DE602005027552D1 - Reparatur an gasturbinen-motorenbauteilen durch dynamisches kaltgasspritzen - Google Patents
Reparatur an gasturbinen-motorenbauteilen durch dynamisches kaltgasspritzenInfo
- Publication number
- DE602005027552D1 DE602005027552D1 DE602005027552T DE602005027552T DE602005027552D1 DE 602005027552 D1 DE602005027552 D1 DE 602005027552D1 DE 602005027552 T DE602005027552 T DE 602005027552T DE 602005027552 T DE602005027552 T DE 602005027552T DE 602005027552 D1 DE602005027552 D1 DE 602005027552D1
- Authority
- DE
- Germany
- Prior art keywords
- turbine engine
- engine components
- repairing
- gas turbine
- dynamic cold
- 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
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P6/00—Restoring or reconditioning objects
- B23P6/002—Repairing turbine components, e.g. moving or stationary blades, rotors
- B23P6/007—Repairing turbine components, e.g. moving or stationary blades, rotors using only additive methods, e.g. build-up welding
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F7/00—Manufacture 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
- B22F7/06—Manufacture 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
- B22F7/08—Manufacture 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
-
- 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
- C23C24/00—Coating starting from inorganic powder
- C23C24/02—Coating starting from inorganic powder by application of pressure only
- C23C24/04—Impact or kinetic deposition of particles
-
- 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
- C23C26/00—Coating not provided for in groups C23C2/00 - C23C24/00
-
- 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
- F01D5/005—Repairing methods or devices
-
- 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
- F05D2230/80—Repairing, retrofitting or upgrading methods
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Composite Materials (AREA)
- Manufacturing & Machinery (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Coating By Spraying Or Casting (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US10/806,727 US6905728B1 (en) | 2004-03-22 | 2004-03-22 | Cold gas-dynamic spray repair on gas turbine engine components |
PCT/US2005/009551 WO2005093128A1 (en) | 2004-03-22 | 2005-03-22 | Cold gas-dynamic spray repair on gas turbine engine components |
Publications (1)
Publication Number | Publication Date |
---|---|
DE602005027552D1 true DE602005027552D1 (de) | 2011-06-01 |
Family
ID=34634670
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE602005027552T Active DE602005027552D1 (de) | 2004-03-22 | 2005-03-22 | Reparatur an gasturbinen-motorenbauteilen durch dynamisches kaltgasspritzen |
Country Status (4)
Country | Link |
---|---|
US (1) | US6905728B1 (de) |
EP (1) | EP1730323B1 (de) |
DE (1) | DE602005027552D1 (de) |
WO (1) | WO2005093128A1 (de) |
Families Citing this family (76)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20030002043A1 (en) * | 2001-04-10 | 2003-01-02 | Kla-Tencor Corporation | Periodic patterns and technique to control misalignment |
US20040086635A1 (en) * | 2002-10-30 | 2004-05-06 | Grossklaus Warren Davis | Method of repairing a stationary shroud of a gas turbine engine using laser cladding |
US20050220995A1 (en) * | 2004-04-06 | 2005-10-06 | Yiping Hu | Cold gas-dynamic spraying of wear resistant alloys on turbine blades |
US20050255329A1 (en) * | 2004-05-12 | 2005-11-17 | General Electric Company | Superalloy article having corrosion resistant coating thereon |
US20060045785A1 (en) * | 2004-08-30 | 2006-03-02 | Yiping Hu | Method for repairing titanium alloy components |
US20060051502A1 (en) * | 2004-09-08 | 2006-03-09 | Yiping Hu | Methods for applying abrasive and environment-resistant coatings onto turbine components |
US20060121183A1 (en) * | 2004-12-03 | 2006-06-08 | United Technologies Corporation | Superalloy repair using cold spray |
US7378132B2 (en) * | 2004-12-14 | 2008-05-27 | Honeywell International, Inc. | Method for applying environmental-resistant MCrAlY coatings on gas turbine components |
US7335427B2 (en) * | 2004-12-17 | 2008-02-26 | General Electric Company | Preform and method of repairing nickel-base superalloys and components repaired thereby |
US20060134320A1 (en) * | 2004-12-21 | 2006-06-22 | United Technologies Corporation | Structural repair using cold sprayed aluminum materials |
US20060134321A1 (en) * | 2004-12-22 | 2006-06-22 | United Technologies Corporation | Blade platform restoration using cold spray |
US7836593B2 (en) * | 2005-03-17 | 2010-11-23 | Siemens Energy, Inc. | Cold spray method for producing gas turbine blade tip |
US7836591B2 (en) * | 2005-03-17 | 2010-11-23 | Siemens Energy, Inc. | Method for forming turbine seal by cold spray process |
US20060216428A1 (en) * | 2005-03-23 | 2006-09-28 | United Technologies Corporation | Applying bond coat to engine components using cold spray |
KR100802329B1 (ko) * | 2005-04-15 | 2008-02-13 | 주식회사 솔믹스 | 금속기지 복합체 형성방법 및 이를 이용하여 제조된 코팅층및 벌크 |
JP4904341B2 (ja) * | 2005-05-05 | 2012-03-28 | ハー.ツェー.スタルク ゲゼルシャフト ミット ベシュレンクテル ハフツング | スパッタターゲット及びx線アノードを製造又は再処理するための被覆方法 |
RU2434073C9 (ru) * | 2005-05-05 | 2012-12-27 | Х.К. Штарк Гмбх | Способ покрытия поверхности субстрата и продукт с нанесенным покрытием |
US7367488B2 (en) * | 2005-05-10 | 2008-05-06 | Honeywell International, Inc. | Method of repair of thin wall housings |
US20070031591A1 (en) * | 2005-08-05 | 2007-02-08 | TDM Inc. | Method of repairing a metallic surface wetted by a radioactive fluid |
KR100946196B1 (ko) * | 2005-08-17 | 2010-03-08 | 아주대학교산학협력단 | 분무 코팅에 의한 금속표면 개질방법 및 이에 의하여 제조되는 금속 |
EP1772228A1 (de) * | 2005-10-07 | 2007-04-11 | Siemens Aktiengesellschaft | Verfahren zum Reparieren eines Bauteils mit einer gerichteten Mikrostruktur |
US20070116890A1 (en) * | 2005-11-21 | 2007-05-24 | Honeywell International, Inc. | Method for coating turbine engine components with rhenium alloys using high velocity-low temperature spray process |
DE102005062225B3 (de) * | 2005-12-21 | 2007-06-21 | Siemens Ag | Legierungsprodukt vom MCrAIX-Typ und Verfahren zur Herstellung einer Schicht aus diesem Legierungsprodukt |
EP1829988A1 (de) * | 2006-03-02 | 2007-09-05 | Praxair Surface Technologies GmbH | Verfahren zur Reparatur und wiederherstellung von dynamisch beanspruchten Komponenten aus Aluminiumlegierungen für luftfahrtechnische Anwendungen |
SG141297A1 (en) | 2006-09-11 | 2008-04-28 | United Technologies Corp | Method for processing titanium alloy components |
US20080078268A1 (en) * | 2006-10-03 | 2008-04-03 | H.C. Starck Inc. | Process for preparing metal powders having low oxygen content, powders so-produced and uses thereof |
US20080099538A1 (en) * | 2006-10-27 | 2008-05-01 | United Technologies Corporation & Pratt & Whitney Canada Corp. | Braze pre-placement using cold spray deposition |
