ATE496151T1 - Abscheidungsreparatur von hohlen gegenständen - Google Patents
Abscheidungsreparatur von hohlen gegenständenInfo
- Publication number
- ATE496151T1 ATE496151T1 AT05252127T AT05252127T ATE496151T1 AT E496151 T1 ATE496151 T1 AT E496151T1 AT 05252127 T AT05252127 T AT 05252127T AT 05252127 T AT05252127 T AT 05252127T AT E496151 T1 ATE496151 T1 AT E496151T1
- Authority
- AT
- Austria
- Prior art keywords
- hollow objects
- deposition repair
- repair
- deposition
- internal space
- Prior art date
Links
- 230000008021 deposition Effects 0.000 title 1
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
-
- 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
- C23C4/01—Selective coating, e.g. pattern coating, without pre-treatment of the material to be coated
-
- 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
- C23C4/02—Pretreatment of the material to be coated, e.g. for coating on selected surface areas
-
- 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
- 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
- F01D5/14—Form or construction
- F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
- F01D5/187—Convection cooling
-
- 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
- F05D2240/00—Components
- F05D2240/10—Stators
- F05D2240/12—Fluid guiding means, e.g. vanes
- F05D2240/122—Fluid guiding means, e.g. vanes related to the trailing edge of a stator vane
-
- 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
- F05D2240/00—Components
- F05D2240/20—Rotors
- F05D2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
- F05D2240/304—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor related to the trailing edge of a rotor blade
-
- 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
- Y10T29/49318—Repairing or disassembling
-
- 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
- Y10T29/49718—Repairing
- Y10T29/49732—Repairing by attaching repair preform, e.g., remaking, restoring, or patching
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Mechanical Engineering (AREA)
- Organic Chemistry (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Materials Engineering (AREA)
- Plasma & Fusion (AREA)
- Metallurgy (AREA)
- Physics & Mathematics (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Physical Vapour Deposition (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Separation Using Semi-Permeable Membranes (AREA)
- Application Of Or Painting With Fluid Materials (AREA)
- Furnace Housings, Linings, Walls, And Ceilings (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US10/818,962 US20050217110A1 (en) | 2004-04-06 | 2004-04-06 | Deposition repair of hollow items |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ATE496151T1 true ATE496151T1 (de) | 2011-02-15 |
Family
ID=34912695
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AT05252127T ATE496151T1 (de) | 2004-04-06 | 2005-04-05 | Abscheidungsreparatur von hohlen gegenständen |
Country Status (9)
| Country | Link |
|---|---|
| US (1) | US20050217110A1 (de) |
| EP (1) | EP1584702B1 (de) |
| JP (1) | JP4121516B2 (de) |
| CN (1) | CN1680068A (de) |
| AT (1) | ATE496151T1 (de) |
| CA (1) | CA2503800A1 (de) |
| DE (1) | DE602005025956D1 (de) |
| SG (1) | SG115822A1 (de) |
| UA (1) | UA90841C2 (de) |
Families Citing this family (30)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7540083B2 (en) * | 2005-09-28 | 2009-06-02 | Honeywell International Inc. | Method to modify an airfoil internal cooling circuit |
| US7552855B2 (en) * | 2005-10-13 | 2009-06-30 | United Technologies Corporation | Hole repair technique and apparatus |
| SG134184A1 (en) * | 2006-01-16 | 2007-08-29 | United Technologies Corp | Chordwidth restoration of a trailing edge of a turbine airfoil by laser clad |
| US20100257733A1 (en) * | 2006-07-20 | 2010-10-14 | Honeywell International, Inc. | High pressure single crystal turbine blade tip repair with laser cladding |
| EP1889680A1 (de) * | 2006-08-16 | 2008-02-20 | Siemens Aktiengesellschaft | Verfahren zum Schweissen von Turbinenbauteilen unter Verwendung eines in einem Hohlraum des Bauteiles eingeführten keramischen Kerns |
