SG144880A1 - A method of manufacturing a component by consolidating powder material - Google Patents
A method of manufacturing a component by consolidating powder materialInfo
- Publication number
- SG144880A1 SG144880A1 SG200800727-0A SG2008007270A SG144880A1 SG 144880 A1 SG144880 A1 SG 144880A1 SG 2008007270 A SG2008007270 A SG 2008007270A SG 144880 A1 SG144880 A1 SG 144880A1
- Authority
- SG
- Singapore
- Prior art keywords
- manufacturing
- component
- powder material
- union piece
- disc
- Prior art date
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
- B23P6/005—Repairing turbine components, e.g. moving or stationary blades, rotors using only replacement pieces of a particular form
-
- 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
- B22F5/00—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product
- B22F5/04—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product of turbine blades
-
- 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
- B22F7/062—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 involving the connection or repairing of preformed parts
-
- 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
- B23P15/00—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
- B23P15/04—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass turbine or like blades from several pieces
-
- 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
- F05D2230/20—Manufacture essentially without removing material
- F05D2230/22—Manufacture essentially without removing material by sintering
-
- 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
- F05D2230/60—Assembly methods
- F05D2230/64—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins
-
- 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
- Y10T29/49718—Repairing
- Y10T29/49732—Repairing by attaching repair preform, e.g., remaking, restoring, or patching
- Y10T29/49734—Repairing by attaching repair preform, e.g., remaking, restoring, or patching and removing damaged material
- Y10T29/49737—Metallurgically attaching preform
-
- 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
- Y10T29/49826—Assembling or joining
- Y10T29/49895—Associating parts by use of aligning means [e.g., use of a drift pin or a "fixture"]
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Materials Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Powder Metallurgy (AREA)
- Pressure Welding/Diffusion-Bonding (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GBGB0701904.5A GB0701904D0 (en) | 2007-02-01 | 2007-02-01 | A method of manufacturing a component by consolidating powder material |
Publications (1)
Publication Number | Publication Date |
---|---|
SG144880A1 true SG144880A1 (en) | 2008-08-28 |
Family
ID=37891091
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SG200800727-0A SG144880A1 (en) | 2007-02-01 | 2008-01-25 | A method of manufacturing a component by consolidating powder material |
Country Status (4)
Country | Link |
---|---|
US (1) | US8141225B2 (de) |
EP (1) | EP1952917B1 (de) |
GB (1) | GB0701904D0 (de) |
SG (1) | SG144880A1 (de) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102009033835B4 (de) | 2009-07-18 | 2012-01-19 | Mtu Aero Engines Gmbh | Verfahren zum Austauschen einer Schaufel eines Rotors mit integrierter Beschaufelung und ein derartiger Rotor |
FR2949366B1 (fr) * | 2009-08-31 | 2011-11-18 | Snecma | Realisation par procede mim d'un morceau de piece pour la reparation d'une aube de distributeur de turbine |
US9700941B2 (en) * | 2012-10-03 | 2017-07-11 | Siemens Energy, Inc. | Method for repairing a component for use in a turbine engine |
CN103624493B (zh) * | 2013-11-26 | 2016-03-23 | 中国南方航空工业(集团)有限公司 | 航空发动机的压气机对半机匣的加工方法 |
GB201405988D0 (en) | 2014-04-03 | 2014-05-21 | Rolls Royce Plc | Bonding method |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3429700A (en) | 1966-09-20 | 1969-02-25 | Teleflex Inc | Method of producing composite metal articles by uniting two identical shapes |
GB1224521A (en) * | 1968-03-27 | 1971-03-10 | Rolls Royce | Method of making an aerofoil-shaped blade or blade blank |
US3905723A (en) * | 1972-10-27 | 1975-09-16 | Norton Co | Composite ceramic turbine rotor |
US4172107A (en) * | 1975-11-10 | 1979-10-23 | Tokyo Shibaura Electric Co., Ltd. | Method of manufacturing composite ceramic articles |
