SG108939A1 - Method for vapor phase aluminiding of a gas turbine blade partially masked with a masking enclosure - Google Patents

Method for vapor phase aluminiding of a gas turbine blade partially masked with a masking enclosure

Info

Publication number
SG108939A1
SG108939A1 SG200305713A SG200305713A SG108939A1 SG 108939 A1 SG108939 A1 SG 108939A1 SG 200305713 A SG200305713 A SG 200305713A SG 200305713 A SG200305713 A SG 200305713A SG 108939 A1 SG108939 A1 SG 108939A1
Authority
SG
Singapore
Prior art keywords
gas turbine
turbine blade
vapor phase
partially masked
blade partially
Prior art date
Application number
SG200305713A
Other languages
English (en)
Inventor
Nigel Brian Thomas Langley
Kwok Heng Yow
Original Assignee
Ge Aviat Service Operation Pte
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 Ge Aviat Service Operation Pte filed Critical Ge Aviat Service Operation Pte
Publication of SG108939A1 publication Critical patent/SG108939A1/en

Links

Classifications

    • 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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/288—Protective coatings for blades
    • 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
    • C23C10/00—Solid state diffusion of only metal elements or silicon into metallic material surfaces
    • C23C10/04—Diffusion into selected surface areas, e.g. using masks
    • 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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2230/00—Manufacture
    • F05B2230/90—Coating; Surface treatment
    • 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
    • F05D2230/90—Coating; Surface treatment

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Other Surface Treatments For Metallic Materials (AREA)
  • Physical Vapour Deposition (AREA)
SG200305713A 2002-09-27 2003-09-26 Method for vapor phase aluminiding of a gas turbine blade partially masked with a masking enclosure SG108939A1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US10/259,342 US6863927B2 (en) 2002-09-27 2002-09-27 Method for vapor phase aluminiding of a gas turbine blade partially masked with a masking enclosure

Publications (1)

Publication Number Publication Date
SG108939A1 true SG108939A1 (en) 2005-02-28

Family

ID=31977899

Family Applications (1)

Application Number Title Priority Date Filing Date
SG200305713A SG108939A1 (en) 2002-09-27 2003-09-26 Method for vapor phase aluminiding of a gas turbine blade partially masked with a masking enclosure

Country Status (7)

Country Link
US (1) US6863927B2 (es)
EP (1) EP1403395B1 (es)
JP (1) JP4279104B2 (es)
BR (1) BR0303896B1 (es)
CA (1) CA2441490C (es)
DE (1) DE60300807T2 (es)
SG (1) SG108939A1 (es)

Families Citing this family (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20040191488A1 (en) * 2002-04-10 2004-09-30 Thomas Berndt Component, method for coating a component, and powder
US7252480B2 (en) * 2004-12-17 2007-08-07 General Electric Company Methods for generation of dual thickness internal pack coatings and objects produced thereby
JP3757418B1 (ja) * 2005-01-19 2006-03-22 石川島播磨重工業株式会社 拡散アルミナイドコーティングの局部施工方法
EP1762303B1 (de) * 2005-09-09 2012-10-17 Siemens Aktiengesellschaft Verfahren zur Vorbereitung von Turbinenschaufeln für die Sprühbeschichtung sowie Halterung zur Fixierung einer solchen Turbinenschaufel
US7632541B2 (en) * 2006-03-13 2009-12-15 General Electric Company Method and device to prevent coating a dovetail of a turbine airfoil
US8708658B2 (en) * 2007-04-12 2014-04-29 United Technologies Corporation Local application of a protective coating on a shrouded gas turbine engine component
EP1980366B1 (de) * 2007-04-12 2009-11-18 Siemens Aktiengesellschaft Anlagen- und Vorrichtungskonzept für eine Shotpeeninganlage zum Verfestigen von Gasturbinen Laufschaufelfüssen
DE102007027474A1 (de) * 2007-06-14 2008-12-18 Burgmann Industries Gmbh & Co. Kg Verfahren zur Ausbildung einer planen Schicht aus einem Diamantmaterial auf einer Werkstückoberfläche
DE102008053394A1 (de) * 2008-10-27 2010-04-29 Mtu Aero Engines Gmbh Vorrichtung zum partiellen Abdecken einer Bauteilzone
EP2181775B1 (de) * 2008-11-04 2012-09-12 Siemens Aktiengesellschaft Halterung für grosse Bauteile mit verbesserten Spritzschutz
US8967078B2 (en) * 2009-08-27 2015-03-03 United Technologies Corporation Abrasive finish mask and method of polishing a component
EP2309016B1 (en) * 2009-10-06 2012-10-03 Siemens Aktiengesellschaft Method and arrangement for a spray coating process
KR101084185B1 (ko) * 2010-01-12 2011-11-17 삼성모바일디스플레이주식회사 패턴 형성 방법 및 유기 발광 소자의 제조방법
EP2359940A1 (en) * 2010-02-12 2011-08-24 Siemens Aktiengesellschaft Overspray shielding device and method
US8839739B2 (en) 2010-03-31 2014-09-23 United Technologies Corporation Masking apparatus
US8516974B2 (en) * 2011-08-29 2013-08-27 General Electric Company Automated wet masking for diffusion coatings
US9309895B2 (en) 2012-06-18 2016-04-12 Kennametal Inc. Closed impeller with a coated vane
FR2992676B1 (fr) * 2012-06-29 2014-08-01 Snecma Plateforme inter-aubes pour une soufflante, rotor d'une soufflante et procede de fabrication associe
EP2733232A1 (de) * 2012-11-16 2014-05-21 Siemens Aktiengesellschaft Vorrichtung zum Schutz äußerer Oberflächen beim Innenalitieren von hohlen Bauteilen
US9249490B2 (en) * 2012-12-06 2016-02-02 United Technologies Corporation Mask system for gas turbine engine component
JP6480662B2 (ja) 2013-03-13 2019-03-13 ハウメット コーポレイションＨｏｗｍｅｔ Ｃｏｒｐｏｒａｔｉｏｎ タービン部品のアルミナイジングに用いられるマスカント
DE102013224566A1 (de) * 2013-11-29 2015-06-03 Siemens Aktiengesellschaft Vorrichtung zur Maskierung auf Wolframlegierungsbasis und eine Wolframlegierung
DE102015203729A1 (de) * 2015-03-03 2016-09-22 MTU Aero Engines AG Vorrichtung und Verfahren zum partiellen Abdecken einer Bauteilzone eines Bauteils
US10570753B2 (en) 2017-01-23 2020-02-25 United Technologies Corporation Apparatus and method for masking under platform areas of airfoil components
US10830093B2 (en) * 2017-06-13 2020-11-10 General Electric Company System and methods for selective cleaning of turbine engine components
US20190194799A1 (en) 2017-12-22 2019-06-27 United Technologies Corporation Line-of-sight coating fixture and apparatus
CN114807843A (zh) * 2022-04-19 2022-07-29 中国航发动力股份有限公司 一种涡轮工作叶片涂层工艺重量控制防护卡具及使用方法
US20240141491A1 (en) * 2022-10-27 2024-05-02 General Electric Company Deposition support apparatus and method for coating a component

