ATE496199T1 - Gasturbinenschaufel mit gekühlter vorderkante - Google Patents
Gasturbinenschaufel mit gekühlter vorderkanteInfo
- Publication number
- ATE496199T1 ATE496199T1 AT05108364T AT05108364T ATE496199T1 AT E496199 T1 ATE496199 T1 AT E496199T1 AT 05108364 T AT05108364 T AT 05108364T AT 05108364 T AT05108364 T AT 05108364T AT E496199 T1 ATE496199 T1 AT E496199T1
- Authority
- AT
- Austria
- Prior art keywords
- film cooling
- leading edge
- gas turbine
- cooling holes
- turbine blade
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US10/956,096 US7300252B2 (en) | 2004-10-04 | 2004-10-04 | Gas turbine airfoil leading edge cooling construction |
Publications (1)
Publication Number | Publication Date |
---|---|
ATE496199T1 true ATE496199T1 (de) | 2011-02-15 |
Family
ID=35241130
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AT05108364T ATE496199T1 (de) | 2004-10-04 | 2005-09-13 | Gasturbinenschaufel mit gekühlter vorderkante |
Country Status (4)
Country | Link |
---|---|
US (1) | US7300252B2 (de) |
EP (1) | EP1645721B1 (de) |
AT (1) | ATE496199T1 (de) |
DE (1) | DE602005025970D1 (de) |
Families Citing this family (24)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7246992B2 (en) | 2005-01-28 | 2007-07-24 | General Electric Company | High efficiency fan cooling holes for turbine airfoil |
EP1898051B8 (de) | 2006-08-25 | 2017-08-02 | Ansaldo Energia IP UK Limited | Gasturbinenschaufel mit Kühlung der Leitkante |
US8105030B2 (en) * | 2008-08-14 | 2012-01-31 | United Technologies Corporation | Cooled airfoils and gas turbine engine systems involving such airfoils |
GB2466791B (en) * | 2009-01-07 | 2011-05-18 | Rolls Royce Plc | An aerofoil |
US8052378B2 (en) * | 2009-03-18 | 2011-11-08 | General Electric Company | Film-cooling augmentation device and turbine airfoil incorporating the same |
US20100239409A1 (en) * | 2009-03-18 | 2010-09-23 | General Electric Company | Method of Using and Reconstructing a Film-Cooling Augmentation Device for a Turbine Airfoil |
US8739508B1 (en) * | 2009-09-29 | 2014-06-03 | The United States Of America As Represented By The Secretary Of The Air Force | Shock cancellation mechanism for the control of unsteady interaction in contra-rotating high- and low-pressure turbines |
US8742279B2 (en) * | 2010-02-01 | 2014-06-03 | United Technologies Corporation | Method of creating an airfoil trench and a plurality of cooling holes within the trench |
JP2012219702A (ja) * | 2011-04-07 | 2012-11-12 | Society Of Japanese Aerospace Co | タービン翼 |
US9022737B2 (en) | 2011-08-08 | 2015-05-05 | United Technologies Corporation | Airfoil including trench with contoured surface |
US8858176B1 (en) * | 2011-12-13 | 2014-10-14 | Florida Turbine Technologies, Inc. | Turbine airfoil with leading edge cooling |
US8707713B2 (en) * | 2012-02-15 | 2014-04-29 | United Technologies Corporation | Cooling hole with crenellation features |
US9429027B2 (en) * | 2012-04-05 | 2016-08-30 | United Technologies Corporation | Turbine airfoil tip shelf and squealer pocket cooling |
US20140003937A1 (en) * | 2012-06-30 | 2014-01-02 | General Electric Company | Component and a method of cooling a component |
US9228440B2 (en) | 2012-12-03 | 2016-01-05 | Honeywell International Inc. | Turbine blade airfoils including showerhead film cooling systems, and methods for forming an improved showerhead film cooled airfoil of a turbine blade |
US9562437B2 (en) | 2013-04-26 | 2017-02-07 | Honeywell International Inc. | Turbine blade airfoils including film cooling systems, and methods for forming an improved film cooled airfoil of a turbine blade |
US10041356B2 (en) * | 2014-08-15 | 2018-08-07 | United Technologies Corporation | Showerhead hole scheme apparatus and system |
US10208602B2 (en) * | 2015-04-27 | 2019-02-19 | United Technologies Corporation | Asymmetric diffuser opening for film cooling holes |
US10077667B2 (en) * | 2015-05-08 | 2018-09-18 | United Technologies Corporation | Turbine airfoil film cooling holes |
US20170298743A1 (en) * | 2016-04-14 | 2017-10-19 | General Electric Company | Component for a turbine engine with a film-hole |
US20190003316A1 (en) * | 2017-06-29 | 2019-01-03 | United Technologies Corporation | Helical skin cooling passages for turbine airfoils |
US20190218917A1 (en) | 2018-01-17 | 2019-07-18 | General Electric Company | Engine component with set of cooling holes |
US11359494B2 (en) * | 2019-08-06 | 2022-06-14 | General Electric Company | Engine component with cooling hole |
IT202100000296A1 (it) | 2021-01-08 | 2022-07-08 | Gen Electric | Motore a turbine con paletta avente un insieme di fossette |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4684323A (en) * | 1985-12-23 | 1987-08-04 | United Technologies Corporation | Film cooling passages with curved corners |
US4738588A (en) * | 1985-12-23 | 1988-04-19 | Field Robert E | Film cooling passages with step diffuser |
US6129515A (en) * | 1992-11-20 | 2000-10-10 | United Technologies Corporation | Turbine airfoil suction aided film cooling means |
US5779437A (en) * | 1996-10-31 | 1998-07-14 | Pratt & Whitney Canada Inc. | Cooling passages for airfoil leading edge |
EP0924384A3 (de) | 1997-12-17 | 2000-08-23 | United Technologies Corporation | Kühlung der Anströmkante einer Turbomaschinenschaufel |
DE59808269D1 (de) * | 1998-03-23 | 2003-06-12 | Alstom Switzerland Ltd | Filmkühlungsbohrung |
US6988872B2 (en) * | 2003-01-27 | 2006-01-24 | Mitsubishi Heavy Industries, Ltd. | Turbine moving blade and gas turbine |
-
2004
- 2004-10-04 US US10/956,096 patent/US7300252B2/en not_active Expired - Fee Related
-
2005
- 2005-09-13 AT AT05108364T patent/ATE496199T1/de not_active IP Right Cessation
- 2005-09-13 EP EP05108364A patent/EP1645721B1/de not_active Not-in-force
- 2005-09-13 DE DE602005025970T patent/DE602005025970D1/de active Active
Also Published As
Publication number | Publication date |
---|---|
US7300252B2 (en) | 2007-11-27 |
EP1645721A3 (de) | 2009-10-07 |
EP1645721B1 (de) | 2011-01-19 |
US20060073016A1 (en) | 2006-04-06 |
DE602005025970D1 (de) | 2011-03-03 |
EP1645721A2 (de) | 2006-04-12 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
RER | Ceased as to paragraph 5 lit. 3 law introducing patent treaties |