RU2297537C2 - Лопатка ротора и турбина высокого давления турбомашины - Google Patents
Лопатка ротора и турбина высокого давления турбомашины Download PDFInfo
- Publication number
- RU2297537C2 RU2297537C2 RU2002132866/06A RU2002132866A RU2297537C2 RU 2297537 C2 RU2297537 C2 RU 2297537C2 RU 2002132866/06 A RU2002132866/06 A RU 2002132866/06A RU 2002132866 A RU2002132866 A RU 2002132866A RU 2297537 C2 RU2297537 C2 RU 2297537C2
- Authority
- RU
- Russia
- Prior art keywords
- blade
- outlet
- base
- feather
- pressure turbine
- Prior art date
Links
- 238000001816 cooling Methods 0.000 claims abstract description 28
- 210000003746 feather Anatomy 0.000 claims abstract description 25
- 230000007704 transition Effects 0.000 claims description 8
- 238000011144 upstream manufacturing Methods 0.000 claims description 7
- 239000000567 combustion gas Substances 0.000 claims description 6
- 238000005192 partition Methods 0.000 claims description 3
- 230000015572 biosynthetic process Effects 0.000 abstract description 2
- 238000011089 mechanical engineering Methods 0.000 abstract 1
- 230000002265 prevention Effects 0.000 abstract 1
- 239000000126 substance Substances 0.000 abstract 1
- 210000001991 scapula Anatomy 0.000 description 4
- 238000002485 combustion reaction Methods 0.000 description 2
- 238000005336 cracking Methods 0.000 description 2
- 239000007789 gas Substances 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 241000191291 Abies alba Species 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000000593 degrading effect Effects 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
Images
Classifications
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR0115904 | 2001-12-10 | ||
| FR0115904A FR2833298B1 (fr) | 2001-12-10 | 2001-12-10 | Perfectionnements apportes au comportement thermique du bord de fuite d'une aube de turbine haute-pression |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| RU2002132866A RU2002132866A (ru) | 2004-08-20 |
| RU2297537C2 true RU2297537C2 (ru) | 2007-04-20 |
Family
ID=8870271
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| RU2002132866/06A RU2297537C2 (ru) | 2001-12-10 | 2002-12-09 | Лопатка ротора и турбина высокого давления турбомашины |
Country Status (9)
| Country | Link |
|---|---|
| US (1) | US6830431B2 (enExample) |
| EP (1) | EP1318274B1 (enExample) |
| JP (1) | JP4012054B2 (enExample) |
| CA (1) | CA2412989C (enExample) |
| DE (1) | DE60201325T2 (enExample) |
| ES (1) | ES2225740T3 (enExample) |
| FR (1) | FR2833298B1 (enExample) |
| RU (1) | RU2297537C2 (enExample) |
| UA (1) | UA80246C2 (enExample) |
Families Citing this family (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2864990B1 (fr) * | 2004-01-14 | 2008-02-22 | Snecma Moteurs | Perfectionnements apportes aux fentes d'evacuation de l'air de refroidissement d'aubes de turbine haute-pression |
| US7503749B2 (en) * | 2005-04-01 | 2009-03-17 | General Electric Company | Turbine nozzle with trailing edge convection and film cooling |
| FR2887287B1 (fr) * | 2005-06-21 | 2007-09-21 | Snecma Moteurs Sa | Circuits de refroidissement pour aube mobile de turbomachine |
| KR100847523B1 (ko) * | 2006-12-29 | 2008-07-22 | 엘지전자 주식회사 | 터보팬 |
| US8002525B2 (en) * | 2007-11-16 | 2011-08-23 | Siemens Energy, Inc. | Turbine airfoil cooling system with recessed trailing edge cooling slot |
| FR2924156B1 (fr) * | 2007-11-26 | 2014-02-14 | Snecma | Aube de turbomachine |
| US8157504B2 (en) * | 2009-04-17 | 2012-04-17 | General Electric Company | Rotor blades for turbine engines |
| FR2954798B1 (fr) | 2009-12-31 | 2012-03-30 | Snecma | Aube a ventilation interieure |
| US8608429B2 (en) * | 2010-05-28 | 2013-12-17 | General Electric Company | System and method for enhanced turbine wake mixing via fluidic-generated vortices |
| US10107108B2 (en) | 2015-04-29 | 2018-10-23 | General Electric Company | Rotor blade having a flared tip |
| DE102020207646A1 (de) * | 2020-06-22 | 2021-12-23 | Siemens Aktiengesellschaft | Turbinenschaufel und Verfahren zum Bearbeiten einer solchen |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5599166A (en) * | 1994-11-01 | 1997-02-04 | United Technologies Corporation | Core for fabrication of gas turbine engine airfoils |
| US5857837A (en) * | 1996-06-28 | 1999-01-12 | United Technologies Corporation | Coolable air foil for a gas turbine engine |
