PL3320127T3 - Zgodna z konturem warstwa ochronna dla elementów konstrukcyjnych sprężarek turbin gazowych - Google Patents

Zgodna z konturem warstwa ochronna dla elementów konstrukcyjnych sprężarek turbin gazowych

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Publication number
PL3320127T3
PL3320127T3 PL16731546.4T PL16731546T PL3320127T3 PL 3320127 T3 PL3320127 T3 PL 3320127T3 PL 16731546 T PL16731546 T PL 16731546T PL 3320127 T3 PL3320127 T3 PL 3320127T3
Authority
PL
Poland
Prior art keywords
contour
protective coating
gas turbines
compressor components
following protective
Prior art date
Application number
PL16731546.4T
Other languages
English (en)
Inventor
Michael Annen
Jochen Barnikel
Arturo Flores Renteria
Andrei Ghicov
Sascha HESSEL
Torsten Neddemeyer
Jürgen RAMM
Original Assignee
Siemens Aktiengesellschaft
Oerlikon Surface Solutions Ag, Pfäffikon
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 Aktiengesellschaft, Oerlikon Surface Solutions Ag, Pfäffikon filed Critical Siemens Aktiengesellschaft
Publication of PL3320127T3 publication Critical patent/PL3320127T3/pl

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    • C—CHEMISTRY; METALLURGY
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    • C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/22—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the process of coating
    • C23C14/24—Vacuum evaporation
    • C23C14/32—Vacuum evaporation by explosion; by evaporation and subsequent ionisation of the vapours, e.g. ion-plating
    • C23C14/325—Electric arc evaporation
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    • C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
    • C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
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    • C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
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    • C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/02—Pretreatment of the material to be coated
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    • C23C14/08—Oxides
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    • 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
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    • C23C14/14—Metallic material, boron or silicon
    • C23C14/16—Metallic material, boron or silicon on metallic substrates or on substrates of boron or silicon
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    • C23C14/06—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the coating material
    • C23C14/14—Metallic material, boron or silicon
    • C23C14/16—Metallic material, boron or silicon on metallic substrates or on substrates of boron or silicon
    • C23C14/165—Metallic material, boron or silicon on metallic substrates or on substrates of boron or silicon by cathodic sputtering
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    • C23C28/3215—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer with at least one metal alloy layer at least one MCrAlX layer
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    • C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
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    • C23C28/322—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer only coatings of metal elements only
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    • C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
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    • C23C28/345—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates with at least one oxide layer
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    • C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
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    • F04D29/32—Rotors specially for elastic fluids for axial flow pumps
    • F04D29/321—Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
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    • F04D29/00—Details, component parts, or accessories
    • F04D29/26—Rotors specially for elastic fluids
    • F04D29/32—Rotors specially for elastic fluids for axial flow pumps
    • F04D29/38—Blades
    • F04D29/388—Blades characterised by construction
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/30—Manufacture with deposition of material
    • F05D2230/31—Layer deposition
    • F05D2230/311—Layer deposition by torch or flame spraying
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/30—Manufacture with deposition of material
    • F05D2230/31—Layer deposition
    • F05D2230/312—Layer deposition by plasma spraying
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/30—Manufacture with deposition of material
    • F05D2230/31—Layer deposition
    • F05D2230/313—Layer deposition by physical vapour deposition

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Materials Engineering (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Inorganic Chemistry (AREA)
  • General Engineering & Computer Science (AREA)
  • Ceramic Engineering (AREA)
  • Physical Vapour Deposition (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Coating By Spraying Or Casting (AREA)
  • Laminated Bodies (AREA)
  • Other Surface Treatments For Metallic Materials (AREA)
PL16731546.4T 2015-07-06 2016-06-14 Zgodna z konturem warstwa ochronna dla elementów konstrukcyjnych sprężarek turbin gazowych PL3320127T3 (pl)

