US3658680A - Apparatus for forming silicon carbide filaments - Google Patents

Apparatus for forming silicon carbide filaments Download PDF

Info

Publication number
US3658680A
US3658680A US852410A US3658680DA US3658680A US 3658680 A US3658680 A US 3658680A US 852410 A US852410 A US 852410A US 3658680D A US3658680D A US 3658680DA US 3658680 A US3658680 A US 3658680A
Authority
US
United States
Prior art keywords
chamber
wire
temperature
silicon carbide
oven
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
Application number
US852410A
Inventor
Christian Combe
Andre Clouet
Michel Marchal
Michel Villard
Pierre Grenier
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Thales SA
Original Assignee
Thomson CSF SA
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Priority claimed from FR6908907A external-priority patent/FR2036618A6/en
Application filed by Thomson CSF SA filed Critical Thomson CSF SA
Application granted granted Critical
Publication of US3658680A publication Critical patent/US3658680A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B82NANOTECHNOLOGY
    • B82YSPECIFIC USES OR APPLICATIONS OF NANOSTRUCTURES; MEASUREMENT OR ANALYSIS OF NANOSTRUCTURES; MANUFACTURE OR TREATMENT OF NANOSTRUCTURES
    • B82Y30/00Nanotechnology for materials or surface science, e.g. nanocomposites
    • 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
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C16/00Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
    • C23C16/22Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the deposition of inorganic material, other than metallic material
    • C23C16/30Deposition of compounds, mixtures or solid solutions, e.g. borides, carbides, nitrides
    • C23C16/32Carbides
    • C23C16/325Silicon carbide
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C16/00Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
    • C23C16/44Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the method of coating
    • C23C16/54Apparatus specially adapted for continuous coating
    • C23C16/545Apparatus specially adapted for continuous coating for coating elongated substrates
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C16/00Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
    • C23C16/56After-treatment
    • CCHEMISTRY; METALLURGY
    • C01INORGANIC CHEMISTRY
    • C01PINDEXING SCHEME RELATING TO STRUCTURAL AND PHYSICAL ASPECTS OF SOLID INORGANIC COMPOUNDS
    • C01P2002/00Crystal-structural characteristics
    • C01P2002/60Compounds characterised by their crystallite size
    • CCHEMISTRY; METALLURGY
    • 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
    • C01P2004/64Nanometer sized, i.e. from 1-100 nanometer
    • 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

