GB1393833A - Carbon fibre reinforced nickel matrix composite having an intermediate layer of metal carbide - Google Patents

Carbon fibre reinforced nickel matrix composite having an intermediate layer of metal carbide

Info

Publication number
GB1393833A
GB1393833A GB3270473A GB3270473A GB1393833A GB 1393833 A GB1393833 A GB 1393833A GB 3270473 A GB3270473 A GB 3270473A GB 3270473 A GB3270473 A GB 3270473A GB 1393833 A GB1393833 A GB 1393833A
Authority
GB
United Kingdom
Prior art keywords
fibres
metal
nickel matrix
carbon
intermediate layer
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
GB3270473A
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.)
Union Carbide Corp
Original Assignee
Union Carbide 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 Union Carbide Corp filed Critical Union Carbide Corp
Publication of GB1393833A publication Critical patent/GB1393833A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING 
    • B63B3/00—Hulls characterised by their structure or component parts
    • B63B3/13—Hulls built to withstand hydrostatic pressure when fully submerged, e.g. submarine hulls
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B41/00—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
    • C04B41/009—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone characterised by the material treated
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B41/00—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
    • C04B41/45—Coating or impregnating, e.g. injection in masonry, partial coating of green or fired ceramics, organic coating compositions for adhering together two concrete elements
    • C04B41/4584—Coating or impregnating of particulate or fibrous ceramic material
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C49/00—Alloys containing metallic or non-metallic fibres or filaments
    • C22C49/14—Alloys containing metallic or non-metallic fibres or filaments characterised by the fibres or filaments
    • D—TEXTILES; PAPER
    • D01—NATURAL OR MAN-MADE THREADS OR FIBRES; SPINNING
    • D01F—CHEMICAL FEATURES IN THE MANUFACTURE OF ARTIFICIAL FILAMENTS, THREADS, FIBRES, BRISTLES OR RIBBONS; APPARATUS SPECIALLY ADAPTED FOR THE MANUFACTURE OF CARBON FILAMENTS
    • D01F11/00—Chemical after-treatment of artificial filaments or the like during manufacture
    • D01F11/10—Chemical after-treatment of artificial filaments or the like during manufacture of carbon
    • D01F11/12—Chemical after-treatment of artificial filaments or the like during manufacture of carbon with inorganic substances ; Intercalation
    • D01F11/126—Carbides
    • H—ELECTRICITY
    • H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
    • H05B3/00—Ohmic-resistance heating
    • H05B3/10—Heating elements characterised by the composition or nature of the materials or by the arrangement of the conductor
    • H05B3/12—Heating elements characterised by the composition or nature of the materials or by the arrangement of the conductor characterised by the composition or nature of the conductive material
    • H05B3/14—Heating elements characterised by the composition or nature of the materials or by the arrangement of the conductor characterised by the composition or nature of the conductive material the material being non-metallic
    • H05B3/145—Carbon only, e.g. carbon black, graphite
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C2001/0054—Fuselage structures substantially made from particular materials
    • B64C2001/0072—Fuselage structures substantially made from particular materials from composite materials
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C2001/0054—Fuselage structures substantially made from particular materials
    • B64C2001/0081—Fuselage structures substantially made from particular materials from metallic materials
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Ceramic Engineering (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Organic Chemistry (AREA)
  • Structural Engineering (AREA)
  • Ocean & Marine Engineering (AREA)
  • General Chemical & Material Sciences (AREA)
  • Textile Engineering (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Metallurgy (AREA)
  • Inorganic Chemistry (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)
  • Chemical Or Physical Treatment Of Fibers (AREA)
  • Inorganic Fibers (AREA)
  • Electroplating Methods And Accessories (AREA)
  • Chemical Treatment Of Fibers During Manufacturing Processes (AREA)

Abstract

1393833 Coating carbon fibres by hotdipping, hot pressed fibres UNION CARBIDE CORP 9 July 1973 [10 July 1972] 32704/73 Headings C7D and C7F The bonding of carbon fibres in a nickel matrix improved by providing the fibres with a carbide layer by immersing them in a molton alloy bath comprising a metal e.g. Ti, Zr, Hfi, V, Nb, Ta, Cr, Mo, W, and Fe which reacts to form a carbide and an acid soluble metal e.g. In, Ge, Ga, Sn, Sb, Bi, Ag, Cu which does not react with carbon, and subsequently removing unreacted metal with an acid, e.g. nitric, hydrochloric or sulphuric. Ni may be deposited on the coated fibres by electrodes or electrolytre methods, thermal decomposition of carbonyls or halides or by sputtering, and the coated fibres hot pressed 700 to 1300‹C. in an atmosphere of e.g. nitrogen, argon xanon, or helium. A further metal may be applied to the Ni-coated fibres before pressing.
GB3270473A 1972-07-10 1973-07-09 Carbon fibre reinforced nickel matrix composite having an intermediate layer of metal carbide Expired GB1393833A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US27020972A 1972-07-10 1972-07-10

Publications (1)

