CH482915A - Leitvorrichtung für Axialturbine - Google Patents
Leitvorrichtung für AxialturbineInfo
- Publication number
- CH482915A CH482915A CH1543767A CH1543767A CH482915A CH 482915 A CH482915 A CH 482915A CH 1543767 A CH1543767 A CH 1543767A CH 1543767 A CH1543767 A CH 1543767A CH 482915 A CH482915 A CH 482915A
- Authority
- CH
- Switzerland
- Prior art keywords
- guide device
- axial turbine
- turbine
- axial
- guide
- 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
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
- F01D25/246—Fastening of diaphragms or stator-rings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2230/00—Manufacture
- F05B2230/60—Assembly methods
- F05B2230/604—Assembly methods using positioning or alignment devices for aligning or centering, e.g. pins
- F05B2230/606—Assembly methods using positioning or alignment devices for aligning or centering, e.g. pins using maintaining alignment while permitting differential dilatation
-
- 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
- F05D2230/64—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins
- F05D2230/642—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins using maintaining alignment while permitting differential dilatation
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH1543767A CH482915A (de) | 1967-11-03 | 1967-11-03 | Leitvorrichtung für Axialturbine |
DE19666601211U DE6601211U (de) | 1967-11-03 | 1967-11-15 | Leitvorrichtung fuer axialturbinen |
US740600A US3532437A (en) | 1967-11-03 | 1968-06-27 | Stator blade assembly for axial-flow turbines |
FR1589865D FR1589865A (de) | 1967-11-03 | 1968-10-23 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH1543767A CH482915A (de) | 1967-11-03 | 1967-11-03 | Leitvorrichtung für Axialturbine |
Publications (1)
Publication Number | Publication Date |
---|---|
CH482915A true CH482915A (de) | 1969-12-15 |
Family
ID=4409093
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CH1543767A CH482915A (de) | 1967-11-03 | 1967-11-03 | Leitvorrichtung für Axialturbine |
Country Status (4)
Country | Link |
---|---|
US (1) | US3532437A (de) |
CH (1) | CH482915A (de) |
DE (1) | DE6601211U (de) |
FR (1) | FR1589865A (de) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3038603A1 (de) * | 1979-10-24 | 1982-03-04 | Rolls-Royce Ltd., London | Gasturbine mit einer einrichtung zur konstanthaltung des schaufelspitzenspielraumes zwischen einem laufrad und einem dieses umgebenden stroemungskanalwandabschnitt |
EP0716219A1 (de) * | 1994-12-07 | 1996-06-12 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" | Aus Segmenten aufgebauter Leitkranz für eine Turbomaschine |
FR2761119A1 (fr) * | 1997-03-20 | 1998-09-25 | Snecma | Stator de compresseur de turbomachine |
Families Citing this family (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3904324A (en) * | 1972-11-06 | 1975-09-09 | Tech Dev Inc | Tip turbine inflating device |
US4248569A (en) * | 1978-11-13 | 1981-02-03 | General Motors Corporation | Stator mounting |
EP0103260A3 (de) * | 1982-09-06 | 1984-09-26 | Hitachi, Ltd. | Einstellung des Spiels zwischen Turbinenschaufelspitzen und Gehäuse |
US4509238A (en) * | 1983-03-21 | 1985-04-09 | General Electric Company | Method for fabricating a steam turbine diaphragm |
FR2552159B1 (fr) * | 1983-09-21 | 1987-07-10 | Snecma | Dispositif de liaison et d'etancheite de secteurs d'aubes de stator de turbine |
