DE602005027140D1 - Geschneiderte Wirbelbildung für Turbinenschaufeln - Google Patents
Geschneiderte Wirbelbildung für TurbinenschaufelnInfo
- Publication number
- DE602005027140D1 DE602005027140D1 DE602005027140T DE602005027140T DE602005027140D1 DE 602005027140 D1 DE602005027140 D1 DE 602005027140D1 DE 602005027140 T DE602005027140 T DE 602005027140T DE 602005027140 T DE602005027140 T DE 602005027140T DE 602005027140 D1 DE602005027140 D1 DE 602005027140D1
- Authority
- DE
- Germany
- Prior art keywords
- tailored
- turbine blades
- vortex formation
- vortex
- formation
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
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
- F01D5/187—Convection 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
- F05D2250/00—Geometry
- F05D2250/30—Arrangement of components
-
- 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
- F05D2260/00—Function
- F05D2260/20—Heat transfer, e.g. cooling
- F05D2260/221—Improvement of heat transfer
- F05D2260/2212—Improvement of heat transfer by creating turbulence
-
- 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
- F05D2260/00—Function
- F05D2260/20—Heat transfer, e.g. cooling
- F05D2260/221—Improvement of heat transfer
- F05D2260/2214—Improvement of heat transfer by increasing the heat transfer surface
- F05D2260/22141—Improvement of heat transfer by increasing the heat transfer surface using fins or ribs
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 |
---|---|---|---|
US10/774,822 US7114916B2 (en) | 2004-02-09 | 2004-02-09 | Tailored turbulation for turbine blades |
Publications (1)
Publication Number | Publication Date |
---|---|
DE602005027140D1 true DE602005027140D1 (de) | 2011-05-12 |
Family
ID=34679412
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE602005027140T Active DE602005027140D1 (de) | 2004-02-09 | 2005-02-08 | Geschneiderte Wirbelbildung für Turbinenschaufeln |
Country Status (5)
Country | Link |
---|---|
US (1) | US7114916B2 (de) |
EP (1) | EP1561903B1 (de) |
CN (1) | CN1654784A (de) |
DE (1) | DE602005027140D1 (de) |
RU (1) | RU2285804C1 (de) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7625178B2 (en) * | 2006-08-30 | 2009-12-01 | Honeywell International Inc. | High effectiveness cooled turbine blade |
US7722327B1 (en) * | 2007-04-03 | 2010-05-25 | Florida Turbine Technologies, Inc. | Multiple vortex cooling circuit for a thin airfoil |
US7901180B2 (en) * | 2007-05-07 | 2011-03-08 | United Technologies Corporation | Enhanced turbine airfoil cooling |
US8511992B2 (en) * | 2008-01-22 | 2013-08-20 | United Technologies Corporation | Minimization of fouling and fluid losses in turbine airfoils |
US8281564B2 (en) * | 2009-01-23 | 2012-10-09 | General Electric Company | Heat transfer tubes having dimples arranged between adjacent fins |
JP2011085084A (ja) | 2009-10-16 | 2011-04-28 | Ihi Corp | タービン翼 |
US8523524B2 (en) * | 2010-03-25 | 2013-09-03 | General Electric Company | Airfoil cooling hole flag region |
US8727724B2 (en) * | 2010-04-12 | 2014-05-20 | General Electric Company | Turbine bucket having a radial cooling hole |
US8961133B2 (en) | 2010-12-28 | 2015-02-24 | Rolls-Royce North American Technologies, Inc. | Gas turbine engine and cooled airfoil |
US8753083B2 (en) * | 2011-01-14 | 2014-06-17 | General Electric Company | Curved cooling passages for a turbine component |
US9739155B2 (en) | 2013-12-30 | 2017-08-22 | General Electric Company | Structural configurations and cooling circuits in turbine blades |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2159585B (en) * | 1984-05-24 | 1989-02-08 | Gen Electric | Turbine blade |
US5232343A (en) * | 1984-05-24 | 1993-08-03 | General Electric Company | Turbine blade |
US5695322A (en) * | 1991-12-17 | 1997-12-09 | General Electric Company | Turbine blade having restart turbulators |
US5413463A (en) * | 1991-12-30 | 1995-05-09 | General Electric Company | Turbulated cooling passages in gas turbine buckets |
US5924843A (en) * | 1997-05-21 | 1999-07-20 | General Electric Company | Turbine blade cooling |
US6234752B1 (en) * | 1999-08-16 | 2001-05-22 | General Electric Company | Method and tool for electrochemical machining |
US6416283B1 (en) * | 2000-10-16 | 2002-07-09 | General Electric Company | Electrochemical machining process, electrode therefor and turbine bucket with turbulated cooling passage |
US6672836B2 (en) * | 2001-12-11 | 2004-01-06 | United Technologies Corporation | Coolable rotor blade for an industrial gas turbine engine |
GB0229908D0 (en) * | 2002-12-21 | 2003-01-29 | Macdonald John | Turbine blade |
-
2004
- 2004-02-09 US US10/774,822 patent/US7114916B2/en not_active Expired - Lifetime
-
2005
- 2005-02-08 CN CNA2005100516463A patent/CN1654784A/zh active Pending
- 2005-02-08 EP EP05250706A patent/EP1561903B1/de not_active Expired - Fee Related
- 2005-02-08 DE DE602005027140T patent/DE602005027140D1/de active Active
- 2005-02-09 RU RU2005103307/06A patent/RU2285804C1/ru not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
EP1561903A2 (de) | 2005-08-10 |
RU2285804C1 (ru) | 2006-10-20 |
CN1654784A (zh) | 2005-08-17 |
US7114916B2 (en) | 2006-10-03 |
EP1561903A3 (de) | 2008-12-24 |
US20050175452A1 (en) | 2005-08-11 |
EP1561903B1 (de) | 2011-03-30 |
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