FR3132323B1 - Ensemble d’aubages statiques à calage variable - Google Patents
Ensemble d’aubages statiques à calage variable Download PDFInfo
- Publication number
- FR3132323B1 FR3132323B1 FR2200973A FR2200973A FR3132323B1 FR 3132323 B1 FR3132323 B1 FR 3132323B1 FR 2200973 A FR2200973 A FR 2200973A FR 2200973 A FR2200973 A FR 2200973A FR 3132323 B1 FR3132323 B1 FR 3132323B1
- Authority
- FR
- France
- Prior art keywords
- variable pitch
- static vanes
- blade
- fixed structure
- defining
- 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
- 230000003068 static effect Effects 0.000 title abstract 3
- 238000011144 upstream manufacturing Methods 0.000 abstract 3
Classifications
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- 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
- 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
- F01D5/148—Blades with variable camber, e.g. by ejection of fluid
-
- 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
- F05D2300/00—Materials; Properties thereof
- F05D2300/40—Organic materials
- F05D2300/43—Synthetic polymers, e.g. plastics; Rubber
-
- 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
- F05D2300/00—Materials; Properties thereof
- F05D2300/40—Organic materials
- F05D2300/43—Synthetic polymers, e.g. plastics; Rubber
- F05D2300/436—Polyetherketones, e.g. PEEK
-
- 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
- F05D2300/00—Materials; Properties thereof
- F05D2300/50—Intrinsic material properties or characteristics
- F05D2300/501—Elasticity
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
Ensemble d’aubages statiques à calage variable Ensemble d’aubages statiques pour turbomachine, l’ensemble comprenant au moins une structure fixe et une pluralité de pales (11) à calage variable, caractérisé en ce que chaque pale (11) comprend : - une partie aval (21) rigide, définissant un bord de fuite (15) de la pale (11), la partie aval (21) étant montée fixe par rapport à chaque structure fixe, - une partie amont (23) rigide, définissant un bord d’attaque (13) de la pale (11), la partie amont (23) étant montée mobile en translation circonférentielle par rapport à chaque structure fixe, et - une partie médiane (25) souple reliant mécaniquement la partie amont (23) et la partie aval (21). Figure à publier avec l’abrégé : figure 3
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR2200973A FR3132323B1 (fr) | 2022-02-03 | 2022-02-03 | Ensemble d’aubages statiques à calage variable |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR2200973 | 2022-02-03 | ||
FR2200973A FR3132323B1 (fr) | 2022-02-03 | 2022-02-03 | Ensemble d’aubages statiques à calage variable |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3132323A1 FR3132323A1 (fr) | 2023-08-04 |
FR3132323B1 true FR3132323B1 (fr) | 2024-01-19 |
Family
ID=81850910
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR2200973A Active FR3132323B1 (fr) | 2022-02-03 | 2022-02-03 | Ensemble d’aubages statiques à calage variable |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR3132323B1 (fr) |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1544288A (en) * | 1923-08-13 | 1925-06-30 | Westinghouse Electric & Mfg Co | Turbine blading |
US4235397A (en) * | 1978-04-29 | 1980-11-25 | British Aerospace | Flow deflector blades |
FR2707338B1 (fr) * | 1993-07-07 | 1995-08-11 | Snecma | Aube de turbomachine à cambrure variable. |
DE10257044B4 (de) * | 2002-12-06 | 2005-01-27 | Mtu Aero Engines Gmbh | Gasturbine |
FR2857404B1 (fr) | 2003-07-10 | 2007-03-09 | Snecma Moteurs | Dispositif de guidage en rotation d'aubes a calage variable dans une turbomachine |
DE102010011708B4 (de) * | 2010-03-15 | 2012-03-01 | Rudolf Huttary | Strömungsmaschine mit passiver Laufschaufelverstellung |
US20160333729A1 (en) * | 2015-05-11 | 2016-11-17 | General Electric Company | Turbine engine having variable pitch outlet guide vanes |
-
2022
- 2022-02-03 FR FR2200973A patent/FR3132323B1/fr active Active
Also Published As
Publication number | Publication date |
---|---|
FR3132323A1 (fr) | 2023-08-04 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PLFP | Fee payment |
Year of fee payment: 2 |
|
PLSC | Publication of the preliminary search report |
Effective date: 20230804 |
|
PLFP | Fee payment |
Year of fee payment: 3 |