FR3062169B1 - Carter de module de turbomachine d'aeronef, comprenant un caloduc associe a un anneau d'etancheite entourant une roue mobile aubagee du module - Google Patents

Carter de module de turbomachine d'aeronef, comprenant un caloduc associe a un anneau d'etancheite entourant une roue mobile aubagee du module Download PDF

Info

Publication number
FR3062169B1
FR3062169B1 FR1750475A FR1750475A FR3062169B1 FR 3062169 B1 FR3062169 B1 FR 3062169B1 FR 1750475 A FR1750475 A FR 1750475A FR 1750475 A FR1750475 A FR 1750475A FR 3062169 B1 FR3062169 B1 FR 3062169B1
Authority
FR
France
Prior art keywords
module
aubagee
heat pump
seal ring
aircraft turbomachine
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
FR1750475A
Other languages
English (en)
Other versions
FR3062169A1 (fr
Inventor
Christophe SCHOLTES
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 FR1750475A priority Critical patent/FR3062169B1/fr
Priority to US15/869,972 priority patent/US11248486B2/en
Priority to GB1800626.2A priority patent/GB2560419B/en
Publication of FR3062169A1 publication Critical patent/FR3062169A1/fr
Application granted granted Critical
Publication of FR3062169B1 publication Critical patent/FR3062169B1/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
    • 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
    • F01D11/16—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing by self-adjusting means
    • F01D11/18—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing by self-adjusting means using stator or rotor components with predetermined thermal response, e.g. selective insulation, thermal inertia, differential expansion
    • 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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/08—Cooling; Heating; Heat-insulation
    • F01D25/14—Casings modified therefor
    • 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
    • F04D29/522—Casings; Connections of working fluid for axial pumps especially adapted for elastic fluid pumps
    • F04D29/526—Details of the casing section radially opposing blade tips
    • 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
    • F04D29/58—Cooling; Heating; Diminishing heat transfer
    • F04D29/582—Cooling; Heating; Diminishing heat transfer specially adapted for elastic fluid pumps
    • F04D29/584—Cooling; Heating; Diminishing heat transfer specially adapted for elastic fluid pumps cooling or heating the machine
    • 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
    • F04D29/58—Cooling; Heating; Diminishing heat transfer
    • F04D29/582—Cooling; Heating; Diminishing heat transfer specially adapted for elastic fluid pumps
    • F04D29/5853—Cooling; Heating; Diminishing heat transfer specially adapted for elastic fluid pumps heat insulation or conduction
    • 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
    • F05D2240/10—Stators
    • F05D2240/11—Shroud seal segments
    • 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
    • F05D2240/10—Stators
    • F05D2240/14—Casings or housings protecting or supporting assemblies within
    • 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
    • F05D2240/55—Seals
    • 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
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/208—Heat transfer, e.g. cooling using heat pipes
    • 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)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

L'invention concerne un carter (26) de module de turbomachine d'aéronef comprenant un carter extérieur de module (28) ainsi qu'au moins un anneau d'étanchéité (30) destiné à entourer une roue mobile aubagée (22) du module et agencé radialement vers l'intérieur par rapport audit carter extérieur (28). Le carter (26) comprend au moins un caloduc capillaire (40) dont une première extrémité (76) est fixée sur l'anneau d'étanchéité (30), et dont une seconde extrémité (78) opposée à la première est fixée sur un élément de carter (48, 52, 60) agencé radialement vers l'extérieur par rapport à l'anneau (30).
FR1750475A 2017-01-20 2017-01-20 Carter de module de turbomachine d'aeronef, comprenant un caloduc associe a un anneau d'etancheite entourant une roue mobile aubagee du module Active FR3062169B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR1750475A FR3062169B1 (fr) 2017-01-20 2017-01-20 Carter de module de turbomachine d'aeronef, comprenant un caloduc associe a un anneau d'etancheite entourant une roue mobile aubagee du module
US15/869,972 US11248486B2 (en) 2017-01-20 2018-01-12 Aircraft turbine-engine module casing, comprising a heat pipe associated with a sealing ring surrounding a movable impeller of the module
GB1800626.2A GB2560419B (en) 2017-01-20 2018-01-15 Aircraft turbine-engine module casing, comprising a heat pipe associated with a sealing ring surrounding a movable impeller of the module

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1750475A FR3062169B1 (fr) 2017-01-20 2017-01-20 Carter de module de turbomachine d'aeronef, comprenant un caloduc associe a un anneau d'etancheite entourant une roue mobile aubagee du module
FR1750475 2017-01-20

Publications (2)

Publication Number Publication Date
FR3062169A1 FR3062169A1 (fr) 2018-07-27
FR3062169B1 true FR3062169B1 (fr) 2019-04-19

Family

ID=58455280

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1750475A Active FR3062169B1 (fr) 2017-01-20 2017-01-20 Carter de module de turbomachine d'aeronef, comprenant un caloduc associe a un anneau d'etancheite entourant une roue mobile aubagee du module

Country Status (3)

Country Link
US (1) US11248486B2 (fr)
FR (1) FR3062169B1 (fr)
GB (1) GB2560419B (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3055353B1 (fr) 2016-08-25 2018-09-21 Safran Aircraft Engines Ensemble formant joint d'etancheite a labyrinthe pour une turbomachine comportant un abradable et des lechettes inclines
FR3086323B1 (fr) 2018-09-24 2020-12-11 Safran Aircraft Engines Carter interne de turmomachine a isolation thermique amelioree

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1541894A (en) * 1976-08-12 1979-03-14 Rolls Royce Gas turbine engines
GB1548836A (en) * 1977-03-17 1979-07-18 Rolls Royce Gasturbine engine
FR2467292A1 (fr) 1979-10-09 1981-04-17 Snecma Dispositif de reglage du jeu entre les aubes mobiles et l'anneau de turbine
US5192186A (en) * 1980-10-03 1993-03-09 Rolls-Royce Plc Gas turbine engine
GB2090333B (en) * 1980-12-18 1984-04-26 Rolls Royce Gas turbine engine shroud/blade tip control
GB2245314B (en) * 1983-05-26 1992-04-22 Rolls Royce Cooling of gas turbine engine shroud rings
US5639210A (en) * 1995-10-23 1997-06-17 United Technologies Corporation Rotor blade outer tip seal apparatus
GB9815611D0 (en) * 1998-07-18 1998-09-16 Rolls Royce Plc Improvements in or relating to turbine cooling
ES2430552T3 (es) * 2005-04-29 2013-11-21 Vlaamse Instelling Voor Technologisch Onderzoek N.V. (Vito) Aparato y procedimiento para la purificación y desinfección de sustancias líquidas o gaseosas
US7900437B2 (en) * 2006-07-28 2011-03-08 General Electric Company Heat transfer system and method for turbine engine using heat pipes
US7900438B2 (en) * 2006-07-28 2011-03-08 General Electric Company Heat transfer system and method for turbine engine using heat pipes
CA2663842C (fr) * 2006-09-22 2013-07-23 The Procter & Gamble Company Systeme de distribution pour generer des matieres liquides actives en utilisant un transducteur electromecanique
US8015788B2 (en) * 2006-12-27 2011-09-13 General Electric Company Heat transfer system for turbine engine using heat pipes
FR2915520B1 (fr) * 2007-04-30 2012-05-25 Snecma Ensemble moteur comprenant un ou plusieurs caloducs pour le refroidissement d'un compresseur haute pression
US20110103939A1 (en) * 2009-10-30 2011-05-05 General Electric Company Turbine rotor blade tip and shroud clearance control
US9598974B2 (en) 2013-02-25 2017-03-21 Pratt & Whitney Canada Corp. Active turbine or compressor tip clearance control
US9797310B2 (en) * 2015-04-02 2017-10-24 General Electric Company Heat pipe temperature management system for a turbomachine
FR3038656B1 (fr) * 2015-07-06 2017-06-23 Snecma Ensemble de turbomachine pour le refroidissement et le controle du jeu a performances ameliorees

Also Published As

Publication number Publication date
GB2560419B (en) 2021-12-22
GB201800626D0 (en) 2018-02-28
GB2560419A (en) 2018-09-12
US20180209291A1 (en) 2018-07-26
FR3062169A1 (fr) 2018-07-27
US11248486B2 (en) 2022-02-15

Similar Documents

Publication Publication Date Title
RU2014132071A (ru) Способ и устройство для удержания фланца на расходомере
EP4234989A3 (fr) Dispositif de couplage de fluide de translation
CL2018000485A1 (es) Montaje de resorte con punto de conexión protegido.
FR3062169B1 (fr) Carter de module de turbomachine d'aeronef, comprenant un caloduc associe a un anneau d'etancheite entourant une roue mobile aubagee du module
FR3018548B1 (fr) Turboreacteur a conduit de decharge
EA201990371A1 (ru) Устройство для герметичной проводки протяженной детали
FR3058756B1 (fr) Turbine pour turbomachine
FR3099801B1 (fr) Ensemble pour une turbine de turbomachine
MX356889B (es) Disposición de sellado para turbomáquinas axialmente divididas.
FR3091720B1 (fr) Ensemble pour une turbomachine
FR3092609B1 (fr) Ensemble de turbine pour turbomachine d’aeronef a circuit de refroidissement de disque ameliore
FR3062679B1 (fr) Virole de reduction de la surpression au voisinage du joint amont d'une enceinte de palier de turboreacteur
PL417106A1 (pl) Maszyna przepływowa zawierająca system regulacji luzu
FR3024996B1 (fr) Anneau de commande d'un etage d'aubes a calage variable pour une turbomachine
ATE549565T1 (de) Volumetrisches dichtungssystem
FR3048017B1 (fr) Redresseur pour compresseur de turbomachine d'aeronef, comprenant des orifices de prelevement d'air de forme etiree selon la direction circonferentielle
FR3099798B1 (fr) Ensemble pour une turbine de turbomachine
FR3092148B1 (fr) Carter de soufflante pour une turbomachine d’aeronef
FR2991376B1 (fr) Alignement de parties statiques dans une turbine a gaz.
FR3071539B1 (fr) Joint d'etancheite a labyrinthe pour une turbomachine d'aeronef
FR3098547B1 (fr) Assemblage de maintien d’un train d’engrenages dans une turbomachine
FR3081927B1 (fr) Dispositif de refroidissement d'un carter de turbomachine
FR3082873B1 (fr) Ensemble de turbomachine, aube de turbomachine et turbomachine
FR3083566B1 (fr) Ensemble de turbine pour turbomachine d'aeronef a circuit de refroidissement de disque equipe d'un dispositif d'etancheite
FR3072713B1 (fr) Secteur d'anneau de turbine pour 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: 20180727

PLFP Fee payment

Year of fee payment: 4

PLFP Fee payment

Year of fee payment: 5

PLFP Fee payment

Year of fee payment: 6

PLFP Fee payment

Year of fee payment: 7

PLFP Fee payment

Year of fee payment: 8