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FR3089585B1 - Rotor de turbomachine - Google Patents

Rotor de turbomachine Download PDF

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Publication number
FR3089585B1
FR3089585B1 FR1872559A FR1872559A FR3089585B1 FR 3089585 B1 FR3089585 B1 FR 3089585B1 FR 1872559 A FR1872559 A FR 1872559A FR 1872559 A FR1872559 A FR 1872559A FR 3089585 B1 FR3089585 B1 FR 3089585B1
Authority
FR
France
Prior art keywords
threaded
turbomachine rotor
rotor
tapped part
nut
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
FR1872559A
Other languages
English (en)
Other versions
FR3089585A1 (fr
Inventor
Alexandre Auduberteau
Julien Fabrice Girardot
Pierre Chabanne
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 Helicopter Engines SAS
Original Assignee
Safran Helicopter 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 Helicopter Engines SAS filed Critical Safran Helicopter Engines SAS
Priority to FR1872559A priority Critical patent/FR3089585B1/fr
Priority to CN201980085664.3A priority patent/CN113423920B/zh
Priority to US17/311,609 priority patent/US11746657B2/en
Priority to PCT/FR2019/000197 priority patent/WO2020115373A1/fr
Priority to EP19835436.7A priority patent/EP3891362A1/fr
Publication of FR3089585A1 publication Critical patent/FR3089585A1/fr
Application granted granted Critical
Publication of FR3089585B1 publication Critical patent/FR3089585B1/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
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/023—Blade-carrying members, e.g. rotors of the screw type
    • 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
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/026—Shaft to shaft connections
    • 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
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/027—Arrangements for balancing
    • 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
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/10—Anti- vibration means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
    • F16F15/10—Suppression of vibrations in rotating systems by making use of members moving with the system
    • F16F15/14—Suppression of vibrations in rotating systems by making use of members moving with the system using masses freely rotating with the system, i.e. uninvolved in transmitting driveline torque, e.g. rotative dynamic dampers
    • F16F15/1485—Suppression of vibrations in rotating systems by making use of members moving with the system using masses freely rotating with the system, i.e. uninvolved in transmitting driveline torque, e.g. rotative dynamic dampers the rotation being unlimited with respect to driving means
    • F16F15/1492—Suppression of vibrations in rotating systems by making use of members moving with the system using masses freely rotating with the system, i.e. uninvolved in transmitting driveline torque, e.g. rotative dynamic dampers the rotation being unlimited with respect to driving means with a dry-friction connection
    • 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
    • F05D2240/55—Seals
    • 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
    • F05D2240/60—Shafts
    • 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
    • F05D2240/60—Shafts
    • F05D2240/61—Hollow
    • 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
    • F05D2260/96—Preventing, counteracting or reducing vibration or noise
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
    • F16D1/00—Couplings for rigidly connecting two coaxial shafts or other movable machine elements
    • F16D1/06—Couplings for rigidly connecting two coaxial shafts or other movable machine elements for attachment of a member on a shaft or on a shaft-end
    • F16D1/076—Couplings for rigidly connecting two coaxial shafts or other movable machine elements for attachment of a member on a shaft or on a shaft-end by clamping together two faces perpendicular to the axis of rotation, e.g. with bolted flanges
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Acoustics & Sound (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

L’invention concerne un rotor (1) de turbomachine, caractérisé en ce qu’il comporte une partie filetée ou taraudée (3, 6) et un écrou d’amortissement (8) vissé sur la partie filetée ou taraudée (3, 6) de façon à autoriser un frottement des filets de l’écrou (8) et de la partie filetée ou taraudée (3, 6) les uns par rapport aux autres en cas de vibration du rotor (1). Figure à publier avec l’abrégé : [Fig. 1]
FR1872559A 2018-12-07 2018-12-07 Rotor de turbomachine Active FR3089585B1 (fr)

Priority Applications (5)

Application Number Priority Date Filing Date Title
FR1872559A FR3089585B1 (fr) 2018-12-07 2018-12-07 Rotor de turbomachine
CN201980085664.3A CN113423920B (zh) 2018-12-07 2019-12-03 具有阻尼螺母的涡轮机转子
US17/311,609 US11746657B2 (en) 2018-12-07 2019-12-03 Turbomachine rotor
PCT/FR2019/000197 WO2020115373A1 (fr) 2018-12-07 2019-12-03 Rotor de turbomachine avec écrou d'amortissement
EP19835436.7A EP3891362A1 (fr) 2018-12-07 2019-12-03 Rotor de turbomachine avec écrou d'amortissement

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1872559A FR3089585B1 (fr) 2018-12-07 2018-12-07 Rotor de turbomachine

Publications (2)