| US20090028707A1 (en) * | 2007-07-26 | 2009-01-29 | United Technologies Corporation | Apparatus and method for repairing airfoil tips |
| US8578579B2 (en) * | 2007-12-11 | 2013-11-12 | General Electric Company | System and method for adaptive machining |
| US20090193656A1 (en) * | 2008-02-04 | 2009-08-06 | General Electric Company | Steam turbine bucket with erosion durability |
| DE102008007820A1 (de) * | 2008-02-05 | 2009-08-06 | Mtu Aero Engines Gmbh | Verfahren zur Reparatur eines metallischen Hohlkörpers |
| US20090324841A1 (en) * | 2008-05-09 | 2009-12-31 | Siemens Power Generation, Inc. | Method of restoring near-wall cooled turbine components |
| DE102011089699B4 (de) * | 2011-12-22 | 2013-09-12 | Lufthansa Technik Ag | Vorrichtung zum Rekonturieren einer Gasturbinenschaufel |
| WO2014158245A1 (en) | 2013-03-14 | 2014-10-02 | Hodgson Benedict N | Airfoil with leading edge reinforcement |
| US20150132143A1 (en) * | 2013-11-11 | 2015-05-14 | Gerald J. Bruck | Welding process and reduced restraint weld joint |
| CN103831574B (zh) * | 2013-12-10 | 2016-03-23 | 贵州黎阳航空动力有限公司 | 空心涡轮叶片叶身堵盖修复工艺 |
| US10450871B2 (en) | 2015-02-26 | 2019-10-22 | Rolls-Royce Corporation | Repair of dual walled metallic components using directed energy deposition material addition |
| US10766105B2 (en) | 2015-02-26 | 2020-09-08 | Rolls-Royce Corporation | Repair of dual walled metallic components using braze material |
| US20160354953A1 (en) * | 2015-06-03 | 2016-12-08 | United Technologies Corporation | Repair or remanufacture of cooled components with an oxidation resistant braze |
| US10544683B2 (en) | 2016-08-30 | 2020-01-28 | Rolls-Royce Corporation | Air-film cooled component for a gas turbine engine |
| US10689984B2 (en) | 2016-09-13 | 2020-06-23 | Rolls-Royce Corporation | Cast gas turbine engine cooling components |
| US20180073390A1 (en) | 2016-09-13 | 2018-03-15 | Rolls-Royce Corporation | Additively deposited gas turbine engine cooling component |
| US10487660B2 (en) * | 2016-12-19 | 2019-11-26 | General Electric Company | Additively manufactured blade extension with internal features |
| US10625342B2 (en) * | 2017-02-22 | 2020-04-21 | General Electric Company | Method of repairing turbine component |
| EP3441181A1 (de) * | 2017-08-09 | 2019-02-13 | General Electric Company | Verfahren zur behandlung von aus äquiaxialem material oder direktional erstarrter struktur geformten komponenten sowie behandelte komponenten |
| CN108213832B (zh) * | 2017-12-29 | 2020-08-18 | 西安交通大学 | 一种实现单晶或定向晶合金叶片内流道复形的修复方法 |
| US11338396B2 (en) | 2018-03-08 | 2022-05-24 | Rolls-Royce Corporation | Techniques and assemblies for joining components |
| US11090771B2 (en) | 2018-11-05 | 2021-08-17 | Rolls-Royce Corporation | Dual-walled components for a gas turbine engine |
| US11305363B2 (en) | 2019-02-11 | 2022-04-19 | Rolls-Royce Corporation | Repair of through-hole damage using braze sintered preform |
| US11692446B2 (en) | 2021-09-23 | 2023-07-04 | Rolls-Royce North American Technologies, Inc. | Airfoil with sintered powder components |
| US11524350B1 (en) * | 2021-10-04 | 2022-12-13 | General Electric Company | Backwall strike braze repair |
| EP4474519A1 (de) * | 2023-06-09 | 2024-12-11 | Pratt & Whitney Canada Corp. | Reparatur von nickelbasierten und kobaltbasierten superlegierungen mittels hoch-entropie legierungen |
Family Cites Families (26)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3576065A (en) * | 1969-03-24 | 1971-04-27 | Chromalloy American Corp | Repair of apertured machine components |
| US4008844A (en) * | 1975-01-06 | 1977-02-22 | United Technologies Corporation | Method of repairing surface defects using metallic filler material |
| US4073639A (en) * | 1975-01-06 | 1978-02-14 | United Technologies Corporation | Metallic filler material |
| US4743462A (en) * | 1986-07-14 | 1988-05-10 | United Technologies Corporation | Method for preventing closure of cooling holes in hollow, air cooled turbine engine components during application of a plasma spray coating |
