FR3096729B1 - Ensemble pour turbomachine - Google Patents

Ensemble pour turbomachine Download PDF

Info

Publication number
FR3096729B1
FR3096729B1 FR1905733A FR1905733A FR3096729B1 FR 3096729 B1 FR3096729 B1 FR 3096729B1 FR 1905733 A FR1905733 A FR 1905733A FR 1905733 A FR1905733 A FR 1905733A FR 3096729 B1 FR3096729 B1 FR 3096729B1
Authority
FR
France
Prior art keywords
angular sector
rotor
bearing
turbomachine assembly
bearing part
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
FR1905733A
Other languages
English (en)
Other versions
FR3096729A1 (fr
Inventor
Philippe Gérard Edmond Joly
Romain Nicolas Lagarde
Jean-Marc Claude Perrollaz
Laurent Jablonski
François Jean Comin
Jaeghere Edouard Antoine Dominique Marie De
Charles Jean-Pierre Douguet
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
Safran Aircraft Engines 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 Safran Aircraft Engines SAS filed Critical Safran Aircraft Engines SAS
Priority to FR1905733A priority Critical patent/FR3096729B1/fr
Priority to US17/614,226 priority patent/US11828191B2/en
Priority to CN202080047903.9A priority patent/CN114080490A/zh
Priority to PCT/EP2020/064645 priority patent/WO2020239803A1/fr
Priority to EP20732122.5A priority patent/EP3976929A1/fr
Publication of FR3096729A1 publication Critical patent/FR3096729A1/fr
Application granted granted Critical
Publication of FR3096729B1 publication Critical patent/FR3096729B1/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
    • F04D29/66—Combating cavitation, whirls, noise, vibration or the like; Balancing
    • F04D29/661—Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps
    • F04D29/668—Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps damping or preventing mechanical vibrations
    • 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
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/16—Form or construction for counteracting blade vibration
    • 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
    • F01D5/12—Blades
    • F01D5/22—Blade-to-blade connections, e.g. for damping vibrations
    • 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
    • F01D5/12—Blades
    • F01D5/26—Antivibration means not restricted to blade form or construction or to blade-to-blade connections or to the use of particular materials
    • 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
    • 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
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/36—Application in turbines specially adapted for the fan of turbofan engines

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Support Of The Bearing (AREA)

Abstract

La présente invention concerne un ensemble pour turbomachine comprenant un amortisseur (2) configuré pour amortir un déplacement d’un premier rotor par rapport à un deuxième rotor, l’amortisseur (2) comprenant :- une première partie d’appui (21) venant en appui sur le premier rotor sur un premier secteur angulaire (A1),- une deuxième partie d’appui (22) venant en appui sur le premier rotor sur un deuxième secteur angulaire (A2), le deuxième secteur angulaire (A2) étant inférieur au premier secteur angulaire (A1), et- une troisième partie d’appui (23) venant en appui sur le premier rotor sur un troisième secteur angulaire (A3), le troisième secteur angulaire (A3) étant inférieur au premier secteur angulaire (A1). Figure pour l’abrégé : Fig. 3
FR1905733A 2019-05-29 2019-05-29 Ensemble pour turbomachine Active FR3096729B1 (fr)

Priority Applications (5)

Application Number Priority Date Filing Date Title
FR1905733A FR3096729B1 (fr) 2019-05-29 2019-05-29 Ensemble pour turbomachine
US17/614,226 US11828191B2 (en) 2019-05-29 2020-05-27 Assembly for turbomachine
CN202080047903.9A CN114080490A (zh) 2019-05-29 2020-05-27 用于涡轮机的组件
PCT/EP2020/064645 WO2020239803A1 (fr) 2019-05-29 2020-05-27 Ensemble pour turbomachine
EP20732122.5A EP3976929A1 (fr) 2019-05-29 2020-05-27 Ensemble pour turbomachine

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1905733 2019-05-29
FR1905733A FR3096729B1 (fr) 2019-05-29 2019-05-29 Ensemble pour turbomachine

Publications (2)

Publication Number Publication Date
FR3096729A1 FR3096729A1 (fr) 2020-12-04
FR3096729B1 true FR3096729B1 (fr) 2021-04-30

Family

ID=68072682

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1905733A Active FR3096729B1 (fr) 2019-05-29 2019-05-29 Ensemble pour turbomachine

Country Status (1)

Country Link
FR (1) FR3096729B1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US12012857B2 (en) 2022-10-14 2024-06-18 Rtx Corporation Platform for an airfoil of a gas turbine engine

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5820346A (en) * 1996-12-17 1998-10-13 General Electric Company Blade damper for a turbine engine
FR2915510B1 (fr) 2007-04-27 2009-11-06 Snecma Sa Amortisseur pour aubes de turbomachines
FR2923557B1 (fr) 2007-11-12 2010-01-22 Snecma Ensemble d'une aube de soufflante et de son amortisseur, amortisseur d'aube de soufflante et methode de calibrage de l'amortisseur
FR2949142B1 (fr) 2009-08-11 2011-10-14 Snecma Cale amortisseuse de vibrations pour aube de soufflante
FR2970033B1 (fr) * 2011-01-04 2015-10-16 Turbomeca Procede d'amortissement de pale de turbine a gaz et amortisseur de vibration de mise en oeuvre
CN204941612U (zh) * 2015-09-16 2016-01-06 中国航空工业集团公司沈阳发动机设计研究所 一种可压缩阻尼块
FR3047512B1 (fr) * 2016-02-05 2019-11-15 Safran Aircraft Engines Dispositif d'amortissement de vibrations pour aubes de turbomachine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US12012857B2 (en) 2022-10-14 2024-06-18 Rtx Corporation Platform for an airfoil of a gas turbine engine

Also Published As

Publication number Publication date
FR3096729A1 (fr) 2020-12-04

Similar Documents

Publication Publication Date Title
FR3089901B1 (fr) Appui-tête de siège de véhicule muni d’enceintes audio
IL145398A0 (en) Eccentric balanced blisk
UA84680C2 (ru) турбовентиляторный двигатель и опора для распределения служебных магистралей
FR3096729B1 (fr) Ensemble pour turbomachine
TR200201762T2 (tr) B östrojen reseptörü ligandları.
JP2005516143A (ja) ターボ過給器のための固定装置
FR3077327B1 (fr) Ensemble pour turbine de turbomachine comprenant un anneau mobile d'etancheite
WO2006040473A3 (fr) Dispositif de traitement de donnees a definition formelle
FR3096734B1 (fr) Ensemble pour turbomachine
FR3096733B1 (fr) Ensemble pour turbomachine
FR3096731B1 (fr) Ensemble pour turbomachine
FR3076925B1 (fr) Fonction cryptographique
JP2013204591A (ja) 側方支持タービンシェル
FR3098239B1 (fr) Dispositif d’amortissement d’un palier à roulement, comprenant un support rigide traversant une cage souple
FR2894037B1 (fr) Instrument optique comprenant une cavite d'entree dans laquelle est place un miroir
FR3088374B1 (fr) Guignol pour turbomachine
FR3091137B1 (fr) Procédé d’assemblage d’un équipement électrique, notamment d’un onduleur
FR3096730B1 (fr) Ensemble pour turbomachine
FR3066226B1 (fr) Verrouillage anneau stator sous distributeur haute pression
FR3104338B1 (fr) Flasque pour machine électrique tournante
FR3129986B1 (fr) Ensemble pour cone d'ejection de turbomachine d'aeronef
FR3105293B1 (fr) Aube de rotor pour une turbomachine d’aeronef
FR3092779B1 (fr) Outillage amélioré pour le revêtement de léchettes
FR3086154B1 (fr) Dispositif d’aspiration pour aspirateur domestique
JP2017025820A (ja) 蒸気タービンのノズルダイアフラム取り付け構造

Legal Events

Date Code Title Description
PLFP Fee payment

Year of fee payment: 2

PLSC Publication of the preliminary search report

Effective date: 20201204

PLFP Fee payment

Year of fee payment: 3

PLFP Fee payment

Year of fee payment: 4

PLFP Fee payment

Year of fee payment: 5

PLFP Fee payment

Year of fee payment: 6