AU2007317650B2 (en) * | 2006-11-07 | 2012-06-14 | H.C. Starck Surface Technology and Ceramic Powders GmbH | Method for coating a substrate and coated product |
US20080145688A1 (en) | 2006-12-13 | 2008-06-19 | H.C. Starck Inc. | Method of joining tantalum clade steel structures |
US8197894B2 (en) | 2007-05-04 | 2012-06-12 | H.C. Starck Gmbh | Methods of forming sputtering targets |
US20080286459A1 (en) * | 2007-05-17 | 2008-11-20 | Pratt & Whitney Canada Corp. | Method for applying abradable coating |
US20090098286A1 (en) * | 2007-06-11 | 2009-04-16 | Honeywell International, Inc. | Method for forming bond coats for thermal barrier coatings on turbine engine components |
US8597724B2 (en) * | 2007-07-06 | 2013-12-03 | United Technologies Corporation | Corrosion protective coating through cold spray |
DE102007046386B3 (de) * | 2007-09-21 | 2008-10-02 | Siemens Ag | Verfahren zur Reparatur eines Bauteils durch Beschichten |
DE102007056451A1 (de) * | 2007-11-23 | 2009-05-28 | Mtu Aero Engines Gmbh | Verfahren zur Reparatur eines Gasturbinenbauteils |
US8109638B2 (en) * | 2008-01-22 | 2012-02-07 | Alcatel Lucent | Diffuser configuration for an image projector |
US20090249603A1 (en) * | 2008-04-08 | 2009-10-08 | Chris Vargas | Cold deposition repair of casting porosity |
US20090301645A1 (en) * | 2008-06-04 | 2009-12-10 | General Electric Company | System and method of joining components |
US20100014977A1 (en) * | 2008-07-15 | 2010-01-21 | Shattuck Colman D | Variable pitch aft propeller vane system |
US8246903B2 (en) | 2008-09-09 | 2012-08-21 | H.C. Starck Inc. | Dynamic dehydriding of refractory metal powders |
US8043655B2 (en) * | 2008-10-06 | 2011-10-25 | H.C. Starck, Inc. | Low-energy method of manufacturing bulk metallic structures with submicron grain sizes |
EP2177643A1 (de) * | 2008-10-07 | 2010-04-21 | Siemens Aktiengesellschaft | Verfahren zum Reparieren einer Superlegierung mit dem gleichen Superlegierungspulver und Keramik |
DE102008052030B4 (de) * | 2008-10-16 | 2011-06-16 | Mtu Aero Engines Gmbh | Verfahren zum Verbinden wenigstens einer Turbinenschaufel mit einer Turbinenscheibe oder einem Turbinenring |
DE102008057162A1 (de) * | 2008-11-13 | 2010-05-20 | Mtu Aero Engines Gmbh | Verfahren zur Reparatur des Bauteils einer Gasturbine |
US8268237B2 (en) * | 2009-01-08 | 2012-09-18 | General Electric Company | Method of coating with cryo-milled nano-grained particles |
DE102009037894A1 (de) * | 2009-08-18 | 2011-02-24 | Mtu Aero Engines Gmbh | Dünnwandiges Strukturbauteil und Verfahren zu seiner Herstellung |
US8261444B2 (en) * | 2009-10-07 | 2012-09-11 | General Electric Company | Turbine rotor fabrication using cold spraying |
DE102010007526B3 (de) | 2010-02-11 | 2011-05-05 | Mtu Aero Engines Gmbh | Verfahren zur Herstellung eines Bauteils und ein derartiges Bauteil |
EP2366488A1 (de) * | 2010-03-19 | 2011-09-21 | Siemens Aktiengesellschaft | Verfahren zum Wiederaufarbeiten einer Turbinenschaufel mit wenigstens einer Plattform |
US8708659B2 (en) | 2010-09-24 | 2014-04-29 | United Technologies Corporation | Turbine engine component having protective coating |
DE102010048336A1 (de) * | 2010-10-13 | 2012-04-19 | Mtu Aero Engines Gmbh | Bauteil und Verfahren zum Ausbilden, Reparieren und/oder Aufbauen eines derartigen Bauteils |
ITTO20110257A1 (it) * | 2011-03-24 | 2012-09-25 | Avio Spa | Metodo per la riparazione di un componente in lega di alluminio |
US8544769B2 (en) | 2011-07-26 | 2013-10-01 | General Electric Company | Multi-nozzle spray gun |
US9412568B2 (en) | 2011-09-29 | 2016-08-09 | H.C. Starck, Inc. | Large-area sputtering targets |
US8601663B2 (en) | 2012-02-13 | 2013-12-10 | Honeywell International Inc. | Methods for structural repair of components having damaged internally threaded openings and components repaired using such methods |
US9175402B2 (en) * | 2012-07-30 | 2015-11-03 | General Electric Company | Turbine repair process, repaired coating, and repaired turbine component |
WO2014028965A1 (en) * | 2012-08-20 | 2014-02-27 | Commonwealth Scientific And Industrial Research Organisation | Formation, repair and modification of lay up tools |
US10441962B2 (en) | 2012-10-29 | 2019-10-15 | South Dakota Board Of Regents | Cold spray device and system |
US10099322B2 (en) * | 2012-10-29 | 2018-10-16 | South Dakota Board Of Regents | Methods for cold spray repair |
AU2013375273B2 (en) * | 2013-01-28 | 2017-08-31 | Raytheon Technologies Corporation | Structured material alloy component fabrication |
US20160024942A1 (en) * | 2013-03-15 | 2016-01-28 | United Technologies Corporation | Abrasive Tipped Blades and Manufacture Methods |
US8991241B1 (en) * | 2013-10-30 | 2015-03-31 | General Electric Company | Gas turbine component monitoring |
US9599210B2 (en) * | 2013-11-06 | 2017-03-21 | Sikorsky Aircraft Corporation | Damage mitigation for gearbox |
US10077499B2 (en) | 2013-11-06 | 2018-09-18 | Sikorsky Aircraft Corporation | Corrosion mitigation for gearbox |
PL3134932T3 (pl) | 2014-04-25 | 2022-01-17 | South Dakota Board Of Regents | Elektrody o dużej pojemności |
US20150377037A1 (en) * | 2014-06-30 | 2015-12-31 | General Electric Company | Braze methods and components for turbine buckets |
US20160175991A1 (en) * | 2014-12-19 | 2016-06-23 | General Electric Company | Weld filler for superalloys |
US20170073806A1 (en) * | 2015-09-10 | 2017-03-16 | General Electric Company | Article treatment methods |
US20170114466A1 (en) * | 2015-10-21 | 2017-04-27 | General Electric Company | Article, turbine component and airfoil treatment methods |
US10610982B2 (en) | 2015-11-12 | 2020-04-07 | General Electric Company | Weld filler metal for superalloys and methods of making |
US20210213535A1 (en) * | 2017-06-20 | 2021-07-15 | Commonwealth Scientific And Industrial Research Organisation | Process for forming wrought structures using cold spray |
US10315218B2 (en) * | 2017-07-06 | 2019-06-11 | General Electric Company | Method for repairing turbine component by application of thick cold spray coating |
DE102017222182A1 (de) * | 2017-12-07 | 2019-06-13 | Helmholtz-Zentrum Geesthacht Zentrum für Material- und Küstenforschung GmbH | Verfahren zum Aufbringen einer Titanaluminidlegierung, Titanaluminidlegierung und Substrat umfassend eine Titanaluminidlegierung |
US10468674B2 (en) | 2018-01-09 | 2019-11-05 | South Dakota Board Of Regents | Layered high capacity electrodes |
CN111411250B (zh) * | 2020-04-07 | 2021-07-09 | 广东广纳新材料有限公司 | 一种可膨胀微球发泡剂、其制备方法与发泡材料 |
CN111783306B (zh) * | 2020-07-06 | 2022-11-18 | 中国航发湖南动力机械研究所 | 涡轮叶片冷气量与冷效特性分析方法 |
Family Cites Families (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4008844A (en) | 1975-01-06 | 1977-02-22 | United Technologies Corporation | Method of repairing surface defects using metallic filler material |
US4050133A (en) | 1976-06-07 | 1977-09-27 | Cretella Salvatore | Method of refurbishing turbine vanes and the like |