| EP0896127A2 (en) * | 1997-08-07 | 1999-02-10 | United Technologies Corporation | Airfoil cooling |
| US6062817A (en) * | 1998-11-06 | 2000-05-16 | General Electric Company | Apparatus and methods for cooling slot step elimination |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| BE794195A (fr) * | 1972-01-18 | 1973-07-18 | Bbc Sulzer Turbomaschinen | Aube directrice refroidie pour des turbines a gaz |
| GB2121483B (en) * | 1982-06-08 | 1985-02-13 | Rolls Royce | Cooled turbine blade for a gas turbine engine |
| US4601638A (en) * | 1984-12-21 | 1986-07-22 | United Technologies Corporation | Airfoil trailing edge cooling arrangement |
| US5403158A (en) * | 1993-12-23 | 1995-04-04 | United Technologies Corporation | Aerodynamic tip sealing for rotor blades |
| CA2334071C (en) * | 2000-02-23 | 2005-05-24 | Mitsubishi Heavy Industries, Ltd. | Gas turbine moving blade |
-
2001
- 2001-12-10 FR FR0115904A patent/FR2833298B1/fr not_active Expired - Fee Related
-
2002
- 2002-11-25 US US10/303,012 patent/US6830431B2/en not_active Expired - Lifetime
- 2002-11-29 CA CA002412989A patent/CA2412989C/fr not_active Expired - Lifetime
- 2002-12-03 ES ES02292970T patent/ES2225740T3/es not_active Expired - Lifetime
- 2002-12-03 DE DE60201325T patent/DE60201325T2/de not_active Expired - Lifetime
- 2002-12-03 EP EP02292970A patent/EP1318274B1/fr not_active Expired - Lifetime
- 2002-12-04 UA UA2002129702A patent/UA80246C2/uk unknown
- 2002-12-04 JP JP2002352590A patent/JP4012054B2/ja not_active Expired - Lifetime
- 2002-12-09 RU RU2002132866/06A patent/RU2297537C2/ru active
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5599166A (en) * | 1994-11-01 | 1997-02-04 | United Technologies Corporation | Core for fabrication of gas turbine engine airfoils |
| US5857837A (en) * | 1996-06-28 | 1999-01-12 | United Technologies Corporation | Coolable air foil for a gas turbine engine |
| EP0896127A2 (en) * | 1997-08-07 | 1999-02-10 | United Technologies Corporation | Airfoil cooling |
| US6062817A (en) * | 1998-11-06 | 2000-05-16 | General Electric Company | Apparatus and methods for cooling slot step elimination |
Also Published As
| Publication number | Publication date |
|---|---|
| EP1318274B1 (fr) | 2004-09-22 |
| CA2412989A1 (fr) | 2003-06-05 |
| EP1318274A1 (fr) | 2003-06-11 |
| US6830431B2 (en) | 2004-12-14 |
| CA2412989C (fr) | 2008-09-23 |
| DE60201325D1 (de) | 2004-10-28 |
| FR2833298A1 (fr) | 2003-06-13 |
| FR2833298B1 (fr) | 2004-08-06 |
| DE60201325T2 (de) | 2005-03-17 |
| JP4012054B2 (ja) | 2007-11-21 |
| US20030108425A1 (en) | 2003-06-12 |
| ES2225740T3 (es) | 2005-03-16 |
| JP2003193804A (ja) | 2003-07-09 |
| UA80246C2 (uk) | 2007-09-10 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| JP4540973B2 (ja) | ベンチュリ出口を有するタービン翼形部 | |
| CN100359134C (zh) | 根部开有缺口的涡轮叶片 | |
| JP4762524B2 (ja) | ガスタービンエンジンロータ組立体を冷却するための方法及び装置 | |
| US11389860B2 (en) | Hollow turbine blade with reduced cooling air extraction | |
| US7278827B2 (en) | Cooling air evacuation slots of turbine blades | |
| US7147440B2 (en) | Methods and apparatus for cooling gas turbine engine rotor assemblies | |
| CN104685160B (zh) | 用于燃气涡轮发动机的涡轮的转子叶片 | |
| JP5357992B2 (ja) | カスケード先端部バッフルエーロフォイル | |
| US7118342B2 (en) | Fluted tip turbine blade | |
| RU2297537C2 (ru) | Лопатка ротора и турбина высокого давления турбомашины | |
| EP1298285A2 (en) | Ramped tip shelf blade | |
| JP2006170198A (ja) | タービン段 | |
| JP2001003704A (ja) | 内部冷却式タービン翼形部 | |
| CN100572757C (zh) | 燃气轮机的叶片及其制造方法 | |
| JP4245873B2 (ja) | ガスタービンエンジン用のタービン翼形部 | |
| JP2006161810A (ja) | ブルノーズ段部付きタービンノズル | |
| US20080050244A1 (en) | Turbine blade with split impingement rib | |
| US6599092B1 (en) | Methods and apparatus for cooling gas turbine nozzles | |
| US20030138322A1 (en) | Moving blade for a high pressure turbine, the blade having a trailing edge of improved thermal behavior | |
| US11230929B2 (en) | Turbine component with dust tolerant cooling system | |
| AU2005201194A1 (en) | Cooled Turbine Airfoil | |
| US11448093B2 (en) | Turbine vane with dust tolerant cooling system | |
| RU2388915C2 (ru) | Охлаждаемая лопатка газовой турбины | |
| JP2003130354A (ja) | ガスタービン燃焼器のプレートフィン構造及びガスタービン燃焼器 |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PD4A | Correction of name of patent owner | ||
| PD4A | Correction of name of patent owner |