DE60021487D1 - Vorgespannte Gasturbinenleitschaufel - Google Patents
Vorgespannte GasturbinenleitschaufelInfo
- Publication number
- DE60021487D1 DE60021487D1 DE60021487T DE60021487T DE60021487D1 DE 60021487 D1 DE60021487 D1 DE 60021487D1 DE 60021487 T DE60021487 T DE 60021487T DE 60021487 T DE60021487 T DE 60021487T DE 60021487 D1 DE60021487 D1 DE 60021487D1
- Authority
- DE
- Germany
- Prior art keywords
- gas turbine
- guide vane
- rod
- turbine guide
- outer ring
- 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
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
-
- 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
- F01D5/188—Convection cooling with an insert in the blade cavity to guide the cooling fluid, e.g. forming a separation wall
- F01D5/189—Convection cooling with an insert in the blade cavity to guide the cooling fluid, e.g. forming a separation wall the insert having a tubular cross-section, e.g. airfoil shape
-
- 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
- F01D5/147—Construction, i.e. structural features, e.g. of weight-saving hollow blades
-
- 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
- F05D2240/00—Components
- F05D2240/10—Stators
-
- 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
- F05D2240/00—Components
- F05D2240/80—Platforms for stationary or moving blades
- F05D2240/81—Cooled platforms
-
- 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
- F05D2260/205—Cooling fluid recirculation, i.e. after cooling one or more components is the cooling fluid recovered and used elsewhere for other purposes
-
- 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
- F05D2260/232—Heat transfer, e.g. cooling characterized by the cooling medium
- F05D2260/2322—Heat transfer, e.g. cooling characterized by the cooling medium steam
-
- 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
- Y10T29/49316—Impeller making
- Y10T29/4932—Turbomachine making
- Y10T29/49323—Assembling fluid flow directing devices, e.g., stators, diaphragms, nozzles
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Architecture (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Control Of Turbines (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US35433699A | 1999-07-16 | 1999-07-16 | |
US354336 | 1999-07-16 |
Publications (2)
Publication Number | Publication Date |
---|---|
DE60021487D1 true DE60021487D1 (de) | 2005-09-01 |
DE60021487T2 DE60021487T2 (de) | 2006-05-18 |
Family
ID=23392859
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE60021487T Expired - Lifetime DE60021487T2 (de) | 1999-07-16 | 2000-05-24 | Vorgespannte Gasturbinenleitschaufel |
Country Status (6)
Country | Link |
---|---|
US (1) | US6402463B2 (de) |
EP (1) | EP1069281B1 (de) |
JP (1) | JP4738567B2 (de) |
KR (1) | KR20010014988A (de) |
AT (1) | ATE300664T1 (de) |
DE (1) | DE60021487T2 (de) |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE10217388A1 (de) * | 2002-04-18 | 2003-10-30 | Siemens Ag | Luft- und dampfgekühlte Plattform einer Turbinenschaufel |
US7090393B2 (en) * | 2002-12-13 | 2006-08-15 | General Electric Company | Using thermal imaging to prevent loss of steam turbine efficiency by detecting and correcting inadequate insulation at turbine startup |
US6742984B1 (en) | 2003-05-19 | 2004-06-01 | General Electric Company | Divided insert for steam cooled nozzles and method for supporting and separating divided insert |
US7857580B1 (en) * | 2006-09-15 | 2010-12-28 | Florida Turbine Technologies, Inc. | Turbine vane with end-wall leading edge cooling |
