EP0872628A3 - Stator vane for steam turbine - Google Patents
Stator vane for steam turbine Download PDFInfo
- Publication number
- EP0872628A3 EP0872628A3 EP98106798A EP98106798A EP0872628A3 EP 0872628 A3 EP0872628 A3 EP 0872628A3 EP 98106798 A EP98106798 A EP 98106798A EP 98106798 A EP98106798 A EP 98106798A EP 0872628 A3 EP0872628 A3 EP 0872628A3
- Authority
- EP
- European Patent Office
- Prior art keywords
- head
- foot
- foot pieces
- turbine housing
- signs
- 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- Withdrawn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
- 230000007797 corrosion Effects 0.000 abstract 1
- 238000005260 corrosion Methods 0.000 abstract 1
- 239000002184 metal Substances 0.000 abstract 1
- 230000002028 premature Effects 0.000 abstract 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
- F01D5/147—Construction, i.e. structural features, e.g. of weight-saving hollow 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
- 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
-
- 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
- F05D2230/00—Manufacture
- F05D2230/60—Assembly methods
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Architecture (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Laser Beam Processing (AREA)
- Butt Welding And Welding Of Specific Article (AREA)
Abstract
Die Erfindung bezieht sich auf eine Leitschaufel für Dampfturbinen, die Kopf- und Fußstücke aufweist und die in Mehrfachanordnung mit ihren Kopf- und Fußstücken im Turbinengehäuse je einen inneren und je einen äußeren Ring bilden.The invention relates to a guide vane for steam turbines, the head and foot pieces has and in multiple arrangement with their head and foot pieces in the turbine housing form an inner and an outer ring.
Aufgabe der Erfindung ist es, Leitschaufeln anzugeben, die einmal verhältnismäßig leicht, also im Materialeinsatz kostengünstig sind, beim Vorliegen von Verzugserscheinungen nur tragbarer Nachbearbeitung bedürfen und zum anderen zumindest die eigentlichen Schaufeln solche Oberflächen und Abreißkanten haben, daß nicht nur vorzeitig Korrosionserscheinungen vermieden sind, sondern vor allem bei einer langen Funktionsfähigkeit ein hoher Wirkungsgrad gesichert erscheint.The object of the invention is to provide guide vanes that are relatively light, that is are inexpensive to use, only when there are signs of distortion portable reworking and secondly at least the actual blades such surfaces and tear-off edges have that not only premature signs of corrosion are avoided, but above all with a long functionality a high efficiency appears secure.
Gelöst wird diese Aufgabe dadurch, daß jede einzelne Leitschaufel (2, vgl. auch 3) hohl ausgebildet ist und zusammen mit je einem Kopf- und je einem Fußstück (4, 5) eine einheitliche Schweißkonstruktion aus Blech bildet und die Fußstücke (4) aller Leitschaufeln (2, vgl. auch 3) im ortsfeste Aufnahmen des Turbinengehäuses einhängbar sind. This object is achieved in that each individual guide vane (2, cf. also 3) is hollow and, together with a head piece and a foot piece (4, 5), forms a uniform welded structure made of sheet metal and the foot pieces (4) of all Guide vanes (2, cf. also 3) can be hooked into the stationary receptacles of the turbine housing.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19715966 | 1997-04-17 | ||
DE19715966A DE19715966A1 (en) | 1997-04-17 | 1997-04-17 | Guide vane for steam turbines |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0872628A2 EP0872628A2 (en) | 1998-10-21 |
