EP3947776A1 - Schweissverfahren mit ummantelten abrasiven teilchen, ummanteltes abrasives teilchen, schichtsystem und dichtungssystem - Google Patents

Schweissverfahren mit ummantelten abrasiven teilchen, ummanteltes abrasives teilchen, schichtsystem und dichtungssystem

Info

Publication number
EP3947776A1
EP3947776A1 EP20725084.6A EP20725084A EP3947776A1 EP 3947776 A1 EP3947776 A1 EP 3947776A1 EP 20725084 A EP20725084 A EP 20725084A EP 3947776 A1 EP3947776 A1 EP 3947776A1
Authority
EP
European Patent Office
Prior art keywords
particles
layer
abrasive particles
coated abrasive
matrix material
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.)
Pending
Application number
EP20725084.6A
Other languages
German (de)
English (en)
French (fr)
Inventor
Johannes Döhnert
Francis Ladru
Andre Mehlhorn
Thorsten Schulz
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.)
Siemens Energy Global GmbH and Co KG
Original Assignee
Siemens Energy Global GmbH and Co KG
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 Siemens Energy Global GmbH and Co KG filed Critical Siemens Energy Global GmbH and Co KG
Publication of EP3947776A1 publication Critical patent/EP3947776A1/de
Pending legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C09DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
    • C09KMATERIALS FOR MISCELLANEOUS APPLICATIONS, NOT PROVIDED FOR ELSEWHERE
    • C09K3/00Materials not provided for elsewhere
    • C09K3/14Anti-slip materials; Abrasives
    • C09K3/1436Composite particles, e.g. coated particles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F10/00Additive manufacturing of workpieces or articles from metallic powder
    • B22F10/20Direct sintering or melting
    • B22F10/25Direct deposition of metal particles, e.g. direct metal deposition [DMD] or laser engineered net shaping [LENS]
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F5/00Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product
    • B22F5/04Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product of turbine blades
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F7/00Manufacture 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
    • B22F7/06Manufacture 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 of composite workpieces or articles from parts, e.g. to form tipped tools
    • B22F7/08Manufacture 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 of composite workpieces or articles from parts, e.g. to form tipped tools with one or more parts not made from powder
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00Working by laser beam, e.g. welding, cutting or boring
    • B23K26/34Laser welding for purposes other than joining
    • B23K26/342Build-up welding
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K35/00Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K35/00Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
    • B23K35/02Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by mechanical features, e.g. shape
    • B23K35/0222Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by mechanical features, e.g. shape for use in soldering, brazing
    • B23K35/0244Powders, particles or spheres; Preforms made therefrom
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K35/00Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
    • B23K35/22Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by the composition or nature of the material
    • B23K35/24Selection of soldering or welding materials proper
    • B23K35/32Selection of soldering or welding materials proper with the principal constituent melting at more than 1550 degrees C
    • B23K35/327Selection of soldering or welding materials proper with the principal constituent melting at more than 1550 degrees C comprising refractory compounds, e.g. carbides
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C1/00Making non-ferrous alloys
    • C22C1/04Making non-ferrous alloys by powder metallurgy
    • C22C1/0433Nickel- or cobalt-based alloys
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C1/00Making non-ferrous alloys
    • C22C1/04Making non-ferrous alloys by powder metallurgy
    • C22C1/05Mixtures of metal powder with non-metallic powder
    • C22C1/051Making hard metals based on borides, carbides, nitrides, oxides or silicides; Preparation of the powder mixture used as the starting material therefor
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C32/00Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ
    • C22C32/0047Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ with carbides, nitrides, borides or silicides as the main non-metallic constituents
    • C22C32/0068Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ with carbides, nitrides, borides or silicides as the main non-metallic constituents only nitrides
    • 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
    • C23C24/00Coating starting from inorganic powder
    • C23C24/08Coating starting from inorganic powder by application of heat or pressure and heat
    • C23C24/10Coating starting from inorganic powder by application of heat or pressure and heat with intermediate formation of a liquid phase in the layer
    • C23C24/103Coating with metallic material, i.e. metals or metal alloys, optionally comprising hard particles, e.g. oxides, carbides or nitrides
    • 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
    • C23C30/00Coating with metallic material characterised only by the composition of the metallic material, i.e. not characterised by the coating process
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F10/00Additive manufacturing of workpieces or articles from metallic powder
    • B22F10/20Direct sintering or melting
    • B22F10/28Powder bed fusion, e.g. selective laser melting [SLM] or electron beam melting [EBM]
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F3/00Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/24After-treatment of workpieces or articles
    • B22F2003/241Chemical after-treatment on the surface
    • B22F2003/242Coating
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F2999/00Aspects linked to processes or compositions used in powder metallurgy
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C26/00Alloys containing diamond or cubic or wurtzitic boron nitride, fullerenes or carbon nanotubes
    • C22C2026/003Cubic boron nitrides only
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C26/00Alloys containing diamond or cubic or wurtzitic boron nitride, fullerenes or carbon nanotubes
    • C22C2026/006Alloys containing diamond or cubic or wurtzitic boron nitride, fullerenes or carbon nanotubes with additional metal compounds being carbides
    • 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02PCLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
    • Y02P10/00Technologies related to metal processing
    • Y02P10/25Process efficiency

