PL2619443T3 - Chłodzona ścianka w silniku turbospalinowym - Google Patents
Chłodzona ścianka w silniku turbospalinowymInfo
- Publication number
- PL2619443T3 PL2619443T3 PL11757504T PL11757504T PL2619443T3 PL 2619443 T3 PL2619443 T3 PL 2619443T3 PL 11757504 T PL11757504 T PL 11757504T PL 11757504 T PL11757504 T PL 11757504T PL 2619443 T3 PL2619443 T3 PL 2619443T3
- Authority
- PL
- Poland
- Prior art keywords
- turbine engine
- component wall
- cooled component
- cooled
- wall
- Prior art date
Links
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
- F01D5/186—Film cooling
-
- 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
- F05D2230/90—Coating; Surface treatment
-
- 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
- F05D2250/00—Geometry
- F05D2250/10—Two-dimensional
- F05D2250/13—Two-dimensional trapezoidal
-
- 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
- F05D2250/00—Geometry
- F05D2250/30—Arrangement of components
- F05D2250/32—Arrangement of components according to their shape
- F05D2250/324—Arrangement of components according to their shape divergent
-
- 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
- Y10T29/4935—Heat exchanger or boiler making
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US12/888,467 US9028207B2 (en) | 2010-09-23 | 2010-09-23 | Cooled component wall in a turbine engine |
EP11757504.3A EP2619443B1 (en) | 2010-09-23 | 2011-09-07 | Cooled component wall in a turbine engine |
PCT/US2011/050594 WO2012039926A2 (en) | 2010-09-23 | 2011-09-07 | Cooled component wall in a turbine engine |
Publications (1)
Publication Number | Publication Date |
---|---|
PL2619443T3 true PL2619443T3 (pl) | 2015-12-31 |
Family
ID=44652011
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PL11757504T PL2619443T3 (pl) | 2010-09-23 | 2011-09-07 | Chłodzona ścianka w silniku turbospalinowym |
Country Status (5)
Country | Link |
---|---|
US (1) | US9028207B2 (pl) |
EP (1) | EP2619443B1 (pl) |
ES (1) | ES2550100T3 (pl) |
PL (1) | PL2619443T3 (pl) |
WO (1) | WO2012039926A2 (pl) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9181809B2 (en) | 2012-12-04 | 2015-11-10 | General Electric Company | Coated article |
US20140360155A1 (en) * | 2013-06-07 | 2014-12-11 | General Electric Company | Microchannel systems and methods for cooling turbine components of a gas turbine engine |
US9394796B2 (en) * | 2013-07-12 | 2016-07-19 | General Electric Company | Turbine component and methods of assembling the same |
DE102013214487A1 (de) * | 2013-07-24 | 2015-01-29 | Rolls-Royce Deutschland Ltd & Co Kg | Brennkammerschindel einer Gasturbine |
EP3167159B1 (en) | 2014-07-09 | 2018-11-28 | Siemens Aktiengesellschaft | Impingement jet strike channel system within internal cooling systems |
US20160090843A1 (en) * | 2014-09-30 | 2016-03-31 | General Electric Company | Turbine components with stepped apertures |
US11280214B2 (en) * | 2014-10-20 | 2022-03-22 | Raytheon Technologies Corporation | Gas turbine engine component |
US9752440B2 (en) * | 2015-05-29 | 2017-09-05 | General Electric Company | Turbine component having surface cooling channels and method of forming same |
KR101839656B1 (ko) * | 2015-08-13 | 2018-04-26 | 두산중공업 주식회사 | 가스터빈 블레이드 |
US10570747B2 (en) * | 2017-10-02 | 2020-02-25 | DOOSAN Heavy Industries Construction Co., LTD | Enhanced film cooling system |
US10933481B2 (en) * | 2018-01-05 | 2021-03-02 | General Electric Company | Method of forming cooling passage for turbine component with cap element |
Family Cites Families (25)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2244673B (en) * | 1990-06-05 | 1993-09-01 | Rolls Royce Plc | A perforated sheet and a method of making the same |
US5660525A (en) | 1992-10-29 | 1997-08-26 | General Electric Company | Film cooled slotted wall |
US5651662A (en) | 1992-10-29 | 1997-07-29 | General Electric Company | Film cooled wall |
US5683600A (en) | 1993-03-17 | 1997-11-04 | General Electric Company | Gas turbine engine component with compound cooling holes and method for making the same |
US5605639A (en) | 1993-12-21 | 1997-02-25 | United Technologies Corporation | Method of producing diffusion holes in turbine components by a multiple piece electrode |
US5458461A (en) | 1994-12-12 | 1995-10-17 | General Electric Company | Film cooled slotted wall |
JP2810023B2 (ja) | 1996-09-18 | 1998-10-15 | 株式会社東芝 | 高温部材冷却装置 |
US5902647A (en) | 1996-12-03 | 1999-05-11 | General Electric Company | Method for protecting passage holes in a metal-based substrate from becoming obstructed, and related compositions |
US6383602B1 (en) * | 1996-12-23 | 2002-05-07 | General Electric Company | Method for improving the cooling effectiveness of a gaseous coolant stream which flows through a substrate, and related articles of manufacture |
DE59802893D1 (de) | 1998-03-23 | 2002-03-14 | Alstom | Nichtkreisförmige Kühlbohrung und Verfahren zur Herstellung derselben |
US6234755B1 (en) * | 1999-10-04 | 2001-05-22 | General Electric Company | Method for improving the cooling effectiveness of a gaseous coolant stream, and related articles of manufacture |
US6617003B1 (en) | 2000-11-06 | 2003-09-09 | General Electric Company | Directly cooled thermal barrier coating system |
US7411150B2 (en) | 2002-06-12 | 2008-08-12 | Alstom Technology Ltd. | Method of producing a composite component |
JP3997986B2 (ja) * | 2003-12-19 | 2007-10-24 | 株式会社Ihi | 冷却タービン部品、及び冷却タービン翼 |
US7328580B2 (en) | 2004-06-23 | 2008-02-12 | General Electric Company | Chevron film cooled wall |
EP1712739A1 (de) * | 2005-04-12 | 2006-10-18 | Siemens Aktiengesellschaft | Bauteil mit Filmkühlloch |
EP1967696B1 (en) * | 2005-11-01 | 2017-03-15 | IHI Corporation | Turbine part |
US7351036B2 (en) | 2005-12-02 | 2008-04-01 | Siemens Power Generation, Inc. | Turbine airfoil cooling system with elbowed, diffusion film cooling hole |
GB2438861A (en) | 2006-06-07 | 2007-12-12 | Rolls Royce Plc | Film-cooled component, eg gas turbine engine blade or vane |
US7553534B2 (en) | 2006-08-29 | 2009-06-30 | General Electric Company | Film cooled slotted wall and method of making the same |
US7992272B2 (en) | 2007-05-29 | 2011-08-09 | Metem Corporation | Method and apparatus for milling thermal barrier coated metals |
US20090246011A1 (en) | 2008-03-25 | 2009-10-01 | General Electric Company | Film cooling of turbine components |
US20110097188A1 (en) * | 2009-10-23 | 2011-04-28 | General Electric Company | Structure and method for improving film cooling using shallow trench with holes oriented along length of trench |
US8905713B2 (en) * | 2010-05-28 | 2014-12-09 | General Electric Company | Articles which include chevron film cooling holes, and related processes |
US8608443B2 (en) | 2010-06-11 | 2013-12-17 | Siemens Energy, Inc. | Film cooled component wall in a turbine engine |
-
2010
- 2010-09-23 US US12/888,467 patent/US9028207B2/en not_active Expired - Fee Related
-
2011
- 2011-09-07 WO PCT/US2011/050594 patent/WO2012039926A2/en active Application Filing
- 2011-09-07 ES ES11757504.3T patent/ES2550100T3/es active Active
- 2011-09-07 EP EP11757504.3A patent/EP2619443B1/en not_active Not-in-force
- 2011-09-07 PL PL11757504T patent/PL2619443T3/pl unknown
Also Published As
Publication number | Publication date |
---|---|
WO2012039926A3 (en) | 2013-05-16 |
WO2012039926A2 (en) | 2012-03-29 |
US9028207B2 (en) | 2015-05-12 |
ES2550100T3 (es) | 2015-11-04 |
US20120076644A1 (en) | 2012-03-29 |
EP2619443A2 (en) | 2013-07-31 |
EP2619443B1 (en) | 2015-06-24 |
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