FR3108362B1 - Etage d’aubes à orientation variable pour une turbomachine axiale comprenant un organe de régulation du débit d’air dépendant de l’orientation des aubes - Google Patents

Etage d’aubes à orientation variable pour une turbomachine axiale comprenant un organe de régulation du débit d’air dépendant de l’orientation des aubes Download PDF

Info

Publication number
FR3108362B1
FR3108362B1 FR2002713A FR2002713A FR3108362B1 FR 3108362 B1 FR3108362 B1 FR 3108362B1 FR 2002713 A FR2002713 A FR 2002713A FR 2002713 A FR2002713 A FR 2002713A FR 3108362 B1 FR3108362 B1 FR 3108362B1
Authority
FR
France
Prior art keywords
blades
orientation
air flow
stage
regulating
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
FR2002713A
Other languages
English (en)
Other versions
FR3108362A1 (fr
Inventor
Lilian Yann Dumas
Baptiste René Roger Batonnet
Romain Nicolas Lagarde
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 FR2002713A priority Critical patent/FR3108362B1/fr
Publication of FR3108362A1 publication Critical patent/FR3108362A1/fr
Application granted granted Critical
Publication of FR3108362B1 publication Critical patent/FR3108362B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • F01D17/105—Final actuators by passing part of the fluid
    • 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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/08—Cooling; Heating; Heat-insulation
    • F01D25/12—Cooling
    • 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
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/08—Heating, heat-insulating or cooling means
    • F01D5/081—Cooling fluid being directed on the side of the rotor disc or at the roots of the blades
    • F01D5/082—Cooling fluid being directed on the side of the rotor disc or at the roots of the blades on the side of the rotor disc
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/04—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
    • F02C6/06—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas
    • F02C6/08—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas the gas being bled from the gas-turbine compressor
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/12—Cooling of plants
    • F02C7/16—Cooling of plants characterised by cooling medium
    • F02C7/18—Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/16—Control of working fluid flow
    • F02C9/18—Control of working fluid flow by bleeding, bypassing or acting on variable working fluid interconnections between turbines or compressors or their stages
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D27/00—Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
    • F04D27/02—Surge control
    • F04D27/0207—Surge control by bleeding, bypassing or recycling fluids
    • F04D27/023—Details or means for fluid extraction
    • 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
    • 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
    • F05D2220/3216—Application in turbines in gas turbines for a special turbine stage for a special compressor stage
    • 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
    • F05D2250/90—Variable geometry
    • 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
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

Etage (30a) d’aubes (32) à orientation variable pour une turbomachine (10) comprenant :- un anneau intérieur (34) ; - un espace (E) axial en amont dudit anneau (34) débouchant dans un circuit de refroidissement (26) ; et- une rangée d’aubes (32) comprenant chacune une pale (32a) s’étendant radialement vers l’extérieur et montée à rotation dans l’anneau intérieur (34) autour de leur axe entre une position ouverte et une position au moins partiellement fermée, chaque aube (32) comprenant un pied (32b) situé à une extrémité intérieure de ladite pale (32a), ledit pied (32b) étant logé dans l’anneau intérieur (34). Ledit étage comprend un organe (40) de régulation du débit d’air configuré pour forcer le passage du flux d’air dans l’espace (E) lorsque les aubes (32) sont en position au moins partiellement fermée. Figure pour l’abrégé : Fig 2
FR2002713A 2020-03-19 2020-03-19 Etage d’aubes à orientation variable pour une turbomachine axiale comprenant un organe de régulation du débit d’air dépendant de l’orientation des aubes Active FR3108362B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR2002713A FR3108362B1 (fr) 2020-03-19 2020-03-19 Etage d’aubes à orientation variable pour une turbomachine axiale comprenant un organe de régulation du débit d’air dépendant de l’orientation des aubes

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR2002713A FR3108362B1 (fr) 2020-03-19 2020-03-19 Etage d’aubes à orientation variable pour une turbomachine axiale comprenant un organe de régulation du débit d’air dépendant de l’orientation des aubes
FR2002713 2020-03-19

Publications (2)

Publication Number Publication Date
FR3108362A1 FR3108362A1 (fr) 2021-09-24
FR3108362B1 true FR3108362B1 (fr) 2022-07-29

Family

ID=71662000

Family Applications (1)

Application Number Title Priority Date Filing Date
FR2002713A Active FR3108362B1 (fr) 2020-03-19 2020-03-19 Etage d’aubes à orientation variable pour une turbomachine axiale comprenant un organe de régulation du débit d’air dépendant de l’orientation des aubes

Country Status (1)

