PL1806198T3 - Sposób obróbki cieplnej remontowanej części turbiny - Google Patents
Sposób obróbki cieplnej remontowanej części turbinyInfo
- Publication number
- PL1806198T3 PL1806198T3 PL07100068T PL07100068T PL1806198T3 PL 1806198 T3 PL1806198 T3 PL 1806198T3 PL 07100068 T PL07100068 T PL 07100068T PL 07100068 T PL07100068 T PL 07100068T PL 1806198 T3 PL1806198 T3 PL 1806198T3
- Authority
- PL
- Poland
- Prior art keywords
- heat treating
- turbine part
- serviced turbine
- serviced
- treating
- Prior art date
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
- F01D5/005—Repairing methods or devices
-
- 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
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/16—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of other metals or alloys based thereon
- C22F1/18—High-melting or refractory metals or alloys based thereon
-
- 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
-
- 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
-
- 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
- F05D2250/00—Geometry
- F05D2250/60—Structure; Surface texture
- F05D2250/62—Structure; Surface texture smooth or fine
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49316—Impeller making
- Y10T29/4932—Turbomachine making
- Y10T29/49325—Shaping integrally bladed rotor
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- General Engineering & Computer Science (AREA)
- Heat Treatment Of Articles (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US11/327,237 US8557063B2 (en) | 2006-01-05 | 2006-01-05 | Method for heat treating serviced turbine part |
| EP07100068A EP1806198B1 (en) | 2006-01-05 | 2007-01-03 | Method for heat treating a serviced turbine part |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| PL1806198T3 true PL1806198T3 (pl) | 2010-09-30 |
Family
ID=38001955
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PL07100068T PL1806198T3 (pl) | 2006-01-05 | 2007-01-03 | Sposób obróbki cieplnej remontowanej części turbiny |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US8557063B2 (pl) |
| EP (1) | EP1806198B1 (pl) |
| JP (1) | JP4993461B2 (pl) |
| CN (1) | CN101003849B (pl) |
| CA (1) | CA2572826A1 (pl) |
| DE (1) | DE602007005702D1 (pl) |
| PL (1) | PL1806198T3 (pl) |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP4898720B2 (ja) * | 2008-02-14 | 2012-03-21 | 三菱重工業株式会社 | タービン動翼の補修方法 |
| EP2405100A1 (en) | 2010-07-05 | 2012-01-11 | Siemens Aktiengesellschaft | Combined sealing and balancing arrangement for a turbine disc |
| JP5527077B2 (ja) * | 2010-07-21 | 2014-06-18 | 株式会社Ihi | 非破壊検査用の試験体製作方法 |
| JP2019112702A (ja) * | 2017-12-26 | 2019-07-11 | 三菱日立パワーシステムズ株式会社 | ニッケル基合金再生部材および該再生部材の製造方法 |
| TWI827418B (zh) * | 2022-12-23 | 2023-12-21 | 台灣電力股份有限公司 | 渦輪機葉片龜裂之修護方法 |
Family Cites Families (22)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4253885A (en) | 1979-08-29 | 1981-03-03 | Special Metals Corporation | Treating nickel base alloys |
| JPS57120619A (en) | 1981-01-20 | 1982-07-27 | Hitachi Ltd | Method for annealing of rotary sleeve |
| US4957567A (en) | 1988-12-13 | 1990-09-18 | General Electric Company | Fatigue crack growth resistant nickel-base article and alloy and method for making |
| US5161950A (en) * | 1989-10-04 | 1992-11-10 | General Electric Company | Dual alloy turbine disk |
| US5080734A (en) | 1989-10-04 | 1992-01-14 | General Electric Company | High strength fatigue crack-resistant alloy article |
