FR2698405B1 - Turbomachine à plusieurs étages d'aubes de stator à orientation variable. - Google Patents
Turbomachine à plusieurs étages d'aubes de stator à orientation variable.Info
- Publication number
- FR2698405B1 FR2698405B1 FR9214163A FR9214163A FR2698405B1 FR 2698405 B1 FR2698405 B1 FR 2698405B1 FR 9214163 A FR9214163 A FR 9214163A FR 9214163 A FR9214163 A FR 9214163A FR 2698405 B1 FR2698405 B1 FR 2698405B1
- Authority
- FR
- France
- Prior art keywords
- stator blades
- variable orientation
- stage turbomachine
- turbomachine
- stage
- 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.)
- Expired - Lifetime
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
- F01D17/00—Regulating or controlling by varying flow
- F01D17/10—Final actuators
- F01D17/12—Final actuators arranged in stator parts
- F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
- F01D17/16—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
- F01D17/162—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes for axial flow, i.e. the vanes turning around axes which are essentially perpendicular to the rotor centre line
-
- 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
- F05D2250/00—Geometry
- F05D2250/20—Three-dimensional
- F05D2250/25—Three-dimensional helical
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Control Of Turbines (AREA)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR9214163A FR2698405B1 (fr) | 1992-11-25 | 1992-11-25 | Turbomachine à plusieurs étages d'aubes de stator à orientation variable. |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR9214163A FR2698405B1 (fr) | 1992-11-25 | 1992-11-25 | Turbomachine à plusieurs étages d'aubes de stator à orientation variable. |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| FR2698405A1 FR2698405A1 (fr) | 1994-05-27 |
| FR2698405B1 true FR2698405B1 (fr) | 1994-12-23 |
Family
ID=9435888
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR9214163A Expired - Lifetime FR2698405B1 (fr) | 1992-11-25 | 1992-11-25 | Turbomachine à plusieurs étages d'aubes de stator à orientation variable. |
Country Status (1)
| Country | Link |
|---|---|
| FR (1) | FR2698405B1 (fr) |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2879684B1 (fr) * | 2004-12-16 | 2007-04-06 | Snecma Moteurs Sa | Turbomachine comprenant un stator equipe d'aubes de redresseur a calage variable commandees par des biellettes a emmanchement conique |
| FR2879685A1 (fr) * | 2004-12-16 | 2006-06-23 | Snecma Moteurs Sa | Turbomachine a stator comprenant un etage d'aubes de redresseur a calage variable avec reglage de jeu au niveau du pivot d'aube |
| FR2889242B1 (fr) | 2005-07-27 | 2007-11-02 | Snecma | Douille pour pivot d'aube a angle de calage variable pour turbomachine |
| FR2904668B1 (fr) | 2006-08-02 | 2008-10-31 | Snecma Sa | Dispositif de commande d'aube a angle de calage variable de turbomachine a biellette cylindrique |
| FR3100272B1 (fr) * | 2019-08-27 | 2025-04-25 | Safran Aircraft Engines | Guignol pour un dispositif de calage variable d’une turbomachine |
Family Cites Families (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CH247831A (de) * | 1942-11-26 | 1947-03-31 | Jendrassik Georg | Turbine für heisses Arbeitsmittel. |
| US2778564A (en) * | 1953-12-01 | 1957-01-22 | Havilland Engine Co Ltd | Stator blade ring assemblies for axial flow compressors and the like |
| FR1096708A (fr) * | 1953-12-30 | 1955-06-23 | Hispano Suiza Sa | Perfectionnements apportés aux appareils à aubage supersonique, notamment aux compresseurs supersoniques |
| US3356288A (en) * | 1965-04-07 | 1967-12-05 | Gen Electric | Stator adjusting means for axial flow compressors or the like |
| DE2005536B2 (de) * | 1969-02-20 | 1972-05-04 | Czkd Praha, Oborovy Podnik, Prag | Stellvorrichtung fuer die leitschaufeln eines mehrstufigen axialverdichters |
| US3887297A (en) * | 1974-06-25 | 1975-06-03 | United Aircraft Corp | Variable leading edge stator vane assembly |
| US3954349A (en) * | 1975-06-02 | 1976-05-04 | United Technologies Corporation | Lever connection to syncring |
| US4767264A (en) * | 1986-10-31 | 1988-08-30 | United Technologies Corporation | Vane lever arm construction |
-
1992
- 1992-11-25 FR FR9214163A patent/FR2698405B1/fr not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| FR2698405A1 (fr) | 1994-05-27 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| CD | Change of name or company name | ||
| TP | Transmission of property | ||
| CD | Change of name or company name |