ITMI20072441A1 - LATEST PRESSURE SECTION STATE STADIUM STAGE OF A STEAM TURBINE - Google Patents
LATEST PRESSURE SECTION STATE STADIUM STAGE OF A STEAM TURBINEInfo
- Publication number
- ITMI20072441A1 ITMI20072441A1 ITMI20072441A ITMI20072441A1 IT MI20072441 A1 ITMI20072441 A1 IT MI20072441A1 IT MI20072441 A ITMI20072441 A IT MI20072441A IT MI20072441 A1 ITMI20072441 A1 IT MI20072441A1
- Authority
- IT
- Italy
- Prior art keywords
- steam turbine
- pressure section
- section state
- latest pressure
- stadium
- Prior art date
Links
- RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 title 1
- 238000004326 stimulated echo acquisition mode for imaging Methods 0.000 title 1
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
-
- 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
- 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
- F05D2200/00—Mathematical features
- F05D2200/20—Special functions
-
- 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
- F05D2220/00—Application
- F05D2220/30—Application in turbines
- F05D2220/31—Application in turbines in steam turbines
-
- 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
- F05D2240/12—Fluid guiding means, e.g. vanes
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| ITMI20072441 ITMI20072441A1 (en) | 2007-12-28 | 2007-12-28 | LATEST PRESSURE SECTION STATE STADIUM STAGE OF A STEAM TURBINE |
| EP08173020A EP2075408A3 (en) | 2007-12-28 | 2008-12-29 | Last stage stator blade of a steam turbine low-pressure section |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| ITMI20072441 ITMI20072441A1 (en) | 2007-12-28 | 2007-12-28 | LATEST PRESSURE SECTION STATE STADIUM STAGE OF A STEAM TURBINE |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ITMI20072441A1 true ITMI20072441A1 (en) | 2009-06-29 |
Family
ID=40315667
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| ITMI20072441 ITMI20072441A1 (en) | 2007-12-28 | 2007-12-28 | LATEST PRESSURE SECTION STATE STADIUM STAGE OF A STEAM TURBINE |
Country Status (2)
| Country | Link |
|---|---|
| EP (1) | EP2075408A3 (en) |
| IT (1) | ITMI20072441A1 (en) |
Families Citing this family (33)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8137062B2 (en) | 2010-05-11 | 2012-03-20 | General Electric Company | Turbomachine nozzle |
| ITMI20101447A1 (en) * | 2010-07-30 | 2012-01-30 | Alstom Technology Ltd | "LOW PRESSURE STEAM TURBINE AND METHOD FOR THE FUNCTIONING OF THE SAME" |
| US9011084B2 (en) | 2010-09-28 | 2015-04-21 | Mitsubishi Hitachi Power Systems, Ltd. | Steam turbine stator vane and steam turbine using the same |
| KR101322554B1 (en) * | 2012-03-27 | 2013-10-28 | 가부시키가이샤 히타치세이사쿠쇼 | Stationary blade of steam turbine and steam turbine with the same |
| ITCO20120061A1 (en) * | 2012-12-13 | 2014-06-14 | Nuovo Pignone Srl | METHODS FOR PRODUCING TURBOMACCHINA POLES WITH SHAPED CHANNELS THROUGH ADDITIVE PRODUCTION, TURBOMACCHINA POLES AND TURBOMACCHINE |
| CN103541774B (en) * | 2013-11-14 | 2015-06-17 | 上海汽轮机厂有限公司 | Method for designing turbine blades |
| EP3108113A4 (en) | 2014-02-19 | 2017-03-15 | United Technologies Corporation | Gas turbine engine airfoil |
| EP3108122B1 (en) | 2014-02-19 | 2023-09-20 | Raytheon Technologies Corporation | Turbofan engine with geared architecture and lpc airfoils |
| US9567858B2 (en) | 2014-02-19 | 2017-02-14 | United Technologies Corporation | Gas turbine engine airfoil |
| EP3108118B1 (en) | 2014-02-19 | 2019-09-18 | United Technologies Corporation | Gas turbine engine airfoil |
