FR2948725B1 - Dispositif anti-usure d'un rotor de turbomachine - Google Patents

Dispositif anti-usure d'un rotor de turbomachine

Info

Publication number
FR2948725B1
FR2948725B1 FR0903695A FR0903695A FR2948725B1 FR 2948725 B1 FR2948725 B1 FR 2948725B1 FR 0903695 A FR0903695 A FR 0903695A FR 0903695 A FR0903695 A FR 0903695A FR 2948725 B1 FR2948725 B1 FR 2948725B1
Authority
FR
France
Prior art keywords
rim
cells
extension
turbomachine rotor
wear device
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
FR0903695A
Other languages
English (en)
Other versions
FR2948725A1 (fr
Inventor
Michael Delapierre
Jerome Paul Marceau Mace
Patrick Jean Louis Reghezza
Nicolas Christian Triconnet
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 FR0903695A priority Critical patent/FR2948725B1/fr
Priority to US12/845,397 priority patent/US8573944B2/en
Publication of FR2948725A1 publication Critical patent/FR2948725A1/fr
Application granted granted Critical
Publication of FR2948725B1 publication Critical patent/FR2948725B1/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
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/06—Rotors for more than one axial stage, e.g. of drum or multiple disc type; Details thereof, e.g. shafts, shaft connections
    • 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
    • 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
    • F01D5/3092—Protective layers between blade root and rotor disc surfaces, e.g. anti-friction layers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D27/00—Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
    • F04D27/001—Testing thereof; Determination or simulation of flow characteristics; Stall or surge detection, e.g. condition monitoring
    • 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
    • F04D29/322—Blade mountings
    • 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
    • F05D2300/50—Intrinsic material properties or characteristics
    • F05D2300/505—Shape memory behaviour
    • 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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

La présent invention porte sur un dispositif anti-usure d'un rotor de turbomachine comprenant un disque (20) avec une jante et des alvéoles (21) axiales usinées sur la jante pour le logement individuel d'aubes, un anneau (43) étant rapporté sur une face de la jante, l'anneau étant percé de trous (44) dans le prolongement axial des alvéoles, au moins une partie desdits trous (44) dans le prolongement des alvéoles étant fermée par un bouchon (50) comprenant une tête métallique (51) formant surface d'appui desdites aubes. Le dispositif est caractérisé par le fait que le bouchon comprend une tige (52) dans le prolongement de la tête métallique, un insert (53) en matériau déformable entourant au moins en partie la tige et un moyen de serrage (54), l'insert en matériau déformable étant déformé par le moyen de serrage de manière à immobiliser le bouchon dans le trou.
FR0903695A 2009-07-28 2009-07-28 Dispositif anti-usure d'un rotor de turbomachine Active FR2948725B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR0903695A FR2948725B1 (fr) 2009-07-28 2009-07-28 Dispositif anti-usure d'un rotor de turbomachine
US12/845,397 US8573944B2 (en) 2009-07-28 2010-07-28 Anti-wear device of a turbomachine rotor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0903695A FR2948725B1 (fr) 2009-07-28 2009-07-28 Dispositif anti-usure d'un rotor de turbomachine

Publications (2)

Publication Number Publication Date
FR2948725A1 FR2948725A1 (fr) 2011-02-04
FR2948725B1 true FR2948725B1 (fr) 2012-10-05

Family

ID=41809216

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0903695A Active FR2948725B1 (fr) 2009-07-28 2009-07-28 Dispositif anti-usure d'un rotor de turbomachine

Country Status (2)

Country Link
US (1) US8573944B2 (fr)
FR (1) FR2948725B1 (fr)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2968363B1 (fr) 2010-12-03 2014-12-05 Snecma Rotor de turbomachine avec une cale anti-usure entre un disque et un anneau
FR2986284B1 (fr) 2012-01-31 2014-03-28 Snecma Procede de reparation de marques d’usure.
FR3003294B1 (fr) * 2013-03-15 2018-03-30 Safran Aircraft Engines Soufflante de turbomoteur a flux multiple, et turbomoteur equipe d'une telle soufflante
EP2933436A1 (fr) * 2014-04-15 2015-10-21 Siemens Aktiengesellschaft Disque de roue doté d'au moins une tôle d'étanchéité
US10006364B2 (en) * 2014-08-20 2018-06-26 United Technologies Corporation Gas turbine rotors
CN107428295A (zh) * 2015-03-19 2017-12-01 三菱电机株式会社 未确认信息输出装置、未确认信息输出方法
FR3119646B1 (fr) * 2021-02-11 2024-03-01 Safran Aircraft Engines Rotor de turbomachine
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 (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4388031A (en) * 1980-10-03 1983-06-14 Rodgers Earl T Blind fastener device
US4376604A (en) * 1981-01-29 1983-03-15 Monogram Industries, Inc. Blind fastener for composite materials
FR2502690B1 (fr) * 1981-03-27 1985-09-13 Snecma Dispositif de verrouillage d'aubes de soufflante et de fixation de capot avant d'un turboreacteur
US4595324A (en) * 1982-09-28 1986-06-17 Monogram Industries, Inc. Impulse resistant blind fastener
FR2566061B1 (fr) 1984-06-14 1988-09-02 Snecma Dispositif de verrouillage axial d'une aube de turbomachine
US5123813A (en) * 1991-03-01 1992-06-23 General Electric Company Apparatus for preloading an airfoil blade in a gas turbine engine
US5120175A (en) * 1991-07-15 1992-06-09 Arbegast William J Shape memory alloy fastener
AT403402B (de) * 1995-11-06 1998-02-25 Mark Rudolf Befestigungselement
FR2844562B1 (fr) * 2002-09-18 2004-10-29 Snecma Moteurs Maitrise de la position axiale d'une aube de rotor de soufflante
FR2888897B1 (fr) * 2005-07-21 2007-10-19 Snecma Dispositif d'amortissement des vibrations d'un anneau de retention axiale des aubes de soufflante d'une turbomachine
FR2903154B1 (fr) * 2006-06-29 2011-10-28 Snecma Rotor de turbomachine et turbomachine comportant un tel rotor
DE102007009692A1 (de) * 2007-02-28 2008-09-04 Robert Bosch Gmbh Unfallsensor

Also Published As

Publication number Publication date
US8573944B2 (en) 2013-11-05
US20110027093A1 (en) 2011-02-03
FR2948725A1 (fr) 2011-02-04

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