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FR2940352B1 - Roue mobile de turbomachine a aubes en materiau composite munies de lechettes metalliques. - Google Patents

Roue mobile de turbomachine a aubes en materiau composite munies de lechettes metalliques.

Info

Publication number
FR2940352B1
FR2940352B1 FR0859000A FR0859000A FR2940352B1 FR 2940352 B1 FR2940352 B1 FR 2940352B1 FR 0859000 A FR0859000 A FR 0859000A FR 0859000 A FR0859000 A FR 0859000A FR 2940352 B1 FR2940352 B1 FR 2940352B1
Authority
FR
France
Prior art keywords
heel
blades
composite material
metal
lechettes
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
FR0859000A
Other languages
English (en)
Other versions
FR2940352A1 (fr
Inventor
Stephane Pierre Guillaume Blanchard
Julien Mateo
Stephane Otin
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 FR0859000A priority Critical patent/FR2940352B1/fr
Priority to US12/636,041 priority patent/US8870531B2/en
Publication of FR2940352A1 publication Critical patent/FR2940352A1/fr
Application granted granted Critical
Publication of FR2940352B1 publication Critical patent/FR2940352B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/28Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/282Selecting composite materials, e.g. blades with reinforcing filaments
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D11/00Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/08Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • F01D11/14Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing
    • F01D11/16Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing by self-adjusting means
    • F01D11/18Adjusting 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/22Blade-to-blade connections, e.g. for damping vibrations
    • F01D5/225Blade-to-blade connections, e.g. for damping vibrations by shrouding
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/30Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/3007Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/02Selection of particular materials
    • F04D29/023Selection of particular materials especially adapted for elastic fluid pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/08Sealings
    • F04D29/16Sealings between pressure and suction sides
    • F04D29/161Sealings between pressure and suction sides especially adapted for elastic fluid pumps
    • F04D29/164Sealings between pressure and suction sides especially adapted for elastic fluid pumps of an axial flow wheel
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/32Rotors specially for elastic fluids for axial flow pumps
    • F04D29/321Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
    • F04D29/324Blades
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00Manufacture
    • F05D2230/20Manufacture essentially without removing material
    • F05D2230/23Manufacture essentially without removing material by permanently joining parts together
    • F05D2230/232Manufacture essentially without removing material by permanently joining parts together by welding
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00Manufacture
    • F05D2230/60Assembly methods
    • F05D2230/64Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00Materials; Properties thereof
    • F05D2300/60Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/603Composites; e.g. fibre-reinforced
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient 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)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

L'invention concerne une roue mobile (2) de turbomachine à aubes en matériau composite, comprenant un disque de montage (4), une pluralité d'aubes (8) en matériau composite montées sur le disque de montage par leur pied (10) et munies chacune à leur extrémité libre d'un talon (14), et une virole métallique (18) positionnée sur le talon des aubes de façon concentrique au disque de montage et comprenant des léchettes (20) faisant saillie radialement vers l'extérieur et destinées à venir abraser un matériau abradable (16) porté par un carter entourant la roue, la virole étant fixe axialement et circonférentiellement par rapport au talon des aubes et apte à se déplacer radialement vers l'extérieur par rapport au talon des aubes.
FR0859000A 2008-12-23 2008-12-23 Roue mobile de turbomachine a aubes en materiau composite munies de lechettes metalliques. Active FR2940352B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR0859000A FR2940352B1 (fr) 2008-12-23 2008-12-23 Roue mobile de turbomachine a aubes en materiau composite munies de lechettes metalliques.
US12/636,041 US8870531B2 (en) 2008-12-23 2009-12-11 Turbomachine rotor having blades of composite material provided with metal labyrinth teeth

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0859000A FR2940352B1 (fr) 2008-12-23 2008-12-23 Roue mobile de turbomachine a aubes en materiau composite munies de lechettes metalliques.

Publications (2)

Publication Number Publication Date
FR2940352A1 FR2940352A1 (fr) 2010-06-25
FR2940352B1 true FR2940352B1 (fr) 2014-11-28

Family

ID=40933787

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0859000A Active FR2940352B1 (fr) 2008-12-23 2008-12-23 Roue mobile de turbomachine a aubes en materiau composite munies de lechettes metalliques.

Country Status (2)

Country Link
US (1) US8870531B2 (fr)
FR (1) FR2940352B1 (fr)

Families Citing this family (6)

* 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.
US9598969B2 (en) * 2012-07-20 2017-03-21 Kabushiki Kaisha Toshiba Turbine, manufacturing method thereof, and power generating system
GB201222973D0 (en) * 2012-12-19 2013-01-30 Composite Technology & Applic Ltd An aerofoil structure
CA2932601C (fr) 2015-06-17 2023-10-03 Rolls-Royce Corporation Joint labyrinthe dote d'un diviseur de flux modulable
BE1025283B1 (fr) * 2017-06-02 2019-01-11 Safran Aero Boosters S.A. Systeme d'etancheite pour compresseur de turbomachine
CN116291762B (zh) * 2023-04-07 2023-10-13 南京航空航天大学 叶尖间隙可控的航空发动机高压涡轮部件及航空发动机

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2610823A (en) * 1947-02-11 1952-09-16 Gen Electric Turbine bucket damping arrangement
US3095138A (en) * 1957-05-28 1963-06-25 Studebaker Corp Rotating shroud
US3048365A (en) * 1959-12-22 1962-08-07 Curtiss Wright Corp Rotor blade shroud and vibration damping structure
US3556675A (en) * 1969-01-29 1971-01-19 Gen Electric Turbomachinery rotor with integral shroud
FR2051912A5 (fr) * 1969-07-01 1971-04-09 Rabouyt Denis
GB1299929A (en) * 1970-04-10 1972-12-13 Secr Defence A bladed rotor for a gas turbine engine
US3728044A (en) * 1970-06-29 1973-04-17 Hitachi Ltd Turbine rotor
IT975329B (it) * 1972-10-23 1974-07-20 Fiat Spa Struttura di parti metalliche e nom metalliche statiche o rotanti per ambienti ad alta temperatura particolarmente per rotori e stato ri di turbine a gas
GB1432994A (en) * 1973-05-02 1976-04-22 Rolls Royce Compressor for gas turbine engines
JPS5330844B2 (fr) * 1975-01-24 1978-08-30
US4832568A (en) * 1982-02-26 1989-05-23 General Electric Company Turbomachine airfoil mounting assembly
DE3842710C1 (fr) * 1988-12-19 1989-08-03 Mtu Muenchen Gmbh
GB9109016D0 (en) * 1991-04-26 1991-06-12 Turbine Blading Ltd Turbine blade repair
DE19531561A1 (de) * 1995-08-28 1997-03-06 Abb Research Ltd Versteifungen für Turbinenschaufeln
US6371725B1 (en) * 2000-06-30 2002-04-16 General Electric Company Conforming platform guide vane
FR2853931A1 (fr) * 2003-04-16 2004-10-22 Snecma Moteurs Reduction de jeux dans une turbine a gaz
EP1825105B1 (fr) * 2004-12-08 2009-03-18 Volvo Aero Corporation Roue pour machine a flux rotatif
US7393182B2 (en) * 2005-05-05 2008-07-01 Florida Turbine Technologies, Inc. Composite tip shroud ring
EP1801357B1 (fr) * 2005-12-22 2010-10-27 Techspace Aero Aubage statorique de turbomachine, turbomachine comportant l'aubage et aube de turbomachine

Also Published As

Publication number Publication date
US8870531B2 (en) 2014-10-28
US20100158675A1 (en) 2010-06-24
FR2940352A1 (fr) 2010-06-25

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