| EP3108106B1 (en) | 2014-02-19 | 2022-05-04 | Raytheon Technologies Corporation | Gas turbine engine airfoil |
| EP3108116B1 (en) | 2014-02-19 | 2024-01-17 | RTX Corporation | Gas turbine engine |
| US10605259B2 (en) | 2014-02-19 | 2020-03-31 | United Technologies Corporation | Gas turbine engine airfoil |
| EP4279706A3 (en) | 2014-02-19 | 2024-02-28 | RTX Corporation | Turbofan engine with geared architecture and lpc blade airfoils |
| EP3108103B1 (en) | 2014-02-19 | 2023-09-27 | Raytheon Technologies Corporation | Fan blade for a gas turbine engine |
| EP3985226B1 (en) | 2014-02-19 | 2024-12-25 | RTX Corporation | Gas turbine engine airfoil |
| WO2015126454A1 (en) | 2014-02-19 | 2015-08-27 | United Technologies Corporation | Gas turbine engine airfoil |
| WO2015175051A2 (en) | 2014-02-19 | 2015-11-19 | United Technologies Corporation | Gas turbine engine airfoil |
| US10557477B2 (en) | 2014-02-19 | 2020-02-11 | United Technologies Corporation | Gas turbine engine airfoil |
| WO2015126793A1 (en) * | 2014-02-19 | 2015-08-27 | United Technologies Corporation | Gas turbine engine airfoil |
| EP3575551B1 (en) | 2014-02-19 | 2021-10-27 | Raytheon Technologies Corporation | Gas turbine engine airfoil |
| EP3108101B1 (en) | 2014-02-19 | 2022-04-20 | Raytheon Technologies Corporation | Gas turbine engine airfoil |
| WO2015126450A1 (en) | 2014-02-19 | 2015-08-27 | United Technologies Corporation | Gas turbine engine airfoil |
| US10495106B2 (en) | 2014-02-19 | 2019-12-03 | United Technologies Corporation | Gas turbine engine airfoil |
| US9140127B2 (en) | 2014-02-19 | 2015-09-22 | United Technologies Corporation | Gas turbine engine airfoil |
| EP3108107B1 (en) | 2014-02-19 | 2023-10-11 | Raytheon Technologies Corporation | Turbofan engine with geared architecture and lpc airfoils |
| WO2015126453A1 (en) | 2014-02-19 | 2015-08-27 | United Technologies Corporation | Gas turbine engine airfoil |
| WO2015178974A2 (en) | 2014-02-19 | 2015-11-26 | United Technologies Corporation | Gas turbine engine airfoil |
| EP3108109B1 (en) | 2014-02-19 | 2023-09-13 | Raytheon Technologies Corporation | Gas turbine engine fan blade |
| GB201707811D0 (en) * | 2017-05-16 | 2017-06-28 | Rolls Royce Plc | Compressor aerofoil member |
| JP6426869B1 (en) | 2018-06-08 | 2018-11-21 | 株式会社グローバルエナジー | Horizontal axis rotor |
| CN113250755B (en) * | 2021-04-15 | 2022-06-07 | 西北工业大学 | Blade profile design method based on non-uniform rational B-spline curve and blade |
| DE102022103319A1 (en) * | 2022-02-11 | 2023-08-17 | MTU Aero Engines AG | Guide vane for a turbomachine |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0916812B1 (en) * | 1997-11-17 | 2003-03-05 | ALSTOM (Switzerland) Ltd | Final stage for an axial turbine |
| US6709239B2 (en) * | 2001-06-27 | 2004-03-23 | Bharat Heavy Electricals Ltd. | Three dimensional blade |
| US20090104023A1 (en) * | 2005-07-19 | 2009-04-23 | Frederic Favray | Variable Nozzle Turbocharger |
| JP2009531593A (en) * | 2006-03-31 | 2009-09-03 | アルストム テクノロジー リミテッド | Guide blades for fluid machinery, especially steam turbines |
-
2007
- 2007-12-28 IT ITMI20072441 patent/ITMI20072441A1/en unknown
-
2008
- 2008-12-29 EP EP08173020A patent/EP2075408A3/en not_active Withdrawn
Also Published As
| Publication number | Publication date |
|---|---|
| EP2075408A2 (en) | 2009-07-01 |
| EP2075408A3 (en) | 2013-03-06 |
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