SG127803A1 - Method of manufacturing a hollow blade that includes a recessed tip cap and method of repairing sucha blade - Google Patents
Method of manufacturing a hollow blade that includes a recessed tip cap and method of repairing sucha bladeInfo
- Publication number
- SG127803A1 SG127803A1 SG200603109A SG200603109A SG127803A1 SG 127803 A1 SG127803 A1 SG 127803A1 SG 200603109 A SG200603109 A SG 200603109A SG 200603109 A SG200603109 A SG 200603109A SG 127803 A1 SG127803 A1 SG 127803A1
- Authority
- SG
- Singapore
- Prior art keywords
- blade
- repairing
- manufacturing
- tip cap
- plate
- 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
- 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
- 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
- F01D5/20—Specially-shaped blade tips to seal space between tips and stator
-
- 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
- F05D2230/21—Manufacture essentially without removing material by casting
-
- 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
- F05D2230/23—Manufacture essentially without removing material by permanently joining parts together
- F05D2230/232—Manufacture essentially without removing material by permanently joining parts together by welding
- F05D2230/237—Brazing
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Devices For Post-Treatments, Processing, Supply, Discharge, And Other Processes (AREA)
- Moulding By Coating Moulds (AREA)
- Polishing Bodies And Polishing Tools (AREA)
- Coating Apparatus (AREA)
- Electrical Discharge Machining, Electrochemical Machining, And Combined Machining (AREA)
Abstract
The invention relates to a method of manufacturing a hollow metal blade (1), comprising at least one side wall (2, 3) and a recessed tip cap (7), characterized in that: a) a hollow blade, which comprises at least one side wall (2, 3) and the tip of which is open, is manufactured by casting; b) a plate of a laminate, comprising at least the metal of the blade and a brazing material, is manufactured; c) the plate is brazed to the top of the side wall (2, 3) of the blade by pressing the plate onto the blade; and d) the recessed tip cap (7), comprising at least a bottom (8) and at least a squealer tip (9, 10), is machined in the plate. Thanks to the invention, since the blade is manufactured beforehand with an open tip, the core can be held in place, during the casting operation, by the top, thereby ensuring great precision in the positioning of the core and therefore in the thickness of the walls (2, 3) of the blade. The invention also relates to a method of repairing a blade (1).
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0504648A FR2885310B1 (en) | 2005-05-09 | 2005-05-09 | METHOD FOR MANUFACTURING A HOLLOW DAWN COMPRISING A TUB SHAPED TOP, A METHOD FOR REPAIRING SUCH A BLADE AND DAWN OBTAINED BY ONE OF THESE PROCESSES |
Publications (1)
Publication Number | Publication Date |
---|---|
SG127803A1 true SG127803A1 (en) | 2006-12-29 |
Family
ID=35106882
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SG200603109A SG127803A1 (en) | 2005-05-09 | 2006-05-09 | Method of manufacturing a hollow blade that includes a recessed tip cap and method of repairing sucha blade |
Country Status (12)
Country | Link |
---|---|
EP (1) | EP1721698B1 (en) |
JP (1) | JP4945166B2 (en) |
CN (1) | CN100528411C (en) |
AT (1) | ATE415237T1 (en) |
BR (1) | BRPI0601517B1 (en) |
CA (1) | CA2546253C (en) |
DE (1) | DE602006003803D1 (en) |
FR (1) | FR2885310B1 (en) |
MX (1) | MXPA06005231A (en) |
RU (1) | RU2410226C2 (en) |
SG (1) | SG127803A1 (en) |
TW (1) | TWI365115B (en) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8092178B2 (en) | 2008-11-28 | 2012-01-10 | Pratt & Whitney Canada Corp. | Turbine blade for a gas turbine engine |
ITCO20110060A1 (en) * | 2011-12-12 | 2013-06-13 | Nuovo Pignone Spa | STEAM TURBINE, PALLET AND METHOD |
US9689265B2 (en) | 2012-04-09 | 2017-06-27 | General Electric Company | Thin-walled reinforcement lattice structure for hollow CMC buckets |
US20130302166A1 (en) * | 2012-05-09 | 2013-11-14 | Ching-Pang Lee | Turbine blade with chamfered squealer tip formed from multiple components and convective cooling holes |
GB201302262D0 (en) | 2013-02-08 | 2013-03-27 | Rolls Royce Plc | Manufacture of hollow aerofoil |