Country Link
FR (1) FR3108362B1 (fr)

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1356827A (fr) * 1963-05-20 1964-03-27 Rolls Royce Compresseurs pour turbo-moteurs à gaz
US3663118A (en) * 1970-06-01 1972-05-16 Gen Motors Corp Turbine cooling control
FR2601074B1 (fr) * 1986-07-03 1990-05-25 Snecma Turbomachine munie d'un dispositif de commande du debit d'air de ventilation preleve en vue du controle des jeux entre rotor et stator.
FR2611230B1 (fr) * 1987-02-25 1991-02-08 Snecma Turbomachine comportant un dispositif de commande du debit d'air de refroidissement de la turbine
FR2874977A1 (fr) 2004-09-07 2006-03-10 Snecma Moteurs Sa Douille de support pivotant pour pivot d'aube a calage variable de turbomachine
FR2920492B1 (fr) 2007-08-30 2009-10-30 Snecma Sa Etage d'aubes a calage variable pour une turbomachine
FR2931873B1 (fr) 2008-05-29 2010-08-20 Snecma Ensemble d'un disque de turbine d'un moteur a turbine a gaz et d'un tourillon support de palier,circuit de refroidissement d'un disque de turbine d'un tel ensemble.
FR2936559B1 (fr) * 2008-09-30 2013-11-22 Snecma Systeme de commande d'equipements a geometrie variable d'une turbomachine faisant partie de corps differents.
WO2015026597A1 (fr) * 2013-08-21 2015-02-26 United Technologies Corporation Agencement de turbine à section variable à modulation de flux secondaire

Also Published As

Publication number Publication date
FR3108362A1 (fr) 2021-09-24

Similar Documents

Publication Publication Date Title
EP3236077B1 (fr) Compresseur centrifuge à compensation réglable pour un turbocompresseur
US7097432B1 (en) Sliding vane turbocharger with graduated vanes
FR2966194A1 (fr) Tuyere de turbine a section variable
EP2960460A1 (fr) Turbocompresseur à géométrie variable
JP6256142B2 (ja) 遠心圧縮機
EP3043045A2 (fr) Compresseur centrifuge à compensation réglable et turbocompresseur muni de celui-ci
EP3103988B1 (fr) Turbocompresseur à buse de turbine d'aube variable ayant un mécanisme de dérivation intégrée avec les aubes
FR2866387A1 (fr) Adaptation aerodynamique de la soufflante arriere d'un turboreacteur double soufflante
EP3054568B1 (fr) Moteur éléctrique avec radiateur extérieur et deux circuits de refroidissement séparés
JP2012087785A5 (fr)
CA2491666A1 (fr) Perfectionnements apportes au dispositif de controle de jeu dans une turbine a gaz
FR3028289B1 (fr) Turbomachine d'aeronef comprenant un boitier d'admission d'air a profil aerodynamique variable
FR2910524A1 (fr) Element profile a agencement de fentes de refroidissement ameliore
US10393143B2 (en) Compressor with annular diffuser having first vanes and second vanes
FR3062876B1 (fr) Compresseur haute pression pour turbomachine
CA2528076A1 (fr) Refroidissement de bord d'attaque d'enveloppe de turbine
EP2620634A3 (fr) Rotor d'hydrolienne comportant au moins une pâle mobile en rotation autour d'un axe radial et des moyens de limitation du mouvement en rotation de ladite pâle, et hydrolienne comprenant un tel rotor
FR3108362B1 (fr) Etage d’aubes à orientation variable pour une turbomachine axiale comprenant un organe de régulation du débit d’air dépendant de l’orientation des aubes
FR3100268B1 (fr) Turbomachine a double flux pour un aeronef
FR3087244B1 (fr) Vanne d'echappement
FR3072719B1 (fr) Anneau de commande d'un etage d'aubes a calage variable pour une turbomachine
FR3085993B1 (fr) Aube mobile pour une roue d'une turbomachine
FR3108658B1 (fr) Rotor de turbine comprenant un dispositif de régulation du débit de fluide de refroidissement et turbomachine comprenant un tel rotor
FR3121171B1 (fr) Rotor de soufflante pour une turbomachine
FR3071539B1 (fr) Joint d'etancheite a labyrinthe pour une turbomachine d'aeronef

Legal Events

Date Code Title Description
PLFP Fee payment

Year of fee payment: 2

PLSC Publication of the preliminary search report

Effective date: 20210924

PLFP Fee payment

Year of fee payment: 3

PLFP Fee payment

Year of fee payment: 4

PLFP Fee payment

Year of fee payment: 5