Definitions

  • the present invention concerns the production of continuous filaments of silicon carbide having extremely high mechanical resistance evolved from a core of tungsten, graphite or any other material that is conductive or that may be rendered surface-conductive.
  • the invention is also concerned with a method for forming such filaments.
  • Silicon carbide filaments can be used as reinforcement elements, whether in the form of a fiber sunk in a metal or in a resin, or as a threadlike support for a variety of bases, so as to furnish composite materials having remarkable mechanical or surface properties.
  • Known techniques for obtaining continuous filaments of silicon-carbide aim at inducing the deposit of this carbide by decomposition of chemical vapors on contact with an electrically conductive wire heated to a high temperature.
  • Silicon carbide has been obtained by pyrolytic decomposition on contact with a hot tungsten wire of organo-silane vapors transported by hydrogen or mixed hydrogen-diluent gas current.
  • the diameter of the tungsten wire increases by reason of the formation of the deposit, and it is necessary to progressively increase power to heat the tungsten wire in such a way as to bring back the surface temperature of the filament to a value for which the speed of increase of the deposit is substantial.
  • Filaments obtained hitherto by this method have in crosssection a microstructure consisting of concentric Stratifications. These stratifications correspond to differences of microstructure depending on deposit conditions and in particular to temperature; each time that it is necessary to adjust the heating power in order to renew an appreciable speed in the increase of the deposit, the formation of a new layer is induced, whose structure is different from that of the immediately preceding layer.
  • This method leads to the appearance of strains between the different strata which are susceptible of causing cracks in the deposit.
  • the present invention has as its principal object improvements in this method with a view to manufacturing filaments whose structure is regular. Another object of the present invention is to provide a device for use with this method.
  • a method for making a silicon carbide filament by pyrolytic reaction of a gaseous organosilane in contact with a heated tungsten wire within a reaction zone as the wire is moved through the zone The temperature of the wire along its length within the zone as it is moved through the zone is substantially constant, and the temperature of the zone is also maintained substantially constant. It is also advantageous to keep substantially constant the gaseous composition, the discharge temperature, and the velocity of the wire through the zone.
  • a reactor for use with said method.
  • the reactor is characterized by a reaction chamber surrounded in part at least with a thermal screen and a thermal gradient oven concentric with each other and an electrolytic cell secured to and communicating with the discharge end of said chamber.
  • the gaseous mixture should flow parallel to the wire in the reaction chamber.
  • the wires surface temperature can be between about l,100 C. and about 1,400 C; preferably, variations do not exceed 30 C. along the length of the wire in the chamber.
  • the most favorable temperature in the case of a gaseous mixture charged with evaporated methyltrichlorosilane cn sicn is between about 1,200" C. and about 1,300 C.
  • it is particularly advantageous to stabilize the overall temperature of the chamber and that of the wire by controlling the wires heating current by means of temperature sensors or transducers (e.g., thermocouples) located at different selected points in the reaction chamber.
  • a thermal screen which can be made of a reflecting metal (e.g., aluminum), is placed around the reaction chamber and along an adjustable length measured from the extremity of the chamber from which the wire issues.
  • the screen has the effect of reducing inequalities of temperature along the wire which, in the absence of the screen, would be colder at the exit end of the chamber because the silicon carbide deposit would necessarily be thicker at this end.
  • the gaseous mixture can be evacuated at atmospheric pressure and be introduced under conditions closely approximating normal conditions of temperature and pressure. Nevertheless, it is advantageous to provide for thermal regulation of the chamber in which the gaseous mixture is formed.
  • the wire enters a vessel in which the electrolytic treatment is effected.
  • this arrangement is preferred, it is also possible to collect the wire on a receptor spool and subsequently subject it to electrolytic treatment.
  • This apparatus includes, with regard to deposit of silicon carbide, two cylindrical chambers l and 2 preferably of glass disposed on a more or less horizontal axis and joined to each other by the horizontal branch of a mercury trap 1:; the nonadjacent extremities of chambers 1 and 2 issue into the horizontal branches of two other mercury traps J l and J;,.
  • the mercury traps utilized here reflect a special concept, so that the temperature of the mercury can be maintained at a low value, of the order of from about 40 C. to about 60 C. and the well-known lgnitron effect can be totally eliminated here.
  • a tungsten wire issues from a reeling drum 3 and unwinds through the chambers by way of the mercury traps.
  • the wire is transformed into a silicon carbide filament in the course of its transit within deposit chamber 2, and, issuing from chamber 2 in this new state, it enters chamber 9 where it undergoes electrolytic treatment.
  • the silicon carbide filament can also be stored on a receptor spool (not shown) for subsequent introduction into structure 9.
  • the wire in chambers 1 and 2 is heated by Joule effect by means of appropriate sources of electric current (not shown), the source being connected to the wire in chamber 1 by the mercury'of traps J and J and to the wire in chamber 2 by the mercury of traps J and J Any type of electrical contact sliding on the wire can also be used to the same effect, but the mercury traps are preferable.
  • a brake (not shown) can be placed to advantage on discharge spool 3.
  • a tensioning device can be used to stretch the wire, at high temperature, so as to eliminate any torsion of the wire which could result from the way in which the wire is drawn.
  • the first chamber 1 is a chamber for cleaning the wire in an atmosphere of hydrogen. It is equipped with inlet line E connected with a hydrogen source (not shown) and exit line 5 communicating with the atmosphere.
  • the role of the first chamber 1 is to clean the surface of the tungsten wire of all grease or any organic material and to free this surface of any occluded oxygen.
  • the wire is heated to a temperature of between about 800 C. and about l,200 C. The cleaning operation is noteworthy in that the wire passes directly into the treatment chamber 2 without returning to the outside air.
  • a gaseous mixture is charged from vessel 5, which contains a liquid organo-silane, preferably methyltrichloro-silane.
  • mixture is made up of silane vapors drawn by bubbling a hydrogen current free of water vapor under normal temperature and pressure conditions into vessel 5.
  • the composition of the mixture ' is carefully controlled and kept constant by insulation of vessel 5 and thermal regulation in a thermostat controlled bath 6.
  • the gaseous mixture is passed through filter 7 before entering depositchamber 2.
