FR2411063A1 - Procede pour recharger des bandages d'ailettes de turbines - Google Patents
Procede pour recharger des bandages d'ailettes de turbinesInfo
- Publication number
- FR2411063A1 FR2411063A1 FR7834743A FR7834743A FR2411063A1 FR 2411063 A1 FR2411063 A1 FR 2411063A1 FR 7834743 A FR7834743 A FR 7834743A FR 7834743 A FR7834743 A FR 7834743A FR 2411063 A1 FR2411063 A1 FR 2411063A1
- Authority
- FR
- France
- Prior art keywords
- fin
- bandages
- refection
- metal alloy
- area
- 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.)
- Granted
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
-
- 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
- F01D5/22—Blade-to-blade connections, e.g. for damping vibrations
- F01D5/225—Blade-to-blade connections, e.g. for damping vibrations by shrouding
-
- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
-
- 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
- Y10T29/49746—Repairing by applying fluent material, e.g., coating, casting
-
- 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
- Y10T29/4998—Combined manufacture including applying or shaping of fluent material
- Y10T29/49982—Coating
- Y10T29/49986—Subsequent to metal working
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Powder Metallurgy (AREA)
- Coating By Spraying Or Casting (AREA)
Abstract
L'INVENTION CONCERNE L'INDUSTRIE DES MOTEURS A TURBINES. LE PROCEDE DE REFECTION D'AILETTES DE TURBINE USEES EN ALLIAGE DE METAL CONSISTE A ARASER PAR MEULAGE JUSQU'A UNE DIMENSION DETERMINEE AVEC PRECISION L'UNE DES ARETES DU BANDAGE DE MONTAGE A L'UNE DES EXTREMITES DE L'AILETTE; A MASQUER LE BANDAGE DE CHAQUE COTE DE LADITE ARETE APRES ARASEMENT; A SOUMETTRE LADITE ARETE ARASEE A UN JET DE PLASMA CONTENANT UN ALLIAGE METALLIQUE DE FACON A RECONSTITUER SENSIBLEMENT LADITE AILETTE DANS SES DIMENSIONS INITIALES; PUIS A FRITTER LADITE AILETTE A DES TEMPERATURES ELEVEES PENDANT UN LAPS DE TEMPS PREDETERMINE POUR CONSOLIDER LADITE REFECTION. APPLICATION NOTAMMENT A LA REFECTION D'AILETTES COMPOSEES EN MAJEURE PARTIE DE COBALT OU DE NICKEL.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US05/859,438 US4155152A (en) | 1977-12-12 | 1977-12-12 | Method of restoring the shrouds of turbine blades |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2411063A1 true FR2411063A1 (fr) | 1979-07-06 |
FR2411063B1 FR2411063B1 (fr) | 1984-02-17 |
Family
ID=25330926
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7834743A Granted FR2411063A1 (fr) | 1977-12-12 | 1978-12-11 | Procede pour recharger des bandages d'ailettes de turbines |
Country Status (13)
Country | Link |
---|---|
US (1) | US4155152A (fr) |
JP (1) | JPS5493657A (fr) |
AU (1) | AU531630B2 (fr) |
BE (1) | BE872693A (fr) |
CA (1) | CA1119896A (fr) |
CH (1) | CH628559A5 (fr) |
DE (1) | DE2853545A1 (fr) |
ES (1) | ES475940A1 (fr) |
FR (1) | FR2411063A1 (fr) |
GB (1) | GB2009635B (fr) |
IT (1) | IT1100539B (fr) |
NL (1) | NL7812087A (fr) |
SE (1) | SE436173B (fr) |
Families Citing this family (46)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4291448A (en) * | 1977-12-12 | 1981-09-29 | Turbine Components Corporation | Method of restoring the shrouds of turbine blades |