FR2577281B1 (fr) * | 1985-02-13 | 1987-03-20 | Snecma | Carter de turbomachine associe a un dispositif pour ajuster le jeu entre aubes mobiles et carter |
DE19850732A1 (de) * | 1998-11-04 | 2000-05-11 | Asea Brown Boveri | Axialturbine |
FR2817285B1 (fr) * | 2000-11-30 | 2003-06-13 | Snecma Moteurs | Virole interne de stator |
GB0218060D0 (en) * | 2002-08-03 | 2002-09-11 | Alstom Switzerland Ltd | Sealing arrangements |
EP1548232A1 (de) * | 2003-12-23 | 2005-06-29 | Siemens Aktiengesellschaft | Strömungsmaschine mit einem Leitschaufelträger und Verfahren zum Montieren von Leitschaufeln an einen Leitschaufelträger |
US8511983B2 (en) * | 2008-02-19 | 2013-08-20 | United Technologies Corporation | LPC exit guide vane and assembly |
US8133019B2 (en) * | 2009-01-21 | 2012-03-13 | General Electric Company | Discrete load fins for individual stator vanes |
US20140037438A1 (en) * | 2012-07-31 | 2014-02-06 | General Electric Company | Turbine shroud for a turbomachine |
DE102015201782A1 (de) | 2015-02-02 | 2016-08-18 | MTU Aero Engines AG | Leitschaufelring für eine Strömungsmaschine |
GB2551164B (en) * | 2016-06-08 | 2019-12-25 | Rolls Royce Plc | Metallic stator vane |
US20200072070A1 (en) * | 2018-09-05 | 2020-03-05 | United Technologies Corporation | Unified boas support and vane platform |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US998820A (en) * | 1908-05-13 | 1911-07-25 | George Westinghouse | Turbine-blading. |
US2282894A (en) * | 1940-04-02 | 1942-05-12 | Gen Electric | Elastic fluid turbine |
FR965713A (de) * | 1947-05-07 | 1950-09-20 | ||
DE852789C (de) * | 1951-02-08 | 1952-10-20 | Maschf Augsburg Nuernberg Ag | Leitschaufeltraeger fuer Axialturbinen |
DE928746C (de) * | 1952-12-04 | 1955-06-10 | Maschf Augsburg Nuernberg Ag | Leitapparat fuer Abgasturbogeblaese |
GB881880A (en) * | 1959-05-22 | 1961-11-08 | Power Jets Res & Dev Ltd | Turbo-machine stator construction |
NL282822A (de) * | 1961-09-04 | |||
US3427000A (en) * | 1966-11-14 | 1969-02-11 | Westinghouse Electric Corp | Axial flow turbine structure |
-
1967
- 1967-11-03 CH CH1543767A patent/CH482915A/de not_active IP Right Cessation
- 1967-11-15 DE DE19666601211U patent/DE6601211U/de not_active Expired
-
1968
- 1968-06-27 US US740600A patent/US3532437A/en not_active Expired - Lifetime
- 1968-10-23 FR FR1589865D patent/FR1589865A/fr not_active Expired
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3038603A1 (de) * | 1979-10-24 | 1982-03-04 | Rolls-Royce Ltd., London | Gasturbine mit einer einrichtung zur konstanthaltung des schaufelspitzenspielraumes zwischen einem laufrad und einem dieses umgebenden stroemungskanalwandabschnitt |
EP0716219A1 (de) * | 1994-12-07 | 1996-06-12 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" | Aus Segmenten aufgebauter Leitkranz für eine Turbomaschine |
FR2728015A1 (fr) * | 1994-12-07 | 1996-06-14 | Snecma | Distributeur monobloc sectorise d'un stator de turbine de turbomachine |
US5752804A (en) * | 1994-12-07 | 1998-05-19 | Societe Nationale D'etude Et De Construction De Monteurs D'aviation "Snecma" | Sectored, one-piece nozzle of a turbine engine turbine stator |
FR2761119A1 (fr) * | 1997-03-20 | 1998-09-25 | Snecma | Stator de compresseur de turbomachine |
Also Published As
Publication number | Publication date |
---|---|
US3532437A (en) | 1970-10-06 |
DE6601211U (de) | 1969-02-27 |
FR1589865A (de) | 1970-04-06 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PL | Patent ceased |