| US4726104A (en) * | 1986-11-20 | 1988-02-23 | United Technologies Corporation | Methods for weld repairing hollow, air cooled turbine blades and vanes |
| US5106010A (en) * | 1990-09-28 | 1992-04-21 | Chromalloy Gas Turbine Corporation | Welding high-strength nickel base superalloys |
| JP3032295B2 (ja) * | 1992-05-06 | 2000-04-10 | ユナイテッド・テクノロジーズ・コーポレイション | コバルトベース超合金物品の熱処理及び修理 |
| US5783318A (en) | 1994-06-22 | 1998-07-21 | United Technologies Corporation | Repaired nickel based superalloy |
| US5511721A (en) * | 1994-11-07 | 1996-04-30 | General Electric Company | Braze blocking insert for liquid phase brazing operations |
| US5640767A (en) * | 1995-01-03 | 1997-06-24 | Gen Electric | Method for making a double-wall airfoil |
| US5553370A (en) * | 1995-02-09 | 1996-09-10 | Pepe; John | Method for repair of steam turbine blades |
| JP3745427B2 (ja) * | 1995-11-14 | 2006-02-15 | Smc株式会社 | 真空圧制御用スロー排気バルブ |
| US5902647A (en) * | 1996-12-03 | 1999-05-11 | General Electric Company | Method for protecting passage holes in a metal-based substrate from becoming obstructed, and related compositions |
| US6049978A (en) * | 1996-12-23 | 2000-04-18 | Recast Airfoil Group | Methods for repairing and reclassifying gas turbine engine airfoil parts |
| US5794338A (en) * | 1997-04-04 | 1998-08-18 | General Electric Company | Method for repairing a turbine engine member damaged tip |
| US6329633B1 (en) * | 1998-11-20 | 2001-12-11 | United Technologies Corporation | Method and material for processing a component for laser machining |
| US6251315B1 (en) * | 1998-11-20 | 2001-06-26 | United Technologies Corporation | Method for disposing a laser blocking material on the interior of an airfoil |
| US6547210B1 (en) * | 2000-02-17 | 2003-04-15 | Wright Medical Technology, Inc. | Sacrificial insert for injection molding |
| US6460754B1 (en) * | 2000-08-02 | 2002-10-08 | Gen Electric | Prevention of braze alloy flow and stopoff material therefor |
| US6427327B1 (en) * | 2000-11-29 | 2002-08-06 | General Electric Company | Method of modifying cooled turbine components |
| EP1350860A1 (de) * | 2002-04-04 | 2003-10-08 | ALSTOM (Switzerland) Ltd | Verfahren zum Abdecken von Kühlungsöffnungen eines Gasturbinebauteils |
| US6754955B1 (en) * | 2003-01-30 | 2004-06-29 | General Electric Company | Method or repairing trailing edge portions of partitions in turbine diaphragms |
| US7216428B2 (en) * | 2003-03-03 | 2007-05-15 | United Technologies Corporation | Method for turbine element repairing |
| US7509734B2 (en) * | 2003-03-03 | 2009-03-31 | United Technologies Corporation | Repairing turbine element |
| US20060248718A1 (en) * | 2005-05-06 | 2006-11-09 | United Technologies Corporation | Superalloy repair methods and inserts |
| US7761989B2 (en) * | 2005-11-22 | 2010-07-27 | United Technologies Corporation | Methods for repairing gas turbine engine components |
-
2004
- 2004-04-06 US US10/818,962 patent/US20050217110A1/en not_active Abandoned
-
2005
- 2005-04-04 CA CA002503800A patent/CA2503800A1/en not_active Abandoned
- 2005-04-05 DE DE602005025956T patent/DE602005025956D1/de not_active Expired - Lifetime
- 2005-04-05 UA UAA200503189A patent/UA90841C2/ru unknown
- 2005-04-05 EP EP05252127A patent/EP1584702B1/de not_active Expired - Lifetime
- 2005-04-05 AT AT05252127T patent/ATE496151T1/de not_active IP Right Cessation
- 2005-04-05 JP JP2005108140A patent/JP4121516B2/ja not_active Expired - Fee Related
- 2005-04-05 SG SG200502022A patent/SG115822A1/en unknown
- 2005-04-06 CN CNA2005100640526A patent/CN1680068A/zh active Pending
Also Published As
| Publication number | Publication date |
|---|---|
| US20050217110A1 (en) | 2005-10-06 |
| EP1584702A1 (de) | 2005-10-12 |
| UA90841C2 (ru) | 2010-06-10 |
| CN1680068A (zh) | 2005-10-12 |
| JP4121516B2 (ja) | 2008-07-23 |
| JP2005299652A (ja) | 2005-10-27 |
| EP1584702B1 (de) | 2011-01-19 |
| DE602005025956D1 (de) | 2011-03-03 |
| SG115822A1 (en) | 2005-10-28 |
| CA2503800A1 (en) | 2005-10-06 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| RER | Ceased as to paragraph 5 lit. 3 law introducing patent treaties |