CH342040A - Stator de turbo-machine - Google Patents
Stator de turbo-machineInfo
- Publication number
- CH342040A CH342040A CH342040DA CH342040A CH 342040 A CH342040 A CH 342040A CH 342040D A CH342040D A CH 342040DA CH 342040 A CH342040 A CH 342040A
- Authority
- CH
- Switzerland
- Prior art keywords
- turbo machine
- machine stator
- stator
- turbo
- machine
- 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
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
- F01D11/14—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing
- F01D11/20—Actively adjusting tip-clearance
- F01D11/22—Actively adjusting tip-clearance by mechanically actuating the stator or rotor components, e.g. moving shroud sections relative to the rotor
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
- F02C3/06—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US408136A US2858104A (en) | 1954-02-04 | 1954-02-04 | Adjustable gas turbine shroud ring segments |
Publications (1)
Publication Number | Publication Date |
---|---|
CH342040A true CH342040A (fr) | 1959-10-31 |
Family
ID=23614997
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CH342040D CH342040A (fr) | 1954-02-04 | 1954-11-02 | Stator de turbo-machine |
Country Status (3)
Country | Link |
---|---|
US (1) | US2858104A (fr) |
CH (1) | CH342040A (fr) |
DE (1) | DE954835C (fr) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4163366A (en) * | 1977-05-23 | 1979-08-07 | Avco Corporation | Apparatus for disposal of leaking fluids in a turbofan engine |
FR2522067A1 (fr) * | 1982-02-19 | 1983-08-26 | Gen Electric | Carter de compresseur |
FR2651831A1 (fr) * | 1989-09-08 | 1991-03-15 | Gen Electric | Dispositif de controle du jeu des extremites des aubes pour moteur a turbine a gaz. |
FR2658242A1 (fr) * | 1990-02-12 | 1991-08-16 | Gen Electric | Dispositif de commande du jeu de l'extremite d'une aube utilisant une modulation de la position d'un segment d'enveloppe. |
FR2683851A1 (fr) * | 1991-11-20 | 1993-05-21 | Snecma | Turbomachine equipee de moyens facilitant le reglage des jeux du stator entree stator et rotor. |
US5238365A (en) * | 1991-07-09 | 1993-08-24 | General Electric Company | Assembly for thermal shielding of low pressure turbine |
Families Citing this family (24)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
BE556215A (fr) * | 1956-03-28 | 1957-04-15 | ||
GB907562A (en) * | 1958-07-07 | 1962-10-10 | Bristol Siddeley Engines Ltd | Improvements in or relating to engines |
US3042367A (en) * | 1958-07-17 | 1962-07-03 | Gen Motors Corp | Fluid seal |
US3062497A (en) * | 1958-11-24 | 1962-11-06 | Ford Motor Co | Gas turbine engine |
US3209537A (en) * | 1960-05-02 | 1965-10-05 | Bendix Corp | Motive fluid control for a re-expansion gas turbine engine |
GB1051244A (fr) * | 1962-10-09 | |||
US3425665A (en) * | 1966-02-24 | 1969-02-04 | Curtiss Wright Corp | Gas turbine rotor blade shroud |
US3391904A (en) * | 1966-11-02 | 1968-07-09 | United Aircraft Corp | Optimum response tip seal |
US4131388A (en) * | 1977-05-26 | 1978-12-26 | United Technologies Corporation | Outer air seal |
FR2521217A1 (fr) * | 1982-02-08 | 1983-08-12 | Jehier Sa | Perfectionnements aux anneaux isolants pour carters de turbines |
US4925364A (en) * | 1988-12-21 | 1990-05-15 | United Technologies Corporation | Adjustable spacer |
US5022816A (en) * | 1989-10-24 | 1991-06-11 | United Technologies Corporation | Gas turbine blade shroud support |
GB2239678B (en) * | 1989-12-08 | 1993-03-03 | Rolls Royce Plc | Gas turbine engine blade shroud assembly |
US5176496A (en) * | 1991-09-27 | 1993-01-05 | General Electric Company | Mounting arrangements for turbine nozzles |
US5271713A (en) * | 1992-10-05 | 1993-12-21 | Deere & Company | Adjustable inlet for a harvester fan |
FR2817285B1 (fr) | 2000-11-30 | 2003-06-13 | Snecma Moteurs | Virole interne de stator |