DE69016433T2 (de) | 1990-05-19 | 1995-07-20 | Papyrin Anatolij Nikiforovic | Beschichtungsverfahren und -vorrichtung. |
US5156321A (en) | 1990-08-28 | 1992-10-20 | Liburdi Engineering Limited | Powder metallurgy repair technique |
DE4310896C1 (de) | 1993-04-02 | 1994-03-24 | Thyssen Industrie | Verfahren zum Herstellen von verschleißfesten Kanten an Turbinenschaufeln |
US20030088980A1 (en) | 1993-11-01 | 2003-05-15 | Arnold James E. | Method for correcting defects in a workpiece |
US5732467A (en) | 1996-11-14 | 1998-03-31 | General Electric Company | Method of repairing directionally solidified and single crystal alloy parts |
US20040031140A1 (en) | 1996-12-23 | 2004-02-19 | Arnold James E. | Methods for salvaging a cast article |
US6049978A (en) | 1996-12-23 | 2000-04-18 | Recast Airfoil Group | Methods for repairing and reclassifying gas turbine engine airfoil parts |
US6626228B1 (en) | 1998-08-24 | 2003-09-30 | General Electric Company | Turbine component repair system and method of using thereof |
US6139913A (en) | 1999-06-29 | 2000-10-31 | National Center For Manufacturing Sciences | Kinetic spray coating method and apparatus |
US6306277B1 (en) | 2000-01-14 | 2001-10-23 | Honeywell International Inc. | Platinum electrolyte for use in electrolytic plating |
US6384365B1 (en) | 2000-04-14 | 2002-05-07 | Siemens Westinghouse Power Corporation | Repair and fabrication of combustion turbine components by spark plasma sintering |
US6365222B1 (en) * | 2000-10-27 | 2002-04-02 | Siemens Westinghouse Power Corporation | Abradable coating applied with cold spray technique |
US6491208B2 (en) | 2000-12-05 | 2002-12-10 | Siemens Westinghouse Power Corporation | Cold spray repair process |
US6444259B1 (en) * | 2001-01-30 | 2002-09-03 | Siemens Westinghouse Power Corporation | Thermal barrier coating applied with cold spray technique |
US6602548B2 (en) | 2001-06-20 | 2003-08-05 | Honeywell International Inc. | Ceramic turbine blade attachment having high temperature, high stress compliant layers and method of fabrication thereof |
US6520401B1 (en) | 2001-09-06 | 2003-02-18 | Sermatech International, Inc. | Diffusion bonding of gaps |
US6706319B2 (en) * | 2001-12-05 | 2004-03-16 | Siemens Westinghouse Power Corporation | Mixed powder deposition of components for wear, erosion and abrasion resistant applications |
US6883224B2 (en) | 2002-02-01 | 2005-04-26 | Honeywell International Inc. | Gas turbine impeller alignment tool and method |
US6623796B1 (en) | 2002-04-05 | 2003-09-23 | Delphi Technologies, Inc. | Method of producing a coating using a kinetic spray process with large particles and nozzles for the same |
US7556695B2 (en) | 2002-05-06 | 2009-07-07 | Honeywell International, Inc. | Apparatus to make nanolaminate thermal barrier coatings |
CA2433613A1 (en) * | 2002-08-13 | 2004-02-13 | Russel J. Ruprecht, Jr. | Spray method for mcralx coating |
-
2004
- 2004-03-22 US US10/806,727 patent/US6905728B1/en not_active Expired - Lifetime
-
2005
- 2005-03-22 DE DE602005027552T patent/DE602005027552D1/de active Active
- 2005-03-22 WO PCT/US2005/009551 patent/WO2005093128A1/en not_active Application Discontinuation
- 2005-03-22 EP EP05729341A patent/EP1730323B1/de not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
EP1730323A1 (de) | 2006-12-13 |
WO2005093128A1 (en) | 2005-10-06 |
EP1730323B1 (de) | 2011-04-20 |
US6905728B1 (en) | 2005-06-14 |
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