FR3139854B1 - Carter inter-turbines - Google Patents
Carter inter-turbines Download PDFInfo
- Publication number
- FR3139854B1 FR3139854B1 FR2209448A FR2209448A FR3139854B1 FR 3139854 B1 FR3139854 B1 FR 3139854B1 FR 2209448 A FR2209448 A FR 2209448A FR 2209448 A FR2209448 A FR 2209448A FR 3139854 B1 FR3139854 B1 FR 3139854B1
- Authority
- FR
- France
- Prior art keywords
- arms
- separating
- inter
- vane
- turbine
- 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
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
- F01D9/041—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades
-
- 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
- F01D5/141—Shape, i.e. outer, aerodynamic form
- F01D5/146—Shape, i.e. outer, aerodynamic form of blades with tandem configuration, split blades or slotted blades
-
- 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
- F05D2220/00—Application
- F05D2220/30—Application in turbines
- F05D2220/32—Application in turbines in gas turbines
- F05D2220/321—Application in turbines in gas turbines for a special turbine stage
- F05D2220/3213—Application in turbines in gas turbines for a special turbine stage an intermediate stage of the turbine
-
- 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
- F05D2260/96—Preventing, counteracting or reducing vibration or noise
- F05D2260/961—Preventing, counteracting or reducing vibration or noise by mistuning rotor blades or stator vanes with irregular interblade spacing, airfoil shape
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
Carter inter-turbines pour turbomachine du type turbine vane frame remplissant la fonction de distributeur de turbine dans une telle turbomachine, comprenant une virole interne (9), une virole externe, une pluralité de bras (11) s’étendant entre la virole interne (9) et la virole externe, et au moins un jeu de N aubes séparatrices (12) positionnées circonférentiellement entre deux bras successifs (11), chaque aube séparatrice (12) présentant une corde axiale à mi-hauteur plus courte que la corde axiale à mi-hauteur des bras (11), dans lequel lesdits deux bras successifs (11) définissent une position de référence pour chacune desdites N aubes séparatrices (12), ces positions de référence étant régulièrement espacées circonférentiellement entre les deux bras successifs (11), et dans lequel au moins une aube séparatrice (12-1) dudit jeu de N aubes séparatrices (12) est décalée circonférentiellement par rapport à sa position de référence. Fig. 3.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR2209448A FR3139854B1 (fr) | 2022-09-19 | 2022-09-19 | Carter inter-turbines |
PCT/FR2023/051402 WO2024062179A1 (fr) | 2022-09-19 | 2023-09-15 | Carter inter-turbines pour turbomachine, ensemble de turbomachine, turbomachine et méthode de positionnement d'une aube séparatrice au sein d'un carter inter-turbines |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR2209448 | 2022-09-19 | ||
FR2209448A FR3139854B1 (fr) | 2022-09-19 | 2022-09-19 | Carter inter-turbines |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3139854A1 FR3139854A1 (fr) | 2024-03-22 |
FR3139854B1 true FR3139854B1 (fr) | 2024-09-13 |
Family
ID=84362488
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR2209448A Active FR3139854B1 (fr) | 2022-09-19 | 2022-09-19 | Carter inter-turbines |
Country Status (2)
Country | Link |
---|---|
FR (1) | FR3139854B1 (fr) |
WO (1) | WO2024062179A1 (fr) |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
ITTO20120517A1 (it) * | 2012-06-14 | 2013-12-15 | Avio Spa | Schiera di profili aerodinamici per un impianto di turbina a gas |
EP2799721B8 (fr) * | 2013-05-03 | 2016-12-07 | Safran Aero Booster S.A. | Redresseur de turbomachine axiale avec aubes auxiliaires en pieds d'aubes |
-
2022
- 2022-09-19 FR FR2209448A patent/FR3139854B1/fr active Active
-
2023
- 2023-09-15 WO PCT/FR2023/051402 patent/WO2024062179A1/fr unknown
Also Published As
Publication number | Publication date |
---|---|
FR3139854A1 (fr) | 2024-03-22 |
WO2024062179A1 (fr) | 2024-03-28 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US3295825A (en) | Multi-stage turbine rotor | |
FR2490722A1 (fr) | Joints d'etancheite a l'air pour turbomachines | |
NO130025B (fr) | ||
US4863343A (en) | Turbine vane shroud sealing system | |
GB785466A (en) | Shroud ring construction for turbines and compressors | |
EP1965034B1 (fr) | Etage de turbine dans une turbomachine | |
JPH0270905A (ja) | 輻流‐軸流式第1段を備えた軸流タービン | |
JP2003269111A (ja) | 円弧のまわりに羽根を支持するディストリビュータセクタを取付ける装置 | |
EP0710766B1 (fr) | Disque de rotor avec garniture d'étanchéité intégrée | |
JP2016125481A (ja) | 非軸対称ハブ流路及びスプリッタブレードを組み込んだ軸流圧縮機ロータ | |
FR3062876B1 (fr) | Compresseur haute pression pour turbomachine | |
FR3102795B1 (fr) | Turbine de turbomachine à distributeur en CMC avec reprise d’effort | |
EP1793092A1 (fr) | Dispositif porte-injecteur sur turbine et turbine à vapeur | |
FR3139854B1 (fr) | Carter inter-turbines | |
US10094390B2 (en) | Rotary assembly for an aviation turbine engine, the assembly comprising a separate fan blade platform mounted on a fan disk | |
JP6877867B2 (ja) | タービンアッセンブリ | |
US10072508B2 (en) | Turbomachine rotor with optimised bearing surfaces | |
US20190120056A1 (en) | Radial turbomachine with axial thrust compensation | |
US10683769B2 (en) | Centrifugally activatable seal for a rotary machine and method of assembling same | |
GB737473A (en) | Turbines and like machines having adjustable guide blades | |
US2838274A (en) | Bladed stator structures for axialflow fluid machines | |
ES2962229T3 (es) | Canal de flujo para turbomaquinaria | |
GB789733A (en) | Improvements in or relating to structural elements for axial-flow compressors or turbines or the like machines | |
FR3109959B1 (fr) | Compresseur de turbomachine comportant une paroi fixe pourvue d’un traitement de forme | |
US20050039333A1 (en) | Method for manufacturing steam turbines |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PLFP | Fee payment |
Year of fee payment: 2 |
|
PLFP | Fee payment |
Year of fee payment: 3 |