EP2075408A3 - Leitschaufel auf letzter Stufe des Niederdruckabschnitts einer Dampfturbine - Google Patents
Leitschaufel auf letzter Stufe des Niederdruckabschnitts einer Dampfturbine Download PDFInfo
- Publication number
- EP2075408A3 EP2075408A3 EP08173020A EP08173020A EP2075408A3 EP 2075408 A3 EP2075408 A3 EP 2075408A3 EP 08173020 A EP08173020 A EP 08173020A EP 08173020 A EP08173020 A EP 08173020A EP 2075408 A3 EP2075408 A3 EP 2075408A3
- Authority
- EP
- European Patent Office
- Prior art keywords
- steam turbine
- last stage
- pressure section
- stator blade
- turbine low
- 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.)
- Withdrawn
Links
- WRRSFOZOETZUPG-FFHNEAJVSA-N (4r,4ar,7s,7ar,12bs)-9-methoxy-3-methyl-2,4,4a,7,7a,13-hexahydro-1h-4,12-methanobenzofuro[3,2-e]isoquinoline-7-ol;hydrate Chemical compound O.C([C@H]1[C@H](N(CC[C@@]112)C)C3)=C[C@H](O)[C@@H]1OC1=C2C3=CC=C1OC WRRSFOZOETZUPG-FFHNEAJVSA-N 0.000 abstract 2
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)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| ITMI20072441 ITMI20072441A1 (it) | 2007-12-28 | 2007-12-28 | Pala statorica di ultimo stadio di sezione di bassa pressione di una turbina a vapore |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP2075408A2 EP2075408A2 (de) | 2009-07-01 |
| EP2075408A3 true EP2075408A3 (de) | 2013-03-06 |
Family
ID=40315667
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP08173020A Withdrawn EP2075408A3 (de) | 2007-12-28 | 2008-12-29 | Leitschaufel auf letzter Stufe des Niederdruckabschnitts einer Dampfturbine |
Country Status (2)
| Country | Link |
|---|---|
| EP (1) | EP2075408A3 (de) |
| IT (1) | ITMI20072441A1 (de) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US12135007B2 (en) | 2018-06-08 | 2024-11-05 | Global Energy Co., Ltd. | Horizontal shaft rotor |
Families Citing this family (32)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8137062B2 (en) | 2010-05-11 | 2012-03-20 | General Electric Company | Turbomachine nozzle |
| ITMI20101447A1 (it) * | 2010-07-30 | 2012-01-30 | Alstom Technology Ltd | "turbina a vapore a bassa pressione e metodo per il funzionamento della stessa" |
| EP2434094A3 (de) | 2010-09-28 | 2018-02-21 | Mitsubishi Hitachi Power Systems, Ltd. | Leitschaufel für Dampfturbine und Dampfturbine |
| KR101322554B1 (ko) * | 2012-03-27 | 2013-10-28 | 가부시키가이샤 히타치세이사쿠쇼 | 증기 터빈의 고정익 및 그것을 사용한 증기 터빈 |
| ITCO20120061A1 (it) * | 2012-12-13 | 2014-06-14 | Nuovo Pignone Srl | Metodi per produrre pale di turbomacchina con canali sagomati mediante produzione additiva, pale di turbomacchina e turbomacchine |
| CN103541774B (zh) * | 2013-11-14 | 2015-06-17 | 上海汽轮机厂有限公司 | 涡轮叶片设计方法 |
| WO2015175052A2 (en) | 2014-02-19 | 2015-11-19 | United Technologies Corporation | Gas turbine engine airfoil |
| EP3108112B1 (de) * | 2014-02-19 | 2023-10-11 | Raytheon Technologies Corporation | Turboluftstrahltriebwerk mit getriebefan und niederdruckverdichterschaufeln |
| US9567858B2 (en) | 2014-02-19 | 2017-02-14 | United Technologies Corporation | Gas turbine engine airfoil |
| US9140127B2 (en) | 2014-02-19 | 2015-09-22 | United Technologies Corporation | Gas turbine engine airfoil |
| WO2015175044A2 (en) | 2014-02-19 | 2015-11-19 | United Technologies Corporation | Gas turbine engine airfoil |
| EP3108120B1 (de) | 2014-02-19 | 2021-03-31 | Raytheon Technologies Corporation | Gasturbinentriebwerk mit einer getriebearchitektur und einer spezifischen festen schaufelstruktur |
| WO2015175043A2 (en) | 2014-02-19 | 2015-11-19 | United Technologies Corporation | Gas turbine engine airfoil |
| US10465702B2 (en) | 2014-02-19 | 2019-11-05 | United Technologies Corporation | Gas turbine engine airfoil |
