produced upon pyrolysis at 1800 C.
for about 30 minutes under argon. Other elevated temperatures can be used to form the stable ceramic char but the length of exposure to the elevated temperature will need to be increased for temperatures less than 18000C. Both the ceramic yield and the silicon and carbon content of the stable ceramic char are then determined. Using a rule of mixtures, the amount of SiC and free carbon of the stable ceramic char can be calculated.
To be useful herein, the borosilazane should also preferably be 1) solid at room temperature, 2) readily spinable into small diameter fibers, and 3) infusible such that the polymer will remain in fiber form during pyrolysis.
More preferably, I) the solid polymers have softening points less than about 100 C. so that they are readily extrudable for conventional fiber spinning techniques and II) the polymers have Si-H functional groups for faster cure rates.
Alternatively, a liquid borosilazane may be utilized to spin the fibers. However, when fibers are spun in this manner, they are generally solidified by rapid curing immediately after exiting the spinning apparatus.
The borosilazanes may, however, be formed into fibers by any conventional spinning technique. For instance, techniques such as melt spinning, dry spinning or wet spinning may all be used in the practice of this invention.
The spun fibers formed in this manner are generally drawn to diameters of less than about 100 micrometers. More preferably, the fibers are drawn to diameters of about 10-50 micrometers. Fibers of this size are generally more flexible than larger fibers and, thus, can be more readily woven into reinforcing matrices for composite materials.
The fibers formed above are then infusibilized to prevent melting during pyrolysis. The fibers may be infusibilized, for example, by exposure to various gases such as HC1, HCl/moist air, HCl/ammonia, boron trichloride/ammonia, borane or chlorine/ammonia. The concentration of HC1 used is generally in the range of about 0.1 to about 50 weight percent, the concentration of water is generally in the range of about 0.1 to about 20 weight percent, the concentration of ammonia gas is in the range of 0.1 to 50 weight percent, the concentration of boron trichloride is in the range of 0.1 to 20 weight percent, the concentration of borane is in the range of 0.01 to 20 weight percent and the concentration of chlorine gas is in the range of 0.1 to 50 weight percent. Generally, the fibers are cured at temperatures in the range of about room temperature to about 4000 C. in a time of from about less than a second to several hours. For example, times of from about 0.1 second to about 6 hours may be used.
If enough boron is not incorporated into the initial polymer, additional boron may be incorporated into the fibers during infusibilization or the early stages of pyrolysis. This can be accomplished, for instance, by exposing the fiber to a boron containing gas such as diborane, a boron halide, diborane, boron hydrides, borazine and/or trichloroborazine.
After infusibilization, the fibers are pyrolyzed by heating to temperatures greater than about 17000C. and preferably at temperatures of about 1800-19000C. in a non-oxidizing environment (eg., argon, vacuum, etc.). The present inventors have found that most of the oxygen and nitrogen are eliminated from the fibers at temperatures above about 14000C. which is believed to result in an initial weakening of the fiber. However, when an appropriate amount of boron is incorporated into fibers and said fibers are pyrolyzed above about 17000C., it is believed the fibers undergo a densification process which decreases porosity and strengthens the fiber. Temperatures in excess of about 20000C. are not preferred as there is undesirable grain size growth of the silicon carbide ceramic which adversely affects fiber strength.
The fibers are heated at the desired temperature for a time sufficient to reduce the oxygen content of the fibers to below about 0.5Z by weight. For example, if the fibers are heated to about 18000C., it has been found that temperature should be maintained for about 1 hour.
During this pyrolysis step, the nitrogen content of the fiber is also lowered. However, since some residual amounts of nitrogen (i.e., up to about 3 weight percent) typically remain in the fibers, it is postulated that a portion of the boron is present as boron nitride.
The ceramic fibers which result from the process of this invention have at least 75% crystallinity and have a density of at least about 2.9 gm/cc, which represents about 90-95% of the theoretical density of SiC. The fibers also have a smooth surface structure and a grain size less than 0.5 micrometers, typically less thail 0.2 micrometers.
Virtually all of the oxygen originally present in, or introduced into, the fibers is removed by the high temperature pyrolysis step and the nitrogen, other than that present as boron nitride, is also lost. Less than about 0.5% and preferably less than about 0.2%, by weight oxygen remains and generally less than about 3% nitrogen remains.
The following non-limiting examples are included in order that one skilled in the art may more readily understand the invention.
In the following examples, Ph = phenyl, Me = Methyl and HMDZ = hexamethyldisilazane.
Carbon and nitrogen analyses were carried out on a CEC 240-XA elemental analyzer. Silicon and boron were determined by a fusion technique which consisted of converting the material to soluble forms of silicon and boron and analyzing the solute for total silicon or boron by atomic absorption spectrometry.
Gel permeation chromatography (GPC) data were obtained on a Waters GPC equipped with a model 600E systems controller, a model 490 W and model 410 Differential Defractometer detectors; all values are relative to polystyrene.
All furnace firings were done in a 2 inch Lindberg tube furnace, a two inch Astro furnace or a six inch Vacuum Industries hot press on graphite foil fiber holders.
Example 1 To prepare a polymer having the formula (PhSi(NH)1.15)0.35(MeSi(NH)1.)0.55(B(NH)1.5)0.1 HMDZ, 362.25 g (2.25 moles) and xylene, 100 g, were placed in a 1 L three necked flask under an argon atmosphere. The flask was fitted with an addition funnel, an overhead stirrer and the argon inlet. The addition funnel was charged with 74 g (0.35 mole) of PhSiC13 and 82.2 g (0.55 mole) of MeSiC13 under argon. The chlorosilane mixture was then added to the HMDZ solution dropwise over a 30 minute period with stirring.
The addition funnel was replaced with a water cooled condenser and the reaction refluxed at 800C. for 20 hours.
The mixture was then cooled to ambient temperature and the condenser replaced with a rubber septum. BBr3 was added (24.8 g, 0.1 mole) via a syringe through the septum over a 10 minute period. This addition resulted in an exotherm and the formation of a milky white suspension. After stirring for 2 hours at ambient temperature, the septum was replaced with a distillation head and the mixture heated to 1700C. over 145 minutes with overhead volatiles beginning at 700C. The warm resin was then quenched with xylene (100 g) and the resulting solution was heated to 2150C. and held for 45 minutes. The warm resin was again quenched with 100 g xylene, allowed to cool and filtered through a medium glass frit. The filtrate was placed in a 500 mL three necked flask fitted with an argon inlet, overhead stirrer and a distillation head connected to a receiver which was cooled in dry ice. The filtrate was stripped for 90 minutes at 2350C. at 10 mm Hg.
The above synthesis yielded 103 g of a brittle resin which is characterized in Table 2.
The above resin (5.9 g) was powdered, using a mortar and pestle and pressed into a spinning evaluation rod using 300 psi in a stainless steel rod mold. The rod sample was loaded into an Ultraspin apparatus. This apparatus heated the polymer and mechanically fed controlled, small amounts of molten polymer through a small diameter orifice.
Once extruded, the filament fell through a draw down zone in which the atmosphere was controlled to allow the option of introducing and removing cure gases. The filaments were collected on a drum rotated at a controlled speed located in an inert take-up chamber.
Fibers were spun at varying temperatures, extrusion rates and take-up speeds. Spinning conditions of 1420C., extrusion rate of 0.0136 g/min and take-up speed of 40 m/min resulted in spinning 19 micron diameter fibers. Spinning conditions of 1420C., extrusion rate of 0.0136 g/min and take-up speed of 70 m/min resulted in spinning 14 micron diameter fibers. Spinning conditions of 1410C., extrusion rate of 0.0208 g/min, take-up speed of 40 m/min and 10% flow of HC1 gas into and out of the draw down zone resulted in spinning 24 micron diameter fibers.
Portions of fiber spun by the above technique (20-80mg; 1420C., extrusion rate of 0.0136 g/min and take-up speed of 40 m/min) were cured in a sealed chamber designed to allow inert transfer and mounting of the fiber samples. The fiber sample was mounted in the chamber and the desired cure gas(s) admitted through a stopcock. The cured fibers were then pyrolyzed at the desired temperature. The following cure/pyrolysis conditions were used: i) 60 mg of the fiber was exposed to 20% HC1 for 10 minutes and then pyrolyzed at 30C./min to 12000C. under argon. The fiber retained its shape.
ii) 108 mg of the fiber was exposed to 20% HC1 for 10 minutes and then 10% moist air for 5 minutes. The sample was then pyrolyzed at 30C./min to 12000C. under argon (46.7% yield). The fiber retained its shape and had a tensile strength of 38 ksi.
iii) 30 mg of the fiber was exposed to 20% C12 for 18 hours and then pyrolyzed at 0.750C./min to 2000C. under 50%ammonia/50%nitrogen, 1.70C./min to 8000C. under argon and 30C./min to 12000C. under argon. The fiber retained its shape and had a tensile strength of'31 ksi.
iv) 26 mg of the fiber was exposed to 0.2% borane and pyrolyzed at 1OC./min to 2000C. (held at 750C. for 45 min) and then at 30C./min to 12000C. under argon (60.4% yield).
The fiber retained its shape and had a tensile strength of 65 ksi.
v) 30 mg of the fiber was exposed to 5% BC13 for 10 minutes, exposed to 5070ammonia/50%nitrogen while pyrolyzed at 0.75 C./min to 1500C., pyrolyzed at 0.750C./min under nitrogen to 2000C., pyrolyzed at 1.70C./min to 8000C. under argon and 3DC./min to 12000C. under argon. The fiber retained its shape and had a tensile strength of 44 ksi.
Portions of the on line HC1 exposed fibers (1410C., extrusion rate of 0.0208 g/min, take-up speed of 40 m/min and 10% flow of HC1 gas into and out of the draw down zone) were batch exposed to 10% moist air for 5 minutes and pyrolyzed at 30C./min to 1200, 1800, 1900 and 20000C. under argon. The results are summarized in the following table.
Table 1 Temp( C) Char Yield Carbon Nitrogen Result 1200 NA NA NA Shape retention 123 ksi 1800 36.1 wt% 36.7 wt% 2.2 wt% beta-SiC 1900 36.8 wt% 36.4 wt% 1.1 wt% beta-SiC 2000 36.4 wt% 45.3 wt% 0.1 wt% beta-SiC 2000 36.4 wt% 35.6 wt% 1.4 wt% beta-SiC **** uncured borosilazane polymer NA = Not Available Example 2 A polymer having the formula (PhSi(NH)l 5)0 25(Mesi(NH)1.5)0.65(B(NH)1-5)0 1 was formed in the same manner as example 1 except the reactants comprised 435 g (2.7 mole) of HMDZ, 53 g (0.25 mole) PhSiC13, 97 g (0.65 mole) MeSiC13 and 24.8 g (0.1 mole) BBr3. The resultant product is characterized in Table 2.
The above resin (5.7 g) was powdered, using a mortar and pestle and pressed into a spinning evaluation rod using 300 psi in a stainless steel rod mold. The rod sample was loaded into the Ultraspin apparatus of Example 1. Fibers were spun at varying temperatures, extrusion rates and take-up speeds. Spinning conditions of 1430C., extrusion rate of 0.0208 g/min and take-up speed of 40 m/min resulted in spinning 0.1 g 24 micron diameter fibers. Spinning conditions of 1430C., extrusion rate of 0.0154 g/min, take-up speed of 40 m/min and 10% flow of HCl gas into and out of the draw down zone resulted in spinning 0.4 g of 22 micron diameter fibers.
Portions of the on line HC1 exposed fibers (1430C., extrusion rate of 0.0154 g/min, take-up speed of 40 m/min and 10% flow of HC1 gas into and out of the draw down zone) were batch exposed to 10% moist air for 8 minutes and pyrolyzed at 30C./min to 12000C. under nitrogen to yield a fiber that retained its shape and had 58.3 wt % yield.
Portions of the on line HC1 exposed fibers (1430C., extrusion rate of 0.0154 g/min, take-up speed of 40 m/min and 10% flow of HC1 gas into and out of the draw down zone) were batch exposed to 10% moist air for 8 minutes and pyrolyzed at 30C./min to 12000C. and 100C./min to 18000C. under argon to yield a fiber that retained its shape and had 34.2 wt % yield.