FR2835563B1 (fr) * | 2002-02-07 | 2004-04-02 | Snecma Moteurs | Agencement d'accrochage de secteurs en arc de cercle de distributeur porteur d'aubes |
US6884025B2 (en) * | 2002-09-30 | 2005-04-26 | United Technologies Corporation | Shim lock/pin anti-rotation bumper design |
GB0318609D0 (en) * | 2003-08-08 | 2003-09-10 | Rolls Royce Plc | An arrangement for mounting a non-rotating component |
DE102007042766A1 (de) * | 2007-09-07 | 2009-03-12 | Mtu Aero Engines Gmbh | Nachstellbares Dichtsegment |
US9416671B2 (en) | 2012-10-04 | 2016-08-16 | General Electric Company | Bimetallic turbine shroud and method of fabricating |
US9322334B2 (en) * | 2012-10-23 | 2016-04-26 | General Electric Company | Deformable mounting assembly |
FR3029562B1 (fr) * | 2014-12-09 | 2016-12-09 | Snecma | Anneau de commande d’un etage d’aubes a calage variable pour une turbomachine |
US11486271B1 (en) * | 2021-10-15 | 2022-11-01 | Pratt & Whitney Canada Corp. | Adjustable mount for engine accessory |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1304412A (en) * | 1919-05-20 | Junta toyoeawa | ||
US890635A (en) * | 1906-02-14 | 1908-06-16 | Gen Electric | Elastic-fluid turbine. |
GB190926383A (en) * | 1909-07-20 | 1910-05-05 | Chantiers De Bretagne Anciens | Improvements in or relating to Turbines. |
US1352276A (en) * | 1918-12-06 | 1920-09-07 | Gen Electric | Elastic-fluid turbine |
DE436567C (de) * | 1924-01-19 | 1926-11-04 | Waggon Und Maschb Akt Ges | Leitschaufelkranz fuer Dampf- und Gasturbinen |
FR981975A (fr) * | 1943-05-21 | 1951-06-01 | Rateau Soc | Perfectionnement aux turbines à gaz |
FR994013A (fr) * | 1944-12-05 | 1951-11-09 | Rateau Soc | Perfectionnement à l'exécution des distributeurs et tuyères de turbines |
GB600057A (en) * | 1945-12-21 | 1948-03-30 | Power Jets Res & Dev Ltd | Improvements in or relating to the mounting of blades in axial flow compressors, turbines, or the like |
NL74168C (fr) * | 1946-02-25 | |||
US2544538A (en) * | 1948-12-01 | 1951-03-06 | Wright Aeronautical Corp | Liner for hot gas chambers |
GB679916A (en) * | 1949-04-29 | 1952-09-24 | Geoffrey Bertram Robert Feilde | Improvements in gas turbines |
FR1003299A (fr) * | 1949-12-13 | 1952-03-17 | Rateau Soc | Perfectionnement aux turbines à gaz et autres turbo-machines axiales |
DE852789C (de) * | 1951-02-08 | 1952-10-20 | Maschf Augsburg Nuernberg Ag | Leitschaufeltraeger fuer Axialturbinen |
-
1954
- 1954-02-04 US US408136A patent/US2858104A/en not_active Expired - Lifetime
- 1954-11-02 CH CH342040D patent/CH342040A/fr unknown
- 1954-11-05 DE DEC10215A patent/DE954835C/de not_active Expired
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4163366A (en) * | 1977-05-23 | 1979-08-07 | Avco Corporation | Apparatus for disposal of leaking fluids in a turbofan engine |
FR2522067A1 (fr) * | 1982-02-19 | 1983-08-26 | Gen Electric | Carter de compresseur |
FR2651831A1 (fr) * | 1989-09-08 | 1991-03-15 | Gen Electric | Dispositif de controle du jeu des extremites des aubes pour moteur a turbine a gaz. |
FR2658242A1 (fr) * | 1990-02-12 | 1991-08-16 | Gen Electric | Dispositif de commande du jeu de l'extremite d'une aube utilisant une modulation de la position d'un segment d'enveloppe. |
US5238365A (en) * | 1991-07-09 | 1993-08-24 | General Electric Company | Assembly for thermal shielding of low pressure turbine |
FR2683851A1 (fr) * | 1991-11-20 | 1993-05-21 | Snecma | Turbomachine equipee de moyens facilitant le reglage des jeux du stator entree stator et rotor. |
US5288206A (en) * | 1991-11-20 | 1994-02-22 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation S.N.E.C.M.A. | Turbo aero engine equipped with means facilitating adjustment of plays of the stator and between the stator and rotor |
Also Published As
Publication number | Publication date |
---|---|
DE954835C (de) | 1956-12-20 |
US2858104A (en) | 1958-10-28 |
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