EP1760258A3 - Dispositif d`immobilisation d`un anneau de rétention axiale d`une aube - Google Patents

Dispositif d`immobilisation d`un anneau de rétention axiale d`une aube Download PDF

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Publication number
EP1760258A3
EP1760258A3 EP06119579A EP06119579A EP1760258A3 EP 1760258 A3 EP1760258 A3 EP 1760258A3 EP 06119579 A EP06119579 A EP 06119579A EP 06119579 A EP06119579 A EP 06119579A EP 1760258 A3 EP1760258 A3 EP 1760258A3
Authority
EP
European Patent Office
Prior art keywords
retention ring
appartus
blade
locking
axial retention
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.)
Granted
Application number
EP06119579A
Other languages
German (de)
English (en)
Other versions
EP1760258A2 (fr
EP1760258B1 (fr
Inventor
Erick Jacques Boston
Alain Marc Lucien Bromann
Pierre Debeneix
Frédéric Paul Eichstadt
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
Publication of EP1760258A2 publication Critical patent/EP1760258A2/fr
Publication of EP1760258A3 publication Critical patent/EP1760258A3/fr
Application granted granted Critical
Publication of EP1760258B1 publication Critical patent/EP1760258B1/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
    • F01D5/30Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/3007Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
    • F01D5/3015Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type with side plates
    • 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
    • F01D11/005Sealing means between non relatively rotating elements
    • F01D11/006Sealing the gap between rotor blades or blades and rotor
    • 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
    • F01D5/32Locking, e.g. by final locking blades or keys
    • F01D5/326Locking of axial insertion type blades by other means
    • 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
    • F05D2260/00Function
    • F05D2260/30Retaining components in desired mutual position

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)
  • Pile Receivers (AREA)

Abstract

Le dispositif d'immobilisation en rotation d'un anneau de rétention (20) sur un disque de rotor (10) comporte :
- un premier (162, 262) et un deuxième (164, 264) crochets d'immobilisation successifs du disque (10),
- au moins un taquet (302, 304, 306) dudit anneau de rétention (20), disposé près d'une fente (24) de l'anneau (20).
La position dudit au moins un taquet (302, 304, 306) sur ledit anneau de rétention (20) est telle que, lorsque ledit anneau de rétention (20) est en place dans une gorge (22) située sur le disque de rotor (10), ledit au moins un taquet (302, 304, 306) est en butée contre ledit premier crochet d'immobilisation (162, 262), et la fente (24) est recouverte par ledit deuxième crochet d'immobilisation (164, 264).
EP06119579A 2005-08-31 2006-08-25 Dispositif d`immobilisation d`un anneau de rétention axiale d`une aube Active EP1760258B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0552635A FR2890104A1 (fr) 2005-08-31 2005-08-31 Dispositif d'immobilisation d'un anneau de retention axiale d'une aube, disque de rotor et anneau de retention associes et rotor et moteur d'aeronef les comportant

Publications (3)

Publication Number Publication Date
EP1760258A2 EP1760258A2 (fr) 2007-03-07
EP1760258A3 true EP1760258A3 (fr) 2007-08-01
EP1760258B1 EP1760258B1 (fr) 2008-10-15

Family

ID=36440914

Family Applications (1)

Application Number Title Priority Date Filing Date
EP06119579A Active EP1760258B1 (fr) 2005-08-31 2006-08-25 Dispositif d`immobilisation d`un anneau de rétention axiale d`une aube

Country Status (5)

