DE60132405D1 - Kühlung von Turbinenschaufeln durch spezifische Schaufelverteilung - Google Patents
Kühlung von Turbinenschaufeln durch spezifische SchaufelverteilungInfo
- Publication number
- DE60132405D1 DE60132405D1 DE60132405T DE60132405T DE60132405D1 DE 60132405 D1 DE60132405 D1 DE 60132405D1 DE 60132405 T DE60132405 T DE 60132405T DE 60132405 T DE60132405 T DE 60132405T DE 60132405 D1 DE60132405 D1 DE 60132405D1
- Authority
- DE
- Germany
- Prior art keywords
- cooling
- turbine blades
- specific blade
- blade distribution
- distribution
- 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.)
- Expired - Lifetime
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
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/08—Cooling; Heating; Heat-insulation
- F01D25/12—Cooling
-
- 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
- F01D5/141—Shape, i.e. outer, aerodynamic form
- F01D5/142—Shape, i.e. outer, aerodynamic form of the blades of successive rotor or stator blade-rows
-
- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US640357 | 1996-04-30 | ||
US09/640,357 US6402458B1 (en) | 2000-08-16 | 2000-08-16 | Clock turbine airfoil cooling |
Publications (2)
Publication Number | Publication Date |
---|---|
DE60132405D1 true DE60132405D1 (de) | 2008-03-06 |
DE60132405T2 DE60132405T2 (de) | 2009-01-02 |
Family
ID=24567918
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE60132405T Expired - Lifetime DE60132405T2 (de) | 2000-08-16 | 2001-08-03 | Kühlung von Turbinenschaufeln durch spezifische Schaufelverteilung |
Country Status (4)
Country | Link |
---|---|
US (1) | US6402458B1 (de) |
EP (1) | EP1182339B1 (de) |
JP (1) | JP4733876B2 (de) |
DE (1) | DE60132405T2 (de) |
Families Citing this family (39)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
IT1320722B1 (it) * | 2000-10-23 | 2003-12-10 | Fiatavio Spa | Metodo per il posizionamento di schiere di stadi di una turbina,particolarmente per motori aeronautici. |
DE10053361C1 (de) * | 2000-10-27 | 2002-06-06 | Mtu Aero Engines Gmbh | Schaufelgitteranordnung für Turbomaschinen |
US6499938B1 (en) * | 2001-10-11 | 2002-12-31 | General Electric Company | Method for enhancing part life in a gas stream |
US7094027B2 (en) * | 2002-11-27 | 2006-08-22 | General Electric Company | Row of long and short chord length and high and low temperature capability turbine airfoils |
US6913441B2 (en) | 2003-09-04 | 2005-07-05 | Siemens Westinghouse Power Corporation | Turbine blade ring assembly and clocking method |
US7140832B2 (en) * | 2005-04-04 | 2006-11-28 | General Electric Company | Method and system for rotating a turbine stator ring |
DE102005021446B3 (de) * | 2005-05-04 | 2006-06-29 | Technische Universität Dresden | Gasturbine |
US8182199B2 (en) * | 2007-02-01 | 2012-05-22 | Pratt & Whitney Canada Corp. | Turbine shroud cooling system |
US7836703B2 (en) * | 2007-06-20 | 2010-11-23 | General Electric Company | Reciprocal cooled turbine nozzle |
FR2925106B1 (fr) * | 2007-12-14 | 2010-01-22 | Snecma | Procede de conception d'une turbine multi-etages de turbomachine |
US8104292B2 (en) * | 2007-12-17 | 2012-01-31 | General Electric Company | Duplex turbine shroud |
US8205458B2 (en) | 2007-12-31 | 2012-06-26 | General Electric Company | Duplex turbine nozzle |
US20090317237A1 (en) * | 2008-06-20 | 2009-12-24 | General Electric Company | System and method for reduction of unsteady pressures in turbomachinery |
US8540490B2 (en) * | 2008-06-20 | 2013-09-24 | General Electric Company | Noise reduction in a turbomachine, and a related method thereof |
US20100054929A1 (en) * | 2008-09-04 | 2010-03-04 | General Electric Company | Turbine airfoil clocking |
US20100054922A1 (en) * | 2008-09-04 | 2010-03-04 | General Electric Company | Turbine airfoil clocking |
US8087253B2 (en) * | 2008-11-20 | 2012-01-03 | General Electric Company | Methods, apparatus and systems concerning the circumferential clocking of turbine airfoils in relation to combustor cans and the flow of cooling air through the turbine hot gas flowpath |
