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GB1214351A - Improvements in and relating to a process for forming stoichiometric carbide coatings on filaments - Google Patents

Improvements in and relating to a process for forming stoichiometric carbide coatings on filaments

Info

Publication number
GB1214351A
GB1214351A GB7446/68A GB744668A GB1214351A GB 1214351 A GB1214351 A GB 1214351A GB 7446/68 A GB7446/68 A GB 7446/68A GB 744668 A GB744668 A GB 744668A GB 1214351 A GB1214351 A GB 1214351A
Authority
GB
United Kingdom
Prior art keywords
filament
sihcl
evaporator
condenser
conduit
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
Application number
GB7446/68A
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.)
RTX Corp
Original Assignee
United Aircraft Corp
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
Application filed by United Aircraft Corp filed Critical United Aircraft Corp
Publication of GB1214351A publication Critical patent/GB1214351A/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C47/00Making alloys containing metallic or non-metallic fibres or filaments
    • C22C47/02Pretreatment of the fibres or filaments
    • C22C47/04Pretreatment of the fibres or filaments by coating, e.g. with a protective or activated covering
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/29Coated or structually defined flake, particle, cell, strand, strand portion, rod, filament, macroscopic fiber or mass thereof
    • Y10T428/2913Rod, strand, filament or fiber
    • Y10T428/2933Coated or with bond, impregnation or core
    • Y10T428/294Coated or with bond, impregnation or core including metal or compound thereof [excluding glass, ceramic and asbestos]
    • Y10T428/296Rubber, cellulosic or silicic material in coating
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/29Coated or structually defined flake, particle, cell, strand, strand portion, rod, filament, macroscopic fiber or mass thereof
    • Y10T428/2913Rod, strand, filament or fiber
    • Y10T428/2933Coated or with bond, impregnation or core
    • Y10T428/2962Silane, silicone or siloxane in coating

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Inorganic Chemistry (AREA)
  • General Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Chemical Vapour Deposition (AREA)
  • Inorganic Fibers (AREA)
  • Carbon And Carbon Compounds (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)

Abstract

1,214,351. Stoichiometric SiC coatings. UNITED AIRCRAFT CORP. 15 Feb., 1968 [24 Feb., 1967], No. 7446/68. Heading C1A. Silicon carbide is stoichiometrically deposited from the vapour phase on to a resistively heated filament by drawing the filament through a reaction zone at a temperature of 1130-1400‹ C. and exposing to a gas stream comprising CH 3 SiHCl 2 , H 2 and a hydrocarbon gas, e.g. CH 4 . The CH 3 SiHCl 2 /H 2 molar ratio is preferably between 1 : 1 and 1 : 3 and the hydrocarbon gas may comprise 15À3-57 mole per cent of the gas flow. The filament may be a boron coated wire. In the preferred embodiment, a condenser is employed to yield a mixture of fixed dew point, e.g. 12-15‹ C. using H 2 or Aq as a carrier gas. In Fig. 2, H 2 is introduced through a conduit 60, pressure regulator 62, flowmeter 64 and a valve 66 to the evaporator 68. Part of the H 2 is bubbled through CH 3 SiHCl 2 70 on the evaporator 68 and the mixture is discharged through a conduit 72 to a condenser 74. The output is fed through an inlet 10 into the reactor 4 through which the filament 2 is drawn. A portion of H 2 may bypass the evaporator and be introduced through a line 76 to a throughway valve 80 for purging and/or finer control of the H 2 content of the reactant mixture. Cooling H 2 is admitted through the inlet 8 from the condenser 82. Methane is introduced through a conduit 90, valve 92 and a flowmeter 94. Fig. 1, not shown, illustrates in more detail the construction of reactor 4.
GB7446/68A 1967-02-24 1968-02-15 Improvements in and relating to a process for forming stoichiometric carbide coatings on filaments Expired GB1214351A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US61851267A 1967-02-24 1967-02-24

Publications (1)

Publication Number Publication Date
GB1214351A true GB1214351A (en) 1970-12-02

Family

ID=24478028

Family Applications (1)

