TWI365115B - Method of manufacturing a hollow blade that includes a recessed tip cap and method of repairing such a blade - Google Patents
Method of manufacturing a hollow blade that includes a recessed tip cap and method of repairing such a bladeInfo
- Publication number
- TWI365115B TWI365115B TW095116231A TW95116231A TWI365115B TW I365115 B TWI365115 B TW I365115B TW 095116231 A TW095116231 A TW 095116231A TW 95116231 A TW95116231 A TW 95116231A TW I365115 B TWI365115 B TW I365115B
- Authority
- TW
- Taiwan
- Prior art keywords
- blade
- repairing
- manufacturing
- layer
- tip cap
- Prior art date
Links
- 238000000034 method Methods 0.000 title abstract 2
- 238000004519 manufacturing process Methods 0.000 title 1
- 238000005219 brazing Methods 0.000 abstract 3
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 abstract 2
- 239000000463 material Substances 0.000 abstract 2
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 abstract 1
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 abstract 1
- 229910000990 Ni alloy Inorganic materials 0.000 abstract 1
- 229910052796 boron Inorganic materials 0.000 abstract 1
- 238000005266 casting Methods 0.000 abstract 1
- 239000002648 laminated material Substances 0.000 abstract 1
- 238000003754 machining Methods 0.000 abstract 1
- 239000002184 metal Substances 0.000 abstract 1
- 229910052751 metal Inorganic materials 0.000 abstract 1
- 229910052759 nickel Inorganic materials 0.000 abstract 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 abstract 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
- B23P6/005—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)
- Coating Apparatus (AREA)
- Polishing Bodies And Polishing Tools (AREA)
- Electrical Discharge Machining, Electrochemical Machining, And Combined Machining (AREA)
- Devices For Post-Treatments, Processing, Supply, Discharge, And Other Processes (AREA)
- Moulding By Coating Moulds (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR0504648A FR2885310B1 (fr) | 2005-05-09 | 2005-05-09 | Procede de fabrication d'une aube creuse comportant un sommet en forme de baignoire, procede de reparation d'une telle aube et aube obtenue par l'un de ces procedes |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| TW200706301A TW200706301A (en) | 2007-02-16 |
| TWI365115B true TWI365115B (en) | 2012-06-01 |
Family
ID=35106882
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| TW095116231A TWI365115B (en) | 2005-05-09 | 2006-05-08 | Method of manufacturing a hollow blade that includes a recessed tip cap and method of repairing such a blade |
Country Status (12)
| Country | Link |
|---|---|
| EP (1) | EP1721698B1 (zh) |
| JP (1) | JP4945166B2 (zh) |
| CN (1) | CN100528411C (zh) |
| AT (1) | ATE415237T1 (zh) |
| BR (1) | BRPI0601517B1 (zh) |
| CA (1) | CA2546253C (zh) |
| DE (1) | DE602006003803D1 (zh) |
| FR (1) | FR2885310B1 (zh) |
| MX (1) | MXPA06005231A (zh) |
| RU (1) | RU2410226C2 (zh) |
| SG (1) | SG127803A1 (zh) |
| TW (1) | TWI365115B (zh) |
Families Citing this family (12)
| 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 (it) * | 2011-12-12 | 2013-06-13 | Nuovo Pignone Spa | Turbina a vapore, paletta e metodo |
| 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 (de) * | 2015-12-28 | 2017-06-29 | Siemens Aktiengesellschaft | Verfahren zur Herstellung eines Schaufelblatts für eine Turbinenschaufel einer Turbinenanlage |
| 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 (zh) * | 2018-08-14 | 2020-05-19 | 中国航发南方工业有限公司 | 空心叶片钎焊用夹具 |