GB2091139B (en) * | 1981-01-12 | 1984-05-23 | Refurbished Turbine Components | Turbine blade repair |
US4370789A (en) * | 1981-03-20 | 1983-02-01 | Schilke Peter W | Fabrication of gas turbine water-cooled composite nozzle and bucket hardware employing plasma spray process |
JPS59131703A (ja) * | 1983-01-18 | 1984-07-28 | Toshiba Corp | 蒸気タ−ビン動翼の補修方法 |
JPH0660563B2 (ja) * | 1984-08-02 | 1994-08-10 | 株式会社東芝 | 動翼カバ− |
US4822248A (en) * | 1987-04-15 | 1989-04-18 | Metallurgical Industries, Inc. | Rebuilt shrouded turbine blade and method of rebuilding the same |
DE3802741C2 (de) * | 1988-01-30 | 1997-02-13 | Asea Brown Boveri | Verfahren zur Verspannung von Schaufeln |
AU605378B2 (en) * | 1988-11-01 | 1991-01-10 | Sermatech International, Inc. | Shrouded turbine blade |
US5272809A (en) * | 1990-09-04 | 1993-12-28 | United Technologies Corporation | Technique for direct bonding cast and wrought materials |
GB2251034B (en) * | 1990-12-20 | 1995-05-17 | Rolls Royce Plc | Shrouded aerofoils |
US5140737A (en) * | 1991-01-10 | 1992-08-25 | Noland Edmund B | In situ flywheel repair method |
US5146679A (en) * | 1991-01-16 | 1992-09-15 | Ortolano Ralph J | Method of converting grouped blading to equivalent integral covered blading |
US5238368A (en) * | 1991-01-16 | 1993-08-24 | Ortolano Ralph J | Converting grouped blading to equivalent integral covered blading |
DE4237052A1 (de) * | 1992-11-03 | 1994-05-05 | Mtu Muenchen Gmbh | Vorrichtung zur Reparaturschweißung der Blattspitzen von Leit- oder Laufschaufeln für Turbomaschinen |
DE4310896C1 (de) * | 1993-04-02 | 1994-03-24 | Thyssen Industrie | Verfahren zum Herstellen von verschleißfesten Kanten an Turbinenschaufeln |
US5525429A (en) * | 1995-03-06 | 1996-06-11 | General Electric Company | Laser shock peening surface enhancement for gas turbine engine high strength rotor alloy repair |
US5735044A (en) * | 1995-12-12 | 1998-04-07 | General Electric Company | Laser shock peening for gas turbine engine weld repair |
JP3178327B2 (ja) * | 1996-01-31 | 2001-06-18 | 株式会社日立製作所 | 蒸気タービン |
US6037004A (en) * | 1997-12-19 | 2000-03-14 | United Technologies Corporation | Shield and method for protecting an airfoil surface |
US5916638A (en) * | 1997-12-19 | 1999-06-29 | United Technologies Corporation | Method for applying a coating to the tip of a flow directing assembly |
US6034344A (en) * | 1997-12-19 | 2000-03-07 | United Technologies Corp. | Method for applying material to a face of a flow directing assembly for a gas turbine engine |
SG80000A1 (en) * | 1997-12-19 | 2001-04-17 | United Technologies Corp | A fixture for use in disposing a region of material on the shroud of a rotor blade |
US6233822B1 (en) * | 1998-12-22 | 2001-05-22 | General Electric Company | Repair of high pressure turbine shrouds |
EP1143030A1 (fr) | 2000-04-03 | 2001-10-10 | ABB Alstom Power N.V. | Matériau pour extrémité d'une aube de turbine et procédé de sa fabrication ou réparation |
US6363612B1 (en) * | 2000-12-27 | 2002-04-02 | General Electric Company | Method of reducing burr formation during turbine bucket cover machining |
GB0112876D0 (en) | 2001-05-26 | 2001-07-18 | Rolls Royce Plc | A method of manufacturing an article |
