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FR2953555B1 - Ensemble d'un jonc de retenue et d'un flasque de maintien dudit jonc - Google Patents

Ensemble d'un jonc de retenue et d'un flasque de maintien dudit jonc

Info

Publication number
FR2953555B1
FR2953555B1 FR0958718A FR0958718A FR2953555B1 FR 2953555 B1 FR2953555 B1 FR 2953555B1 FR 0958718 A FR0958718 A FR 0958718A FR 0958718 A FR0958718 A FR 0958718A FR 2953555 B1 FR2953555 B1 FR 2953555B1
Authority
FR
France
Prior art keywords
job
assembly
retaining ring
holding flange
flange
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
FR0958718A
Other languages
English (en)
Other versions
FR2953555A1 (fr
Inventor
Olivier Belmonte
Gregory Nicolas Gerald Gillant
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 FR0958718A priority Critical patent/FR2953555B1/fr
Priority to GB1208894.4A priority patent/GB2487696B/en
Priority to US13/513,227 priority patent/US9284847B2/en
Priority to PCT/EP2010/068927 priority patent/WO2011069940A1/fr
Publication of FR2953555A1 publication Critical patent/FR2953555A1/fr
Application granted granted Critical
Publication of FR2953555B1 publication Critical patent/FR2953555B1/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
    • 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
    • F05D2260/00Function
    • F05D2260/30Retaining components in desired mutual position

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR0958718A 2009-12-07 2009-12-07 Ensemble d'un jonc de retenue et d'un flasque de maintien dudit jonc Active FR2953555B1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR0958718A FR2953555B1 (fr) 2009-12-07 2009-12-07 Ensemble d'un jonc de retenue et d'un flasque de maintien dudit jonc
GB1208894.4A GB2487696B (en) 2009-12-07 2010-12-06 Retaining ring assembly for a turbine blade
US13/513,227 US9284847B2 (en) 2009-12-07 2010-12-06 Retaining ring assembly and supporting flange for said ring
PCT/EP2010/068927 WO2011069940A1 (fr) 2009-12-07 2010-12-06 Ensemble d'un jonc de retenue et d'un flasque de maintien dudit jonc

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0958718A FR2953555B1 (fr) 2009-12-07 2009-12-07 Ensemble d'un jonc de retenue et d'un flasque de maintien dudit jonc

Publications (2)

Publication Number Publication Date
FR2953555A1 FR2953555A1 (fr) 2011-06-10
FR2953555B1 true FR2953555B1 (fr) 2012-04-06

Family

ID=42272529

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0958718A Active FR2953555B1 (fr) 2009-12-07 2009-12-07 Ensemble d'un jonc de retenue et d'un flasque de maintien dudit jonc

Country Status (4)

Country Link
US (1) US9284847B2 (fr)
FR (1) FR2953555B1 (fr)
GB (1) GB2487696B (fr)
WO (1) WO2011069940A1 (fr)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2953555B1 (fr) * 2009-12-07 2012-04-06 Snecma Ensemble d'un jonc de retenue et d'un flasque de maintien dudit jonc
FR2978793B1 (fr) * 2011-08-03 2015-12-04 Snecma Rotor de turbine pour une turbomachine
EP3073052B1 (fr) 2015-02-17 2018-01-24 Rolls-Royce Corporation Ensemble de soufflant
US11085309B2 (en) * 2017-09-22 2021-08-10 General Electric Company Outer drum rotor assembly
US10961853B2 (en) * 2018-07-31 2021-03-30 Pratt & Whitney Canada Corp. Spigot assembly for rotating components
FR3088672B1 (fr) * 2018-11-16 2020-12-18 Safran Aircraft Engines Dispositif pour le centrage et le guidage en rotation d'une piece rotative avec bras entrelaces
GB201903703D0 (en) * 2019-03-19 2019-05-01 Rolls Royce Plc A gas turbine engine bearing support structure
US11428160B2 (en) 2020-12-31 2022-08-30 General Electric Company Gas turbine engine with interdigitated turbine and gear assembly
US12331646B1 (en) 2024-05-13 2025-06-17 Rtx Corporation Air seal for a turbine engine

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2694046B1 (fr) * 1992-07-22 1994-09-23 Snecma Dispositif d'étanchéité et de rétention pour un rotor entaillé de brochages recevant des pieds d'aubes.
US5257909A (en) * 1992-08-17 1993-11-02 General Electric Company Dovetail sealing device for axial dovetail rotor blades
GB2320526B (en) * 1996-12-20 2000-09-20 Rolls Royce Plc Ducted fan gas turbine engine
US5984636A (en) * 1997-12-17 1999-11-16 Pratt & Whitney Canada Inc. Cooling arrangement for turbine rotor
AU2001248281A1 (en) * 2000-04-06 2001-10-23 Pantheco A/S Pharmaceutical composition of modified pna molecules
FR2841933B1 (fr) * 2002-07-04 2004-12-03 Snecma Moteurs Cale autobloquante
US6884028B2 (en) * 2002-09-30 2005-04-26 General Electric Company Turbomachinery blade retention system
GB2410984B (en) * 2004-02-14 2006-03-08 Rolls Royce Plc Securing assembly
FR2918104B1 (fr) * 2007-06-27 2009-10-09 Snecma Sa Dispositif de refroidissement des alveoles d'un disque de rotor de turbomachine a double alimentation en air.
FR2953555B1 (fr) * 2009-12-07 2012-04-06 Snecma Ensemble d'un jonc de retenue et d'un flasque de maintien dudit jonc
FR2959271B1 (fr) * 2010-04-26 2012-09-28 Snecma Element d'interface entre un pied d'une aube et un logement du pied d'aube d'un disque de turbine, rotor de turbine comprenant un element d'interface
FR2967453B1 (fr) * 2010-11-17 2012-12-21 Snecma Disque de retention d'aubes
FR3003494B1 (fr) * 2013-03-19 2015-06-19 Snecma Brut de fonderie pour la realisation d'une aube de rotor de turbomachine et aube de rotor fabriquee a partir de ce brut

Also Published As

Publication number Publication date
GB201208894D0 (en) 2012-07-04
US20120244001A1 (en) 2012-09-27
GB2487696B (en) 2015-12-23
FR2953555A1 (fr) 2011-06-10
GB2487696A (en) 2012-08-01
US9284847B2 (en) 2016-03-15
WO2011069940A1 (fr) 2011-06-16

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