FR2940353B1 - Roue mobile de turbomachine a aubes en materiau composite. - Google Patents

Roue mobile de turbomachine a aubes en materiau composite.

Info

Publication number
FR2940353B1
FR2940353B1 FR0858997A FR0858997A FR2940353B1 FR 2940353 B1 FR2940353 B1 FR 2940353B1 FR 0858997 A FR0858997 A FR 0858997A FR 0858997 A FR0858997 A FR 0858997A FR 2940353 B1 FR2940353 B1 FR 2940353B1
Authority
FR
France
Prior art keywords
composite material
disc
groove
aubes
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
FR0858997A
Other languages
English (en)
Other versions
FR2940353A1 (fr
Inventor
Stephane Pierre Guillaume Blanchard
Stephane Otin
Guillaume Jean Claude Robert Renon
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
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 SAS filed Critical SNECMA SAS
Priority to FR0858997A priority Critical patent/FR2940353B1/fr
Priority to US12/646,454 priority patent/US8282355B2/en
Publication of FR2940353A1 publication Critical patent/FR2940353A1/fr
Application granted granted Critical
Publication of FR2940353B1 publication Critical patent/FR2940353B1/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
    • 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
    • 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
    • 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
    • F01D5/3023—Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses
    • F01D5/303—Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses in a circumferential slot
    • F01D5/3038—Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses in a circumferential slot the slot having inwardly directed abutment faces on both sides
    • 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
    • F01D5/3069—Fixing blades to rotors; Blade roots ; Blade spacers between two discs or rings
    • 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
    • F01D5/32—Locking, e.g. by final locking blades or keys
    • 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
    • F04D29/02—Selection of particular materials
    • F04D29/023—Selection of particular materials especially adapted for elastic fluid pumps
    • 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
    • F04D29/08—Sealings
    • F04D29/16—Sealings between pressure and suction sides
    • F04D29/161—Sealings between pressure and suction sides especially adapted for elastic fluid pumps
    • F04D29/164—Sealings between pressure and suction sides especially adapted for elastic fluid pumps of an axial flow wheel
    • 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
    • F04D29/26—Rotors specially for elastic fluids
    • F04D29/32—Rotors specially for elastic fluids for axial flow pumps
    • F04D29/321—Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
    • 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/603—Composites; e.g. fibre-reinforced
    • 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

Abstract

L'invention concerne une roue mobile (1) de turbomachine à aubes en matériau composite, comportant un disque glissière (10) comprenant à sa périphérie extérieure une rainure circonférentielle (12) dont l'ouverture est plus étroite que son fond, une pluralité d'aubes (100) en matériau composite ayant chacune un pied d'aube (102) engagé dans la rainure du disque glissière et présentant une section longitudinale adaptée à la section longitudinale de la rainure du disque glissière afin d'y être maintenu radialement par coopération de forme, et un disque d'orientation (200) fixé coaxialement autour du disque glissière et comprenant à sa périphérie extérieure une pluralité de fentes axiales (208) ouvertes à une extrémité, chaque fente présentant une section transversale adaptée à la section transversale d'un pied d'aube afin de le maintenir angulairement par coopération de forme.
FR0858997A 2008-12-23 2008-12-23 Roue mobile de turbomachine a aubes en materiau composite. Active FR2940353B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR0858997A FR2940353B1 (fr) 2008-12-23 2008-12-23 Roue mobile de turbomachine a aubes en materiau composite.
US12/646,454 US8282355B2 (en) 2008-12-23 2009-12-23 Turbomachine rotor wheel having composite material blades

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0858997A FR2940353B1 (fr) 2008-12-23 2008-12-23 Roue mobile de turbomachine a aubes en materiau composite.

Publications (2)

Publication Number Publication Date
FR2940353A1 FR2940353A1 (fr) 2010-06-25
FR2940353B1 true FR2940353B1 (fr) 2011-02-11

Family

ID=40908470

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0858997A Active FR2940353B1 (fr) 2008-12-23 2008-12-23 Roue mobile de turbomachine a aubes en materiau composite.