  • a substantially uniform deposit of silicon carbide is formed by pyrolytic reaction of the silane-containing gaseous mixture on contact with the hot wire, the surface temperature of this wire being maintained practically constant throughout the length of the wire inside deposit chamber 2 during the entire duration of the process.
  • the temperature which depends on the silane utilized, is between about l,000 C. and about l,400 C. with a minimum variation of 30 C. between any two points of the wire.
  • the most favorable temperature used with methyltrichlorosilane is between about l,200 C. and about 1,300 C.
  • the temperature prevailing in deposit chamber 2 is likewise kept substantially constant,.as are the dynamic flow characteristics of the gaseous mixture with regard to any point of the wire within chamber 2; it has already been mentioned above that the composition and the temperature of the gaseous mixture are controlled before their entrance into chamber 2.
  • gas intake and exit lines E and S respectively, of chamber 2 are oriented so as to direct the gases along the length of the wire. This prevents local cooling in the wire and favors a stable temperature of the gaseous mixture as well as its laminar displacement around the filament.
  • the gases can be introduced in the same direction as the movement of the wire, as is indicated in the drawing by arrows, or in the opposite direction. Gas flow is best con-' ducted under normal atmospheric pressure. This is why deposit chamber 2 is surrounded, to an adjustable length counted from the wire exit end thereof, by thermal screen 8 which can, for example, be made of a reflecting metal, and by an oven having a thermal gradient. ln the area of its extension, screen 8 and oven 15 compensate for heat losses occuring by way of the walls of deposit chamber 2.
  • temperature variations along the wire can be limited so as to maintain this temperature within the limits of plus or minus 15 C.
  • a pyrometer not shown
  • thermocouples of which one (Th) is represented in the drawing.
  • a single deposit chamber 2 has been represented, by way of simplifying the figure, but it is preferred to arrange several similar deposit chambers in series.
  • the reactive gaseous mixture can be distributed in each chamber individually, but it is also possible to make the gases pass directly from one chamber to the other.
  • the number of deposit chambers and the length of each of them are directly related, the combination of the two determining the final diameter of the silicon carbide filaments produced.
  • Cleaning chamber 1 is charged with pure hydrogen containing less than about 30 parts per million (ppm) of water vapor via line E
  • Deposit chamber or chambers 2 are charged with a reactive gaseous mixture containing about 15 volumes of vaporized methyltrichlorosilane per volumes of hydrogen via line E
  • the reactive gases are passed in the direction of the wires movement at a velocity of approximately 1 meter per minute; these gases escape thereafter into the outside air through line 8;.
  • a heating current is introduced into the wire between mercury traps J, and J on the one hand, and J and 1;, on the other.
  • the temperature of the wire in cleaning chamber 1 is maintained at approximately l,250 C.
  • the temperature of the wire in deposit chamber 2 is maintained at approximately l,250 C. As soon as indications given by several thermocouples Th, of which only one is shown, placed at representative points within the deposit chamber 2 show that thermal equilibrium has been achieved within this chamber,.oven 15 is adjusted so that temperature variations along the wire will not exceed about 20 C. to about 30 C. The heating current is then regulated so that the average temperature of the wire can be as close as possible to 1,240" C. deposit chamber 2 being in thermal equilibrium.
  • thermocouples placed in deposit chamber 2 permit the regulation of the heating current so that the thermal equilibrium temperature of chamber 2 will remain practically unchanged during the entire process.
  • the final diameter of the silicon carbide filaments depends on the length of time the wire stays in the deposit chamber or chambers 2. It is usually agreed that a final diameter of the order of from about 100 to about 200 microns is a satisfactory compromise between the volume of the tungsten, the overall volume of the wire, the mechanical behavior of the silicon carbide filament and its utilization as a reinforcement element.
  • the linear speed at which the wire moves through the system can vary widely, as from a few centimeters to tens of meters per minute. Adjustment ranges and conditions for the temperature and 'gas discharge in the chambers are increasingly narrow in proportion to the increase in velocity with which the filament moves through the system.
  • the layer of silicon carbide is deposited in concentric fashion, resulting in a fairly circular cross-section in the product obtained.
  • the tungsten filament is embedded in the central portion and is more often than not decomposed into fragile carburization products.
  • the polycrystalline state of the silicon carbide deposit in forms alpha and beta-and beta-is highly pronounced, since the diameter of elementary crystallite attains values of the order of 0.025 micron.
  • the mechanical resistance of the filaments obtained depends essentially on the conditions for depositing the silicon carbide and the uniformity of the surface state. At this stage of the process, the breaking strength attains commonly average values of from about 220 to about 240 kg./mm. values due to the excellence of the surface state.
  • a suitable technique comprises mounting in series after Chambers 1 and 2, electrolysis cell 9 made up of a metallic tube 10, preferably of stainless steel, provided with two plugs 11 and 12 each of which is traversed by a capillary tube through which the wire is passed.
  • Tube 10 is carried, with regard to the wire, to a negative potential by means of a feed mechanism (not shown).
  • the wire is rolled onto a receptor spool 4 actuated by a motor (not shown).
  • Electrolyte 5% KOl-l solution Temperature: 20 C. to C.
  • Duration of contact between wire and elecrolyte 2 minutes Difference of potential between wire and tube: 12 volts.
  • breaking strengths ranging in average value between about 220 and about 240 kgJmm. are commonly observed, the breaking test being effected on samples whose length is of the order of 100 mm.
  • breaking strength commonly increases to from about 20 to about percent, and average values ranging between about 260 and about 320 kg./mm. are attained, the modulus of elasticity remaining equal on the average of 45,000 kg./mm
  • methyltrichlorosilane is preferred organosilane
  • related silanes can also be employed such as: dimethydichlorosilane and trimethylchlorosilane.
  • Apparatus for the treatment of a tungsten filament to form a silicon carbide filament comprising an elongated reaction chamber (2) having inlet and outlet means for passing a filament of tungsten therethrough, and removing the treated filament from said chamber;
  • thermal screen (8) surrounding the chamber to equalize the temperature within the chamber
  • thermocouples located within the chamber and sensing the temperature at selected locations therein, the thermocouples being connected to the thermal gradient oven to regulate the heat gradient of the oven and thus the average temperature within the oven;
  • Apparatus according to claim 1 including means (5, 6) supplying a gaseous silane mixture to the chamber, said means comprising an insulated vessel (5) and a thermostatically controlled bath (6) surrounding said insulated vessel and maintaining the temperature of said vessel constant.

Abstract

Apparatus to form silicon carbide filaments which are essentially uniform throughout their cross-section, which includes a reaction chamber, a thermal screen surrounding the reaction chamber to equalize the temperature therein, a thermal gradient oven concentric with the thermal screen and surrounding the chamber, and a plurality of thermocouples located in the chamber and sensing temperature, and controlling the oven to provide for essentially uniform temperature distribution within the oven, the chamber having inlet means for the admission of organosilane so that conversion of heated tungsten to tungsten carbide is carried out essentially at uniform temperatures throughout the entire chamber; an electrolytic cell follows the chamber in the path of the filament.

Description

United States Patent Combe et a1.
1151 3,658,680 1451 Apr. 25, 1972 [54] APPARATUS FOR FORMING SIL ICON CARBIDE F ILAMENTS [72] inventors: Christian Combe, St. Maur; Andre Clouet, Paris; Michel Mnrchal, Palaiseau; Michel Vlllard, Vitry sur Seine; Pierre Grenler,
Sceaux, all of France [73] Assignee: Thomson-CSF, Paris, France [22] Filed: Aug. 22, 1969 [21 Appl. No.: 852,410
[30] Foreign Application Priority Data Sept. 4, 1968 France... ..l65067 Mar. 26, 1969 France ..698907 [52] U.S. Cl ..204/206, 1 17/106 A, 117/106C,
[51] Int. Cl. ...B0lk 3/00, B011: [[00, C231) 3/06 [58] Field of Search ..1 18/48-49.5'; l17/107.1, 106 C;204/130, 140, 206
[56] References Cited UNITED STATES PATENTS 1,077,696 11/1913 Fuller ..'..'.'....2o4/14o 'IIIIIIIII- 1,731,269 10/ 1 929 Rich .;204/14O 3,409,469 11/1968 Kuntz ....l17/107.l
3,424,603 H1969 Schwartz ..1 17/107. 1
FOREIGN PATENTS OR APPLICATIONS 402,893 12/ l 933 Great Britain ..204/ l 40 Primary Examiner-John H. Mack Assistant Examiner-T. Tufariello Attorney-Flynn and Frishauf 1 ABSTRACT Apparatus to form silicon carbide filaments which are essentially uniform throughout their cross-section, which includes a reaction chamber, a thermal screen surrounding the reaction chamber to equalize the temperature therein, a thermal gradient oven concentric with the thermal screen and surrounding the chamber, and a plurality of thermocouples located in the chamber and sensing temperature, and controlling the oven to provide for essentially uniform temperature distribution within the oven, the chamber having inlet means for the admission of organosilane so that conversion of heated tungsten to tungsten carbide is carried out essentially at uniform temperatures throughout the entire chamber; an electrolytic cell follows the chamber in the path of the filament.
2 Claims, 1 Drawing Figure rl/pliril) APPARATUS FOR FORMING SILICON CARBIDE FILAMENTS The present invention concerns the production of continuous filaments of silicon carbide having extremely high mechanical resistance evolved from a core of tungsten, graphite or any other material that is conductive or that may be rendered surface-conductive. The invention is also concerned with a method for forming such filaments.
BACKGROUND OF THE INVENTION Silicon carbide filaments can be used as reinforcement elements, whether in the form of a fiber sunk in a metal or in a resin, or as a threadlike support for a variety of bases, so as to furnish composite materials having remarkable mechanical or surface properties.
Known techniques for obtaining continuous filaments of silicon-carbide aim at inducing the deposit of this carbide by decomposition of chemical vapors on contact with an electrically conductive wire heated to a high temperature.
Silicon carbide has been obtained by pyrolytic decomposition on contact with a hot tungsten wire of organo-silane vapors transported by hydrogen or mixed hydrogen-diluent gas current. In the course of this process, the diameter of the tungsten wire increases by reason of the formation of the deposit, and it is necessary to progressively increase power to heat the tungsten wire in such a way as to bring back the surface temperature of the filament to a value for which the speed of increase of the deposit is substantial.
Filaments obtained hitherto by this method have in crosssection a microstructure consisting of concentric Stratifications. These stratifications correspond to differences of microstructure depending on deposit conditions and in particular to temperature; each time that it is necessary to adjust the heating power in order to renew an appreciable speed in the increase of the deposit, the formation of a new layer is induced, whose structure is different from that of the immediately preceding layer.
This method leads to the appearance of strains between the different strata which are susceptible of causing cracks in the deposit.
The present invention has as its principal object improvements in this method with a view to manufacturing filaments whose structure is regular. Another object of the present invention is to provide a device for use with this method.
SUMMARY OF THE INVENTION In accordance with the invention, there is provided a method for making a silicon carbide filament by pyrolytic reaction of a gaseous organosilane in contact with a heated tungsten wire within a reaction zone as the wire is moved through the zone. The temperature of the wire along its length within the zone as it is moved through the zone is substantially constant, and the temperature of the zone is also maintained substantially constant. It is also advantageous to keep substantially constant the gaseous composition, the discharge temperature, and the velocity of the wire through the zone.
In accordance with the invention, there is also provided a reactor for use with said method. The reactor is characterized by a reaction chamber surrounded in part at least with a thermal screen and a thermal gradient oven concentric with each other and an electrolytic cell secured to and communicating with the discharge end of said chamber.
BRIEF DESCRIPTION OF THE DRAWING Advantages of the invention will become apparent to those skilled in the art from the following description considered in conjunction with the drawing which is a schematic flow diagram illustrating the preparation of a silicon carbide filament.
DESCRlPTION OF THE SPECIFIC EMBODIMENTS it is preferable that the gaseous mixture should flow parallel to the wire in the reaction chamber.
The wires surface temperature can be between about l,100 C. and about 1,400 C; preferably, variations do not exceed 30 C. along the length of the wire in the chamber. The most favorable temperature in the case of a gaseous mixture charged with evaporated methyltrichlorosilane cn sicn is between about 1,200" C. and about 1,300 C. In order to maintain the surface temperature of the wire at its proper value after thermal equilibrium has been established in the reaction chamber, it is particularly advantageous to stabilize the overall temperature of the chamber and that of the wire by controlling the wires heating current by means of temperature sensors or transducers (e.g., thermocouples) located at different selected points in the reaction chamber.