JP4028442B2 (ja) * | 2002-06-26 | 2007-12-26 | 株式会社東芝 | ガスタービン翼の変形修正装置及び方法 |
US6875476B2 (en) * | 2003-01-15 | 2005-04-05 | General Electric Company | Methods and apparatus for manufacturing turbine engine components |
US7009137B2 (en) | 2003-03-27 | 2006-03-07 | Honeywell International, Inc. | Laser powder fusion repair of Z-notches with nickel based superalloy powder |
FR2860741B1 (fr) * | 2003-10-10 | 2007-04-13 | Snecma Moteurs | Procede de reparation de pieces metalliques notamment d'aubes de turbine de moteur a turbine a gaz |
US8205334B2 (en) * | 2005-07-15 | 2012-06-26 | United Technologies Corporation | Method for repairing a gas turbine engine component |
US20070141261A1 (en) * | 2005-12-20 | 2007-06-21 | General Electric Company | Method and apparatus for fabricating turbine engine components |
US8703044B2 (en) * | 2006-01-03 | 2014-04-22 | General Electric Company | Machine components and methods of fabricating and repairing |
US7653994B2 (en) * | 2006-03-22 | 2010-02-02 | General Electric Company | Repair of HPT shrouds with sintered preforms |
EP2213837A1 (fr) * | 2009-01-29 | 2010-08-04 | Siemens Aktiengesellschaft | Système de pale de turbine |
US8277189B2 (en) * | 2009-11-12 | 2012-10-02 | General Electric Company | Turbine blade and rotor |
US8708655B2 (en) | 2010-09-24 | 2014-04-29 | United Technologies Corporation | Blade for a gas turbine engine |
US9810069B2 (en) * | 2012-07-02 | 2017-11-07 | Ansaldo Energia Switzerland AG | Repair of a shrouded blade |
US9863249B2 (en) | 2012-12-04 | 2018-01-09 | Siemens Energy, Inc. | Pre-sintered preform repair of turbine blades |
FR3001758B1 (fr) * | 2013-02-01 | 2016-07-15 | Snecma | Aube de rotor de turbomachine |
RU2542035C2 (ru) * | 2013-03-22 | 2015-02-20 | Александр Александрович Макушин | Способ ремонта цилиндропоршневой группы двигателей внутреннего сгорания |
RU2533236C1 (ru) * | 2013-08-15 | 2014-11-20 | Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Саратовский государственный аграрный университет имени Н.И. Вавилова" | Способ восстановления изношенного крестового ножа |
DE102016207863A1 (de) * | 2016-05-09 | 2017-11-09 | MTU Aero Engines AG | Verfahren zum Bearbeiten wenigstens eines Bauteilbereichs eines Bauteils und Maskierungselement zum partiellen Abdecken eines zu bearbeitenden Bauteils |
CN106862789A (zh) * | 2017-03-03 | 2017-06-20 | 贵州凯阳航空发动机有限公司 | K4208合金在低压涡轮转子叶片叶冠耐磨合金焊接的应用 |
CN108326510A (zh) * | 2018-03-02 | 2018-07-27 | 河钢股份有限公司承德分公司 | 离心风机叶轮修复结构及修复方法 |
FR3079847B1 (fr) * | 2018-04-10 | 2023-11-10 | Safran Aircraft Engines | Procede de fabrication d'un element aubage metallique d'une turbomachine d'aeronef |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3711310A (en) * | 1971-07-26 | 1973-01-16 | United Aircraft Corp | Repair process for aluminum and magnesium articles |
DE2640755A1 (de) * | 1975-09-15 | 1977-03-17 | Cretella Salvatore | Verfahren zur erneuernden oberflaechenbehandlung von aerodynamischen turbinen-komponenten, wie laufschaufeln und leitschaufeln |
US4028788A (en) * | 1976-01-12 | 1977-06-14 | Demusis Ralph T | Method of refurbishing turbine blade air seal flanges |