Country Status (2)

Country Link
US (1) US8282355B2 (fr)
FR (1) FR2940353B1 (fr)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2940350B1 (fr) 2008-12-23 2011-03-18 Snecma Roue mobile de turbomachine a aubes en materiau composite munie d'un anneau ressort.
FR2961847B1 (fr) * 2010-06-25 2012-08-17 Snecma Roue mobile a aubes en materiau composite pour moteur a turbine a gaz a liaison pied d'aube/disque par serrage
FR2967453B1 (fr) * 2010-11-17 2012-12-21 Snecma Disque de retention d'aubes
FR2982635B1 (fr) * 2011-11-15 2013-11-15 Snecma Roue a aubes pour une turbomachine
WO2014190008A1 (fr) * 2013-05-23 2014-11-27 General Electric Company Pale de compresseur composite et procédé d'assemblage
FR3020408B1 (fr) 2014-04-24 2018-04-06 Safran Aircraft Engines Ensemble rotatif pour turbomachine
JP2017524091A (ja) * 2014-05-08 2017-08-24 ゼネラル・エレクトリック・カンパニイ 分離可能な複合材ブレードを有する複合材ブースター・スプール
US10280768B2 (en) 2014-11-12 2019-05-07 Rolls-Royce North American Technologies Inc. Turbine blisk including ceramic matrix composite blades and methods of manufacture
US9909430B2 (en) 2014-11-13 2018-03-06 Rolls-Royce North American Technologies Inc. Turbine disk assembly including seperable platforms for blade attachment
US10029336B2 (en) * 2014-11-26 2018-07-24 United Technologies Corporation Rotor with blades secured by woven fiber attachment system
US9777593B2 (en) 2015-02-23 2017-10-03 General Electric Company Hybrid metal and composite spool for rotating machinery
US10047763B2 (en) 2015-12-14 2018-08-14 General Electric Company Rotor assembly for use in a turbofan engine and method of assembling
CN107120294B (zh) * 2016-02-25 2019-12-13 奇鋐科技股份有限公司 散热风扇之扇轮结构
TWI612223B (zh) * 2016-02-25 2018-01-21 Asia Vital Components Co Ltd 散熱風扇之扇輪結構
CN107120308B (zh) * 2016-02-25 2019-11-26 奇鋐科技股份有限公司 风扇扇轮结构
US10294954B2 (en) * 2016-11-09 2019-05-21 Rolls-Royce North American Technologies Inc. Composite blisk
US10563665B2 (en) 2017-01-30 2020-02-18 Rolls-Royce North American Technologies, Inc. Turbomachine stage and method of making same
BE1027992B1 (fr) * 2020-01-15 2021-08-17 Safran Aero Boosters Méthode et ensemble pour la sélection d’un jeu d’aubes
IT202100029963A1 (it) * 2021-11-26 2023-05-26 Ge Avio Srl Motore a turbina a gas comprendente un complesso di pale rotanti.

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE165854C (de) * 1904-10-18 1905-12-01 Hohenzollern Ag Für Lokomotivbau Befestigung der schaufeln achsialer dampf- oder gasturbinen
FR389268A (fr) * 1907-04-20 1908-09-04 Carl Roth Système de fixation des aubes de turbines à vapeur et autres machines analogues
US955648A (en) * 1907-10-29 1910-04-19 Joseph Knight Power-turbine.
FR398666A (fr) * 1909-04-19 1909-06-11 Thomson Houston Ateliers Dispositif de montage des aubes d'une turbine à fluide élastique
DE439567C (de) * 1921-10-29 1927-01-14 Lorenzen G M B H C Einrichtung zur Befestigung von Hohlschaufeln fuer Gasturbinen
GB277663A (en) * 1926-09-20 1928-01-26 Lorenzen Turbinen Ag Improvements in or relating to turbines
FR2679599A1 (fr) * 1991-07-24 1993-01-29 Snecma Perfectionnement aux roues a aubes de turbomachines.
GB9405473D0 (en) * 1994-03-19 1994-05-04 Rolls Royce Plc A gas turbine engine fan blade assembly

Also Published As

Publication number Publication date
FR2940353A1 (fr) 2010-06-25
US8282355B2 (en) 2012-10-09
US20100166560A1 (en) 2010-07-01

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