| US10570916B2 (en) | 2014-02-19 | 2020-02-25 | United Technologies Corporation | Gas turbine engine airfoil |
| WO2015175073A2 (en) | 2014-02-19 | 2015-11-19 | United Technologies Corporation | Gas turbine engine airfoil |
| EP3108100B1 (de) | 2014-02-19 | 2021-04-14 | Raytheon Technologies Corporation | Gasturbinengebläseschaufel |
| EP3575551B1 (de) | 2014-02-19 | 2021-10-27 | Raytheon Technologies Corporation | Gasturbinenmotorschaufel |
| EP3108103B1 (de) | 2014-02-19 | 2023-09-27 | Raytheon Technologies Corporation | Fanschaufel für ein gastrubinentriebwerk |
| US10570915B2 (en) | 2014-02-19 | 2020-02-25 | United Technologies Corporation | Gas turbine engine airfoil |
| WO2015126941A1 (en) | 2014-02-19 | 2015-08-27 | United Technologies Corporation | Gas turbine engine airfoil |
| US10584715B2 (en) | 2014-02-19 | 2020-03-10 | United Technologies Corporation | Gas turbine engine airfoil |
| EP3108106B1 (de) | 2014-02-19 | 2022-05-04 | Raytheon Technologies Corporation | Schaufelblatt eines gasturbinenmotors |
| EP3985226B1 (de) | 2014-02-19 | 2024-12-25 | RTX Corporation | Gasturbinentriebwerk-schaufelprofil |
| EP3108105B1 (de) | 2014-02-19 | 2021-05-12 | Raytheon Technologies Corporation | Gasturbinenmotor-tragfläche |
| US10495106B2 (en) | 2014-02-19 | 2019-12-03 | United Technologies Corporation | Gas turbine engine airfoil |
| WO2015126454A1 (en) | 2014-02-19 | 2015-08-27 | United Technologies Corporation | Gas turbine engine airfoil |
| EP3108101B1 (de) | 2014-02-19 | 2022-04-20 | Raytheon Technologies Corporation | Gasturbinenmotor-tragfläche |
| EP3108123B1 (de) | 2014-02-19 | 2023-10-04 | Raytheon Technologies Corporation | Turboluftstrahltriebwerk mit getriebefan und niederdruckverdichterschaufeln |
| GB201707811D0 (en) * | 2017-05-16 | 2017-06-28 | Rolls Royce Plc | Compressor aerofoil member |
| CN113250755B (zh) * | 2021-04-15 | 2022-06-07 | 西北工业大学 | 基于非均匀有理b样条曲线的叶型的设计方法及叶片 |
| DE102022103319A1 (de) | 2022-02-11 | 2023-08-17 | MTU Aero Engines AG | Leitschaufel für eine Strömungsmaschine |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0916812A1 (de) * | 1997-11-17 | 1999-05-19 | Asea Brown Boveri AG | Endstufe für axialdurchströmte Turbine |
| US20030086788A1 (en) * | 2001-06-27 | 2003-05-08 | Chandraker A. L. | Three dimensional blade |
| WO2007011355A1 (en) * | 2005-07-19 | 2007-01-25 | Honeywell International Inc. | Variable nozzle turbocharger |
| WO2007113149A1 (de) * | 2006-03-31 | 2007-10-11 | Alstom Technology Ltd | Leitschaufel für eine strömungsmaschine, insbesondere für eine dampfturbine |
-
2007
- 2007-12-28 IT ITMI20072441 patent/ITMI20072441A1/it unknown
-
2008
- 2008-12-29 EP EP08173020A patent/EP2075408A3/de not_active Withdrawn
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0916812A1 (de) * | 1997-11-17 | 1999-05-19 | Asea Brown Boveri AG | Endstufe für axialdurchströmte Turbine |
| US20030086788A1 (en) * | 2001-06-27 | 2003-05-08 | Chandraker A. L. | Three dimensional blade |
| WO2007011355A1 (en) * | 2005-07-19 | 2007-01-25 | Honeywell International Inc. | Variable nozzle turbocharger |
| WO2007113149A1 (de) * | 2006-03-31 | 2007-10-11 | Alstom Technology Ltd | Leitschaufel für eine strömungsmaschine, insbesondere für eine dampfturbine |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US12135007B2 (en) | 2018-06-08 | 2024-11-05 | Global Energy Co., Ltd. | Horizontal shaft rotor |
Also Published As
| Publication number | Publication date |
|---|---|
| ITMI20072441A1 (it) | 2009-06-29 |
| EP2075408A2 (de) | 2009-07-01 |
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| RIC1 | Information provided on ipc code assigned before grant |
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