FR2354391A1 (fr) * | 1976-06-07 | 1978-01-06 | Cretella Salvatore | Procede pour remettre a neuf notamment des composants de turbines |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3004336A (en) * | 1959-10-12 | 1961-10-17 | Harijs B Timuska | Method of reconditioning worn-out surfaces of aluminum alloy pistons |
US3436512A (en) * | 1966-04-13 | 1969-04-01 | Coast Metals Inc | Method of spray coating gas seals of gas turbines and the like |
US3607381A (en) * | 1968-06-14 | 1971-09-21 | Platron Corp | Spray process for creating electrical circuits |
US3642519A (en) * | 1969-03-21 | 1972-02-15 | Us Air Force | Method for the development of hard coat seal surfaces |
US3606665A (en) * | 1969-09-11 | 1971-09-21 | Harold Glucoft | Method of restoring worn brake surfaces |
US3814447A (en) * | 1972-11-02 | 1974-06-04 | Ramsey Corp | Sealing element for use in internal combustion engines |
US3981688A (en) * | 1973-07-05 | 1976-09-21 | Ford Motor Company | Coating for rotary engine rotor housings and method of making |
-
1977
- 1977-12-12 US US05/859,438 patent/US4155152A/en not_active Expired - Lifetime
-
1978
- 1978-12-08 CA CA000317593A patent/CA1119896A/fr not_active Expired
- 1978-12-11 FR FR7834743A patent/FR2411063A1/fr active Granted
- 1978-12-11 GB GB7847998A patent/GB2009635B/en not_active Expired
- 1978-12-11 SE SE7812706A patent/SE436173B/sv unknown
- 1978-12-12 CH CH1264778A patent/CH628559A5/fr not_active IP Right Cessation
- 1978-12-12 DE DE19782853545 patent/DE2853545A1/de not_active Withdrawn
- 1978-12-12 AU AU42411/78A patent/AU531630B2/en not_active Expired
- 1978-12-12 NL NL7812087A patent/NL7812087A/xx not_active Application Discontinuation
- 1978-12-12 BE BE192268A patent/BE872693A/fr not_active IP Right Cessation
- 1978-12-12 JP JP15407578A patent/JPS5493657A/ja active Pending
- 1978-12-12 ES ES475940A patent/ES475940A1/es not_active Expired
- 1978-12-12 IT IT30745/78A patent/IT1100539B/it active
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3711310A (en) * | 1971-07-26 | 1973-01-16 | United Aircraft Corp | Repair process for aluminum and magnesium articles |
DE2640755A1 (de) * | 1975-09-15 | 1977-03-17 | Cretella Salvatore | Verfahren zur erneuernden oberflaechenbehandlung von aerodynamischen turbinen-komponenten, wie laufschaufeln und leitschaufeln |
US4028788A (en) * | 1976-01-12 | 1977-06-14 | Demusis Ralph T | Method of refurbishing turbine blade air seal flanges |
FR2354391A1 (fr) * | 1976-06-07 | 1978-01-06 | Cretella Salvatore | Procede pour remettre a neuf notamment des composants de turbines |
Also Published As
Publication number | Publication date |
---|---|
SE7812706L (sv) | 1979-06-13 |
GB2009635B (en) | 1982-03-17 |
AU4241178A (en) | 1979-06-21 |
GB2009635A (en) | 1979-06-20 |
CH628559A5 (fr) | 1982-03-15 |
SE436173B (sv) | 1984-11-19 |
JPS5493657A (en) | 1979-07-24 |
ES475940A1 (es) | 1979-05-01 |
IT1100539B (it) | 1985-09-28 |
US4155152A (en) | 1979-05-22 |
CA1119896A (fr) | 1982-03-16 |
DE2853545A1 (de) | 1979-06-13 |
NL7812087A (nl) | 1979-06-14 |
BE872693A (fr) | 1979-03-30 |
AU531630B2 (en) | 1983-09-01 |
FR2411063B1 (fr) | 1984-02-17 |
IT7830745A0 (it) | 1978-12-12 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |