CH363540A - Pièce présentant une surface pourvue d'une couche de revêtement - Google Patents
Pièce présentant une surface pourvue d'une couche de revêtementInfo
- Publication number
- CH363540A CH363540A CH3396256A CH3396256A CH363540A CH 363540 A CH363540 A CH 363540A CH 3396256 A CH3396256 A CH 3396256A CH 3396256 A CH3396256 A CH 3396256A CH 363540 A CH363540 A CH 363540A
- Authority
- CH
- Switzerland
- Prior art keywords
- sep
- refractory
- part according
- carbide
- coating layer
- Prior art date
Links
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05B—SPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
- B05B7/00—Spraying apparatus for discharge of liquids or other fluent materials from two or more sources, e.g. of liquid and air, of powder and gas
- B05B7/0006—Spraying by means of explosions
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B02—CRUSHING, PULVERISING, OR DISINTEGRATING; PREPARATORY TREATMENT OF GRAIN FOR MILLING
- B02C—CRUSHING, PULVERISING, OR DISINTEGRATING IN GENERAL; MILLING GRAIN
- B02C19/00—Other disintegrating devices or methods
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B02—CRUSHING, PULVERISING, OR DISINTEGRATING; PREPARATORY TREATMENT OF GRAIN FOR MILLING
- B02C—CRUSHING, PULVERISING, OR DISINTEGRATING IN GENERAL; MILLING GRAIN
- B02C19/00—Other disintegrating devices or methods
- B02C19/06—Jet mills
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B02—CRUSHING, PULVERISING, OR DISINTEGRATING; PREPARATORY TREATMENT OF GRAIN FOR MILLING
- B02C—CRUSHING, PULVERISING, OR DISINTEGRATING IN GENERAL; MILLING GRAIN
- B02C19/00—Other disintegrating devices or methods
- B02C19/18—Use of auxiliary physical effects, e.g. ultrasonics, irradiation, for disintegrating
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D26/00—Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces
- B21D26/02—Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces by applying fluid pressure
- B21D26/06—Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces by applying fluid pressure by shock waves
- B21D26/08—Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces by applying fluid pressure by shock waves generated by explosives, e.g. chemical explosives
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F1/00—Metallic powder; Treatment of metallic powder, e.g. to facilitate working or to improve properties
- B22F1/14—Treatment of metallic powder
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
- B22F3/004—Filling molds with powder
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F7/00—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B24—GRINDING; POLISHING
- B24C—ABRASIVE OR RELATED BLASTING WITH PARTICULATE MATERIAL
- B24C5/00—Devices or accessories for generating abrasive blasts
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B30—PRESSES
- B30B—PRESSES IN GENERAL
- B30B1/00—Presses, using a press ram, characterised by the features of the drive therefor, pressure being transmitted directly, or through simple thrust or tension members only, to the press ram or platen
- B30B1/001—Presses, using a press ram, characterised by the features of the drive therefor, pressure being transmitted directly, or through simple thrust or tension members only, to the press ram or platen by explosive charges
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- C—CHEMISTRY; METALLURGY
- C03—GLASS; MINERAL OR SLAG WOOL
- C03C—CHEMICAL COMPOSITION OF GLASSES, GLAZES OR VITREOUS ENAMELS; SURFACE TREATMENT OF GLASS; SURFACE TREATMENT OF FIBRES OR FILAMENTS MADE FROM GLASS, MINERALS OR SLAGS; JOINING GLASS TO GLASS OR OTHER MATERIALS
- C03C17/00—Surface treatment of glass, not in the form of fibres or filaments, by coating
- C03C17/06—Surface treatment of glass, not in the form of fibres or filaments, by coating with metals
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- C—CHEMISTRY; METALLURGY
- C23—COATING 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
- C23C—COATING 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
- C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
- C23C4/04—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the coating material
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- C—CHEMISTRY; METALLURGY
- C23—COATING 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
- C23C—COATING 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
- C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
- C23C4/04—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the coating material
- C23C4/06—Metallic material
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- C—CHEMISTRY; METALLURGY
- C23—COATING 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
- C23C—COATING 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
- C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
- C23C4/04—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the coating material
- C23C4/10—Oxides, borides, carbides, nitrides or silicides; Mixtures thereof
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- C—CHEMISTRY; METALLURGY
- C23—COATING 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
- C23C—COATING 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
- C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
- C23C4/12—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the method of spraying
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- C—CHEMISTRY; METALLURGY
- C23—COATING 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
- C23C—COATING 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
- C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
- C23C4/12—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the method of spraying
- C23C4/126—Detonation spraying
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- C—CHEMISTRY; METALLURGY
- C23—COATING 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
- C23C—COATING 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
- C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
- C23C4/12—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the method of spraying
- C23C4/129—Flame spraying
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
- F02K7/02—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof the jet being intermittent, i.e. pulse-jet
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
- F41A1/00—Missile propulsion characterised by the use of explosive or combustible propellant charges
- F41A1/04—Missile propulsion using the combustion of a liquid, loose powder or gaseous fuel, e.g. hypergolic fuel
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- C—CHEMISTRY; METALLURGY
- C03—GLASS; MINERAL OR SLAG WOOL
- C03C—CHEMICAL COMPOSITION OF GLASSES, GLAZES OR VITREOUS ENAMELS; SURFACE TREATMENT OF GLASS; SURFACE TREATMENT OF FIBRES OR FILAMENTS MADE FROM GLASS, MINERALS OR SLAGS; JOINING GLASS TO GLASS OR OTHER MATERIALS
- C03C2217/00—Coatings on glass
- C03C2217/20—Materials for coating a single layer on glass
- C03C2217/25—Metals
- C03C2217/263—Metals other than noble metals, Cu or Hg
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- C—CHEMISTRY; METALLURGY
- C03—GLASS; MINERAL OR SLAG WOOL
- C03C—CHEMICAL COMPOSITION OF GLASSES, GLAZES OR VITREOUS ENAMELS; SURFACE TREATMENT OF GLASS; SURFACE TREATMENT OF FIBRES OR FILAMENTS MADE FROM GLASS, MINERALS OR SLAGS; JOINING GLASS TO GLASS OR OTHER MATERIALS
- C03C2218/00—Methods for coating glass
- C03C2218/10—Deposition methods
- C03C2218/17—Deposition methods from a solid phase
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- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S264/00—Plastic and nonmetallic article shaping or treating: processes
- Y10S264/72—Processes of molding by spraying
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- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S428/00—Stock material or miscellaneous articles
- Y10S428/922—Static electricity metal bleed-off metallic stock
- Y10S428/9335—Product by special process
- Y10S428/937—Sprayed metal
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- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12014—All metal or with adjacent metals having metal particles
- Y10T428/12028—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, etc.]
- Y10T428/12063—Nonparticulate metal component
- Y10T428/12139—Nonmetal particles in particulate component
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Mechanical Engineering (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Materials Engineering (AREA)
- Organic Chemistry (AREA)
- Physics & Mathematics (AREA)
- Plasma & Fusion (AREA)
- Metallurgy (AREA)
- Combustion & Propulsion (AREA)
- Food Science & Technology (AREA)
- Manufacturing & Machinery (AREA)
- General Engineering & Computer Science (AREA)
- General Chemical & Material Sciences (AREA)
- Life Sciences & Earth Sciences (AREA)
- Geochemistry & Mineralogy (AREA)
- Toxicology (AREA)
- Health & Medical Sciences (AREA)
- Fluid Mechanics (AREA)
- Composite Materials (AREA)
- Coating By Spraying Or Casting (AREA)
- Other Surface Treatments For Metallic Materials (AREA)
- Nozzles (AREA)
- Cutting Tools, Boring Holders, And Turrets (AREA)
Description
Pièce présentant une surface pourvue d'une couche de revêtement La présente invention a pour objet une pièce présentant une surface pourvue d'une couche de revê tement, selon la revendication III du brevet princi pal, c'est-à-dire présentant une surface pourvue d'une couche de revêtement formée de nombreuses, lamel les minces se recouvrant entre elles et adhérant for tement à cette surface, ces lamelles étant en une ma tière autre que celle de la pièce. Cette pièce est ca ractérisée en ce que ledit revêtement contient au moins 70 % en poids d'une substance réfractaire ayant un point de fusion supérieur à 12990 C, ladite couche de revêtement ayant une dureté supérieure à 600 à l'essai à la pyramide de diamant avec une charge de 300 g et une porosité de moins de 3 %. Le corps de la pièce peut être par exemple de métal, de verre ou de matière plastique. Le revêtement peut comprendre un métal ou alliage métallique comme liant, pour lier la substance réfractaire à elle-même et au corps à revêtir. On donne à titre d'exemple dans le tableau ci- dessous la composition des couches de revêtement de diverses formes d'exécution de la pièce selon l'inven tion, les pourcentages étant rapportés au revêtement total EMI0001.0022 <U>Substance <SEP> réfractaire <SEP> Liant</U> <tb> <I>Métaux</I> <tb> Tungstène <SEP> . <SEP> . <SEP> . <SEP> . <SEP> . <SEP> . <SEP> . <SEP> . <SEP> . <SEP> . <SEP> sans <SEP> liant <SEP> ou <SEP> Co <tb> Tantale <SEP> . <SEP> . <SEP> . <SEP> . <SEP> . <SEP> . <SEP> . <SEP> . <SEP> . <SEP> . <SEP> . <SEP> . <SEP> sans <SEP> liant <tb> Niobium <SEP> . <SEP> . <SEP> . <SEP> . <SEP> . <SEP> . <SEP> . <SEP> . <SEP> . <SEP> . <SEP> sans <SEP> liant <tb> Molybdène <SEP> . <SEP> . <SEP> . <SEP> . <SEP> . <SEP> . <SEP> . <SEP> . <SEP> sans <SEP> liant <SEP> ou <SEP> 18 <SEP> % <SEP> Co EMI0001.0023 Substance <SEP> réfractaire <SEP> Liant <tb> <I>Carbures</I> <tb> Carbure <SEP> de <SEP> tungstène <SEP> . <SEP> , <SEP> sans <SEP> liant <SEP> ou <SEP> Fe-Ni <SEP> ou <tb> (WC) <SEP> 12 <SEP> % <SEP> Co <SEP> ou <SEP> 12 <SEP> % <SEP> Ni <SEP> ou <tb> 6 <SEP> % <SEP> Cu, <SEP> 2 <SEP> % <SEP> Al <SEP> et <SEP> 6 <SEP> % <tb> Cr <SEP> ou <SEP> Cr-Mo <SEP> ou <SEP> Cr <SEP> ou <SEP> Ag. <tb> Carbure <SEP> de <SEP> titane <SEP> (TiC) <SEP> 20 <SEP> % <SEP> Co <SEP> ou <SEP> 20 <SEP> % <SEP> Ni <tb> Carbure <SEP> de <SEP> bore <SEP> (B4C) <SEP> sans <SEP> liant <SEP> ou <SEP> Fe <SEP> ou <SEP> Ni <tb> ou <SEP> Fe-Cr <tb> Carbure <SEP> de <SEP> chrome <SEP> sans <SEP> liant <SEP> ou <SEP> 25 <SEP> % <SEP> Co <tb> (Cr3C2) <SEP> .......... <SEP> ou <SEP> 25 <SEP> % <SEP> Ni <tb> Carburedetantale <SEP> (TaC) <SEP> 20 <SEP> % <SEP> Co <tb> <I>Borures</I> <tb> Borure <SEP> de <SEP> titane <SEP> (TiB2) <SEP> Fe <SEP> ou <SEP> Co-Ta <tb> Borure <SEP> de <SEP> chrome <tb> (CrB2) <SEP> .......... <SEP> 20 <SEP> % <SEP> Fe <tb> <I>Nitrures</I> <tb> Nitrure <SEP> de <SEP> titane <SEP> (TiN) <SEP> sans <SEP> liant <SEP> ou <SEP> 25 <SEP> % <SEP> Cu <tb> ou <SEP> 25 <SEP> % <SEP> Co <SEP> ou <SEP> 25 <SEP> % <SEP> Ni <tb> <I>Siliciures</I> <tb> I?isiliciure <SEP> de <SEP> molyb- <SEP> sans <SEP> liant <SEP> ou <SEP> 10 <SEP> % <SEP> Co <tb> dène <SEP> (MoSi2) <SEP> <B>....</B> <SEP> ou <SEP> 15 <SEP> % <SEP> Cr <SEP> ou <SEP> 20, <SEP> % <SEP> Si <tb> <I>Oxydes</I> <tb> Oxyde <SEP> d'aluminium <SEP> . <SEP> . <SEP> sans <SEP> liant <SEP> ou <SEP> Ni <SEP> ou <SEP> Cr <tb> Bioxyde <SEP> de <SEP> titane <SEP> <B>....</B> <SEP> sans <SEP> liant <tb> Oxyde <SEP> de <SEP> chrome <SEP> <B>....</B> <SEP> sans <SEP> liant <tb> Oxyde <SEP> de <SEP> tantale <SEP> <B>....</B> <SEP> sans <SEP> liant EMI0002.0001 Substance <SEP> réfractaire <SEP> Liant <tb> <I>Mélanges <SEP> et <SEP> alliages</I> <tb> Alliage <SEP> TiC <SEP> et <SEP> WC <SEP> . <SEP> . <SEP> Co <tb> Alliage <SEP> TiC <SEP> et <SEP> TaC <SEP> . <SEP> . <SEP> Co <tb> 50 <SEP> % <SEP> Cr, <SEP> 40 <SEP> % <SEP> Mo <SEP> et <tb> 10 <SEP> % <SEP> oxyde <SEP> de <SEP> Ta <SEP> sans <SEP> liant <tb> 50 <SEP> %- <SEP> Cr, <SEP> 40 <SEP> % <SEP> W <SEP> et <tb> 10 <SEP> % <SEP> oxyde <SEP> de <SEP> Ta <SEP> sans <SEP> liant <tb> 40 <SEP> % <SEP> CrB2 <SEP> et <tb> 40 <SEP> % <SEP> TiB2. <SEP> . <SEP> <B>......</B> <SEP> 20 <SEP> % <SEP> Ni <tb> WC, <SEP> 25 <SEP> % <SEP> Cr, <tb> 20 <SEP> % <SEP> Mo <SEP> et <SEP> 5 <SEP> % <tb> oxyde <SEP> de <SEP> Ta <SEP> <B>......</B> <SEP> sans <SEP> liant <tb> WC <SEP> et <SEP> 2,4 <SEP> % <SEP> TiB2 <SEP> . <SEP> . <SEP> 9,6 <SEP> % <SEP> Co <tb> 86,7 <SEP> % <SEP> TaC <SEP> et <tb> 13,3 <SEP> % <SEP> <B>B4C <SEP> ......</B> <SEP> sans <SEP> liant <tb> 80 <SEP> % <SEP> ZrO2 <SEP> et <tb> 20 <SEP> % <SEP> TiO2 <SEP> . <SEP> <B>.....</B> <SEP> sans <SEP> liant <tb> 65 <SEP> % <SEP> W <SEP> et <SEP> 35 <SEP> % <SEP> Mo <SEP> sans, <SEP> liant <tb> 50 <SEP> % <SEP> W <SEP> et <SEP> 25 <SEP> % <SEP> SiO2 <SEP> 25 <SEP> % <SEP> Ni Voici par exemple, comment on peut fabriquer une forme d'exécution de la pièce selon l'invention On fournit un mélange finement pulvérisé (à grandeur de particules principalement entre 10 et 40 microns) contenant environ 9 % en poids de cobalt et 4 % en poids. de carbone, le reste étant du tungstène, à raison d'environ 4,53 à 6,80 kg par heure, à un canon de détonation d'environ 1,5 m de long et ayant un diamètre interne de 2,54 cm. De l'acétylène et de l'oxygène sont fournis dans, un rap- port 1 mètre cube du premier pour 1 à 2 mètres cubes du second, à une vitesse moyenne d7en- viron 10,2 mètres cubes du mélange par heure. L'écoulement moyen de l'azote de purgeage est réglé à environ 5,1 mètres cubes à l'heure, et la fréquence d'inflammation à environ quatre à la seconde. On projette le mélange au moyen du canon sur la surface propre d'une pièce d'acier S préalablement rendue rugueuse par sablage, en plaçant cette surface à 7,6 cm de l'extrémité de sortie du canon. Il se forme ainsi sur la surface de la pièce une couche de revê tement dense et adhérente. L'épaisseur de la couche de revêtement peut aller jusqu'à 1/2 mm. Dans le cas des conditions indiquées ci-dessus, une couche de revêtement de cette épaisseur peut être appliquée à une vitesse d'environ 6,5 cm2 par minute. Le dessin. annexé montre, à un grossissement li néaire de 300, l'aspect en coupe de la forme d'exé cution obtenue de la façon décrite ci-dessus. La couche de revêtement, WC, comme on le voit au dessin, est d'une structure dense, à grains fins, en lamelles. On a constaté que la couche de revêtement de la forme d'exécution décrite ci-dessus avait une densité apparente sensiblement identique à celle de la ma tière solide appliquée, à savoir de 14,5 g/cc. La poro sité était inférieure à 1 %. L'adhérence de la couche de revêtement au support était excellente, comme l'a démontré le fait qu'il a été possible d'en enlever des parties à la meule jusque et à travers l'interface sans produire d'écaillement. Grâce aux propriétés de sa couche de revêtement, la pièce selon l'invention pourrait être avantageuse- ment une pièce devant présenter une surface non glissante (à haute friction), telle que par exemple un pilon ; une pièce devant présenter une surface d'usure de forme irrégulière, telle que par exemple une ai guille de triage du coton; une pièce devant présen ter une surface d'usure de précision, telle que par exemple un fuseau, une barre ou une broche de bru nissage ; ou une pièce de faible inertie devant pré senter une surface d'usure résistante telle qu'un guide de fibres textiles ou un élément de coussinet à billes ; ou encore une pièce rotative devant présenter une surface abrasive pour assurer son propre jeu, telle que par exemple l'élément rotatif d'un joint à labyrinthe pour turbine à gaz. La pièce selon l'invention pourrait aussi être, par exemple, une tige de noyau pour l'emboutissage et pour la frappe des monnaies, un calibre de vérifica tion, une mâchoire de concasseur, une rondelle ou une plaque de garniture d'arbre, un contact électri que, un alésoir, une lame de scie, une lame de cou teau, un siège ou une tête de soupape.
Claims (1)
- REVENDICATION Pièce présentant une surface pourvue d'une cou che de revêtement, selon la revendication III du brevet principal, caractérisée en ce que ladite couche de revêtement contient au moins 70 % en poids d'une substance réfractaire ayant un point de fusion supérieur à 1299 C, ladite couche de revêtement ayant une dureté supérieure à 600 à l'essai à la pyra mide de diamant avec une charge de 300 g et une porosité de moins de 3 %. SOUS-REVENDICATIONS 1. Pièce selon la revendication, caractérisée en ce que ladite substance réfractaire contient au moins un métal réfractaire. 2.Pièce selon la revendication, caractérisée en ce que ladite substance réfractaire contient au moins un carbure réfractaire. 3. Pièce selon la sous-revendication 2, caractéri sée en ce que ledit carbure est du carbure de bore. 4. Pièce selon la sous-revendication 2, caracté risée en ce que ledit carbure est du carbure de tungstène. 5. Pièce selon la sous-revendication 3, caracté risée en ce que ledit carbure est sous forme d'alliage. 6.Pièce selon la sous-revendication 4, caracté risée en ce que ledit carbure est sous forme d'alliage. 7. Pièce selon la sous-revendication 2, caracté risée en ce que ladite substance réfractaire contient au moins deux composants choisis dans le groupe comprenant le carbure de bore, le carbure de tungs- tène, un alliage de carbure de bore et un alliage de carbure de tungstène. 8. Pièce selon la revendication, caractérisée en ce que ladite substance réfractaire contient au moins un borure réfractaire.9. Pièce selon la revendication, caractérisée en ce que ladite substance réfractaire contient au moins un nitrure réfractaire. 