DE60300807T2 - Verfahren zur Gasphasenaluminisierung einer teilweise mit einem Maskierungsgehäuse maskierten Gasturbinenschaufel - Google Patents

Verfahren zur Gasphasenaluminisierung einer teilweise mit einem Maskierungsgehäuse maskierten Gasturbinenschaufel Download PDF

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Publication number
DE60300807T2
DE60300807T2 DE60300807T DE60300807T DE60300807T2 DE 60300807 T2 DE60300807 T2 DE 60300807T2 DE 60300807 T DE60300807 T DE 60300807T DE 60300807 T DE60300807 T DE 60300807T DE 60300807 T2 DE60300807 T2 DE 60300807T2
Authority
DE
Germany
Prior art keywords
housing
gas turbine
airfoil
providing
masking
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.)
Expired - Lifetime
Application number
DE60300807T
Other languages
German (de)
English (en)
Other versions
DE60300807D1 (de
Inventor
Nigel Brian Thomas Danvers Langley
Kwok Heng Yow
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.)
GE Aviation Service Operation LLP
Original Assignee
GE Aviation Service Operation LLP
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 Aviation Service Operation LLP filed Critical GE Aviation Service Operation LLP
Application granted granted Critical
Publication of DE60300807D1 publication Critical patent/DE60300807D1/de
Publication of DE60300807T2 publication Critical patent/DE60300807T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/28Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/288Protective coatings for blades
    • 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
    • C23C10/00Solid state diffusion of only metal elements or silicon into metallic material surfaces
    • C23C10/04Diffusion into selected surface areas, e.g. using masks
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/28Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2230/00Manufacture
    • F05B2230/90Coating; Surface treatment
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00Manufacture
    • F05D2230/90Coating; 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)
DE60300807T 2002-09-27 2003-09-25 Verfahren zur Gasphasenaluminisierung einer teilweise mit einem Maskierungsgehäuse maskierten Gasturbinenschaufel Expired - Lifetime DE60300807T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US259342 2002-09-27
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 (2)

Publication Number Publication Date
DE60300807D1 DE60300807D1 (de) 2005-07-14
DE60300807T2 true DE60300807T2 (de) 2006-03-23

Family

ID=31977899

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60300807T Expired - Lifetime DE60300807T2 (de) 2002-09-27 2003-09-25 Verfahren zur Gasphasenaluminisierung einer teilweise mit einem Maskierungsgehäuse maskierten Gasturbinenschaufel

Country Status (7)

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

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
DE102013224566A1 (de) * 2013-11-29 2015-06-03 Siemens Aktiengesellschaft Vorrichtung zur Maskierung auf Wolframlegierungsbasis und eine Wolframlegierung

Families Citing this family (25)

* 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
DE502007002038D1 (de) * 2007-04-12 2009-12-31 Siemens Ag Anlagen- und Vorrichtungskonzept für eine Shotpeeninganlage zum Verfestigen von Gasturbinen Laufschaufelfüssen
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
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)

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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

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
DE102013224566A1 (de) * 2013-11-29 2015-06-03 Siemens Aktiengesellschaft Vorrichtung zur Maskierung auf Wolframlegierungsbasis und eine Wolframlegierung

Also Published As

Publication number Publication date
CA2441490A1 (en) 2004-03-27
EP1403395B1 (en) 2005-06-08
US20040062864A1 (en) 2004-04-01
EP1403395A1 (en) 2004-03-31
BR0303896A (pt) 2004-09-08
US6863927B2 (en) 2005-03-08
JP2004116529A (ja) 2004-04-15
CA2441490C (en) 2010-03-30
JP4279104B2 (ja) 2009-06-17
SG108939A1 (en) 2005-02-28
BR0303896B1 (pt) 2013-05-07
DE60300807D1 (de) 2005-07-14

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