| US5143563A (en) | 1989-10-04 | 1992-09-01 | General Electric Company | Creep, stress rupture and hold-time fatigue crack resistant alloys |
| US5393483A (en) | 1990-04-02 | 1995-02-28 | General Electric Company | High-temperature fatigue-resistant nickel based superalloy and thermomechanical process |
| US5111570A (en) * | 1990-08-10 | 1992-05-12 | United Technologies Corporation | Forge joining repair technique |
| US5359770A (en) * | 1992-09-08 | 1994-11-01 | General Motors Corporation | Method for bonding abrasive blade tips to the tip of a gas turbine blade |
| US5413752A (en) | 1992-10-07 | 1995-05-09 | General Electric Company | Method for making fatigue crack growth-resistant nickel-base article |
| US5584947A (en) | 1994-08-18 | 1996-12-17 | General Electric Company | Method for forming a nickel-base superalloy having improved resistance to abnormal grain growth |
| JPH1018003A (ja) * | 1996-07-02 | 1998-01-20 | Hitachi Ltd | ガスタービン及びガスタービン用ディスクとその製造法 |
| US20020005233A1 (en) * | 1998-12-23 | 2002-01-17 | John J. Schirra | Die cast nickel base superalloy articles |
| JP2001055928A (ja) * | 1999-08-12 | 2001-02-27 | Toshiba Corp | ガスタービン高温部品の補修再生処理方法 |
| AU2001243302A1 (en) | 2000-02-29 | 2001-09-12 | General Electric Company | Nickel base superalloys and turbine components fabricated therefrom |
| RU2190686C2 (ru) | 2000-11-16 | 2002-10-10 | Государственное предприятие "Всероссийский научно-исследовательский институт авиационных материалов" | Способ термической обработки жаропрочных никелевых сплавов и изделие, полученное этим способом |
| US6536110B2 (en) * | 2001-04-17 | 2003-03-25 | United Technologies Corporation | Integrally bladed rotor airfoil fabrication and repair techniques |
| JP2002371803A (ja) * | 2001-06-13 | 2002-12-26 | Mitsubishi Heavy Ind Ltd | 動翼用耐摩耗層の形成方法、耐摩耗層及びその再生方法 |
| US6974508B1 (en) | 2002-10-29 | 2005-12-13 | The United States Of America As Represented By The United States National Aeronautics And Space Administration | Nickel base superalloy turbine disk |
| US7051435B1 (en) | 2003-06-13 | 2006-05-30 | General Electric Company | Process for repairing turbine components |
| US7138020B2 (en) | 2003-10-15 | 2006-11-21 | General Electric Company | Method for reducing heat treatment residual stresses in super-solvus solutioned nickel-base superalloy articles |
| KR100504381B1 (ko) * | 2004-10-04 | 2005-07-27 | 캐스텍 주식회사 | 천이액상 확산법에 의한 방향성 및 단결정 가스터빈블레이드 수리방법 |
-
2006
- 2006-01-05 US US11/327,237 patent/US8557063B2/en active Active
- 2006-12-27 JP JP2006351400A patent/JP4993461B2/ja active Active
-
2007
- 2007-01-03 DE DE602007005702T patent/DE602007005702D1/de active Active
- 2007-01-03 PL PL07100068T patent/PL1806198T3/pl unknown
- 2007-01-03 EP EP07100068A patent/EP1806198B1/en active Active
- 2007-01-04 CA CA002572826A patent/CA2572826A1/en not_active Abandoned
- 2007-01-05 CN CN200710005278.8A patent/CN101003849B/zh active Active
Also Published As
| Publication number | Publication date |
|---|---|
| JP2007182886A (ja) | 2007-07-19 |
| US8557063B2 (en) | 2013-10-15 |
| CN101003849A (zh) | 2007-07-25 |
| CA2572826A1 (en) | 2007-07-05 |
| EP1806198A1 (en) | 2007-07-11 |
| CN101003849B (zh) | 2014-11-26 |
| JP4993461B2 (ja) | 2012-08-08 |
| US20070151100A1 (en) | 2007-07-05 |
| EP1806198B1 (en) | 2010-04-07 |
| DE602007005702D1 (de) | 2010-05-20 |
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