Application Number Title Priority Date Filing Date
GB7446/68A Expired GB1214351A (en) 1967-02-24 1968-02-15 Improvements in and relating to a process for forming stoichiometric carbide coatings on filaments

Country Status (5)

Country Link
US (1) US3622369A (en)
JP (1) JPS4939738B1 (en)
DE (1) DE1696621C3 (en)
FR (1) FR1568920A (en)
GB (1) GB1214351A (en)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4029844A (en) * 1973-04-24 1977-06-14 Atlantic Research Corporation Rocket nozzle comprising pyrolytic graphite-silicon carbide inserts
SE8004352L (en) * 1979-06-14 1980-12-15 Atomic Energy Authority Uk TRANSMISSION ELEMENT AND SYSTEM
US4628002A (en) * 1985-05-28 1986-12-09 Avco Corporation Silicon carbide monofilament for transverse composite properties
US4726319A (en) * 1985-10-31 1988-02-23 M&T Chemicals Inc Apparatus and method for coating optical fibers
GB8910182D0 (en) * 1989-05-04 1989-06-21 British Petroleum Co Plc Process for depositing a silicon carbide coating on a filament
GB8910181D0 (en) * 1989-05-04 1989-06-21 British Petroleum Co Plc Process for depositing a ceramic coating on a filament
US5221353A (en) * 1989-05-04 1993-06-22 The British Petroleum Company Apparatus for depositing a ceramic coating on a filament
GB9015921D0 (en) * 1990-07-19 1990-09-05 Secr Defence Coreless refractory fibres
GB2462846B (en) * 2008-08-22 2013-03-13 Tisics Ltd Coated filaments and their manufacture
GB2462843B (en) * 2008-08-22 2013-03-20 Tisics Ltd Coated filaments and their manufacture
US8993172B2 (en) 2011-12-10 2015-03-31 Kalptree Energy, Inc. Li-ion battery and battery active components on metal wire
EP3514129A1 (en) 2018-01-18 2019-07-24 Heraeus GMSI LLC Process for manufacturing a silicon carbide coated body
EP3514128A1 (en) 2018-01-18 2019-07-24 Heraeus GMSI LLC Process for manufacturing a silicon carbide coated body
EP3514257A1 (en) 2018-01-18 2019-07-24 Heraeus GMSI LLC Process for manufacturing a silicon carbide coated body
EP3514127A1 (en) 2018-01-18 2019-07-24 Heraeus GMSI LLC Process for manufacturing a silicon carbide coated body
EP3514130A1 (en) 2018-01-18 2019-07-24 Heraeus GMSI LLC Process for manufacturing a silicon carbide coated body
EP3514259A1 (en) 2018-01-18 2019-07-24 Heraeus GMSI LLC Process for manufacturing a silicon carbide coated body

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL244520A (en) * 1958-10-23
US3011912A (en) * 1959-12-22 1961-12-05 Union Carbide Corp Process for depositing beta silicon carbide
SU145106A1 (en) * 1961-05-27 1961-11-30 С.Н. Горин Silicon Carbide Coating Method
GB1106291A (en) * 1963-11-25 1968-03-13 Nat Res Dev Boron-containing materials
US3409469A (en) * 1964-03-05 1968-11-05 United Aircraft Corp Vapor coating conductive filaments utilizing uniform temperature
US3317356A (en) * 1964-03-31 1967-05-02 Texas Instruments Inc Process for applying a protective coat of silicon carbide to refractory metals
US3410715A (en) * 1965-06-28 1968-11-12 Air Force Usa Process for metal finishing boron and tungsten filaments
US3416951A (en) * 1965-07-28 1968-12-17 Air Force Usa Method for the pyrolytic deposition of silicon carbide

Also Published As

Publication number Publication date
JPS4939738B1 (en) 1974-10-28
DE1696621C3 (en) 1978-09-14
DE1696621B2 (en) 1978-01-12
FR1568920A (en) 1969-05-30
DE1696621A1 (en) 1971-11-18
US3622369A (en) 1971-11-23

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PCNP Patent ceased through non-payment of renewal fee