DE102015226766A1 (en) * | 2015-12-28 | 2017-06-29 | Siemens Aktiengesellschaft | Method for producing an airfoil for a turbine blade of a turbine plant |
US10702958B2 (en) * | 2017-02-22 | 2020-07-07 | General Electric Company | Method of manufacturing turbine airfoil and tip component thereof using ceramic core with witness feature |
CN108581346B (en) * | 2018-08-14 | 2020-05-19 | 中国航发南方工业有限公司 | Hollow blade anchor clamps for brazing |
US11143033B2 (en) * | 2018-11-08 | 2021-10-12 | General Electric Company | Turbomachine blade tip attachment |
FR3088839B1 (en) * | 2018-11-23 | 2022-09-09 | Safran Aircraft Engines | METHOD FOR MANUFACTURING A METAL PART FOR AN AIRCRAFT TURBOMACHINE |
CN112031878A (en) * | 2020-11-05 | 2020-12-04 | 中国航发沈阳黎明航空发动机有限责任公司 | Turbine rotor blade apex double-wall structure |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS58172406A (en) * | 1982-04-05 | 1983-10-11 | Hitachi Ltd | Laminated blade for gas turbine |
US4487550A (en) * | 1983-01-27 | 1984-12-11 | The United States Of America As Represented By The Secretary Of The Air Force | Cooled turbine blade tip closure |
FR2691658B1 (en) * | 1992-05-27 | 1994-07-22 | Snecma | SUPERALLOY PART COMPRISING A SUPPORT AND METHOD FOR PRODUCING THE SUPPORT. |
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 |
US6004683A (en) * | 1992-11-04 | 1999-12-21 | C. A. Patents, L.L.C. | Plural layered metal repair tape |
WO1997037800A1 (en) * | 1996-04-10 | 1997-10-16 | Tmt Research Development, Inc. | Coating methods, coating products and coated articles |
US5794338A (en) * | 1997-04-04 | 1998-08-18 | General Electric Company | Method for repairing a turbine engine member damaged tip |
US5822852A (en) * | 1997-07-14 | 1998-10-20 | General Electric Company | Method for replacing blade tips of directionally solidified and single crystal turbine blades |
DE19922012C1 (en) * | 1999-05-12 | 2000-10-19 | Mtu Muenchen Gmbh | Rotor unit machining takes measurements of the actual surfaces at the fused joint for the flash to be removed and a nominal surface structure is machined from stored data to give the required flow characteristics |
US6332272B1 (en) * | 2000-01-07 | 2001-12-25 | Siemens Westinghouse Power Corporation | Method of repairing a turbine blade |
US6908288B2 (en) * | 2001-10-31 | 2005-06-21 | General Electric Company | Repair of advanced gas turbine blades |
US6838190B2 (en) * | 2001-12-20 | 2005-01-04 | General Electric Company | Article with intermediate layer and protective layer, and its fabrication |
JP2003222026A (en) * | 2002-01-30 | 2003-08-08 | Hitachi Ltd | Method for manufacturing turbine blade, and turbine blade |
US20050091848A1 (en) * | 2003-11-03 | 2005-05-05 | Nenov Krassimir P. | Turbine blade and a method of manufacturing and repairing a turbine blade |
-
2005
- 2005-05-09 FR FR0504648A patent/FR2885310B1/en not_active Expired - Fee Related
-
2006
- 2006-05-05 AT AT06113599T patent/ATE415237T1/en not_active IP Right Cessation
- 2006-05-05 DE DE602006003803T patent/DE602006003803D1/en active Active
- 2006-05-05 EP EP06113599A patent/EP1721698B1/en active Active
- 2006-05-05 CA CA2546253A patent/CA2546253C/en active Active
- 2006-05-06 RU RU2006115833/02A patent/RU2410226C2/en active
- 2006-05-08 TW TW095116231A patent/TWI365115B/en active
- 2006-05-08 JP JP2006129031A patent/JP4945166B2/en active Active
- 2006-05-09 BR BRPI0601517-4A patent/BRPI0601517B1/en active IP Right Grant
- 2006-05-09 CN CN200610078305.XA patent/CN100528411C/en active Active
- 2006-05-09 MX MXPA06005231A patent/MXPA06005231A/en active IP Right Grant
- 2006-05-09 SG SG200603109A patent/SG127803A1/en unknown
Also Published As
Publication number | Publication date |
---|---|
RU2410226C2 (en) | 2011-01-27 |
TW200706301A (en) | 2007-02-16 |
CN100528411C (en) | 2009-08-19 |
CA2546253A1 (en) | 2006-11-09 |
BRPI0601517B1 (en) | 2018-04-03 |
BRPI0601517A (en) | 2007-07-17 |
RU2006115833A (en) | 2007-11-20 |
JP4945166B2 (en) | 2012-06-06 |
TWI365115B (en) | 2012-06-01 |
DE602006003803D1 (en) | 2009-01-08 |
JP2006316790A (en) | 2006-11-24 |
CN1931475A (en) | 2007-03-21 |
FR2885310B1 (en) | 2008-12-26 |
FR2885310A1 (en) | 2006-11-10 |
MXPA06005231A (en) | 2007-02-16 |
EP1721698A1 (en) | 2006-11-15 |
EP1721698B1 (en) | 2008-11-26 |
CA2546253C (en) | 2013-07-30 |
ATE415237T1 (en) | 2008-12-15 |
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