In accordance with an important characteristic of the present invention, a thermal screen, which can be made of a reflecting metal (e.g., aluminum), is placed around the reaction chamber and along an adjustable length measured from the extremity of the chamber from which the wire issues. The screen has the effect of reducing inequalities of temperature along the wire which, in the absence of the screen, would be colder at the exit end of the chamber because the silicon carbide deposit would necessarily be thicker at this end.
The gaseous mixture can be evacuated at atmospheric pressure and be introduced under conditions closely approximating normal conditions of temperature and pressure. Nevertheless, it is advantageous to provide for thermal regulation of the chamber in which the gaseous mixture is formed.
At the exit from the deposit chamber in which the coating of silicon carbide is achieved, the wire enters a vessel in which the electrolytic treatment is effected. Although this arrangement is preferred, it is also possible to collect the wire on a receptor spool and subsequently subject it to electrolytic treatment.
The method in accordance with the present invention can be executed with the apparatus represented schematically in the drawing. This apparatus includes, with regard to deposit of silicon carbide, two cylindrical chambers l and 2 preferably of glass disposed on a more or less horizontal axis and joined to each other by the horizontal branch of a mercury trap 1:; the nonadjacent extremities of chambers 1 and 2 issue into the horizontal branches of two other mercury traps J l and J;,. The mercury traps utilized here reflect a special concept, so that the temperature of the mercury can be maintained at a low value, of the order of from about 40 C. to about 60 C. and the well-known lgnitron effect can be totally eliminated here.
The extremities of the horizontal branch of the mercurycontaining glass trap J are joined to capillary tubes traversed by the wire. Capillary forces suffice to prevent any escape of mercury by way of the annular space existing between the wire and the inner wall of the capillary tube. As illustrated by the drawing, a tungsten wire issues from a reeling drum 3 and unwinds through the chambers by way of the mercury traps. As will be shown in greater detail below, the wire is transformed into a silicon carbide filament in the course of its transit within deposit chamber 2, and, issuing from chamber 2 in this new state, it enters chamber 9 where it undergoes electrolytic treatment. Alternatively, the silicon carbide filament can also be stored on a receptor spool (not shown) for subsequent introduction into structure 9.
The wire in chambers 1 and 2 is heated by Joule effect by means of appropriate sources of electric current (not shown), the source being connected to the wire in chamber 1 by the mercury'of traps J and J and to the wire in chamber 2 by the mercury of traps J and J Any type of electrical contact sliding on the wire can also be used to the same effect, but the mercury traps are preferable.
A brake (not shown) can be placed to advantage on discharge spool 3. A tensioning device can be used to stretch the wire, at high temperature, so as to eliminate any torsion of the wire which could result from the way in which the wire is drawn.
The first chamber 1 is a chamber for cleaning the wire in an atmosphere of hydrogen. It is equipped with inlet line E connected with a hydrogen source (not shown) and exit line 5 communicating with the atmosphere. The role of the first chamber 1 is to clean the surface of the tungsten wire of all grease or any organic material and to free this surface of any occluded oxygen. In chamber 1, the wire is heated to a temperature of between about 800 C. and about l,200 C. The cleaning operation is noteworthy in that the wire passes directly into the treatment chamber 2 without returning to the outside air.
A gaseous mixture is charged from vessel 5, which contains a liquid organo-silane, preferably methyltrichloro-silane. The
mixture is made up of silane vapors drawn by bubbling a hydrogen current free of water vapor under normal temperature and pressure conditions into vessel 5. The composition of the mixture 'is carefully controlled and kept constant by insulation of vessel 5 and thermal regulation in a thermostat controlled bath 6. The gaseous mixture is passed through filter 7 before entering depositchamber 2.
In accordance with the invention, a substantially uniform deposit of silicon carbide is formed by pyrolytic reaction of the silane-containing gaseous mixture on contact with the hot wire, the surface temperature of this wire being maintained practically constant throughout the length of the wire inside deposit chamber 2 during the entire duration of the process. The temperature, which depends on the silane utilized, is between about l,000 C. and about l,400 C. with a minimum variation of 30 C. between any two points of the wire. The most favorable temperature used with methyltrichlorosilane is between about l,200 C. and about 1,300 C. At the same time, the temperature prevailing in deposit chamber 2 is likewise kept substantially constant,.as are the dynamic flow characteristics of the gaseous mixture with regard to any point of the wire within chamber 2; it has already been mentioned above that the composition and the temperature of the gaseous mixture are controlled before their entrance into chamber 2.
By reason of the operating conditions, gas intake and exit lines E and S respectively, of chamber 2 are oriented so as to direct the gases along the length of the wire. This prevents local cooling in the wire and favors a stable temperature of the gaseous mixture as well as its laminar displacement around the filament.
As a modification, notably in function of the heating power of the wire, the gases can be introduced in the same direction as the movement of the wire, as is indicated in the drawing by arrows, or in the opposite direction. Gas flow is best con-' ducted under normal atmospheric pressure. This is why deposit chamber 2 is surrounded, to an adjustable length counted from the wire exit end thereof, by thermal screen 8 which can, for example, be made of a reflecting metal, and by an oven having a thermal gradient. ln the area of its extension, screen 8 and oven 15 compensate for heat losses occuring by way of the walls of deposit chamber 2. By regulation of the temperature gradient and position of oven 15 and by observing the surface temperature of the wire, for example by means of a pyrometer (not shown), temperature variations along the wire can be limited so as to maintain this temperature within the limits of plus or minus 15 C. Along the entire length of the wire in chamer 2.
When, within deposit chamber 2, overall thermal equilibrium is established, for which the wire possesses the selected temperature, this equilibrium is controlled by temperature points at various points of the chamber by means of thermocouples, of which one (Th) is represented in the drawing.
A single deposit chamber 2 has been represented, by way of simplifying the figure, but it is preferred to arrange several similar deposit chambers in series. The reactive gaseous mixture can be distributed in each chamber individually, but it is also possible to make the gases pass directly from one chamber to the other. The number of deposit chambers and the length of each of them are directly related, the combination of the two determining the final diameter of the silicon carbide filaments produced.
By way of illustration, a more detailed example is now given of the method whereby the methyltrichlorosilane is decomposed to produce a silicon carbide filament.
A tungsten wire having a diameter of from about 10 to about 20 microns and moving at a linear velocity of from about 0.2 to about 2 meters per minute, is introduced into chambers 1 and 2. Cleaning chamber 1 is charged with pure hydrogen containing less than about 30 parts per million (ppm) of water vapor via line E Deposit chamber or chambers 2 are charged with a reactive gaseous mixture containing about 15 volumes of vaporized methyltrichlorosilane per volumes of hydrogen via line E The reactive gases are passed in the direction of the wires movement at a velocity of approximately 1 meter per minute; these gases escape thereafter into the outside air through line 8;.
Wire velocityas well as composition and discharge of the gaseous mixture are kept constant.
A heating current is introduced into the wire between mercury traps J, and J on the one hand, and J and 1;, on the other. The temperature of the wire in cleaning chamber 1 is maintained at approximately l,250 C.
The temperature of the wire in deposit chamber 2 is maintained at approximately l,250 C. As soon as indications given by several thermocouples Th, of which only one is shown, placed at representative points within the deposit chamber 2 show that thermal equilibrium has been achieved within this chamber,.oven 15 is adjusted so that temperature variations along the wire will not exceed about 20 C. to about 30 C. The heating current is then regulated so that the average temperature of the wire can be as close as possible to 1,240" C. deposit chamber 2 being in thermal equilibrium.
Thereafter, the thermocouples placed in deposit chamber 2 permit the regulation of the heating current so that the thermal equilibrium temperature of chamber 2 will remain practically unchanged during the entire process.
The final diameter of the silicon carbide filaments depends on the length of time the wire stays in the deposit chamber or chambers 2. It is usually agreed that a final diameter of the order of from about 100 to about 200 microns is a satisfactory compromise between the volume of the tungsten, the overall volume of the wire, the mechanical behavior of the silicon carbide filament and its utilization as a reinforcement element.
The linear speed at which the wire moves through the system can vary widely, as from a few centimeters to tens of meters per minute. Adjustment ranges and conditions for the temperature and 'gas discharge in the chambers are increasingly narrow in proportion to the increase in velocity with which the filament moves through the system.
The layer of silicon carbide is deposited in concentric fashion, resulting in a fairly circular cross-section in the product obtained. The tungsten filament is embedded in the central portion and is more often than not decomposed into fragile carburization products. The polycrystalline state of the silicon carbide deposit in forms alpha and beta-and beta-is highly pronounced, since the diameter of elementary crystallite attains values of the order of 0.025 micron. The mechanical resistance of the filaments obtained depends essentially on the conditions for depositing the silicon carbide and the uniformity of the surface state. At this stage of the process, the breaking strength attains commonly average values of from about 220 to about 240 kg./mm. values due to the excellence of the surface state. However, despite this excellent surface state whose irregularities have a depth generally not exceeding 0.02 micron, it has been found to be advantageous to provide a super-fine finish to the filaments surface by electrolytic treatment. A suitable technique comprises mounting in series after Chambers 1 and 2, electrolysis cell 9 made up of a metallic tube 10, preferably of stainless steel, provided with two plugs 11 and 12 each of which is traversed by a capillary tube through which the wire is passed.
An electrolyte is charged to tube 10 through line 13; the electrolyte leaves tube 10 by line 14 nd is recycled to the tube by a pump (not shown). Tube 10 is carried, with regard to the wire, to a negative potential by means of a feed mechanism (not shown). At the exit of cell 9, the wire is rolled onto a receptor spool 4 actuated by a motor (not shown). For a tube of stainless steel whose diameter is approximately mm. and length 400 mm., advantageous results have been obtained under the following conditions:
Electrolyte: 5% KOl-l solution Temperature: 20 C. to C.
Duration of contact between wire and elecrolyte: 2 minutes Difference of potential between wire and tube: 12 volts.
Before subjecting the wire to this electrolytic treatment, breaking strengths ranging in average value between about 220 and about 240 kgJmm. are commonly observed, the breaking test being effected on samples whose length is of the order of 100 mm.
Following the wires electrolytic treatment, breaking strength commonly increases to from about 20 to about percent, and average values ranging between about 260 and about 320 kg./mm. are attained, the modulus of elasticity remaining equal on the average of 45,000 kg./mm
These mechanical properties explain the excellent rigidity and elasticity of the silicon carbide filament as well as ability to accept bending with very small curvature.
While methyltrichlorosilane is preferred organosilane, related silanes can also be employed such as: dimethydichlorosilane and trimethylchlorosilane.
The preceding description is given as a nonlimiting example and the present invention encompasses such variations or modifications as defined by the language of the appended claims.
What is claimed is:
1. Apparatus for the treatment of a tungsten filament to form a silicon carbide filament comprising an elongated reaction chamber (2) having inlet and outlet means for passing a filament of tungsten therethrough, and removing the treated filament from said chamber;
a thermal screen (8) surrounding the chamber to equalize the temperature within the chamber;
a thermal gradient oven (15) concentric with the thermal screen surrounding said chamber;
a plurality of thermocouples (Th) located within the chamber and sensing the temperature at selected locations therein, the thermocouples being connected to the thermal gradient oven to regulate the heat gradient of the oven and thus the average temperature within the oven;
means (1,) connected to the outlet means of the chamber to isolate the atmosphere within the chamber;
means introducing and removing gases to, and from the chamber;
and an electrolytic cell (9) located to follow, in the path of the filament, said isolating means.
2. Apparatus according to claim 1, including means (5, 6) supplying a gaseous silane mixture to the chamber, said means comprising an insulated vessel (5) and a thermostatically controlled bath (6) surrounding said insulated vessel and maintaining the temperature of said vessel constant.

