DE60211061D1 - Axialturbine mit einer Stufe in einem Abströmkanal - Google Patents
Axialturbine mit einer Stufe in einem AbströmkanalInfo
- Publication number
- DE60211061D1 DE60211061D1 DE60211061T DE60211061T DE60211061D1 DE 60211061 D1 DE60211061 D1 DE 60211061D1 DE 60211061 T DE60211061 T DE 60211061T DE 60211061 T DE60211061 T DE 60211061T DE 60211061 D1 DE60211061 D1 DE 60211061D1
- Authority
- DE
- Germany
- Prior art keywords
- stage
- discharge channel
- axial turbine
- turbine
- axial
- 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
- 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
- F01D5/143—Contour of the outer or inner working fluid flow path wall, i.e. shroud or hub contour
-
- 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
- F01D25/30—Exhaust heads, chambers, or the like
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2001132962A JP3564420B2 (ja) | 2001-04-27 | 2001-04-27 | ガスタービン |
JP2001132962 | 2001-04-27 |
Publications (2)
Publication Number | Publication Date |
---|---|
DE60211061D1 true DE60211061D1 (de) | 2006-06-08 |
DE60211061T2 DE60211061T2 (de) | 2006-12-07 |
Family
ID=18980902
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE60211061T Expired - Lifetime DE60211061T2 (de) | 2001-04-27 | 2002-02-22 | Axialturbine mit einer Stufe in einem Abströmkanal |
Country Status (5)
Country | Link |
---|---|
US (1) | US6733238B2 (de) |
EP (1) | EP1253295B1 (de) |
JP (1) | JP3564420B2 (de) |
CA (1) | CA2372623C (de) |
DE (1) | DE60211061T2 (de) |
Families Citing this family (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE10255389A1 (de) * | 2002-11-28 | 2004-06-09 | Alstom Technology Ltd | Niederdruckdampfturbine mit Mehrkanal-Diffusor |
TWI226683B (en) * | 2004-02-10 | 2005-01-11 | Powerchip Semiconductor Corp | Method of fabricating a flash memory |
EP1574667B1 (de) * | 2004-03-02 | 2013-07-17 | Siemens Aktiengesellschaft | Verdichterdiffusor |
CN1309055C (zh) * | 2004-03-25 | 2007-04-04 | 力晶半导体股份有限公司 | 闪速存储器的制造方法 |
US20110176917A1 (en) * | 2004-07-02 | 2011-07-21 | Brian Haller | Exhaust Gas Diffuser Wall Contouring |
GB2415749B (en) * | 2004-07-02 | 2009-10-07 | Demag Delaval Ind Turbomachine | A gas turbine engine including an exhaust duct comprising a diffuser for diffusing the exhaust gas produced by the engine |
US7909569B2 (en) * | 2005-06-09 | 2011-03-22 | Pratt & Whitney Canada Corp. | Turbine support case and method of manufacturing |
US8500399B2 (en) * | 2006-04-25 | 2013-08-06 | Rolls-Royce Corporation | Method and apparatus for enhancing compressor performance |
US7731475B2 (en) * | 2007-05-17 | 2010-06-08 | Elliott Company | Tilted cone diffuser for use with an exhaust system of a turbine |
EP2146054A1 (de) * | 2008-07-17 | 2010-01-20 | Siemens Aktiengesellschaft | Axialturbine für eine Gasturbine |
US8647057B2 (en) * | 2009-06-02 | 2014-02-11 | Siemens Energy, Inc. | Turbine exhaust diffuser with a gas jet producing a coanda effect flow control |
US8668449B2 (en) * | 2009-06-02 | 2014-03-11 | Siemens Energy, Inc. | Turbine exhaust diffuser with region of reduced flow area and outer boundary gas flow |
US8337153B2 (en) * | 2009-06-02 | 2012-12-25 | Siemens Energy, Inc. | Turbine exhaust diffuser flow path with region of reduced total flow area |
