FR2888621B1 - Dispositif de retention d'un support de palier dans une turbomachine comportant un dispositif de decouplage - Google Patents

Dispositif de retention d'un support de palier dans une turbomachine comportant un dispositif de decouplage

Info

Publication number
FR2888621B1
FR2888621B1 FR0552219A FR0552219A FR2888621B1 FR 2888621 B1 FR2888621 B1 FR 2888621B1 FR 0552219 A FR0552219 A FR 0552219A FR 0552219 A FR0552219 A FR 0552219A FR 2888621 B1 FR2888621 B1 FR 2888621B1
Authority
FR
France
Prior art keywords
turbomachine
retention
bearing support
decoupling
decoupling 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
FR0552219A
Other languages
English (en)
Other versions
FR2888621A1 (fr
Inventor
Michel Brault
Patrick Morel
Monique Thore
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
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
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 Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA, SNECMA SAS filed Critical Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Priority to FR0552219A priority Critical patent/FR2888621B1/fr
Publication of FR2888621A1 publication Critical patent/FR2888621A1/fr
Application granted granted Critical
Publication of FR2888621B1 publication Critical patent/FR2888621B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • F04D29/05—Shafts or bearings, or assemblies thereof, specially adapted for elastic fluid pumps
    • F04D29/056—Bearings
    • F04D29/059—Roller bearings
    • 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
    • F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
    • F01D21/04—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position
    • F01D21/045—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position special arrangements in stators or in rotors dealing with breaking-off of part of 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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/16—Arrangement of bearings; Supporting or mounting bearings in casings
    • F01D25/162—Bearing supports
    • 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
    • F04D27/02—Surge control
    • F04D27/0292—Stop safety or alarm devices, e.g. stop-and-go control; Disposition of check-valves
    • 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
    • F04D29/05—Shafts or bearings, or assemblies thereof, specially adapted for elastic fluid pumps
    • F04D29/056—Bearings
    • F04D29/0563—Bearings cartridges
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2260/00—Function
    • F05B2260/30—Retaining components in desired mutual position
    • F05B2260/301—Retaining bolts or nuts
    • F05B2260/3011—Retaining bolts or nuts of the frangible or shear type
    • 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
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/36—Application in turbines specially adapted for the fan of turbofan engines
    • 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
    • F05D2260/00—Function
    • F05D2260/30—Retaining 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)
FR0552219A 2005-07-15 2005-07-15 Dispositif de retention d'un support de palier dans une turbomachine comportant un dispositif de decouplage Active FR2888621B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR0552219A FR2888621B1 (fr) 2005-07-15 2005-07-15 Dispositif de retention d'un support de palier dans une turbomachine comportant un dispositif de decouplage

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0552219A FR2888621B1 (fr) 2005-07-15 2005-07-15 Dispositif de retention d'un support de palier dans une turbomachine comportant un dispositif de decouplage

Publications (2)

Publication Number Publication Date
FR2888621A1 FR2888621A1 (fr) 2007-01-19
FR2888621B1 true FR2888621B1 (fr) 2007-10-05

Family

ID=36284030

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0552219A Active FR2888621B1 (fr) 2005-07-15 2005-07-15 Dispositif de retention d'un support de palier dans une turbomachine comportant un dispositif de decouplage

Country Status (1)

Country Link
FR (1) FR2888621B1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2478800C2 (ru) * 2008-01-23 2013-04-10 Снекма Направляющий элемент вала в турбомашине

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2925122B1 (fr) * 2007-12-14 2015-09-04 Snecma Dispositif de decouplage d'un support de palier
GB2459646B (en) * 2008-04-28 2011-03-30 Rolls Royce Plc A fan assembly
FR2960026B1 (fr) * 2010-05-11 2014-05-16 Snecma Turboreacteur a montage frangible et moyen de retenue axiale de la soufflante
FR2960907B1 (fr) 2010-06-02 2012-07-27 Snecma Palier de roulement pour turboreacteur d'aeronef equipe de moyens ameliores de retention axiale de sa bague exterieure
FR2965298B1 (fr) * 2010-09-28 2012-09-28 Snecma Moteur a turbine a gaz comprenant des moyens de retention axiale d'une soufflante dudit moteur
FR2966208B1 (fr) 2010-10-13 2012-12-28 Snecma Boitier de liaison entre un arbre d'entrainement de soufflante de moteur et un palier de roulement
FR2976623B1 (fr) * 2011-06-20 2013-06-28 Snecma Dispositif de decouplage pour turbomoteur a double flux
US10197102B2 (en) 2016-10-21 2019-02-05 General Electric Company Load reduction assemblies for a gas turbine engine
FR3066534B1 (fr) * 2017-05-22 2020-01-10 Safran Aircraft Engines Ensemble pour turbomachine d'aeronef presentant un systeme de decouplage ameliore en cas de perte d'aube de soufflante
JP7032279B2 (ja) * 2018-10-04 2022-03-08 本田技研工業株式会社 ガスタービンエンジン
RU2729579C1 (ru) * 2019-04-24 2020-08-11 Публичное акционерное общество "ОДК-Уфимское моторостроительное производственное объединение" Передняя опора ротора компрессора
US11420755B2 (en) 2019-08-08 2022-08-23 General Electric Company Shape memory alloy isolator for a gas turbine engine
US11105223B2 (en) 2019-08-08 2021-08-31 General Electric Company Shape memory alloy reinforced casing
RU2730565C1 (ru) * 2019-09-24 2020-08-24 Публичное акционерное общество "ОДК-Уфимское моторостроительное производственное объединение" Двухконтурный турбореактивный двигатель
US11274557B2 (en) 2019-11-27 2022-03-15 General Electric Company Damper assemblies for rotating drum rotors of gas turbine engines
US11280219B2 (en) 2019-11-27 2022-03-22 General Electric Company Rotor support structures for rotating drum rotors of gas turbine engines
US11828235B2 (en) 2020-12-08 2023-11-28 General Electric Company Gearbox for a gas turbine engine utilizing shape memory alloy dampers

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2749883B1 (fr) * 1996-06-13 1998-07-31 Snecma Procede et support de palier permettant de maintenir en fonctionnement un turbomoteur pour aeronef apres apparition d'un balourd accidentel sur un rotor
FR2752024B1 (fr) * 1996-08-01 1998-09-04 Snecma Support d'arbre cassant a l'apparition d'un balourd
GB2320526B (en) * 1996-12-20 2000-09-20 Rolls Royce Plc Ducted fan gas turbine engine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2478800C2 (ru) * 2008-01-23 2013-04-10 Снекма Направляющий элемент вала в турбомашине

Also Published As

Publication number Publication date
FR2888621A1 (fr) 2007-01-19

Similar Documents

Publication Publication Date Title
FR2888621B1 (fr) Dispositif de retention d'un support de palier dans une turbomachine comportant un dispositif de decouplage
FR2868808B1 (fr) Dispositif de retenue axiale d'aubes sur un disque de rotor d'une turbomachine
FR2865012B1 (fr) Dispositif d'etancheite pour turbine haute-pression de turbomachine
FR2900133B1 (fr) Dispositif et ensemble de maintien pour balai d'essuie glace
FR2925118B1 (fr) Panneau de support d'abradable dans une turbomachine
FR2885196B1 (fr) Dispositif d'equilibrage d'un rotor de turbomachine
DE602005018568D1 (de) Bildschirmhalterungsvorrichtung
FR2887931B1 (fr) Dispositif de support et de logement de servitudes dans un turboreacteur a double flux
FR2893367B1 (fr) Dispositif de securisation d'un insert dans une structure
FR2868814B1 (fr) Dispositif d'assemblage de brides annulaires, en particulier dans une turbomachine
FR2877721B1 (fr) Dispositif de representation cartographique des vitesses verticales minimales
FR2899636B1 (fr) Dispositif de retention axiale d'un flasque de disque de rotor de turbomachine
FR2888876B1 (fr) Dispositif d'amortissement des vibrations d'un rotor dans une turbomachine
FR2883700B1 (fr) Dispositif d'accrochage d'une cage de conchyliculture, notamment d'ostreiculture, a un support essentiellement tubulaire
FR2925122B1 (fr) Dispositif de decouplage d'un support de palier
FR2907840B1 (fr) Dispositif de limitation de survitesse de turbine dans une turbomachine
FR2877036B1 (fr) Dispositif de lubrification d'un composant dans une turbomachine
FR2897124B1 (fr) Dispositif d'immobilisation en rotation d'un ecrou a sertir
FR2937679B1 (fr) Dispositif de prelevement d'air de refroidissement dans une turbomachine
FR2933128B1 (fr) Dispositif de prelevement d'air de refroidissement dans une turbomachine
FR2924991B1 (fr) Dispositif d'appui de voyageurs
FR2905823B1 (fr) Dispositif pour l'accrochage de poches de conchyliculture a un support, et ensemble d'accrochage correspondant.
FR2906784B1 (fr) Dispositif de support d'une personne sur une bicyclette.
FR2919056B1 (fr) Dispositif de support d'echantillons metalliques
FR2916793B1 (fr) Patte pour la fixation d'une joue support et dispositif de fixation d'une joue sur une telle patte de fixation.

Legal Events

Date Code Title Description
PLFP Fee payment

Year of fee payment: 11

PLFP Fee payment

Year of fee payment: 12

PLFP Fee payment

Year of fee payment: 13

CD Change of name or company name

Owner name: SAFRAN AIRCRAFT ENGINES, FR

Effective date: 20170717

PLFP Fee payment

Year of fee payment: 14

PLFP Fee payment

Year of fee payment: 15

PLFP Fee payment

Year of fee payment: 16

PLFP Fee payment

Year of fee payment: 17

PLFP Fee payment

Year of fee payment: 18

PLFP Fee payment

Year of fee payment: 19

PLFP Fee payment

Year of fee payment: 20