FR2963382B1 - Roue de turbine a aubes en composite a matrice ceramique - Google Patents

Roue de turbine a aubes en composite a matrice ceramique

Info

Publication number
FR2963382B1
FR2963382B1 FR1056392A FR1056392A FR2963382B1 FR 2963382 B1 FR2963382 B1 FR 2963382B1 FR 1056392 A FR1056392 A FR 1056392A FR 1056392 A FR1056392 A FR 1056392A FR 2963382 B1 FR2963382 B1 FR 2963382B1
Authority
FR
France
Prior art keywords
blades
turbine wheel
matrix composite
ceramic matrix
aubes
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.)
Expired - Fee Related
Application number
FR1056392A
Other languages
English (en)
Other versions
FR2963382A1 (fr
Inventor
Christian Michel Jacques Gosselin
Maurice Guy Judet
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
Safran Ceramics SA
Original Assignee
SNECMA Propulsion Solide SA
SNECMA 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 SNECMA Propulsion Solide SA, SNECMA SAS filed Critical SNECMA Propulsion Solide SA
Priority to FR1056392A priority Critical patent/FR2963382B1/fr
Publication of FR2963382A1 publication Critical patent/FR2963382A1/fr
Application granted granted Critical
Publication of FR2963382B1 publication Critical patent/FR2963382B1/fr
Expired - Fee Related 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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/26—Antivibration means not restricted to blade form or construction or to blade-to-blade connections or to the use of particular materials
    • 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
    • F01D11/005—Sealing means between non relatively rotating elements
    • F01D11/006—Sealing the gap between rotor blades or blades and rotor
    • 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
    • F01D11/005—Sealing means between non relatively rotating elements
    • F01D11/006—Sealing the gap between rotor blades or blades and rotor
    • F01D11/008—Sealing the gap between rotor blades or blades and rotor by spacer elements between the blades, e.g. independent interblade platforms
    • 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
    • F01D5/22—Blade-to-blade connections, e.g. for damping vibrations
    • 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
    • F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/282—Selecting composite materials, e.g. blades with reinforcing filaments
    • 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
    • F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/3007—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
    • F01D5/3015—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type with side plates
    • 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)
  • Materials Engineering (AREA)
  • Composite Materials (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

Roue de turbine pour une turbomachine, comprenant un disque portant des aubes (35), et des amortisseurs (30) montés entre les échasses (33) des aubes et destinés à frotter sur les plates-formes de ces aubes pour dissiper leurs vibrations, caractérisé en ce que les aubes sont réalisées en composite à matrice céramique (CMC), et en ce que les amortisseurs sont recouverts d'une couche mince de matériau dur sur au moins une partie de leurs surfaces de frottement sur les plates-formes des aubes, et comprennent des moyens d'étanchéité axiale limitant ou empêchant le passage d'air entre les échasses.
FR1056392A 2010-08-02 2010-08-02 Roue de turbine a aubes en composite a matrice ceramique Expired - Fee Related FR2963382B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1056392A FR2963382B1 (fr) 2010-08-02 2010-08-02 Roue de turbine a aubes en composite a matrice ceramique

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1056392A FR2963382B1 (fr) 2010-08-02 2010-08-02 Roue de turbine a aubes en composite a matrice ceramique

Publications (2)

Publication Number Publication Date
FR2963382A1 FR2963382A1 (fr) 2012-02-03
FR2963382B1 true FR2963382B1 (fr) 2016-01-29

Family

ID=43734164

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1056392A Expired - Fee Related FR2963382B1 (fr) 2010-08-02 2010-08-02 Roue de turbine a aubes en composite a matrice ceramique

Country Status (1)

Country Link
FR (1) FR2963382B1 (fr)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2974387B1 (fr) 2011-04-19 2015-11-20 Snecma Roue de turbine pour une turbomachine
SG11201502166VA (en) * 2012-09-28 2015-05-28 United Technologies Corp Seal damper with improved retention
FR3006365B1 (fr) * 2013-05-30 2015-05-22 Snecma Roue de turbomachine, notamment pour turbine basse pression
FR3027950B1 (fr) 2014-11-04 2019-10-18 Safran Aircraft Engines Roue de turbine pour une turbomachine
FR3027949B1 (fr) * 2014-11-04 2019-07-26 Safran Aircraft Engines Roue de turbine pour une turbomachine
JP6554882B2 (ja) * 2015-04-07 2019-08-07 株式会社Ihi シールド部材及びそれを用いたジェットエンジン
FR3047512B1 (fr) * 2016-02-05 2019-11-15 Safran Aircraft Engines Dispositif d'amortissement de vibrations pour aubes de turbomachine
EP3438410B1 (fr) 2017-08-01 2021-09-29 General Electric Company Système d'étanchéité pour machine rotative
US11773731B2 (en) 2022-01-04 2023-10-03 Rtx Corporation Bathtub damper seal arrangement for gas turbine engine

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5281097A (en) * 1992-11-20 1994-01-25 General Electric Company Thermal control damper for turbine rotors
US5478207A (en) * 1994-09-19 1995-12-26 General Electric Company Stable blade vibration damper for gas turbine engine
JPH1162502A (ja) * 1997-08-21 1999-03-05 Ishikawajima Harima Heavy Ind Co Ltd タービン動翼のシールダンパー
DE19937577A1 (de) * 1999-08-09 2001-02-15 Abb Alstom Power Ch Ag Reibungsbehaftete Gasturbinenkomponente
DE10256778A1 (de) * 2001-12-11 2004-01-08 Alstom (Switzerland) Ltd. Schwingungsdämpfer
US8070448B2 (en) * 2008-10-30 2011-12-06 Honeywell International Inc. Spacers and turbines

Also Published As

Publication number Publication date
FR2963382A1 (fr) 2012-02-03

Similar Documents

Publication Publication Date Title
FR2963382B1 (fr) Roue de turbine a aubes en composite a matrice ceramique
ATE435389T1 (de) Lamellendichtung, insbesondere für eine gasturbine
ATE534841T1 (de) Bremsscheibe
BR112014017505A8 (pt) pá móvel de turbomáquina e turbomáquina correspondente
BR112012026131A2 (pt) aparelho e método para controlar seletivamente o fluxo.
ATE540280T1 (de) Einbauelement einer einbaupackung
DK1963022T3 (da) Selvregulerende højtryksrotationsdyse med fluidleje og afbalanceret trykkraft
SE0402441L (sv) Lagerstativstruktur och gasturbinmotor som innefattar lagerstativstrukturen
EP2644580A3 (fr) Structure en nid d'abeille
BR112012022437A2 (pt) sistema de propulsão
NO20092349L (no) System og fremgangsmate for redusering av drag og/eller virvelindusert vibrasjon
FR2950322B1 (fr) Element d'accrochage d'un moteur d'aeronef, ensemble d'aeronef comprenant cet element et aeronef associe
DE502005000209D1 (de) Dichtungs- und Dämpfungssystem für Turbinenschaufeln
FR2926791B1 (fr) Entree d'air pour nacelle d'aeronef, et ensemble propulsif comprenant une telle entree d'air
BRPI0923327A2 (pt) junta de estanqueidade de plataforma intercalar, plataforma intacalar de rotor de turbomáquina, e, rotor de tubomáquina
BR112015020351A2 (pt) conjunto de disco de turbina e de lâmina, sistema para prevenir o vazamento de ar dentro de uma turbina, método de montagem de um conjunto de disco de turbina e de lâmina e método para prevenir vazamento de ar em uma turbina
WO2013025472A3 (fr) Bague d'usure à diffusion d'énergie et procédés de diffusion d'énergie
WO2011020458A3 (fr) Élément de rotor autour duquel un fluide doit circuler et rotor
EP2412933A3 (fr) Joint à labyrinthe
FR2896289B1 (fr) Masselotte d'equilibrage, disque de rotor en etant equipe, rotor et moteur d'aeronef les comportant
BR112013001178A2 (pt) aperfeiçoamento de válvulas divididas.
FR3064667B1 (fr) Dispositif de refroidissement d'un rotor de turbomachine
ATE541137T1 (de) Bremsband einer scheibe für eine scheibenbremse
BR112012024545A2 (pt) materiais compósitos
FR2887919B1 (fr) Rotor de turbomachine comprenant au moins un disque renforce par un anneau composite

Legal Events

Date Code Title Description
TQ Partial transmission of property

Owner name: HERAKLES, FR

Effective date: 20131121

Owner name: SNECMA PROPULSION SOLIDE, FR

Effective date: 20131121

Owner name: SNECMA, FR

Effective date: 20131121

PLFP Fee payment

Year of fee payment: 6

ST Notification of lapse

Effective date: 20170428

PLFP Fee payment

Year of fee payment: 8

CD Change of name or company name

Owner name: SNECMA PROPULSION SOLIDE, FR

Effective date: 20170630

Owner name: HERAKLES, FR

Effective date: 20170630

Owner name: SAFRAN AIRCRAFT ENGINES, FR

Effective date: 20170630

CJ Change in legal form

Effective date: 20170630

RN Application for restoration

Effective date: 20170811

FC Decision of inpi director general to approve request for restoration

Effective date: 20170830

PLFP Fee payment

Year of fee payment: 9

PLFP Fee payment

Year of fee payment: 10

CD Change of name or company name

Owner name: SAFRAN AIRCRAFT ENGINES, FR

Effective date: 20200409

Owner name: SNECMA PROPULSION SOLIDE, FR

Effective date: 20200409

Owner name: SAFRAN CERAMICS, FR

Effective date: 20200409

PLFP Fee payment

Year of fee payment: 11

PLFP Fee payment

Year of fee payment: 12

PLFP Fee payment

Year of fee payment: 13

PLFP Fee payment

Year of fee payment: 14