JPS5841775A (ja) | 1981-09-07 | 1983-03-11 | 大同特殊鋼株式会社 | セラミツクス−金属複合体の製造方法 |
JPS5964185A (ja) | 1982-10-06 | 1984-04-12 | Toyota Motor Corp | 焼結部材の接合方法 |
JPS61197476A (ja) | 1985-02-26 | 1986-09-01 | 株式会社東芝 | 複合体およびその製造方法 |
US4594219A (en) | 1985-08-02 | 1986-06-10 | Metals, Ltd. | Powder metal consolidation of multiple preforms |
JPS6372804A (ja) | 1986-09-12 | 1988-04-02 | Fujitsu Ltd | 焼結部品の製造方法 |
JPH08225811A (ja) | 1995-02-20 | 1996-09-03 | Olympus Optical Co Ltd | 金属粉末またはセラミクス粉末焼結体 およびその製造方法 |
FR2739583B1 (fr) | 1995-10-04 | 1997-12-12 | Snecma | Procede d'assemblage par frittage reactif de pieces en materiau intermetallique et applications derivees |
DE102005019077A1 (de) * | 2005-04-23 | 2006-10-26 | Mtu Aero Engines Gmbh | Schaufel einer Strömungsmaschine und Verfahren zur Herstellung und/oder Reparatur derselben |
-
2007
- 2007-02-01 GB GBGB0701904.5A patent/GB0701904D0/en not_active Ceased
-
2008
- 2008-01-16 EP EP08250213A patent/EP1952917B1/de not_active Expired - Fee Related
- 2008-01-17 US US12/007,961 patent/US8141225B2/en not_active Expired - Fee Related
- 2008-01-25 SG SG200800727-0A patent/SG144880A1/en unknown
Also Published As
Publication number | Publication date |
---|---|
EP1952917A3 (de) | 2010-01-20 |
EP1952917A2 (de) | 2008-08-06 |
US8141225B2 (en) | 2012-03-27 |
US20100281669A1 (en) | 2010-11-11 |
EP1952917B1 (de) | 2011-12-21 |
GB0701904D0 (en) | 2007-03-14 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
SG169281A1 (en) | A method of joining components | |
EP1816112A3 (de) | Verfahren zur Bildung einer Keramik-Keramik-Verbindung | |
SG144880A1 (en) | A method of manufacturing a component by consolidating powder material | |
MX2009012142A (es) | Metodo para producir una conexion de soldadura por friccion entre componentes planos multiples localizados uno sobre otro con dfeformacion de un collar despues de la soldadura por friccion; conexion de soldadura por friccion producida usando el metod | |
WO2011035858A8 (de) | Verfahren zur herstellung eines verbundbauteils | |
TW200633947A (en) | Joined body and manufacturing method for the same | |
WO2008022615A3 (de) | Selbstaushärtendes material und verfahren zum schichtweisen aufbau von modellen | |
ATE438040T1 (de) | Verfahren zum herstellen einer nagelverbindung sowie nagel hierfür | |
MX2017005764A (es) | Union de objetos juntos. | |
WO2011133850A3 (en) | Cutting elements for earth-boring tools, earth-boring tools including such cutting elements and related methods | |
WO2008089873A3 (de) | Verfahren zur herstellung eines aus kunststoff und metall bestehenden hybrid-bauteiles sowie metall-kunststoff-verbundkörper | |
WO2008085570A3 (en) | Flux formulations | |
MX349599B (es) | Ensamble de pistón, cilindro de presión de fluido, método para fabricar el ensamble de pistón. | |
WO2012094160A3 (en) | Dual hardness steel article and method of making | |
WO2008141637A3 (de) | Phosphoreszente metallkomplexverbindung, strahlungsemittierendes bauelement aufweisend eine phosphoreszente metallkomplexverbindung und verfahren zur herstellung einer phosphoreszenten metallkomplexverbindung | |
EP2418297A3 (de) | Verfahren zur Herstellung eines faserverstärkten Metallmatrizenverbundstoffartikels | |
WO2009047010A3 (de) | Verfahren zum verbinden eines ersten materials mit einem zweiten material im flugzeugbau | |
WO2009111504A8 (en) | Tools having compacted powder metal work surfaces, and method | |
WO2008119900A3 (fr) | Procede de fabrication d'un dispositif de type echangeur de chaleur en ceramique et dispositifs obtenus par le procede | |
WO2010012255A3 (de) | Verfahren zum erzeugen einer fügeverbindung zwischen einem werkstoff und einem einkristallinen oder gerichtet erstarrten werkstoff durch erzeugung einer polykristallinen schicht an diesem letzten werkstoff | |
EP1743724A3 (de) | Verfahren zur Herstellung einer formschlüssigen Verbindung zwischen einem Werkzeugeinsatz und einem Werkzeugträger eines rotierenden Werkzeugs | |
WO2009015984A3 (de) | Waferfügeverfahren mit senterschritt, waferverbund sowie chip | |
WO2011082377A3 (en) | Abrasive article incorporating an infiltrated abrasive segment | |
WO2008087299A3 (fr) | Procede de fabrication et element de structure | |
GB0622691D0 (en) | Method and apparatus for controlling the geometry of a composite component |