Definitions

  • the invention relates to a welding method that uses particles, in which a hard material layer is applied around abrasive particles such as cubic boron nitride (cBN) and protects against oxidation during welding, a layer system and a sealing system.
  • abrasive particles such as cubic boron nitride (cBN)
  • the optimal gap in gas turbines or aircraft engines has a decisive influence on the efficiency and performance of these machines.
  • An established system for setting this is a rub-in layer on the housing side / stator (e.g. honeycombs) into which the rotating parts (e.g. turbine blades, rotor) rub themselves.
  • the optimum gap is ground in regardless of manufacturing tolerances, asymmetrical housing deformation, rotor displacement, etc.
  • cBN does not bond particularly well with other materials.
  • the embedding material (matrix) for the turbine area must be resistant to high temperatures. Embeddings in e.g. Resin derivatives such as those used in the manufacture of abrasives (US 2013/004938 Al) are therefore not possible.
  • US Pat. No. 8,308,830 B2 discloses coated particles made of cubic boron nitride which have two layers of coatings.
  • US 4,399,167 discloses the metallic coating of abrasive particles.
  • No. 10,183,312 B2 discloses coated abrasive particles with a soldering layer, this soldering layer representing the matrix of the layer to be produced.
  • the embedding matrix is not particularly corrosion-resistant.
  • the layer thickness cannot be set arbitrarily.
  • the object is achieved by a particle according to claim 1, a method according to claim 4, a layer system according to claim 7 and a sealing system according to claim 10.
  • the solution has three aspects:
  • the coating has increased hot gas corrosion resistance.
  • the functional layer can therefore still fulfill its function even after many hundreds of operating hours.
  • FIG. 1 shows schematically an exemplary particle that was applied in an exemplary layer system according to FIG.
  • FIG. 1 shows a coated particle 4, in particular cubic boron nitride (cBN), which has a blocky part of an abrasive material, in this case cubic boron nitride, in its interior, and has a coating 7 and thus forms the particle 1.
  • cBN cubic boron nitride
  • the abrasive particle 4 is encased in a casing 7 made of a hard material compound, such as preferably a carbide, in particular titanium carbide (TiC).
  • a hard material compound such as preferably a carbide, in particular titanium carbide (TiC).
  • Such particles 1 can be used in the build-up welding process, these coated abrasive particles 4 with the other metallic powder, preferably with one
  • Nickel-based or a cobalt-based superalloy as well a NiCoCrAlY alloy are mixed or pressed or processed in a wire that is used in build-up welding.
  • the matrix material is different from the abrasive particle 4 and its casing 7 because it is metallic, i. preferably represents a metallic alloy before.
  • a layer system 10 according to FIG. 2 can be produced, in which a component 10, preferably a turbine component, a substrate 13 has a surface 14 on which 13 or 14 has a layer 16 has been applied with the particles.
  • the particles 1 are completely in the layer 16 within the matrix or protrude from the layer 16.
  • the layer 16 is then preferably applied only to the blade tip of a turbine blade.
  • the turbine rotor blade can and generally will also have metallic and / or ceramic coatings on the blade and / or the blade platform, but these do not have the particles 1.
  • the stator or the housing of a turbine also has a protective coating into which this abrasive layer 16 rubs.
  • the coating on the housing or stator can only be metallic, only kera mixed or have a layer system of metallic adhesion promoter layer and outer ceramic layer.
  • the layers or the layer system of the housing are designed such that they are mechanically softer than the abrasive layer 16, so that grinding is possible. This can be achieved through the composition of the metallic or ceramic coating and / or also through setting the porosity of the layer or layers.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Materials Engineering (AREA)
  • Organic Chemistry (AREA)
  • Manufacturing & Machinery (AREA)
  • Metallurgy (AREA)
  • Composite Materials (AREA)
  • Physics & Mathematics (AREA)
  • Optics & Photonics (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Plasma & Fusion (AREA)
  • Other Surface Treatments For Metallic Materials (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Laser Beam Processing (AREA)
  • Polishing Bodies And Polishing Tools (AREA)
  • Mechanical Treatment Of Semiconductor (AREA)
EP20725084.6A 2019-05-20 2020-04-20 Schweissverfahren mit ummantelten abrasiven teilchen, ummanteltes abrasives teilchen, schichtsystem und dichtungssystem Pending EP3947776A1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102019207350.6A DE102019207350A1 (de) 2019-05-20 2019-05-20 Schweißverfahren mit ummantelten abrasiven Teilchen, ummanteltes abrasives Teilchen, Schichtsystem und Dichtungssystem
PCT/EP2020/060951 WO2020233919A1 (de) 2019-05-20 2020-04-20 Schweissverfahren mit ummantelten abrasiven teilchen, ummanteltes abrasives teilchen, schichtsystem und dichtungssystem

Publications (1)

Publication Number Publication Date
EP3947776A1 true EP3947776A1 (de) 2022-02-09

Family

ID=70680450

Family Applications (1)

Application Number Title Priority Date Filing Date
EP20725084.6A Pending EP3947776A1 (de) 2019-05-20 2020-04-20 Schweissverfahren mit ummantelten abrasiven teilchen, ummanteltes abrasives teilchen, schichtsystem und dichtungssystem

Country Status (6)

Country Link
US (1) US20220213366A1 (zh)
EP (1) EP3947776A1 (zh)
JP (1) JP7379535B2 (zh)
CN (1) CN113853453A (zh)
DE (1) DE102019207350A1 (zh)
WO (1) WO2020233919A1 (zh)

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ZA781390B (en) 1978-03-09 1979-04-25 De Beers Ind Diamond The metal coating of abrasive particles
US4505720A (en) * 1983-06-29 1985-03-19 Minnesota Mining And Manufacturing Company Granular silicon carbide abrasive grain coated with refractory material, method of making the same and articles made therewith
JPH03277472A (ja) * 1990-03-27 1991-12-09 Sumitomo Metal Ind Ltd ダイヤモンド砥石
JPH04202490A (ja) * 1990-11-30 1992-07-23 Sumitomo Electric Ind Ltd 被覆ダイヤモンド砥粒
US5211726A (en) * 1991-03-14 1993-05-18 General Electric Company Products and process for making multigrain abrasive compacts
US5935407A (en) * 1997-11-06 1999-08-10 Chromalloy Gas Turbine Corporation Method for producing abrasive tips for gas turbine blades
JP2001322067A (ja) * 2000-05-15 2001-11-20 Allied Material Corp 金属炭化物被覆超砥粒の製造方法、金属炭化物被覆超砥粒および超砥粒工具
JP3801452B2 (ja) * 2001-02-28 2006-07-26 三菱重工業株式会社 耐摩耗性コーティング及びその施工方法
DE102005030848A1 (de) * 2005-07-01 2007-01-11 Mtu Aero Engines Gmbh Verfahren zum Herstellen einer Schaufelspitzenpanzerung
CN103451460B (zh) * 2006-12-11 2016-08-03 六号元素(产品)(控股)公司 立方氮化硼压块
KR101372342B1 (ko) * 2007-05-04 2014-03-12 리버디 엔지니어링 리미티드 가스 터빈 부품에 연마 코팅을 제조하기 위한 방법
EP2155832A1 (en) 2007-05-22 2010-02-24 Element Six Limited Coated cbn
US20110164961A1 (en) * 2009-07-14 2011-07-07 Thomas Alan Taylor Coating system for clearance control in rotating machinery
GB201004614D0 (en) 2010-03-19 2010-05-05 Ge Healthcare Uk Ltd A system and method for automated extraction of multi-cellular physiological parameters
US8790078B2 (en) * 2010-10-25 2014-07-29 United Technologies Corporation Abrasive rotor shaft ceramic coating
US10183312B2 (en) * 2014-05-23 2019-01-22 United Technologies Corporation Abrasive blade tip treatment
US10072506B2 (en) * 2014-06-30 2018-09-11 Rolls-Royce Corporation Coated gas turbine engine components
WO2018160297A1 (en) * 2017-02-28 2018-09-07 3M Innovative Properties Company Metal bond abrasive articles and methods of making metal bond abrasive articles
GB201704133D0 (en) * 2017-03-15 2017-04-26 Element Six (Uk) Ltd Sintered polycrystalline cubic boron nitride material

Also Published As

Publication number Publication date
JP7379535B2 (ja) 2023-11-14
DE102019207350A1 (de) 2020-11-26
US20220213366A1 (en) 2022-07-07
JP2022533332A (ja) 2022-07-22
WO2020233919A1 (de) 2020-11-26
CN113853453A (zh) 2021-12-28

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