US8439626B2 (en) * | 2008-12-29 | 2013-05-14 | General Electric Company | Turbine airfoil clocking |
JP2010190057A (ja) * | 2009-02-16 | 2010-09-02 | Ihi Corp | タービンの設計方法及びタービン |
US8677763B2 (en) * | 2009-03-10 | 2014-03-25 | General Electric Company | Method and apparatus for gas turbine engine temperature management |
JP5374199B2 (ja) * | 2009-03-19 | 2013-12-25 | 三菱重工業株式会社 | ガスタービン |
JP2011241791A (ja) * | 2010-05-20 | 2011-12-01 | Kawasaki Heavy Ind Ltd | ガスタービンエンジンのタービン |
US8684685B2 (en) * | 2010-10-20 | 2014-04-01 | General Electric Company | Rotary machine having grooves for control of fluid dynamics |
US8678752B2 (en) * | 2010-10-20 | 2014-03-25 | General Electric Company | Rotary machine having non-uniform blade and vane spacing |
US9115594B2 (en) | 2010-12-28 | 2015-08-25 | Rolls-Royce Corporation | Compressor casing treatment for gas turbine engine |
US20130074509A1 (en) * | 2011-09-23 | 2013-03-28 | General Electric Company | Turbomachine configured to burn ash-bearing fuel oils and method of burning ash-bearing fuel oils in a turbomachine |
US20130081402A1 (en) * | 2011-10-03 | 2013-04-04 | General Electric Company | Turbomachine having a gas flow aeromechanic system and method |
US9267687B2 (en) | 2011-11-04 | 2016-02-23 | General Electric Company | Combustion system having a venturi for reducing wakes in an airflow |
US8899975B2 (en) | 2011-11-04 | 2014-12-02 | General Electric Company | Combustor having wake air injection |
US20130209216A1 (en) * | 2012-02-09 | 2013-08-15 | General Electric Company | Turbomachine including flow improvement system |
US9200520B2 (en) | 2012-06-22 | 2015-12-01 | General Electric Company | Gas turbine conical flange bolted joint |
US9500085B2 (en) | 2012-07-23 | 2016-11-22 | General Electric Company | Method for modifying gas turbine performance |
WO2014055104A1 (en) * | 2012-10-01 | 2014-04-10 | United Technologies Corporation | Gas turbine engine with first turbine vane clocking |
US9739201B2 (en) | 2013-05-08 | 2017-08-22 | General Electric Company | Wake reducing structure for a turbine system and method of reducing wake |
US9322553B2 (en) | 2013-05-08 | 2016-04-26 | General Electric Company | Wake manipulating structure for a turbine system |
US9435221B2 (en) * | 2013-08-09 | 2016-09-06 | General Electric Company | Turbomachine airfoil positioning |
DE102013224081B4 (de) * | 2013-11-26 | 2015-11-05 | Man Diesel & Turbo Se | Verdichter |
EP3059391A1 (de) * | 2015-02-18 | 2016-08-24 | United Technologies Corporation | Kühlung der turbinenschaufel eines gasturbinenmotors mit vorgelagerter statorschaufel |
US11415002B2 (en) * | 2019-10-18 | 2022-08-16 | Raytheon Technologies Corporation | Baffle with impingement holes |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS54114618A (en) * | 1978-02-28 | 1979-09-06 | Toshiba Corp | Moving and stator blades arranging method of turbine |
JPH04284101A (ja) * | 1991-03-11 | 1992-10-08 | Mitsubishi Heavy Ind Ltd | 回転機械の翼列構成 |
US5486091A (en) * | 1994-04-19 | 1996-01-23 | United Technologies Corporation | Gas turbine airfoil clocking |
US6174129B1 (en) * | 1999-01-07 | 2001-01-16 | Siemens Westinghouse Power Corporation | Turbine vane clocking mechanism and method of assembling a turbine having such a mechanism |
-
2000
- 2000-08-16 US US09/640,357 patent/US6402458B1/en not_active Expired - Fee Related
-
2001
- 2001-08-03 DE DE60132405T patent/DE60132405T2/de not_active Expired - Lifetime
- 2001-08-03 EP EP01306653A patent/EP1182339B1/de not_active Expired - Lifetime
- 2001-08-15 JP JP2001246341A patent/JP4733876B2/ja not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
EP1182339A3 (de) | 2004-03-03 |
DE60132405T2 (de) | 2009-01-02 |
US6402458B1 (en) | 2002-06-11 |
JP4733876B2 (ja) | 2011-07-27 |
EP1182339B1 (de) | 2008-01-16 |
JP2002155701A (ja) | 2002-05-31 |
EP1182339A2 (de) | 2002-02-27 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |