FR2974387B1 - Roue de turbine pour une turbomachine - Google Patents

Roue de turbine pour une turbomachine

Info

Publication number
FR2974387B1
FR2974387B1 FR1153373A FR1153373A FR2974387B1 FR 2974387 B1 FR2974387 B1 FR 2974387B1 FR 1153373 A FR1153373 A FR 1153373A FR 1153373 A FR1153373 A FR 1153373A FR 2974387 B1 FR2974387 B1 FR 2974387B1
Authority
FR
France
Prior art keywords
turbomachine
turbine wheel
turbine
wheel
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
FR1153373A
Other languages
English (en)
Other versions
FR2974387A1 (fr
Inventor
Emmanuel Berche
Jean Luc Bacha
Tangi Brusq
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
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 SNECMA SAS filed Critical SNECMA SAS
Priority to FR1153373A priority Critical patent/FR2974387B1/fr
Priority to GB1206497.8A priority patent/GB2490216B/en
Priority to US13/448,830 priority patent/US8961137B2/en
Publication of FR2974387A1 publication Critical patent/FR2974387A1/fr
Application granted granted Critical
Publication of FR2974387B1 publication Critical patent/FR2974387B1/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
    • F01D5/08—Heating, heat-insulating or cooling means
    • F01D5/081—Cooling fluid being directed on the side of the rotor disc or at the roots of the blades
    • F01D5/082—Cooling fluid being directed on the side of the rotor disc or at the roots of the blades on the side of the rotor disc
    • 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
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/005—Sealing means between non relatively rotating elements
    • 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
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/005—Sealing means between non relatively rotating elements
    • F01D11/006—Sealing the gap between rotor blades or blades and rotor
    • F01D11/008—Sealing the gap between rotor blades or blades and rotor by spacer elements between the blades, e.g. independent interblade platforms
    • 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
    • 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
    • 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
    • F05B2240/00—Components
    • F05B2240/20—Rotors
    • F05B2240/33—Shrouds which are part of or which are rotating with the rotor
    • 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
    • F05D2240/81—Cooled platforms
    • 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
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/201—Heat transfer, e.g. cooling by impingement of a fluid
    • 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
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/221—Improvement of heat transfer
    • F05D2260/2214—Improvement of heat transfer by increasing the heat transfer surface
    • 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
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/221—Improvement of heat transfer
    • F05D2260/2214—Improvement of heat transfer by increasing the heat transfer surface
    • F05D2260/22141—Improvement of heat transfer by increasing the heat transfer surface using fins or ribs
    • 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
    • F05D2260/36—Retaining components in desired mutual position by a form fit connection, e.g. by interlocking
    • 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
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S416/00—Fluid reaction surfaces, i.e. impellers
    • Y10S416/50—Vibration damping features

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR1153373A 2011-04-19 2011-04-19 Roue de turbine pour une turbomachine Active FR2974387B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR1153373A FR2974387B1 (fr) 2011-04-19 2011-04-19 Roue de turbine pour une turbomachine
GB1206497.8A GB2490216B (en) 2011-04-19 2012-04-13 A turbine wheel for a turbine engine
US13/448,830 US8961137B2 (en) 2011-04-19 2012-04-17 Turbine wheel for a turbine engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1153373A FR2974387B1 (fr) 2011-04-19 2011-04-19 Roue de turbine pour une turbomachine

Publications (2)

Publication Number Publication Date
FR2974387A1 FR2974387A1 (fr) 2012-10-26
FR2974387B1 true FR2974387B1 (fr) 2015-11-20

Family

ID=46208998

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1153373A Active FR2974387B1 (fr) 2011-04-19 2011-04-19 Roue de turbine pour une turbomachine

Country Status (3)

Country Link
US (1) US8961137B2 (fr)
FR (1) FR2974387B1 (fr)
GB (1) GB2490216B (fr)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2981979B1 (fr) 2011-10-28 2013-11-29 Snecma Roue de turbine pour une turbomachine
FR3006364B1 (fr) * 2013-05-30 2018-07-13 Safran Aircraft Engines Roue de turbomachine, notamment pour turbine basse pression
WO2015026416A2 (fr) 2013-06-03 2015-02-26 United Technologies Corporation Amortisseurs de vibrations pour pales de turbine
US10030523B2 (en) * 2015-02-13 2018-07-24 United Technologies Corporation Article having cooling passage with undulating profile
US9810075B2 (en) 2015-03-20 2017-11-07 United Technologies Corporation Faceted turbine blade damper-seal
US10196903B2 (en) * 2016-01-15 2019-02-05 General Electric Company Rotor blade cooling circuit
US10662784B2 (en) 2016-11-28 2020-05-26 Raytheon Technologies Corporation Damper with varying thickness for a blade
US10731479B2 (en) 2017-01-03 2020-08-04 Raytheon Technologies Corporation Blade platform with damper restraint
US10677073B2 (en) * 2017-01-03 2020-06-09 Raytheon Technologies Corporation Blade platform with damper restraint
FR3139359A1 (fr) * 2022-09-06 2024-03-08 Safran Helicopter Engines Amortisseur configuré pour amortir un mouvement d’aube de turbomachine et ensemble comprenant l’amortisseur
FR3139358B1 (fr) * 2022-09-06 2024-08-16 Safran Helicopter Engines Ensemble pour turbomachine

