DE502006009452D1 - Verfahren zum herstellen eines einlaufbelags - Google Patents

Verfahren zum herstellen eines einlaufbelags

Info

Publication number
DE502006009452D1
DE502006009452D1 DE502006009452T DE502006009452T DE502006009452D1 DE 502006009452 D1 DE502006009452 D1 DE 502006009452D1 DE 502006009452 T DE502006009452 T DE 502006009452T DE 502006009452 T DE502006009452 T DE 502006009452T DE 502006009452 D1 DE502006009452 D1 DE 502006009452D1
Authority
DE
Germany
Prior art keywords
run
manufacturing
inlet belt
coating
belt
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.)
Active
Application number
DE502006009452T
Other languages
English (en)
Inventor
Manfred A Daeubler
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.)
MTU Aero Engines AG
Original Assignee
MTU Aero Engines GmbH
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 MTU Aero Engines GmbH filed Critical MTU Aero Engines GmbH
Publication of DE502006009452D1 publication Critical patent/DE502006009452D1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • C23C4/18—After-treatment
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • F01D11/12—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part
    • F01D11/122—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part with erodable or abradable material
    • 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
    • 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
    • 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
    • F05D2230/40—Heat treatment

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Plasma & Fusion (AREA)
  • Physics & Mathematics (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Lubricants (AREA)
  • Application Of Or Painting With Fluid Materials (AREA)
DE502006009452T 2005-12-07 2006-11-30 Verfahren zum herstellen eines einlaufbelags Active DE502006009452D1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102005058324A DE102005058324A1 (de) 2005-12-07 2005-12-07 Verfahren zum Herstellen eines Einlaufbelags
PCT/DE2006/002122 WO2007065403A1 (de) 2005-12-07 2006-11-30 Verfahren zum herstellen eines einlaufbelags

Publications (1)

Publication Number Publication Date
DE502006009452D1 true DE502006009452D1 (de) 2011-06-16

Family

ID=37852354

Family Applications (2)

Application Number Title Priority Date Filing Date
DE102005058324A Withdrawn DE102005058324A1 (de) 2005-12-07 2005-12-07 Verfahren zum Herstellen eines Einlaufbelags
DE502006009452T Active DE502006009452D1 (de) 2005-12-07 2006-11-30 Verfahren zum herstellen eines einlaufbelags

Family Applications Before (1)

Application Number Title Priority Date Filing Date
DE102005058324A Withdrawn DE102005058324A1 (de) 2005-12-07 2005-12-07 Verfahren zum Herstellen eines Einlaufbelags

Country Status (7)

Country Link
US (1) US20110020560A1 (de)
EP (1) EP1957756B1 (de)
JP (1) JP2009518571A (de)
AT (1) ATE508254T1 (de)
CA (1) CA2631362A1 (de)
DE (2) DE102005058324A1 (de)
WO (1) WO2007065403A1 (de)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102008005480A1 (de) * 2008-01-23 2009-07-30 Rolls-Royce Deutschland Ltd & Co Kg Gasturbine mit einem Verdichter mit Einlaufschicht mit luftaushärtendem Material
DE102008005479A1 (de) * 2008-01-23 2009-07-30 Rolls-Royce Deutschland Ltd & Co Kg Gasturbine mit einem Verdichter mit flüssigkeitsbeaufschlagter Einlaufschicht
US8257016B2 (en) 2008-01-23 2012-09-04 Rolls-Royce Deutschland Ltd & Co Kg Gas turbine with a compressor with self-healing abradable coating
EP2647795B1 (de) * 2012-04-04 2018-11-07 MTU Aero Engines AG Dichtungssystem für eine Strömungsmaschine
EP2876172A1 (de) * 2013-11-26 2015-05-27 MTU Aero Engines GmbH Verfahren zur Herstellung und Reparatur von Bauteilen einer Strömungsmaschine aus Nickelbasis-Superlegierungen

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2742224A (en) * 1951-03-30 1956-04-17 United Aircraft Corp Compressor casing lining
US3010843A (en) * 1958-04-28 1961-11-28 Gen Motors Corp Abradable protective coating for compressor casings
FR2049448A5 (de) * 1969-06-10 1971-03-26 Onera (Off Nat Aerospatiale)
US4049428A (en) * 1971-03-25 1977-09-20 Union Carbide Corporation Metal porous abradable seal
US3839234A (en) * 1973-01-26 1974-10-01 C Roscoe Multi-purpose cleaning concentrate
DE3579684D1 (de) * 1984-12-24 1990-10-18 United Technologies Corp Abschleifbare dichtung mit besonderem erosionswiderstand.
US5536022A (en) * 1990-08-24 1996-07-16 United Technologies Corporation Plasma sprayed abradable seals for gas turbine engines
US5391234A (en) * 1991-08-05 1995-02-21 Henkel Corporation Cleaning or stripping composition and method
JPH06128036A (ja) * 1992-10-16 1994-05-10 Shin Etsu Chem Co Ltd 半導体用炭化珪素質部材
US5792562A (en) * 1995-01-12 1998-08-11 Applied Materials, Inc. Electrostatic chuck with polymeric impregnation and method of making
JPH09328376A (ja) * 1996-06-06 1997-12-22 Sumitomo Metal Ind Ltd 半導体製造装置用セラミックス部材の製造方法
US5951892A (en) * 1996-12-10 1999-09-14 Chromalloy Gas Turbine Corporation Method of making an abradable seal by laser cutting
US6089825A (en) * 1998-12-18 2000-07-18 United Technologies Corporation Abradable seal having improved properties and method of producing seal
JP3283238B2 (ja) * 1999-01-06 2002-05-20 株式会社東芝 窒化ケイ素系セラミックス部品およびその製造方法
US6383658B1 (en) * 1999-11-18 2002-05-07 General Electric Company Thermally sprayed coatings having an interface with controlled cleanliness
WO2001044533A1 (en) * 1999-12-15 2001-06-21 Pratt & Whitney Canada Corp. Abradable coatings
GB2397307A (en) * 2003-01-20 2004-07-21 Rolls Royce Plc Abradable Coatings
US7732056B2 (en) * 2005-01-18 2010-06-08 Applied Materials, Inc. Corrosion-resistant aluminum component having multi-layer coating
DE102006028297A1 (de) * 2006-06-20 2007-12-27 Mtu Aero Engines Gmbh Verfahren zur Reparatur von Einlaufbelägen

Also Published As

Publication number Publication date
WO2007065403A1 (de) 2007-06-14
EP1957756A1 (de) 2008-08-20
ATE508254T1 (de) 2011-05-15
EP1957756B1 (de) 2011-05-04
DE102005058324A1 (de) 2007-06-14
JP2009518571A (ja) 2009-05-07
US20110020560A1 (en) 2011-01-27
CA2631362A1 (en) 2007-06-14

Similar Documents

Publication Publication Date Title
DE502005011190D1 (de) Verfahren zum aufbringen einer schützenden beschic
DE502006009452D1 (de) Verfahren zum herstellen eines einlaufbelags
DE102005051506A1 (de) Elektromotor und Verfahren zum Herstellen eines Elektromotors
SG138539A1 (en) High coverage cooling hole shape
DE602008000344D1 (de) Verfahren zum Einstellen der Messeignungskonfiguration für die Gasturbinenleistungsdiagnose
DE602008006004D1 (de) Aluminisierungsverfahren in der Dampfphase eines Metallteils eines Turbotriebwerks
DE502005010233D1 (de) Verfahren zum herstellen eines metall-keramik-substrates
DE602006020567D1 (de) Rotor für dampfturbine und verfahren zu dessen herstellung
DE502008001450D1 (de) Verfahren zum herstellen von beschichteten turbinenlaufschaufeln
WO2010121597A3 (de) Verfahren zur herstellung einer panzerung einer schaufespitze gasturbinenschaufel
EP2805019A4 (de) Verfahren zur herstellung einer turbomaschinenkomponente, schaufel und gasturbinenmotor
DE112006003408A5 (de) Verfahren zum Herstellen eines geschweissten Rotors einer Niederdruck-Dampfturbine
PL1869292T3 (pl) Część składowa instalacji turbiny parowej, instalacja turbiny parowej, zastosowanie i sposób wytwarzania
EA200870038A1 (ru) Способ получения аминов
DE502005010678D1 (de) Verfahren zum herstellen einer nockenwelle
PL1934387T3 (pl) Sposób odwarstwiania elementu turbiny gazowej
TWI265204B (en) Method for coating substrates in inline installations
ATE521722T1 (de) Verfahren und vorrichtung zum abschnittsweisen durchhärten von aus stahlblech fertig geformten bauteilen
DE60224344D1 (de) Gasturbine, Brennkammer dafür und Verfahren zum Kühlen der Brennkammer
EA200900301A1 (ru) Уголь с улучшенными параметрами сгорания
ATE417188T1 (de) Verfahren zum hochfahren einer gas- und dampfturbinenanlage
DE502007000169D1 (de) Verfahren zum Herstellen eines tribologischen Bauteils
ATE476597T1 (de) Hochdruckverbindung und verfahren zum herstellen einer hochdruckverbindung
DE602007005702D1 (de) Wärmebehandlungsverfahren für gebrauchte Turbinenteile
ATE521445T1 (de) Verfahren zum herstellen eines integral beschaufelten rotors