PL2661542T3 - Wirnik turbiny gazowej z tłumikiem drgań - Google Patents

Wirnik turbiny gazowej z tłumikiem drgań

Info

Publication number
PL2661542T3
PL2661542T3 PL11817404T PL11817404T PL2661542T3 PL 2661542 T3 PL2661542 T3 PL 2661542T3 PL 11817404 T PL11817404 T PL 11817404T PL 11817404 T PL11817404 T PL 11817404T PL 2661542 T3 PL2661542 T3 PL 2661542T3
Authority
PL
Poland
Prior art keywords
gas
vibration damper
turbine rotor
rotor disk
disk
Prior art date
Application number
PL11817404T
Other languages
English (en)
Inventor
Jean-Luc Pierre Sahores
Michel François Léon Beaucoueste
Original Assignee
Safran Helicopter Engines
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 filed Critical Safran Helicopter Engines
Publication of PL2661542T3 publication Critical patent/PL2661542T3/pl

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
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/04Antivibration arrangements
    • F01D25/06Antivibration arrangements for preventing blade vibration
    • 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
    • F01D5/12Blades
    • F01D5/22Blade-to-blade connections, e.g. for damping vibrations
    • 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
    • F01D11/00Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • 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
    • F01D11/00Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/005Sealing means between non relatively rotating elements
    • F01D11/006Sealing the gap between rotor blades or blades and rotor
    • F01D11/008Sealing the gap between rotor blades or blades and rotor by spacer elements between the blades, e.g. independent interblade platforms
    • 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
    • F01D5/12Blades
    • F01D5/26Antivibration means not restricted to blade form or construction or to blade-to-blade connections or to the use of particular materials
    • 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
    • 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
    • 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
    • F05D2260/96Preventing, counteracting or reducing vibration or noise
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

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)
PL11817404T 2011-01-04 2011-12-20 Wirnik turbiny gazowej z tłumikiem drgań PL2661542T3 (pl)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1150042A FR2970033B1 (fr) 2011-01-04 2011-01-04 Procede d'amortissement de pale de turbine a gaz et amortisseur de vibration de mise en oeuvre
PCT/FR2011/053067 WO2012093217A1 (fr) 2011-01-04 2011-12-20 Procede d'amortissement de pale de turbine a gaz et amortisseur de vibration de mise en œuvre
EP11817404.4A EP2661542B1 (fr) 2011-01-04 2011-12-20 Roue de turbine a gaz avec amortisseur de vibration

Publications (1)

Publication Number Publication Date
PL2661542T3 true PL2661542T3 (pl) 2020-08-24

Family

ID=44243379

Family Applications (1)

Application Number Title Priority Date Filing Date
PL11817404T PL2661542T3 (pl) 2011-01-04 2011-12-20 Wirnik turbiny gazowej z tłumikiem drgań

Country Status (10)

Country Link
US (1) US10138756B2 (pl)
EP (1) EP2661542B1 (pl)
JP (1) JP6113663B2 (pl)
KR (1) KR101857314B1 (pl)
CN (1) CN103282604B (pl)
CA (1) CA2823504C (pl)
FR (1) FR2970033B1 (pl)
PL (1) PL2661542T3 (pl)
RU (1) RU2609125C2 (pl)
WO (1) WO2012093217A1 (pl)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB201322668D0 (en) 2013-12-20 2014-02-05 Rolls Royce Deutschland & Co Kg Vibration Damper
EP2924245B1 (en) * 2014-03-24 2017-03-01 General Electric Technology GmbH Steam turbine with resonance chamber
EP3724453A1 (fr) 2017-12-12 2020-10-21 Safran Helicopter Engines Amortisseur de vibrations pour une aube de rotor de turbomachine
US11828191B2 (en) 2019-05-29 2023-11-28 Safran Aircraft Engines Assembly for turbomachine
FR3096733B1 (fr) * 2019-05-29 2022-11-18 Safran Aircraft Engines Ensemble pour turbomachine
FR3096730B1 (fr) * 2019-05-29 2021-04-30 Safran Aircraft Engines Ensemble pour turbomachine
FR3096729B1 (fr) * 2019-05-29 2021-04-30 Safran Aircraft Engines Ensemble pour turbomachine
CN111677589B (zh) * 2020-06-10 2024-07-19 中国船舶重工集团公司第七0三研究所 复合弹性悬臂式燃气轮机涡轮支撑环减振抗冲组件

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2999631A (en) * 1958-09-05 1961-09-12 Gen Electric Dual airfoil
US3037741A (en) * 1958-12-29 1962-06-05 Gen Electric Damping turbine buckets
SU435360A1 (ru) * 1972-06-13 1974-07-05 В. Э. Гохберг, В. Д. Шалаев , В. Н. Шеповалов Устройство для демпфирования колебаний рабочих лопаток турбомашины
GB1549152A (en) 1977-01-11 1979-08-01 Rolls Royce Rotor stage for a gas trubine engine
FR2503247B1 (fr) * 1981-04-07 1985-06-14 Snecma Perfectionnements aux etages de turbine a gaz de turboreacteurs munis de moyens de refroidissement par air du disque de la roue de la turbine
EP0437977A1 (en) * 1990-01-18 1991-07-24 United Technologies Corporation Turbine rim configuration
JPH0618602U (ja) * 1992-08-10 1994-03-11 石川島播磨重工業株式会社 タービン動翼のダンパー
FR2726323B1 (fr) * 1994-10-26 1996-12-13 Snecma Ensemble d'un disque rotatif et d'aubes, notamment utilise dans une turbomachine
US5573375A (en) * 1994-12-14 1996-11-12 United Technologies Corporation Turbine engine rotor blade platform sealing and vibration damping device
US5513955A (en) * 1994-12-14 1996-05-07 United Technologies Corporation Turbine engine rotor blade platform seal
US5827047A (en) * 1996-06-27 1998-10-27 United Technologies Corporation Turbine blade damper and seal
US6171058B1 (en) * 1999-04-01 2001-01-09 General Electric Company Self retaining blade damper
US6851932B2 (en) * 2003-05-13 2005-02-08 General Electric Company Vibration damper assembly for the buckets of a turbine
US6932575B2 (en) * 2003-10-08 2005-08-23 United Technologies Corporation Blade damper
US7121800B2 (en) * 2004-09-13 2006-10-17 United Technologies Corporation Turbine blade nested seal damper assembly
US8011892B2 (en) 2007-06-28 2011-09-06 United Technologies Corporation Turbine blade nested seal and damper assembly
CN101131093A (zh) * 2007-09-25 2008-02-27 西安交通大学 高炉煤气透平叶片的叶根平台阻尼结构

Also Published As

Publication number Publication date
US10138756B2 (en) 2018-11-27
KR101857314B1 (ko) 2018-05-11
JP2014502693A (ja) 2014-02-03
CN103282604B (zh) 2016-01-06
CA2823504A1 (fr) 2012-07-12
CN103282604A (zh) 2013-09-04
FR2970033A1 (fr) 2012-07-06
WO2012093217A1 (fr) 2012-07-12
EP2661542A1 (fr) 2013-11-13
KR20130135889A (ko) 2013-12-11
FR2970033B1 (fr) 2015-10-16
CA2823504C (fr) 2018-12-04
RU2013136190A (ru) 2015-02-10
US20130280068A1 (en) 2013-10-24
EP2661542B1 (fr) 2020-06-03
JP6113663B2 (ja) 2017-04-12
RU2609125C2 (ru) 2017-01-30

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