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DE102015212588.2A DE102015212588A1 (de) 2015-07-06 2015-07-06 Konturtreue Schutzschicht für Verdichterbauteile von Gasturbinen
PCT/EP2016/063557 WO2017005460A1 (de) 2015-07-06 2016-06-14 Konturtreue schutzschicht für verdichterbauteile von gasturbinen

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KR (1) KR102568312B1 (pl)
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BR (1) BR112018000215B1 (pl)
CA (1) CA2990731C (pl)
DE (1) DE102015212588A1 (pl)
HU (1) HUE059675T2 (pl)
MX (1) MX2018000192A (pl)
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DE102016125042A1 (de) * 2015-12-28 2017-06-29 Oerlikon Surface Solutions Ag, Pfäffikon Infrarotspiegel mit einer thermisch stabilen Schicht
US10294962B2 (en) * 2017-06-30 2019-05-21 United Technologies Corporation Turbine engine seal for high erosion environment
JP7162336B2 (ja) * 2017-10-20 2022-10-28 国立大学法人東北大学 ナノ粒子およびナノ粒子の製造方法
EP3728695B1 (de) 2017-12-22 2022-08-03 Oerlikon Surface Solutions AG, Pfäffikon Korrosions- und erosionsbeständige beschichtung für turbinenschaufeln von gasturbinen
KR20230116003A (ko) 2020-12-02 2023-08-03 외를리콘 서피스 솔루션즈 아게, 페피콘 Al-Si 부식 방지 코팅
US20240026793A1 (en) * 2020-12-15 2024-01-25 Oerlikon Surface Solutions Ag, Pfäffikon Coating for thermally and abrasively loaded turbine blades

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US4873152A (en) * 1988-02-17 1989-10-10 Air Products And Chemicals, Inc. Heat treated chemically vapor deposited products
US5714202A (en) 1995-06-07 1998-02-03 Lemelson; Jerome H. Synthetic diamond overlays for gas turbine engine parts having thermal barrier coatings
US6620525B1 (en) * 2000-11-09 2003-09-16 General Electric Company Thermal barrier coating with improved erosion and impact resistance and process therefor
RU2228387C2 (ru) 2002-07-22 2004-05-10 Падеров Анатолий Николаевич Способ нанесения многослойного покрытия на металлические изделия
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WO2007121954A1 (de) * 2006-04-21 2007-11-01 Cemecon Ag Beschichteter körper
EP1862568A1 (en) 2006-05-30 2007-12-05 Siemens Aktiengesellschaft Thermal barrier coating with tungsten-bronze structure
US20090075115A1 (en) * 2007-04-30 2009-03-19 Tryon Brian S Multi-layered thermal barrier coating
US8790789B2 (en) * 2008-05-29 2014-07-29 General Electric Company Erosion and corrosion resistant coatings, methods and articles
DE102008040766A1 (de) * 2008-07-28 2010-02-11 Robert Bosch Gmbh Verschleißschutzschichtanordnung sowie Bauelement mit Verschleißschutzschichtanordnung
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US20210292910A1 (en) * 2010-02-26 2021-09-23 Friedhelm Schmitz Two layered metallic bondcoat
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RU2691822C1 (ru) 2019-06-18
EP3320127B1 (de) 2022-06-01
US10697068B2 (en) 2020-06-30
CN107709617A (zh) 2018-02-16
JP2018529016A (ja) 2018-10-04
BR112018000215A2 (pt) 2018-09-04
CN114774862A (zh) 2022-07-22
KR20180026532A (ko) 2018-03-12
JP7002443B2 (ja) 2022-01-20
US20180195176A1 (en) 2018-07-12
CA2990731A1 (en) 2017-01-12
WO2017005460A1 (de) 2017-01-12
BR112018000215B1 (pt) 2022-07-05
EP3320127A1 (de) 2018-05-16
MX2018000192A (es) 2018-04-11
HUE059675T2 (hu) 2022-12-28
KR102568312B1 (ko) 2023-08-18
CA2990731C (en) 2023-09-05
DE102015212588A1 (de) 2017-01-12

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