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3119595A (en) * 1961-02-23 1964-01-28 Gen Electric Bladed rotor and baffle assembly
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
US4712979A (en) * 1985-11-13 1987-12-15 The United States Of America As Represented By The Secretary Of The Air Force Self-retained platform cooling plate for turbine vane
JPS62251404A (ja) * 1986-04-24 1987-11-02 Yanmar Diesel Engine Co Ltd ガスタ−ビンの動翼の自然内部冷却装置
US5281097A (en) * 1992-11-20 1994-01-25 General Electric Company Thermal control damper for turbine rotors
FR2758855B1 (fr) * 1997-01-30 1999-02-26 Snecma Systeme de ventilation des plates-formes des aubes mobiles
FR2810365B1 (fr) * 2000-06-15 2002-10-11 Snecma Moteurs Systeme de ventilation d'une paire de plates-formes d'aubes juxtaposees
FR2840352B1 (fr) * 2002-05-30 2005-12-16 Snecma Moteurs Maitrise de la zone de fuite sous plate-forme d'aube
US6887039B2 (en) * 2002-07-10 2005-05-03 Mitsubishi Heavy Industries, Ltd. Stationary blade in gas turbine and gas turbine comprising the same
EP1413715A1 (fr) * 2002-10-21 2004-04-28 Siemens Aktiengesellschaft Dispositif de refroidissement pour une plate-forme d'une aube d'une turbine à gaz
FR2915510B1 (fr) * 2007-04-27 2009-11-06 Snecma Sa Amortisseur pour aubes de turbomachines
GB0806893D0 (en) * 2008-04-16 2008-05-21 Rolls Royce Plc A damper
US8240987B2 (en) * 2008-08-15 2012-08-14 United Technologies Corp. Gas turbine engine systems involving baffle assemblies
EP2180142B1 (fr) * 2008-10-23 2014-01-22 Alstom Technology Ltd Aube de turbine à gaz
US8393869B2 (en) * 2008-12-19 2013-03-12 Solar Turbines Inc. Turbine blade assembly including a damper
WO2010103551A1 (fr) * 2009-03-09 2010-09-16 Avio S.P.A. Rotor pour turbomachines
FR2963382B1 (fr) * 2010-08-02 2016-01-29 Snecma Roue de turbine a aubes en composite a matrice ceramique

Also Published As

Publication number Publication date
GB2490216B (en) 2017-05-03
GB201206497D0 (en) 2012-05-30
GB2490216A (en) 2012-10-24
US8961137B2 (en) 2015-02-24
US20120269650A1 (en) 2012-10-25
FR2974387A1 (fr) 2012-10-26

Similar Documents

Publication Publication Date Title
FR2974387B1 (fr) Roue de turbine pour une turbomachine
FR2975428B1 (fr) Roue a aubes de turbomachine
FR2989724B1 (fr) Etage de turbine pour une turbomachine
GB2493976B (en) Turbomachine
FR2980235B1 (fr) Anneau pour une turbine de turbomachine
EP2787181A4 (fr) Turbine radiale
ZA201405188B (en) High speed turbine
FR2997444B1 (fr) Moyeu de carter pour une turbomachine
FR2978796B1 (fr) Roue a aubes de turbomachine
FR2995003B1 (fr) Rotor de turbine pour une turbomachine
EP2669473A4 (fr) Turbine radiale
GB2493972B (en) Rotor assembly for a turbomachine
GB2493975B (en) Turbomachine
GB2496293B (en) A turbine wheel for a turbine engine
FR2977909B1 (fr) Aube de rotor pour une turbomachine
GB2487921B (en) Rotor for a turbomachine
GB201114669D0 (en) Turbine engine
FR2971822B1 (fr) Rotor de soufflante, en particulier pour une turbomachine
EP2836683A4 (fr) Ensemble arbre d'accouplement pour turbomachine
GB2493973B (en) Rotor assembly for a turbomachine
FR2986046B1 (fr) Ensemble pour un rotor de soufflante de turbomachine
FR2978793B1 (fr) Rotor de turbine pour une turbomachine
FR3006366B1 (fr) Roue de turbine dans une turbomachine
FR2983535B1 (fr) Hydrolienne
EP2800897A4 (fr) Raccordement d'auget pour une roue de turbine

Legal Events

Date Code Title Description
PLFP Fee payment

Year of fee payment: 5

PLFP Fee payment

Year of fee payment: 6

PLFP Fee payment

Year of fee payment: 7

CD Change of name or company name

Owner name: SAFRAN AIRCRAFT ENGINES, FR

Effective date: 20170719

PLFP Fee payment

Year of fee payment: 8

PLFP Fee payment

Year of fee payment: 9

PLFP Fee payment

Year of fee payment: 10

PLFP Fee payment

Year of fee payment: 11

PLFP Fee payment

Year of fee payment: 12

PLFP Fee payment

Year of fee payment: 13

PLFP Fee payment

Year of fee payment: 14