| US11143033B2 (en) * | 2018-11-08 | 2021-10-12 | General Electric Company | Turbomachine blade tip attachment |
| FR3088839B1 (fr) * | 2018-11-23 | 2022-09-09 | Safran Aircraft Engines | Procede de fabrication d’une piece metallique pour une turbomachine d’aeronef |
| CN112008082A (zh) * | 2020-07-30 | 2020-12-01 | 中国航发商用航空发动机有限责任公司 | 一种空心风扇叶片粉末热等静压近净成形制备方法 |
| CN112031878A (zh) * | 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 | 一种涡轮转子叶片叶尖双层壁结构 |
Family Cites Families (18)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS58172406A (ja) * | 1982-04-05 | 1983-10-11 | Hitachi Ltd | ガスタ−ビン用の積層翼 |
| 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 |
| SU1815873A1 (ru) * | 1991-06-28 | 1994-05-15 | Научно-исследовательский институт технологии и организации производства двигателей | Способ изготовления полых лопаток с заполнителем |
| FR2691658B1 (fr) * | 1992-05-27 | 1994-07-22 | Snecma | Piece en superalliage comportant un apport et procede de realisation de l'apport. |
| 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 |
| JP3137527B2 (ja) * | 1994-04-21 | 2001-02-26 | 三菱重工業株式会社 | ガスタービン動翼チップ冷却装置 |
| UA23886C2 (uk) * | 1996-03-12 | 2002-04-15 | Юнайтед Технолоджіз Корп. Пратт Енд Уітні | Спосіб виготовлення пустотілих виробів складної форми |
| 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 (de) * | 1999-05-12 | 2000-10-19 | Mtu Muenchen Gmbh | Verfahren zur Fertigung angepaßter, strömungstechnischer Oberflächen |
| US6332272B1 (en) * | 2000-01-07 | 2001-12-25 | Siemens Westinghouse Power Corporation | Method of repairing a turbine blade |
| US6502303B2 (en) * | 2001-05-07 | 2003-01-07 | Chromalloy Gas Turbine Corporation | Method of repairing a turbine blade tip |
| 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 (ja) * | 2002-01-30 | 2003-08-08 | Hitachi Ltd | タービン翼の製作方法およびタービン翼 |
| 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/fr not_active Expired - Fee Related
-
2006
- 2006-05-05 DE DE602006003803T patent/DE602006003803D1/de active Active
- 2006-05-05 CA CA2546253A patent/CA2546253C/fr active Active
- 2006-05-05 AT AT06113599T patent/ATE415237T1/de not_active IP Right Cessation
- 2006-05-05 EP EP06113599A patent/EP1721698B1/fr active Active
- 2006-05-06 RU RU2006115833/02A patent/RU2410226C2/ru active
- 2006-05-08 JP JP2006129031A patent/JP4945166B2/ja active Active
- 2006-05-08 TW TW095116231A patent/TWI365115B/zh active
- 2006-05-09 MX MXPA06005231A patent/MXPA06005231A/es active IP Right Grant
- 2006-05-09 SG SG200603109A patent/SG127803A1/en unknown
- 2006-05-09 CN CN200610078305.XA patent/CN100528411C/zh active Active
- 2006-05-09 BR BRPI0601517-4A patent/BRPI0601517B1/pt active IP Right Grant
Also Published As
| Publication number | Publication date |
|---|---|
| FR2885310B1 (fr) | 2008-12-26 |
| EP1721698B1 (fr) | 2008-11-26 |
| SG127803A1 (en) | 2006-12-29 |
| DE602006003803D1 (de) | 2009-01-08 |
| FR2885310A1 (fr) | 2006-11-10 |
| ATE415237T1 (de) | 2008-12-15 |
| JP2006316790A (ja) | 2006-11-24 |
| CN1931475A (zh) | 2007-03-21 |
| RU2410226C2 (ru) | 2011-01-27 |
| TW200706301A (en) | 2007-02-16 |
| CN100528411C (zh) | 2009-08-19 |
| CA2546253C (fr) | 2013-07-30 |
| MXPA06005231A (es) | 2007-02-16 |
| JP4945166B2 (ja) | 2012-06-06 |
| BRPI0601517B1 (pt) | 2018-04-03 |
| BRPI0601517A (pt) | 2007-07-17 |
| CA2546253A1 (fr) | 2006-11-09 |
| RU2006115833A (ru) | 2007-11-20 |
| EP1721698A1 (fr) | 2006-11-15 |
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