Portions of the on line HC1 exposed fibers (1430C., extrusion rate of 0.0154 g/min, take-up speed of 40 m/min and 10% flow of HC1 gas into and out of the draw down zone) were pyrolyzed at 30C./min to 12000C. under nitrogen to yield a fiber that retained its shape, had 61.7 wt % yield and tensile strength of 81 ksi.
Table 2 Characterization of Borosilazanes Ex Tg Mn Mw Char Wt % Wt % Wt % Wt % No C Yield C N B Si 1 77 1468 8590 36.4 35.6 1.37 2.3 57.9 2 79 1772 10974 37.1 32.7 0.8 Example 3 To prepare a polymer having the formula (PhSi(NH)1.5)0.30(HSi(NH)l.5)o.6o(B(NH)l.5)0.1 HMDZ, 3864.0 g (24.0 moles) was placed in a 12 L four necked flask under an argon atmosphere. The flask was fitted with an addition funnel, an overhead stirrer and the argon inlet.
The addition funnel was charged with 634.1 g (3.0 moles) of PhSiCl3. The chlorosilane was then added to the HMDZ dropwise over a 30 minute period with stirring. The addition funnel was replaced with a water cooled condenser and the reaction refluxes at 900C. for 60 hours. The mixture was then cooled to ambient temperature and the condenser replaced with an addition funnel and a solution of 813.2 g (6.0 moles) HSiCl3 in 501 g xylene was added over a 30 minute period BC13 was added (117.4 g, 1.0 mole) then added to the mixture over a 45 minute period. This addition resulted in an exotherm and the formation of a milky white suspension.
After stirring for 20 hours at ambient temperature, the addition funnel was replaced with a distillation head and the reaction heated to 1900C. over 7 hours with overhead volatiles beginning at 700C. The warm resin was then quenched with xylene (1000 g) and the resulting solution was filtered through a medium glass frit. The filtrate was filtered, bodied and stripped to yield the final product.
This product had a Tg of 820C., Mn of 1822, Mw of 6260, char yield (at 20000C.) of 45.3 weight percent and the following chemical composition: C = 94 weight percent, N = 0.21 weight percent and SiH = 0.123 weight percent.
The above resin was melted and mechanically fed through a multifilament spinning apparatus having 200 14 mM diameter orifices. The molten polymer was fed at 2.5 g/min and pulled down approximately 12 feet to a take up spool affording a 200 filament tow. Over the course of the 12 feet, some of the fibers were exposed to HC1 followed by moist inert gas. 35 micron cured and uncured fibers were thus produced.
Portions of the uncured fiber spun by the above technique were cured in a sealed chamber by exposure to HC1, BC13 or C12 followed by exposure to ammonia. The cured fibers were then pyrolyzed in 2 steps - first to 12000C. and then to 18000C. The following table provides the results: Table 3 Cure Post Treat* Char Yield Tensile StrenRth lZHCl/NH3 yes 47.4 99ksi l%HCl/NH3 no 33.4 2iksi 2%Bcl3/NH3 yes 49.7 lOOksi 2%C12/NH3 yes 22.3 *-heated to 2000C. at 0.750C./min under argon Portions of the on line HC1 exposed fibers were post cured at 1.1OC./min to 2000C. under vacuum (A) or at 0.750C./min to 2000C. under vacuum. The post cured samples were pyrolyzed under argon in either a one step or 2-step process. All of the fibers retained their shape. The results are summarized in the following table: Table 4 Post Pyrolysis Char ZHC1 %H20 Cure type/temp Yield %C / %N Tensile Strength 1.8 1.8 A 1 step/1800 45.6 28.9/1.25 3.0 1.8 A 1 step/1800 48.1 29.7/4.12 4.5 1.8 B 1 step/1200 72.7 NA 270 ksi 4.5 1.8 B 2 step/1800 48.5 33.8/0.36 75 ksi* 4.5 1.8 B 2 step/1800 43.7 34.4/1.61 4.5 1.8 A 1 step/1800 40.9 27.5/0.17 118 ksi * 98 weight percent beta SiC by x-ray diffraction

Claims (5)

Claims:
1. A process for the preparation of substantially polycrystalline silicon carbide fibers comprising: forming fibers from 'a preceramic polymer comprising a borosilazane resin characterized by containing at least about 0.2Z by weight boron and by its ceramic char containing at least about 0.1% by weight free carbon; infusibilizing said fibers; and pyrolyzing said fibers at a temperature greater than about 17000C. in a nonoxidizing environment.
