FR3055355B1 - Dispositif et procede de reglage de jeux entre un rotor et un stator concentrique d'une turbomachine - Google Patents

Dispositif et procede de reglage de jeux entre un rotor et un stator concentrique d'une turbomachine Download PDF

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Publication number
FR3055355B1
FR3055355B1 FR1658045A FR1658045A FR3055355B1 FR 3055355 B1 FR3055355 B1 FR 3055355B1 FR 1658045 A FR1658045 A FR 1658045A FR 1658045 A FR1658045 A FR 1658045A FR 3055355 B1 FR3055355 B1 FR 3055355B1
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FR
France
Prior art keywords
rotor
stator
turbomachine
games
adjusting
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
FR1658045A
Other languages
English (en)
Other versions
FR3055355A1 (fr
Inventor
Marie Aubin Pierre Jouy Baptiste
Claude Descamps Laurent
Guillaume Robin Pellaton Bertrand
Fabien Francois Villard Loic
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 FR1658045A priority Critical patent/FR3055355B1/fr
Priority to GB1902521.2A priority patent/GB2567602B/en
Priority to US16/327,170 priority patent/US11149577B2/en
Priority to PCT/FR2017/052291 priority patent/WO2018042116A1/fr
Publication of FR3055355A1 publication Critical patent/FR3055355A1/fr
Application granted granted Critical
Publication of FR3055355B1 publication Critical patent/FR3055355B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • F01D11/14—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing
    • F01D11/20—Actively adjusting tip-clearance
    • F01D11/24—Actively adjusting tip-clearance by selectively cooling-heating stator or rotor components
    • 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
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • F01D11/14—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing
    • F01D11/20—Actively adjusting tip-clearance
    • 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
    • F01D17/20—Devices dealing with sensing elements or final actuators or transmitting means between them, e.g. power-assisted
    • 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
    • F01D9/06—Fluid supply conduits to nozzles or the like
    • F01D9/065—Fluid supply or removal conduits traversing the working fluid flow, e.g. for lubrication-, cooling-, or sealing fluids
    • 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
    • F02C9/20—Control of working fluid flow by throttling; by adjusting vanes
    • 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
    • F02C9/26—Control of fuel supply
    • F02C9/28—Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed
    • 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
    • F05D2240/00—Components
    • F05D2240/20—Rotors
    • F05D2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
    • F05D2240/307—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor related to the tip of a rotor blade

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

Ce dispositif de pilotage de jeux entre un rotor (1) et un stator (2) l'environnant est réalisé en modifiant le débit de soufflage acheminé dans une cavité de rotor (9) pour réaliser un débit de purge qui empêche les gaz de la veine (3) de pénétrer dans la cavité. Une vanne (22) peut fermer partiellement le circuit de soufflage, ce qui diminue le rafraîchissement de la structure de rotor (10) et permet sa dilatation et la réduction des jeux avec le stator (2), pour certains régimes dont les régimes de croisière. Et l'air soufflé s'échauffe plus à débit réduit, surtout si on lui fait emprunter une dérivation (24) pourvue de méandres (26) dans les portions (17) les plus chaudes du circuit.
FR1658045A 2016-08-30 2016-08-30 Dispositif et procede de reglage de jeux entre un rotor et un stator concentrique d'une turbomachine Active FR3055355B1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR1658045A FR3055355B1 (fr) 2016-08-30 2016-08-30 Dispositif et procede de reglage de jeux entre un rotor et un stator concentrique d'une turbomachine
GB1902521.2A GB2567602B (en) 2016-08-30 2017-08-28 Device for adjusting the clearance between a rotor and a concentric stator of an aircraft turbine engine
US16/327,170 US11149577B2 (en) 2016-08-30 2017-08-28 Method and device for adjusting the clearance between a rotor and a concentric stator of an aircraft turbine engine
PCT/FR2017/052291 WO2018042116A1 (fr) 2016-08-30 2017-08-28 Procede et dispositif de reglage de jeux entre un rotor et un stator concentrique d'une turbomachine d'aeronef

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1658045A FR3055355B1 (fr) 2016-08-30 2016-08-30 Dispositif et procede de reglage de jeux entre un rotor et un stator concentrique d'une turbomachine
FR1658045 2016-08-30

Publications (2)

Publication Number Publication Date
FR3055355A1 FR3055355A1 (fr) 2018-03-02
FR3055355B1 true FR3055355B1 (fr) 2020-06-19

Family

ID=57539383

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1658045A Active FR3055355B1 (fr) 2016-08-30 2016-08-30 Dispositif et procede de reglage de jeux entre un rotor et un stator concentrique d'une turbomachine

Country Status (4)

Country Link
US (1) US11149577B2 (fr)
FR (1) FR3055355B1 (fr)
GB (1) GB2567602B (fr)
WO (1) WO2018042116A1 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3084907B1 (fr) * 2018-08-07 2020-10-30 Safran Aircraft Engines Dispositif et procede de refroidissement d'une turbine dans une turbomachine

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6250061B1 (en) * 1999-03-02 2001-06-26 General Electric Company Compressor system and methods for reducing cooling airflow
US6615574B1 (en) * 2000-01-14 2003-09-09 General Electric Co. System for combining flow from compressor bleeds of an industrial gas turbine for gas turbine performance optimization
US6968696B2 (en) * 2003-09-04 2005-11-29 Siemens Westinghouse Power Corporation Part load blade tip clearance control
FR2883926B1 (fr) * 2005-03-31 2010-09-03 Snecma Moteurs Ventilation de la roue de turbine haute pression d'un moteur a turbine a gaz aeronautique
CN102112703B (zh) * 2009-01-20 2014-07-23 三菱重工业株式会社 燃气轮机设备
US9261022B2 (en) * 2012-12-07 2016-02-16 General Electric Company System for controlling a cooling flow from a compressor section of a gas turbine
US9945251B2 (en) * 2012-12-29 2018-04-17 United Technologies Corporation Cooling architecture for turbine exhaust case
US9316153B2 (en) * 2013-01-22 2016-04-19 Siemens Energy, Inc. Purge and cooling air for an exhaust section of a gas turbine assembly
FR3002972B1 (fr) 2013-03-06 2015-04-17 Snecma Dispositif de ventilation d'un carter de stator d'une turbomachine comprenant un ajustement en direction axiale
FR3002971B1 (fr) * 2013-03-06 2015-04-17 Snecma Dispositif de ventilation d'un carter de stator d'une turbomachine, comprenant un ajustement sur des circonferences
FR3010729B1 (fr) * 2013-09-17 2017-12-29 Snecma Turbomachine comprenant un systeme de pilotage de jeux a double entree de gaz
GB201322832D0 (en) * 2013-12-23 2014-02-12 Rolls Royce Plc A flow outlet
JP6320063B2 (ja) * 2014-02-03 2018-05-09 三菱日立パワーシステムズ株式会社 ガスタービン、ガスタービンの制御装置、ガスタービンの冷却方法
US9963994B2 (en) * 2014-04-08 2018-05-08 General Electric Company Method and apparatus for clearance control utilizing fuel heating
JP6432110B2 (ja) * 2014-08-29 2018-12-05 三菱日立パワーシステムズ株式会社 ガスタービン

Also Published As

Publication number Publication date
US20200240281A1 (en) 2020-07-30
GB201902521D0 (en) 2019-04-10
FR3055355A1 (fr) 2018-03-02
US11149577B2 (en) 2021-10-19
GB2567602A (en) 2019-04-17
GB2567602B (en) 2021-11-03
WO2018042116A1 (fr) 2018-03-08

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