FR2914944B1 - Calage variable d'aubes de compresseur dans une turbomachine - Google Patents
Calage variable d'aubes de compresseur dans une turbomachineInfo
- Publication number
- FR2914944B1 FR2914944B1 FR0702683A FR0702683A FR2914944B1 FR 2914944 B1 FR2914944 B1 FR 2914944B1 FR 0702683 A FR0702683 A FR 0702683A FR 0702683 A FR0702683 A FR 0702683A FR 2914944 B1 FR2914944 B1 FR 2914944B1
- Authority
- FR
- France
- Prior art keywords
- aubes
- turbomachine
- compressor
- variable setting
- variable
- 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.)
- Active
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/52—Casings; Connections of working fluid for axial pumps
- F04D29/54—Fluid-guiding means, e.g. diffusers
- F04D29/56—Fluid-guiding means, e.g. diffusers adjustable
- F04D29/563—Fluid-guiding means, e.g. diffusers adjustable specially adapted for elastic fluid pumps
-
- 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
- F05D2250/10—Two-dimensional
- F05D2250/18—Two-dimensional patterned
- F05D2250/181—Two-dimensional patterned ridged
-
- 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
- F05D2250/10—Two-dimensional
- F05D2250/18—Two-dimensional patterned
- F05D2250/182—Two-dimensional patterned crenellated, notched
-
- 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
- F05D2260/00—Function
- F05D2260/40—Transmission of power
- F05D2260/403—Transmission of power through the shape of the drive components
- F05D2260/4031—Transmission of power through the shape of the drive components as in toothed gearing
-
- 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
- F05D2260/00—Function
- F05D2260/50—Kinematic linkage, i.e. transmission of position
- F05D2260/53—Kinematic linkage, i.e. transmission of position using gears
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0702683A FR2914944B1 (fr) | 2007-04-13 | 2007-04-13 | Calage variable d'aubes de compresseur dans une turbomachine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0702683A FR2914944B1 (fr) | 2007-04-13 | 2007-04-13 | Calage variable d'aubes de compresseur dans une turbomachine |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2914944A1 FR2914944A1 (fr) | 2008-10-17 |
FR2914944B1 true FR2914944B1 (fr) | 2011-04-01 |
Family
ID=38669751
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0702683A Active FR2914944B1 (fr) | 2007-04-13 | 2007-04-13 | Calage variable d'aubes de compresseur dans une turbomachine |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2914944B1 (fr) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3108670A1 (fr) | 2020-03-31 | 2021-10-01 | Safran Aircraft Engines | Module de soufflante pour un banc d’essai de turbomachine d’aeronef |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2362071A1 (fr) * | 2010-02-19 | 2011-08-31 | Siemens Aktiengesellschaft | Dispositif d'entraînement pour le pivotement d'aubes réglables d'une turbomachine |
CN103291383B (zh) * | 2013-06-26 | 2015-02-25 | 上海交通大学 | 含有齿轮传动的压气机多级静叶调节机构 |
US10358934B2 (en) * | 2016-04-11 | 2019-07-23 | United Technologies Corporation | Method and apparatus for adjusting variable vanes |
BE1024982B1 (fr) | 2017-02-09 | 2018-09-10 | Safran Aero Boosters Sa | Compresseur de turbomachine avec aubes a calage variable |
FR3069013B1 (fr) * | 2017-07-17 | 2019-08-30 | Safran Aircraft Engines | Dispositif de calage reglable d'une aube pivotante pour un redresseur de flux |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CA930670A (en) * | 1969-10-23 | 1973-07-24 | Klompas Nicholas | Variable pitch fan with rolling contact |
US6450763B1 (en) * | 2000-11-17 | 2002-09-17 | General Electric Company | Replaceable variable stator vane for gas turbines |
GB2410530A (en) * | 2004-01-27 | 2005-08-03 | Rolls Royce Plc | Electrically actuated stator vane arrangement |
-
2007
- 2007-04-13 FR FR0702683A patent/FR2914944B1/fr active Active
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3108670A1 (fr) | 2020-03-31 | 2021-10-01 | Safran Aircraft Engines | Module de soufflante pour un banc d’essai de turbomachine d’aeronef |
Also Published As
Publication number | Publication date |
---|---|
FR2914944A1 (fr) | 2008-10-17 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PLFP | Fee payment |
Year of fee payment: 10 |
|
PLFP | Fee payment |
Year of fee payment: 11 |
|
CD | Change of name or company name |
Owner name: SAFRAN AIRCRAFT ENGINES, FR Effective date: 20170717 |
|
PLFP | Fee payment |
Year of fee payment: 12 |
|
PLFP | Fee payment |
Year of fee payment: 14 |
|
PLFP | Fee payment |
Year of fee payment: 15 |
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PLFP | Fee payment |
Year of fee payment: 16 |
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PLFP | Fee payment |
Year of fee payment: 17 |
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PLFP | Fee payment |
Year of fee payment: 18 |