Country Link
US (1) US7290988B2 (fr)
EP (1) EP1760258B1 (fr)
CA (1) CA2557765C (fr)
DE (1) DE602006003155D1 (fr)
FR (1) FR2890104A1 (fr)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2890105A1 (fr) * 2005-08-31 2007-03-02 Snecma Dispositif d'immobilisation d'un anneau de retention axiale d'une aube, disque de rotor et anneau de retention associes et rotor et motor d'aeronef les comportant
US20090264785A1 (en) * 2008-04-18 2009-10-22 Brainscope Company, Inc. Method and Apparatus For Assessing Brain Function Using Diffusion Geometric Analysis
FR2930603B1 (fr) * 2008-04-24 2010-04-30 Snecma Dispositif de retention axiale d'aubes mobiles sur un disque de rotor
FR2951224B1 (fr) * 2009-10-13 2011-12-09 Turbomeca Roue de turbine equipee d'un jonc de retenue axiale verrouillant des pales par rapport a un disque
FR2955904B1 (fr) * 2010-02-04 2012-07-20 Snecma Soufflante de turbomachine
FR2974142B1 (fr) * 2011-04-14 2013-05-24 Snecma Dispositif d'immobilisation en rotation d'un anneau de retention d'aubes
US9476310B2 (en) * 2012-10-18 2016-10-25 General Electric Company Systems and methods to axially retain blades
FR3000763B1 (fr) * 2013-01-04 2016-07-15 Snecma Disque de rotor muni d’une pluralite de crochets
US9790803B2 (en) * 2013-03-08 2017-10-17 United Technologies Corporation Double split blade lock ring
EP2971693B1 (fr) * 2013-03-14 2017-09-27 United Technologies Corporation Dispositif d'étanchéité de disque de rotor de turbine à gaz
FR3029962B1 (fr) * 2014-12-11 2019-08-23 Safran Aircraft Engines Blocage axial des aubes dans une roue de turbomachine
US10125619B2 (en) 2015-11-19 2018-11-13 General Electric Company Rotor assembly for use in a turbofan engine and method of assembling
US10145249B2 (en) * 2016-02-23 2018-12-04 Mechanical Dynamics & Analysis Llc Turbine bucket lockwire anti-rotation device for gas turbine engine
JP7213835B2 (ja) * 2020-02-10 2023-01-27 三菱重工業株式会社 タービンホイール

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4221542A (en) * 1977-12-27 1980-09-09 General Electric Company Segmented blade retainer
US5320492A (en) * 1992-07-22 1994-06-14 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Sealing and retaining device for a rotor notched with pin settings receiving blade roots
FR2729709A1 (fr) * 1995-01-25 1996-07-26 Snecma Dispositif d'etancheite et de retention des aubes de rotor de turbomachine
US6234756B1 (en) * 1998-10-26 2001-05-22 Allison Advanced Development Company Segmented ring blade retainer
EP1443179A2 (fr) * 2003-01-30 2004-08-04 ROLLS-ROYCE plc Rotor et sa plaque de maintien

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4033705A (en) * 1976-04-26 1977-07-05 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Blade retainer assembly
FR2603333B1 (fr) * 1986-09-03 1990-07-20 Snecma Rotor de turbomachine comportant un moyen de verrouillage axial et d'etancheite d'aubes montees dans des brochages axiaux du disque et procede de montage

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4221542A (en) * 1977-12-27 1980-09-09 General Electric Company Segmented blade retainer
US5320492A (en) * 1992-07-22 1994-06-14 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Sealing and retaining device for a rotor notched with pin settings receiving blade roots
FR2729709A1 (fr) * 1995-01-25 1996-07-26 Snecma Dispositif d'etancheite et de retention des aubes de rotor de turbomachine
US6234756B1 (en) * 1998-10-26 2001-05-22 Allison Advanced Development Company Segmented ring blade retainer
EP1443179A2 (fr) * 2003-01-30 2004-08-04 ROLLS-ROYCE plc Rotor et sa plaque de maintien

Also Published As

Publication number Publication date
US20070048141A1 (en) 2007-03-01
US7290988B2 (en) 2007-11-06
CA2557765C (fr) 2013-07-02
CA2557765A1 (fr) 2007-02-28
FR2890104A1 (fr) 2007-03-02
EP1760258A2 (fr) 2007-03-07
DE602006003155D1 (de) 2008-11-27
EP1760258B1 (fr) 2008-10-15

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