10. Pièce selon la revendication, caractérisée en ce que ladite substance réfractaire contient au moins un oxyde réfractaire. 11. Pièce selon la revendication, caractérisée en ce que ladite substance réfractaire contient au moins un siliciure réfractaire.12. Pièce selon la revendication, caractérisée en ce que ladite substance réfractaire contient au moins deux composants choisis dans le groupe comprenant les carbures, borures, nitrures, oxydes et siliciures réfractaires. 13. Pièce composée selon la revendication, carac térisée en ce que ladite couche de revêtement con tient un métal ou alliage métallique liant la substance réfractaire à elle-même et au corps de la pièce.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US349856XA | 1955-03-28 | 1955-03-28 | |
US515484A US2964420A (en) | 1955-06-14 | 1955-06-14 | Refractory coated body |
CH329742T | 1956-06-05 |
Publications (1)
Publication Number | Publication Date |
---|---|
CH363540A true CH363540A (fr) | 1962-07-31 |
Family
ID=25736582
Family Applications (3)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CH329742D CH329742A (fr) | 1955-03-28 | 1952-07-01 | Procédé pour former une couche de revêtement sur une surface d'une pièce, et appareil pour la mise en oeuvre de ce procédé |
CH349856D CH349856A (fr) | 1955-03-28 | 1956-03-17 | Appareil pour former une couche de revêtement sur une surface d'une pièce |
CH3396256A CH363540A (fr) | 1955-03-28 | 1956-06-05 | Pièce présentant une surface pourvue d'une couche de revêtement |
Family Applications Before (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CH329742D CH329742A (fr) | 1955-03-28 | 1952-07-01 | Procédé pour former une couche de revêtement sur une surface d'une pièce, et appareil pour la mise en oeuvre de ce procédé |
CH349856D CH349856A (fr) | 1955-03-28 | 1956-03-17 | Appareil pour former une couche de revêtement sur une surface d'une pièce |
Country Status (8)
Country | Link |
---|---|
US (1) | US2714563A (fr) |
BE (2) | BE546121A (fr) |
CH (3) | CH329742A (fr) |
DE (1) | DE1184176B (fr) |
FR (1) | FR1058357A (fr) |
GB (3) | GB742387A (fr) |
LU (3) | LU34279A1 (fr) |
NL (1) | NL91125C (fr) |
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US1375653A (en) * | 1917-06-01 | 1921-04-19 | Quick Mclain Machine Gun Compa | Machine-gun |
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DE813360C (de) * | 1949-11-04 | 1951-09-13 | Willi Lehmann | Verfahren zur Herstellung von UEberzuegen |
-
0
- NL NL91125D patent/NL91125C/xx active
- LU LU33526D patent/LU33526A1/xx unknown
- BE BE512449D patent/BE512449A/xx unknown
- LU LU31550D patent/LU31550A1/xx unknown
- BE BE546121D patent/BE546121A/xx unknown
- LU LU34279D patent/LU34279A1/xx unknown
-
1952
- 1952-03-07 US US275332A patent/US2714563A/en not_active Expired - Lifetime
- 1952-06-11 GB GB14663/52A patent/GB742387A/en not_active Expired
- 1952-06-11 GB GB17034/54A patent/GB742458A/en not_active Expired
- 1952-06-14 FR FR1058357D patent/FR1058357A/fr not_active Expired
- 1952-06-26 DE DEU1705A patent/DE1184176B/de active Pending
- 1952-07-01 CH CH329742D patent/CH329742A/fr unknown
-
1956
- 1956-03-02 GB GB6533/56A patent/GB787222A/en not_active Expired
- 1956-03-17 CH CH349856D patent/CH349856A/fr unknown
- 1956-06-05 CH CH3396256A patent/CH363540A/fr unknown
Also Published As
Publication number | Publication date |
---|---|
BE546121A (fr) | 1900-01-01 |
LU34279A1 (fr) | |
DE1184176B (de) | 1964-12-23 |
CH329742A (fr) | 1958-05-15 |
US2714563A (en) | 1955-08-02 |
LU33526A1 (fr) | |
GB787222A (en) | 1957-12-04 |
BE512449A (fr) | 1900-01-01 |
GB742458A (en) | 1955-12-30 |
NL91125C (fr) | 1900-01-01 |
CH349856A (fr) | 1960-10-31 |
LU31550A1 (fr) | |
FR1058357A (fr) | 1954-03-16 |
GB742387A (en) | 1955-12-30 |
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