Publication Number Publication Date
FR3089585A1 FR3089585A1 (fr) 2020-06-12
FR3089585B1 true FR3089585B1 (fr) 2021-09-17

Family

ID=66530181

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1872559A Active FR3089585B1 (fr) 2018-12-07 2018-12-07 Rotor de turbomachine

Country Status (5)

Country Link
US (1) US11746657B2 (fr)
EP (1) EP3891362A1 (fr)
CN (1) CN113423920B (fr)
FR (1) FR3089585B1 (fr)
WO (1) WO2020115373A1 (fr)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US12517843B2 (en) * 2022-01-21 2026-01-06 Synaptics Incorporated Third party applications for a network-capable docking station
US12442303B1 (en) 2024-04-10 2025-10-14 General Electric Company Method of mitigating rotor bow in a turbine engine rotor
US12467365B1 (en) * 2025-01-27 2025-11-11 Pratt & Whitney Canada Corp. In situ balancing mass(es) for aircraft powerplant

Family Cites Families (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2633023B1 (fr) * 1988-06-15 1992-11-27 Snecma Dispositif et procede d'accouplement d'un arbre de turbine sur un tourillon
US4973221A (en) * 1989-04-17 1990-11-27 General Electric Company Gas turbine engine motor assembly
US5205189A (en) * 1990-12-17 1993-04-27 General Electric Company Engine shaft balance assembly
US5537814A (en) * 1994-09-28 1996-07-23 General Electric Company High pressure gas generator rotor tie rod system for gas turbine engine
US5931051A (en) * 1996-02-16 1999-08-03 Ott; Vern D. Vibration dampener for a rotating shaft
US6024615A (en) * 1998-07-22 2000-02-15 Brunswick Corporation Vibration absorbing apparatus for a rotating system
US6747378B2 (en) * 2001-08-20 2004-06-08 Beacon Power Corporation Dual stiffness bearing damping system
DE10239941A1 (de) * 2002-03-05 2003-04-03 Abb Turbo Systems Ag Baden Torsionsschwingungsdämpfer für einen Turbolader
US7510380B2 (en) * 2004-07-13 2009-03-31 Honeywell International Inc. Non-parallel spacer for improved rotor group balance
US20070022735A1 (en) * 2005-07-29 2007-02-01 General Electric Company Pto assembly for a gas turbine engine
JP4985026B2 (ja) * 2007-03-28 2012-07-25 株式会社デンソー 緩衝装置
GB2463453B (en) * 2008-09-06 2012-08-08 Cummins Turbo Tech Ltd Turbomachine
FR2949138B1 (fr) * 2009-08-13 2012-03-16 Snecma Turbomachine comportant des moyens d'anti-rotation d'un ecrou de palier
FR2963062B1 (fr) * 2010-07-20 2012-08-31 Snecma Assemblage entre un tourillon d'arbre de compresseur et un pignon conique pour l'entrainement d'un boitier d'accessoires d'une turbomachine
FR2979681B1 (fr) 2011-09-05 2014-05-16 Snecma Turbomachine comportant un film fluide d'amortissement d'un palier de guidage d'un arbre de turbomachine et procede de reglage de l'epaisseur d'un tel film fluide d'amortissement
US8979502B2 (en) * 2011-12-15 2015-03-17 Pratt & Whitney Canada Corp. Turbine rotor retaining system
US9140133B2 (en) * 2012-08-14 2015-09-22 United Technologies Corporation Threaded full ring inner air-seal
WO2015084467A2 (fr) * 2013-09-19 2015-06-11 Obermeyer Henry K Fixation de rotor de machine hydromotrice
EP2860405B1 (fr) * 2013-10-14 2016-05-25 Techspace Aero S.A. Système amortisseur piézoélectrique pour rotor de turbomachine axiale
DE102014001061A1 (de) * 2014-01-28 2015-07-30 Lucas Automotive Gmbh Scheibenbremse umfassend eine Schwingungsdämpfungseinrichtung mit einer Zusatzmasse und Bausatz mit einer derartigen Scheibenbremse
FR3033890B1 (fr) * 2015-03-20 2019-08-23 Safran Aircraft Engines Fixation d'un disque fan a un arbre d'entrainement
US10883424B2 (en) * 2016-07-19 2021-01-05 Pratt & Whitney Canada Corp. Multi-spool gas turbine engine architecture

Also Published As

Publication number Publication date
US20220034228A1 (en) 2022-02-03
WO2020115373A1 (fr) 2020-06-11
EP3891362A1 (fr) 2021-10-13
US11746657B2 (en) 2023-09-05
CN113423920A (zh) 2021-09-21
CN113423920B (zh) 2023-08-11
FR3089585A1 (fr) 2020-06-12

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