Claims (1)

  1. 2. Apparatus according to claim 1, including means (5, 6) supplying a gaseous silane mixture to the chamber, said means comprising an insulated vessel (5) and a thermostatically controlled bath (6) surrounding said insulated vessel and maintaining the temperature of said vessel constant.
US852410A 1968-09-04 1969-08-22 Apparatus for forming silicon carbide filaments Expired - Lifetime US3658680A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR165067 1968-09-04
FR6908907A FR2036618A6 (en) 1969-03-26 1969-03-26 Silicon carbide whiskers prodn

Publications (1)

Publication Number Publication Date
US3658680A true US3658680A (en) 1972-04-25

Family

ID=26182207

Family Applications (1)

Application Number Title Priority Date Filing Date
US852410A Expired - Lifetime US3658680A (en) 1968-09-04 1969-08-22 Apparatus for forming silicon carbide filaments

Country Status (5)

Country Link
US (1) US3658680A (en)
BE (1) BE737899A (en)
DE (1) DE1944504A1 (en)
GB (1) GB1269540A (en)
NL (1) NL6913481A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3901182A (en) * 1972-05-18 1975-08-26 Harris Corp Silicon source feed process
US3908585A (en) * 1974-04-25 1975-09-30 Goodyear Tire & Rubber Apparatus using super-heated vapor for drying solvent-treated tire cord fabric
US3964434A (en) * 1974-11-04 1976-06-22 Technicon Instruments Corporation Coating apparatus including liquid sealant between compartments
US4109157A (en) * 1975-12-18 1978-08-22 Kawasaki Jukogyo Kabushiki Kaisha Apparatus for ion-nitriding
US4444636A (en) * 1980-06-25 1984-04-24 Siemens Aktiengesellschaft System for the galvanic deposition of metals such as aluminum
US4628002A (en) * 1985-05-28 1986-12-09 Avco Corporation Silicon carbide monofilament for transverse composite properties
US20050208737A1 (en) * 2003-01-23 2005-09-22 Sony Corporation Steam oxidation apparatus