EP0872628A3 true EP0872628A3 (en) | 1999-12-08 |
Family
ID=7826729
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP98106798A Withdrawn EP0872628A3 (en) | 1997-04-17 | 1998-04-15 | Stator vane for steam turbine |
Country Status (3)
Country | Link |
---|---|
US (1) | US6135711A (en) |
EP (1) | EP0872628A3 (en) |
DE (1) | DE19715966A1 (en) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
ITCO20130051A1 (en) * | 2013-10-23 | 2015-04-24 | Nuovo Pignone Srl | METHOD FOR THE PRODUCTION OF A STAGE OF A STEAM TURBINE |
JP6284447B2 (en) * | 2014-06-27 | 2018-02-28 | 三菱日立パワーシステムズ株式会社 | Stator blade unit and steam turbine |
US11225875B1 (en) * | 2021-01-27 | 2022-01-18 | Raytheon Technologies Corporation | Rail support beams |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3056582A (en) * | 1960-08-26 | 1962-10-02 | Gen Electric | Turbine stator construction |
FR1340331A (en) * | 1962-09-07 | 1963-10-18 | Rateau Soc | Improvements to devices for connecting the ends of mobile turbine blades |
US3302924A (en) * | 1965-03-12 | 1967-02-07 | Gen Motors Corp | Dual airfoil bladed rotor |
DE1902031A1 (en) * | 1969-01-16 | 1970-09-10 | Siteg Siebtech Gmbh | Continuous vibrating disc mill |
US4195396A (en) * | 1977-12-15 | 1980-04-01 | Trw Inc. | Method of forming an airfoil with inner and outer shroud sections |
US4437810A (en) * | 1981-04-24 | 1984-03-20 | Rolls-Royce Limited | Cooled vane for a gas turbine engine |
US4639189A (en) * | 1984-02-27 | 1987-01-27 | Rockwell International Corporation | Hollow, thermally-conditioned, turbine stator nozzle |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US925218A (en) * | 1908-12-08 | 1909-06-15 | Schroeder Headlight Company | Elastic-fluid turbine. |
US2771622A (en) * | 1952-05-09 | 1956-11-27 | Westinghouse Electric Corp | Diaphragm apparatus |
US3365173A (en) * | 1966-02-28 | 1968-01-23 | Gen Electric | Stator structure |
DE2320064B2 (en) * | 1973-04-19 | 1975-05-28 | Jurij Fedorowitsch Kosjak | Diffuser of a steam turbine stage with axial flow |
US5022818A (en) * | 1989-02-21 | 1991-06-11 | Westinghouse Electric Corp. | Compressor diaphragm assembly |
JPH06248903A (en) * | 1993-02-24 | 1994-09-06 | Toshiba Corp | Waterdrop removing device for steam turbine |
-
1997
- 1997-04-17 DE DE19715966A patent/DE19715966A1/en not_active Withdrawn
-
1998
- 1998-04-14 US US09/060,006 patent/US6135711A/en not_active Expired - Lifetime
- 1998-04-15 EP EP98106798A patent/EP0872628A3/en not_active Withdrawn
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3056582A (en) * | 1960-08-26 | 1962-10-02 | Gen Electric | Turbine stator construction |
FR1340331A (en) * | 1962-09-07 | 1963-10-18 | Rateau Soc | Improvements to devices for connecting the ends of mobile turbine blades |
US3302924A (en) * | 1965-03-12 | 1967-02-07 | Gen Motors Corp | Dual airfoil bladed rotor |
DE1902031A1 (en) * | 1969-01-16 | 1970-09-10 | Siteg Siebtech Gmbh | Continuous vibrating disc mill |
US4195396A (en) * | 1977-12-15 | 1980-04-01 | Trw Inc. | Method of forming an airfoil with inner and outer shroud sections |
US4437810A (en) * | 1981-04-24 | 1984-03-20 | Rolls-Royce Limited | Cooled vane for a gas turbine engine |
US4639189A (en) * | 1984-02-27 | 1987-01-27 | Rockwell International Corporation | Hollow, thermally-conditioned, turbine stator nozzle |
Also Published As
Publication number | Publication date |
---|---|
EP0872628A2 (en) | 1998-10-21 |
US6135711A (en) | 2000-10-24 |
DE19715966A1 (en) | 1998-10-29 |
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