FR3096733B1 - Ensemble pour turbomachine - Google Patents

Ensemble pour turbomachine Download PDF

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Publication number
FR3096733B1
FR3096733B1 FR1905755A FR1905755A FR3096733B1 FR 3096733 B1 FR3096733 B1 FR 3096733B1 FR 1905755 A FR1905755 A FR 1905755A FR 1905755 A FR1905755 A FR 1905755A FR 3096733 B1 FR3096733 B1 FR 3096733B1
Authority
FR
France
Prior art keywords
rotor
bearing
angular sector
longitudinal axis
turbomachine
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
FR1905755A
Other languages
English (en)
Other versions
FR3096733A1 (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 FR1905755A priority Critical patent/FR3096733B1/fr
Priority to US17/614,226 priority patent/US11828191B2/en
Priority to PCT/EP2020/064645 priority patent/WO2020239803A1/fr
Priority to CN202080047903.9A priority patent/CN114080490A/zh
Priority to EP20732122.5A priority patent/EP3976929A1/fr
Publication of FR3096733A1 publication Critical patent/FR3096733A1/fr
Application granted granted Critical
Publication of FR3096733B1 publication Critical patent/FR3096733B1/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
    • F01D5/12—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
    • 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
    • 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
    • F05D2230/00—Manufacture
    • F05D2230/20—Manufacture essentially without removing material
    • F05D2230/23—Manufacture essentially without removing material by permanently joining parts together
    • 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
    • F05D2240/00—Components
    • F05D2240/80—Platforms for stationary or moving blades

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 présente invention concerne un ensemble pour turbomachine comprenant :- un premier rotor comprenant :○ un disque (120), et○ une pluralité d’aubes (122) susceptibles de battre par rapport au disque (120),- un deuxième rotor (140), et- un amortisseur (2) configuré pour amortir un déplacement du premier rotor par rapport au deuxième rotor (140), dans un plan orthogonal à l’axe longitudinal, l’amortisseur (2) comprenant :○ une première partie d’appui (21) venant en appui sur le premier rotor en une première zone d’appui s’étendant sur un premier secteur angulaire autour de l’axe longitudinal,○ une deuxième partie d’appui (22) venant en appui sur le premier rotor en une deuxième zone d’appui, différente de la première zone d’appui, la deuxième zone d’appui s’étendant sur un deuxième secteur angulaire autour de l’axe longitudinal, le deuxième secteur angulaire étant inférieur au premier secteur angulaire. Figure pour l’abrégé : Fig. 3
FR1905755A 2019-05-29 2019-05-29 Ensemble pour turbomachine Active FR3096733B1 (fr)

Priority Applications (5)

Application Number Priority Date Filing Date Title
FR1905755A FR3096733B1 (fr) 2019-05-29 2019-05-29 Ensemble pour turbomachine
US17/614,226 US11828191B2 (en) 2019-05-29 2020-05-27 Assembly for turbomachine
PCT/EP2020/064645 WO2020239803A1 (fr) 2019-05-29 2020-05-27 Ensemble pour turbomachine
CN202080047903.9A CN114080490A (zh) 2019-05-29 2020-05-27 用于涡轮机的组件
EP20732122.5A EP3976929A1 (fr) 2019-05-29 2020-05-27 Ensemble pour turbomachine

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1905755A FR3096733B1 (fr) 2019-05-29 2019-05-29 Ensemble pour turbomachine
FR1905755 2019-05-29

Publications (2)

Publication Number Publication Date
FR3096733A1 FR3096733A1 (fr) 2020-12-04
FR3096733B1 true FR3096733B1 (fr) 2022-11-18

Family

ID=68072686

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1905755A Active FR3096733B1 (fr) 2019-05-29 2019-05-29 Ensemble pour turbomachine

Country Status (1)

Country Link
FR (1) FR3096733B1 (fr)

Family Cites Families (6)

* 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

Also Published As

Publication number Publication date
FR3096733A1 (fr) 2020-12-04

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