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2934236C2 (en) * 1979-08-24 1983-02-24 Aeg-Telefunken Ag, 1000 Berlin Und 6000 Frankfurt Surge arrester with spark gap

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1077696A (en) * 1912-03-29 1913-11-04 Gen Electric Working tungsten.
US1731269A (en) * 1925-01-23 1929-10-15 Westinghouse Lamp Co Pliable tungsten and method of producing the same
GB402893A (en) * 1932-08-16 1933-12-14 Mallory & Co Inc P R Improvements in electrical make-and-break contacts and method of making same
US3409469A (en) * 1964-03-05 1968-11-05 United Aircraft Corp Vapor coating conductive filaments utilizing uniform temperature
US3424603A (en) * 1965-10-06 1969-01-28 Us Air Force Method for the manufacture of pyrolytically coated filaments

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1077696A (en) * 1912-03-29 1913-11-04 Gen Electric Working tungsten.
US1731269A (en) * 1925-01-23 1929-10-15 Westinghouse Lamp Co Pliable tungsten and method of producing the same
GB402893A (en) * 1932-08-16 1933-12-14 Mallory & Co Inc P R Improvements in electrical make-and-break contacts and method of making same
US3409469A (en) * 1964-03-05 1968-11-05 United Aircraft Corp Vapor coating conductive filaments utilizing uniform temperature
US3424603A (en) * 1965-10-06 1969-01-28 Us Air Force Method for the manufacture of pyrolytically coated filaments

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3901182A (en) * 1972-05-18 1975-08-26 Harris Corp Silicon source feed process
US3908585A (en) * 1974-04-25 1975-09-30 Goodyear Tire & Rubber Apparatus using super-heated vapor for drying solvent-treated tire cord fabric
US3964434A (en) * 1974-11-04 1976-06-22 Technicon Instruments Corporation Coating apparatus including liquid sealant between compartments
US4109157A (en) * 1975-12-18 1978-08-22 Kawasaki Jukogyo Kabushiki Kaisha Apparatus for ion-nitriding
US4444636A (en) * 1980-06-25 1984-04-24 Siemens Aktiengesellschaft System for the galvanic deposition of metals such as aluminum
US4628002A (en) * 1985-05-28 1986-12-09 Avco Corporation Silicon carbide monofilament for transverse composite properties
US20050208737A1 (en) * 2003-01-23 2005-09-22 Sony Corporation Steam oxidation apparatus
US7438872B2 (en) * 2003-01-23 2008-10-21 Sony Corporation Steam oxidation apparatus

Also Published As

Publication number Publication date
DE1944504A1 (en) 1970-03-26
BE737899A (en) 1970-02-25
NL6913481A (en) 1970-03-06
GB1269540A (en) 1972-04-06

Similar Documents

Publication Publication Date Title
US4863760A (en) High speed chemical vapor deposition process utilizing a reactor having a fiber coating liquid seal and a gas sea;
US3098763A (en) Chemical reactor
US3900540A (en) Method for making a film of refractory material having bi-directional reinforcing properties
JP4812938B2 (en) Chemical vapor deposition for the production of polycrystalline silicon rods.
US3200009A (en) Method of producing hyperpure silicon
US20020014197A1 (en) Chemical vapor deposition system for polycrystalline silicon rod production
US4859503A (en) Process for coating carbon fibers with a carbide, and carbon fibers thus coated
US3658680A (en) Apparatus for forming silicon carbide filaments
NO813770L (en) HOEYTRYKT PLASMA DISPOSAL OF SILICONE.
US3622369A (en) Process for forming stoichiometric silicon carbide coatings and filaments
GB1142080A (en) Deposition chamber for manufacture of refractory coated filaments
US4410504A (en) Method of producing high density carbon
US3399980A (en) Metallic carbides and a process of producing the same
US3637423A (en) Pyrolytic deposition of silicon nitride films
US3729335A (en) Method of depositing inorganic coatings from vapour phase
US5141595A (en) Method and apparatus for carbon coating and boron-doped carbon coating
Yarbrough et al. Diamond deposition at low substrate temperatures
US3549413A (en) Reinforcing filaments comprising coated tungsten wires
US3554782A (en) Method for depositing carbide compound
Berjonneau et al. Understanding the CVD process of (Si)–B–C ceramics through FTIR spectroscopy gas phase analysis
JPS6156162B2 (en)
EP0772699A1 (en) Diamond-phase carbon tubes and cvd process for their production
US3985917A (en) Method of depositing material on a heated substrate
US4699800A (en) Process for the production of superconducting fiber bundles
US5268062A (en) Method and apparatus for carbon coating and boron-doped carbon coating a porous refractory substrate