2. The process of claim 1 additionally comprising incorporating boron into the fibers during infusibilization or the early stages of pyrolysis by exposure to a boron containing gas.
3. The process of claim 1 wherein the borosilazane has between about 0.1 and about 5% by weight free carbon incorporated therein.
4. A method of infusibilizing borosilazane fibers comprising exposing the fibers to an atmosphere comprising gases selected from the groupaconsisting of HC1, HC1 followed by water, HCl followed by ammonia, boron trichloride followed by ammonia, borane and chlorine followed by ammonia.
5. A process according to claim 4 in which the fibres have a nitrogen content of less than 3 weight percent.
5. Substantially polycrystalline silicon carbide fibers having at least about 75% crystallinity, a density of at least about 2.9 g/cc, less than about 0.5 % by weight oxygen and a nitrogen content of greater than 1 weight percent nitrogen.
Claims:
1. A process for the preparation of substantially polycrystalline silicon carbide fibers comprising: forming fibers from a preceramic polymer comprising a borosilazane resin characterized by containing at least 0.2% by weight boron and by its ceramic char containing at least 0.1% by weight free carbon; infusibilizing said fibers; and pyrolyzing said fibers at a temperature greater than 17000C. in a nonoxidizing environment.
2. The process of claim 1 additionally comprising incorporating boron into the fibers during infusibilization or the early stages of pyrolysis by exposure to a boron containing gas.
3. The process of claim 1 wherein the borosilazane has between 0.1 and 5% by weight free carbon incorporated therein.
4. A process according to any of claims 1 to 3 in which said substantially polycrystalline silicon carbide fibres prepared additionally have at least about 75k crystallinity, a density of at least 2.9 g/cc, less than 0.5k by weight oxygen and a nitrogen content of greater than 1 weight percent nitrogen.
GB9226641A 1992-12-22 1992-12-22 Preparation of substantionally crystalline silicon carbide fibers from borosilazanes Expired - Fee Related GB2319022B (en)

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GB9226641A GB2319022B (en) 1992-12-22 1992-12-22 Preparation of substantionally crystalline silicon carbide fibers from borosilazanes
CA002086266A CA2086266A1 (en) 1992-12-22 1992-12-24 Preparation of substantially crystalline silicon carbide fibers from borosilazanes
FR9300240A FR2746417B1 (en) 1992-12-22 1993-01-13 PREPARATION OF SUBSTANTIALLY CRYSTALLINE SILICON CARBIDE FIBERS FROM BOROSILAZANES
DE4302211A DE4302211C2 (en) 1992-12-22 1993-01-27 Process for the production of essentially polycrystalline silicon carbide fibers

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GB9226641A GB2319022B (en) 1992-12-22 1992-12-22 Preparation of substantionally crystalline silicon carbide fibers from borosilazanes
CA002086266A CA2086266A1 (en) 1992-12-22 1992-12-24 Preparation of substantially crystalline silicon carbide fibers from borosilazanes
FR9300240A FR2746417B1 (en) 1992-12-22 1993-01-13 PREPARATION OF SUBSTANTIALLY CRYSTALLINE SILICON CARBIDE FIBERS FROM BOROSILAZANES
DE4302211A DE4302211C2 (en) 1992-12-22 1993-01-27 Process for the production of essentially polycrystalline silicon carbide fibers

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JPS51126300A (en) * 1975-04-26 1976-11-04 Res Inst Iron Steel Tohoku Univ Method for manufacturing an organoo silicon polymer having silicon and carbon atoms as main skeleton component
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GB9226641D0 (en) 1997-04-09
DE4302211A1 (en) 1997-09-04
FR2746417B1 (en) 1998-07-24
FR2746417A1 (en) 1997-09-26
CA2086266A1 (en) 1997-03-12
GB2319022B (en) 1998-09-02
DE4302211C2 (en) 2001-10-04

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