Publication Number Publication Date
GB1393833A true GB1393833A (en) 1975-05-14

Family

ID=23030365

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3270473A Expired GB1393833A (en) 1972-07-10 1973-07-09 Carbon fibre reinforced nickel matrix composite having an intermediate layer of metal carbide

Country Status (5)

Country Link
US (1) US3796587A (en)
JP (2) JPS5224500B2 (en)
FR (1) FR2192067B1 (en)
GB (1) GB1393833A (en)
IT (1) IT989793B (en)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3894863A (en) * 1973-03-22 1975-07-15 Fiber Materials Graphite composite
US3953647A (en) * 1973-10-05 1976-04-27 United Technologies Corporation Graphite fiber reinforced metal matrix composite
US4072516A (en) * 1975-09-15 1978-02-07 Fiber Materials, Inc. Graphite fiber/metal composites
JPS5253720A (en) * 1975-10-29 1977-04-30 Hitachi Ltd Non-orientated cu-carbon fiber compoite and its manufacturing method
US4240145A (en) * 1977-12-01 1980-12-16 Nissan Motor Company, Limited Closed loop controlled auxiliary air delivery system for internal combustion engine
NO801818L (en) * 1979-07-20 1981-01-21 Conradty Nuernberg RECOVERABLE, FORM-STABLE ELECTRODE FOR HIGH TEMPERATURE USE
US4489138A (en) * 1980-07-30 1984-12-18 Sumitomo Chemical Company, Limited Fiber-reinforced metal composite material
JPS57158912A (en) * 1981-03-25 1982-09-30 Mitsubishi Electric Corp Electric contact material and method of producing same
JPH03206172A (en) * 1989-08-24 1991-09-09 Tsuboi Sewing Mach Shokai:Kk Cloth-cutting device
US4979998A (en) * 1989-10-10 1990-12-25 Union Carbide Corporation Process for forming a metal boride coating on a carbonaceous substrate
EP0492436A3 (en) * 1990-12-21 1992-10-21 Ucar Carbon Technology Corp. Silicon carbide coating process
JP4869799B2 (en) * 2006-06-16 2012-02-08 株式会社ミクニ Idle air flow control device
DE102007050289A1 (en) * 2007-10-18 2009-04-23 Heraeus Noblelight Gmbh Carbon emitter with getter
KR20100087542A (en) * 2009-01-28 2010-08-05 삼성전자주식회사 Carbon fiber coated with dilectric films and fiber-type light emitting device
JP2014033104A (en) * 2012-08-03 2014-02-20 Shinko Electric Ind Co Ltd Heat radiation component and manufacturing method of the same

Also Published As

Publication number Publication date
IT989793B (en) 1975-06-10
JPS5224500B2 (en) 1977-07-01
FR2192067B1 (en) 1976-04-30
US3796587A (en) 1974-03-12
JPS5132830A (en) 1976-03-19
FR2192067A1 (en) 1974-02-08
DE2334219B2 (en) 1976-09-09
JPS5343236B2 (en) 1978-11-17
DE2334219A1 (en) 1974-01-31
JPS4953118A (en) 1974-05-23

Similar Documents

Publication Publication Date Title
GB1393833A (en) Carbon fibre reinforced nickel matrix composite having an intermediate layer of metal carbide
GB1371889A (en) Carbon fibre reinforced nickel matrix composite having an intermediate layer of metal carbide
GB1260300A (en) IMPROVEMENTS IN OR RELATING TO THE PRODUCTION OF VAPOUR-DEPOSITED Nb3Sn CONDUCTOR MATERIAL
GB1333554A (en) Superconducting members and methods of manufacture thereof
GB1388172A (en) Metal coating of diamonds
GB1521455A (en) Fibre-reinforced metal panels and production thereof
GB1249933A (en) Improvements in diffusion metallic coating method
GB1525868A (en) Method of plating metals
GB1444886A (en) Process for the anticorrosion properties of steel coated with nickel or cobalt
GB1198360A (en) Production of composite metal products
GB1195904A (en) Process for the production of Coloured Coatings
GB1355927A (en) Process for manufacturing metallic foil
DAHSHAN The oxidation of cobalt-chromium-carbon alloys
GB1325291A (en) Methods of producing a metal and carbon fibre composite
Baskey Fiber Reinforcement of Metallic and Nonmetallic Composites
GB1146611A (en) Method of obtaining an intermetallic compound of niobium and tin in fabricated form
US3407061A (en) Metal coating process
IT1006388B (en) METALLIC COATING OF A DIAMOND
GB1358233A (en) Deposition of a silver layer on titanium or titanium-based alloy
GB1263304A (en) A method of coating, with a metallic coating obtained by metallization under vacuum, steel products such as strip, bar and wire
Mirotvorskii et al. The Interaction of Thoriated Tungsten at 1200-1600 deg C With Matrixes Based on Different Metals
US2856682A (en) Method of making silver lined steel structure
GB1342157A (en) Superconductors
IE35390B1 (en) Diamond compacts
Nishida Vacuum Deposition Film Production to Provide High Adhesive Strength

Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
732 Registration of transactions, instruments or events in the register (sect. 32/1977)
PCNP Patent ceased through non-payment of renewal fee