US8475125B2 (en) * | 2010-04-13 | 2013-07-02 | General Electric Company | Shroud vortex remover |
US8628297B2 (en) * | 2010-08-20 | 2014-01-14 | General Electric Company | Tip flowpath contour |
US9284853B2 (en) * | 2011-10-20 | 2016-03-15 | General Electric Company | System and method for integrating sections of a turbine |
DE102011118735A1 (de) * | 2011-11-17 | 2013-05-23 | Alstom Technology Ltd. | Diffusor, insbesondere für eine axiale strömungsmaschine |
JP5761763B2 (ja) * | 2011-12-07 | 2015-08-12 | 三菱日立パワーシステムズ株式会社 | タービン動翼 |
US9032721B2 (en) * | 2011-12-14 | 2015-05-19 | Siemens Energy, Inc. | Gas turbine engine exhaust diffuser including circumferential vane |
US9121285B2 (en) * | 2012-05-24 | 2015-09-01 | General Electric Company | Turbine and method for reducing shock losses in a turbine |
US9598981B2 (en) * | 2013-11-22 | 2017-03-21 | Siemens Energy, Inc. | Industrial gas turbine exhaust system diffuser inlet lip |
EP3054086B1 (de) * | 2015-02-05 | 2017-09-13 | General Electric Technology GmbH | Dampfturbinendiffusorkonfiguration |
US10794397B2 (en) | 2015-04-03 | 2020-10-06 | Mitsubishi Heavy Industries, Ltd. | Rotor blade and axial flow rotary machine |
RU2612309C1 (ru) * | 2015-10-26 | 2017-03-06 | Государственный научный центр Российской Федерации - федеральное государственное унитарное предприятие "Исследовательский Центр имени М.В. Келдыша" | Центростремительная турбина |
RU2694560C1 (ru) * | 2018-09-12 | 2019-07-16 | Государственный научный центр Российской Федерации - федеральное государственное унитарное предприятие "Исследовательский Центр имени М.В. Келдыша" | Центростремительная турбина |
JP7458947B2 (ja) * | 2020-09-15 | 2024-04-01 | 三菱重工コンプレッサ株式会社 | 蒸気タービン |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CH216489A (de) | 1940-04-04 | 1941-08-31 | Sulzer Ag | Mehrstufiger Axialverdichter. |
FR996967A (fr) | 1949-09-06 | 1951-12-31 | Rateau Soc | Perfectionnement aux aubages de turbomachines |
FR1338515A (fr) | 1962-08-14 | 1963-09-27 | Rateau Soc | Perfectionnement au dispositif d'échappement des turbines |
US3625630A (en) * | 1970-03-27 | 1971-12-07 | Caterpillar Tractor Co | Axial flow diffuser |
JP3104395B2 (ja) | 1992-05-15 | 2000-10-30 | 株式会社日立製作所 | 軸流圧縮機 |
JPH08260905A (ja) * | 1995-03-28 | 1996-10-08 | Mitsubishi Heavy Ind Ltd | 軸流タービン用排気ディフューザ |
JPH11148497A (ja) | 1997-11-17 | 1999-06-02 | Hitachi Ltd | 軸流圧縮機動翼 |
JP3912989B2 (ja) * | 2001-01-25 | 2007-05-09 | 三菱重工業株式会社 | ガスタービン |
-
2001
- 2001-04-27 JP JP2001132962A patent/JP3564420B2/ja not_active Expired - Lifetime
-
2002
- 2002-02-20 CA CA002372623A patent/CA2372623C/en not_active Expired - Lifetime
- 2002-02-22 US US10/079,853 patent/US6733238B2/en not_active Expired - Lifetime
- 2002-02-22 DE DE60211061T patent/DE60211061T2/de not_active Expired - Lifetime
- 2002-02-22 EP EP02004029A patent/EP1253295B1/de not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
EP1253295B1 (de) | 2006-05-03 |
DE60211061T2 (de) | 2006-12-07 |
US20020159886A1 (en) | 2002-10-31 |
EP1253295A3 (de) | 2004-01-14 |
CA2372623C (en) | 2005-04-26 |
JP2002327604A (ja) | 2002-11-15 |
US6733238B2 (en) | 2004-05-11 |
CA2372623A1 (en) | 2002-10-27 |
JP3564420B2 (ja) | 2004-09-08 |
EP1253295A2 (de) | 2002-10-30 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |