ATE487025T1 - Leitschaufel für eine gasturbine - Google Patents
Leitschaufel für eine gasturbineInfo
- Publication number
- ATE487025T1 ATE487025T1 AT08761302T AT08761302T ATE487025T1 AT E487025 T1 ATE487025 T1 AT E487025T1 AT 08761302 T AT08761302 T AT 08761302T AT 08761302 T AT08761302 T AT 08761302T AT E487025 T1 ATE487025 T1 AT E487025T1
- Authority
- AT
- Austria
- Prior art keywords
- gas turbine
- shroud
- clearance
- side wall
- trailing edge
- 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
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
- F01D9/041—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades
-
- 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
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/005—Sealing means between non relatively rotating elements
-
- 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
- F05D2230/00—Manufacture
- F05D2230/10—Manufacture by removing material
-
- 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
- F05D2240/11—Shroud seal segments
-
- 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
- F05D2240/55—Seals
- F05D2240/57—Leaf seals
-
- 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
-
- 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
- F05D2250/20—Three-dimensional
- F05D2250/29—Three-dimensional machined; miscellaneous
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Control Of Turbines (AREA)
- Valve-Gear Or Valve Arrangements (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH10442007 | 2007-06-28 | ||
PCT/EP2008/057947 WO2009000802A2 (de) | 2007-06-28 | 2008-06-23 | Leitschaufel für eine gasturbine |
Publications (1)
Publication Number | Publication Date |
---|---|
ATE487025T1 true ATE487025T1 (de) | 2010-11-15 |
Family
ID=38566219
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AT08761302T ATE487025T1 (de) | 2007-06-28 | 2008-06-23 | Leitschaufel für eine gasturbine |
Country Status (8)
Country | Link |
---|---|
US (1) | US8152454B2 (de) |
EP (1) | EP2158381B1 (de) |
AT (1) | ATE487025T1 (de) |
CA (1) | CA2691186C (de) |
DE (1) | DE502008001731D1 (de) |
SI (1) | SI2158381T1 (de) |
TW (1) | TWI440768B (de) |
WO (1) | WO2009000802A2 (de) |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8376705B1 (en) | 2011-09-09 | 2013-02-19 | Siemens Energy, Inc. | Turbine endwall with grooved recess cavity |
US9840917B2 (en) * | 2011-12-13 | 2017-12-12 | United Technologies Corporation | Stator vane shroud having an offset |
US9683446B2 (en) * | 2013-03-07 | 2017-06-20 | Rolls-Royce Energy Systems, Inc. | Gas turbine engine shrouded blade |
EP2964934B1 (de) * | 2013-03-08 | 2018-10-03 | United Technologies Corporation | Gasturbinenmotorkomponente mit einem federdichtungsschlitz von variabler breite |
EP2811118B1 (de) * | 2013-06-06 | 2018-03-14 | MTU Aero Engines GmbH | Leitschaufelsegment einer Strömungsmaschine und Turbine |
US10352180B2 (en) | 2013-10-23 | 2019-07-16 | General Electric Company | Gas turbine nozzle trailing edge fillet |
EP2985419B1 (de) | 2014-08-13 | 2020-01-08 | United Technologies Corporation | Turbomaschinenlaufschaufelanordnung mit schaufelfussdichtungen |
US10329931B2 (en) * | 2014-10-01 | 2019-06-25 | United Technologies Corporation | Stator assembly for a gas turbine engine |
US10876417B2 (en) * | 2017-08-17 | 2020-12-29 | Raytheon Technologies Corporation | Tuned airfoil assembly |
US11506129B2 (en) | 2020-04-24 | 2022-11-22 | Raytheon Technologies Corporation | Feather seal mateface cooling pockets |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3542483A (en) * | 1968-07-17 | 1970-11-24 | Westinghouse Electric Corp | Turbine stator structure |
US3938906A (en) * | 1974-10-07 | 1976-02-17 | Westinghouse Electric Corporation | Slidable stator seal |
US4524980A (en) | 1983-12-05 | 1985-06-25 | United Technologies Corporation | Intersecting feather seals for interlocking gas turbine vanes |
GB2195403A (en) * | 1986-09-17 | 1988-04-07 | Rolls Royce Plc | Improvements in or relating to sealing and cooling means |
JP2001152804A (ja) * | 1999-11-19 | 2001-06-05 | Mitsubishi Heavy Ind Ltd | ガスタービン設備及びタービン翼 |
US7625174B2 (en) * | 2005-12-16 | 2009-12-01 | General Electric Company | Methods and apparatus for assembling gas turbine engine stator assemblies |
US7922444B2 (en) * | 2007-01-19 | 2011-04-12 | United Technologies Corporation | Chamfer rail pockets for turbine vane shrouds |
-
2008
- 2008-06-23 AT AT08761302T patent/ATE487025T1/de active
- 2008-06-23 DE DE502008001731T patent/DE502008001731D1/de active Active
- 2008-06-23 SI SI200830147T patent/SI2158381T1/sl unknown
- 2008-06-23 CA CA2691186A patent/CA2691186C/en not_active Expired - Fee Related
- 2008-06-23 EP EP08761302A patent/EP2158381B1/de not_active Not-in-force
- 2008-06-23 WO PCT/EP2008/057947 patent/WO2009000802A2/de active Application Filing
- 2008-06-27 TW TW097124405A patent/TWI440768B/zh not_active IP Right Cessation
-
2009
- 2009-12-23 US US12/646,365 patent/US8152454B2/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
SI2158381T1 (sl) | 2011-03-31 |
EP2158381B1 (de) | 2010-11-03 |
WO2009000802A3 (de) | 2009-03-19 |
CA2691186A1 (en) | 2008-12-31 |
TW200925390A (en) | 2009-06-16 |
WO2009000802A2 (de) | 2008-12-31 |
US20100150710A1 (en) | 2010-06-17 |
US8152454B2 (en) | 2012-04-10 |
TWI440768B (zh) | 2014-06-11 |
CA2691186C (en) | 2015-08-04 |
DE502008001731D1 (de) | 2010-12-16 |
EP2158381A2 (de) | 2010-03-03 |
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