[go: up one dir, main page]

FR3139854B1 - Carter inter-turbines - Google Patents

Carter inter-turbines Download PDF

Info

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
Application number
FR2209448A
Other languages
English (en)
Other versions
FR3139854A1 (fr
Inventor
Emanuele Tavolo
Cyril Verbrugge
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safran Aircraft Engines SAS
Original Assignee
Safran Aircraft Engines SAS
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Safran Aircraft Engines SAS filed Critical Safran Aircraft Engines SAS
Priority to FR2209448A priority Critical patent/FR3139854B1/fr
Priority to PCT/FR2023/051402 priority patent/WO2024062179A1/fr
Publication of FR3139854A1 publication Critical patent/FR3139854A1/fr
Application granted granted Critical
Publication of FR3139854B1 publication Critical patent/FR3139854B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00Stators
    • F01D9/02Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/041Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/141Shape, i.e. outer, aerodynamic form
    • F01D5/146Shape, i.e. outer, aerodynamic form of blades with tandem configuration, split blades or slotted blades
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00Application
    • F05D2220/30Application in turbines
    • F05D2220/32Application in turbines in gas turbines
    • F05D2220/321Application in turbines in gas turbines for a special turbine stage
    • F05D2220/3213Application in turbines in gas turbines for a special turbine stage an intermediate stage of the turbine
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/96Preventing, counteracting or reducing vibration or noise
    • F05D2260/961Preventing, 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.
FR2209448A 2022-09-19 2022-09-19 Carter inter-turbines Active FR3139854B1 (fr)

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)

* Cited by examiner, † Cited by third party
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

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