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4617202A (en) 1970-11-18 1986-10-14 Alloy Surfaces Company, Inc. Diffusion coating mixtures
US4291448A (en) 1977-12-12 1981-09-29 Turbine Components Corporation Method of restoring the shrouds of turbine blades
US4271005A (en) 1979-12-03 1981-06-02 United Technologies Corporation Workpiece support apparatus for use with cathode sputtering devices
US4530861A (en) 1983-12-19 1985-07-23 General Electric Company Method and apparatus for masking a surface of a blade member
US5225246A (en) 1990-05-14 1993-07-06 United Technologies Corporation Method for depositing a variable thickness aluminide coating on aircraft turbine blades
US5565035A (en) * 1996-03-14 1996-10-15 United Technologies Corporation Fixture for masking a portion of an airfoil during application of a coating
US5792267A (en) 1997-05-16 1998-08-11 United Technologies Corporation Coating fixture for a turbine engine blade
US6109873A (en) * 1998-06-17 2000-08-29 United Technologies Corporation Shield for masking a flow directing assembly
US6224673B1 (en) 1999-08-11 2001-05-01 General Electric Company Apparatus for masking turbine components during vapor phase diffusion coating
US6332926B1 (en) 1999-08-11 2001-12-25 General Electric Company Apparatus and method for selectively coating internal and external surfaces of an airfoil
US6296705B1 (en) 1999-12-15 2001-10-02 United Technologies Corporation Masking fixture and method
US6391115B1 (en) * 2000-10-10 2002-05-21 United Technologies Corporation Underplatform coating tool

Also Published As

Publication number Publication date
BR0303896B1 (pt) 2013-05-07
DE60300807D1 (de) 2005-07-14
US6863927B2 (en) 2005-03-08
JP2004116529A (ja) 2004-04-15
DE60300807T2 (de) 2006-03-23
CA2441490C (en) 2010-03-30
EP1403395B1 (en) 2005-06-08
EP1403395A1 (en) 2004-03-31
JP4279104B2 (ja) 2009-06-17
CA2441490A1 (en) 2004-03-27
BR0303896A (pt) 2004-09-08
US20040062864A1 (en) 2004-04-01

Similar Documents

Publication Publication Date Title
SG108939A1 (en) Method for vapor phase aluminiding of a gas turbine blade partially masked with a masking enclosure
AU2003222712A1 (en) Process of masking cooling holes of a gas turbine component
GB2382382B (en) A fan for a turbofan gas turbine engine
GB2418957B (en) A liner for a gas turbine engine casing
GB0326541D0 (en) A gas turbine engine blade containment assembly
GB2390402B (en) Gas turbine shroud structure
GB2402978B (en) A combination of an aircraft and a gas turbine engine
GB0203447D0 (en) A cowl structure for a gas turbine engine
GB0211350D0 (en) A gas turbine engine
GB2406615B (en) A gas turbine engine blade containment assembly
GB9901218D0 (en) Cooled aerofoil for a gas turbine engine
GB0216561D0 (en) Diffuser for gas turbine engine
GB0110264D0 (en) Method of operating a gas turbine
SG125103A1 (en) Aluminide coating of gas turbine engine blade
GB0107973D0 (en) A gas turbine engine blade containment assembly
GB0107970D0 (en) A gas turbine engine blade containment assembly
GB2388875B (en) A vane for a rotor arrangement for a gas turbine engine
PL1651841T3 (pl) Chłodzony w systemie otwartym element dla turbiny gazowej, komora spalania i turbina gazowa
GB2383380B (en) Rotor assemblies for gas turbine engines
SG120972A1 (en) Aluminide coating of gas turbine engine blade
GB2387203B (en) Rotor disc for gas turbine engine
GB0228050D0 (en) Compressor for gas turbine engine
SG112093A1 (en) Method for assembling gas turbine engine components
AU2003213998A1 (en) Method for producing gas turbines and gas turbine assembly
PL1627132T3 (pl) Łożysko do osiowego ułożyskowania wirnika turbiny gazowej i turbina gazowa