US8197210B1 (en) * | 2007-09-07 | 2012-06-12 | Florida Turbine Technologies, Inc. | Turbine vane with leading edge insert |
EP2626519A1 (de) * | 2012-02-09 | 2013-08-14 | Siemens Aktiengesellschaft | Turbinenbaugruppe, zugehöriges Prallkühlungsrohr und Gasturbinenkraftwerk. |
CN103306742B (zh) * | 2012-03-13 | 2015-10-28 | 马重芳 | 冷却燃气轮机叶片的方法 |
US20140053403A1 (en) * | 2012-08-22 | 2014-02-27 | General Electric Company | Method for extending an original service life of gas turbine components |
US11415006B2 (en) * | 2020-09-17 | 2022-08-16 | Raytheon Technologies Corporation | CMC vane with support spar and baffle |
Family Cites Families (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1075910A (en) * | 1966-04-04 | 1967-07-19 | Rolls Royce | Improvements in or relating to blades for mounting in fluid flow ducts |
GB1187978A (en) * | 1966-10-01 | 1970-04-15 | Plessey Co Ltd | Improvements in or relating to Gas-Turbine Rotors. |
US3844728A (en) * | 1968-03-20 | 1974-10-29 | United Aircraft Corp | Gas contacting element leading edge and trailing edge insert |
GB1290134A (de) * | 1970-01-23 | 1972-09-20 | ||
US3741681A (en) * | 1971-05-28 | 1973-06-26 | Westinghouse Electric Corp | Hollow turbine rotor assembly |
US4314794A (en) * | 1979-10-25 | 1982-02-09 | Westinghouse Electric Corp. | Transpiration cooled blade for a gas turbine engine |
DE3110098C2 (de) * | 1981-03-16 | 1983-03-17 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | Turbinenleitschaufel für Gasturbinentriebwerke |
JPS58161103A (ja) * | 1982-03-19 | 1983-09-24 | Matsushita Electric Ind Co Ltd | 磁石式消去ヘツド装置の製造方法 |
GB2121115A (en) * | 1982-06-03 | 1983-12-14 | Rolls Royce | Aerofoil vane assembly |
DE3539903A1 (de) * | 1985-11-11 | 1987-05-14 | Kloeckner Humboldt Deutz Ag | Gasturbine mit einem keramischen laufrad |
JPS6380004A (ja) * | 1986-09-22 | 1988-04-11 | Hitachi Ltd | ガスタ−ビン静翼 |
JPS63223302A (ja) * | 1987-03-13 | 1988-09-16 | Hitachi Ltd | ガスタ−ビン用セラミツク静翼 |
US4987736A (en) * | 1988-12-14 | 1991-01-29 | General Electric Company | Lightweight gas turbine engine frame with free-floating heat shield |
US5076049A (en) * | 1990-04-02 | 1991-12-31 | General Electric Company | Pretensioned frame |
JP2984767B2 (ja) * | 1990-11-29 | 1999-11-29 | 株式会社日立製作所 | セラミック静翼 |
JPH05156901A (ja) * | 1991-12-02 | 1993-06-22 | Hitachi Ltd | ガスタービン冷却静翼 |
US6000906A (en) * | 1997-09-12 | 1999-12-14 | Alliedsignal Inc. | Ceramic airfoil |
US6164903A (en) * | 1998-12-22 | 2000-12-26 | United Technologies Corporation | Turbine vane mounting arrangement |
-
2000
- 2000-05-24 DE DE60021487T patent/DE60021487T2/de not_active Expired - Lifetime
- 2000-05-24 AT AT00304399T patent/ATE300664T1/de not_active IP Right Cessation
- 2000-05-24 EP EP00304399A patent/EP1069281B1/de not_active Expired - Lifetime
- 2000-06-01 KR KR1020000029915A patent/KR20010014988A/ko not_active Application Discontinuation
- 2000-06-12 JP JP2000174587A patent/JP4738567B2/ja not_active Expired - Fee Related
-
2001
- 2001-02-07 US US09/778,033 patent/US6402463B2/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
US20010018019A1 (en) | 2001-08-30 |
US6402463B2 (en) | 2002-06-11 |
JP4738567B2 (ja) | 2011-08-03 |
ATE300664T1 (de) | 2005-08-15 |
JP2001041003A (ja) | 2001-02-13 |
EP1069281A2 (de) | 2001-01-17 |
EP1069281B1 (de) | 2005-07-27 |
DE60021487T2 (de) | 2006-05-18 |
EP1069281A3 (de) | 2002-12-11 |
KR20010014988A (ko) | 2001-02-26 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |