FR2957969B1 - Dispositif d'etancheite entre les talons d'aubes adjacentes en materiau compositie d'une roue mobile de turbomachine - Google Patents

Dispositif d'etancheite entre les talons d'aubes adjacentes en materiau compositie d'une roue mobile de turbomachine

Info

Publication number
FR2957969B1
FR2957969B1 FR1052224A FR1052224A FR2957969B1 FR 2957969 B1 FR2957969 B1 FR 2957969B1 FR 1052224 A FR1052224 A FR 1052224A FR 1052224 A FR1052224 A FR 1052224A FR 2957969 B1 FR2957969 B1 FR 2957969B1
Authority
FR
France
Prior art keywords
sealing
material composed
adjacent blade
mobile wheel
blade heads
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
FR1052224A
Other languages
English (en)
Other versions
FR2957969A1 (fr
Inventor
Stephane Pierre Guillaume Blanchard
Guillaume Jean Claude Robert Renon
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
Safran Ceramics SA
Original Assignee
SNECMA Propulsion Solide SA
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 Propulsion Solide SA, SNECMA SAS filed Critical SNECMA Propulsion Solide SA
Priority to FR1052224A priority Critical patent/FR2957969B1/fr
Publication of FR2957969A1 publication Critical patent/FR2957969A1/fr
Application granted granted Critical
Publication of FR2957969B1 publication Critical patent/FR2957969B1/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
    • F01D5/22—Blade-to-blade connections, e.g. for damping vibrations
    • F01D5/225—Blade-to-blade connections, e.g. for damping vibrations by shrouding
    • 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
    • F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/282—Selecting composite materials, e.g. blades with reinforcing filaments
    • 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
    • F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/284—Selection of ceramic materials
    • 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
    • F05D2240/55—Seals
    • F05D2240/56—Brush 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
    • F05D2260/00—Function
    • F05D2260/30—Retaining components in desired mutual position
    • 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/603—Composites; e.g. fibre-reinforced
    • F05D2300/6033—Ceramic matrix composites [CMC]

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Composite Materials (AREA)
  • Ceramic Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR1052224A 2010-03-26 2010-03-26 Dispositif d'etancheite entre les talons d'aubes adjacentes en materiau compositie d'une roue mobile de turbomachine Active FR2957969B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1052224A FR2957969B1 (fr) 2010-03-26 2010-03-26 Dispositif d'etancheite entre les talons d'aubes adjacentes en materiau compositie d'une roue mobile de turbomachine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1052224A FR2957969B1 (fr) 2010-03-26 2010-03-26 Dispositif d'etancheite entre les talons d'aubes adjacentes en materiau compositie d'une roue mobile de turbomachine

Publications (2)

Publication Number Publication Date
FR2957969A1 FR2957969A1 (fr) 2011-09-30
FR2957969B1 true FR2957969B1 (fr) 2013-03-29

Family

ID=42985718

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1052224A Active FR2957969B1 (fr) 2010-03-26 2010-03-26 Dispositif d'etancheite entre les talons d'aubes adjacentes en materiau compositie d'une roue mobile de turbomachine

Country Status (1)

Country Link
FR (1) FR2957969B1 (fr)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8951013B2 (en) * 2011-10-24 2015-02-10 United Technologies Corporation Turbine blade rail damper
US20140023506A1 (en) * 2012-07-20 2014-01-23 General Electric Company Damper system and a turbine
FR3065986B1 (fr) 2017-05-02 2021-07-09 Safran Aircraft Engines Ensemble pour turbine a gaz, turbine a gaz associee
FR3081188B1 (fr) * 2018-05-15 2021-03-19 Safran Aircraft Engines Aubage de stator pour une turbomachine
US11105209B2 (en) * 2018-08-28 2021-08-31 General Electric Company Turbine blade tip shroud

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4557412A (en) * 1983-12-05 1985-12-10 United Technologies Corporation Intersecting feather seals and construction thereof
US5154577A (en) * 1991-01-17 1992-10-13 General Electric Company Flexible three-piece seal assembly
US5738490A (en) * 1996-05-20 1998-04-14 Pratt & Whitney Canada, Inc. Gas turbine engine shroud seals
DE50307673D1 (de) * 2003-02-19 2007-08-23 Alstom Technology Ltd Dichtungsanordnung, insbesondere für die schaufelsegmente von gasturbinen
US7625174B2 (en) * 2005-12-16 2009-12-01 General Electric Company Methods and apparatus for assembling gas turbine engine stator assemblies
US20070212214A1 (en) * 2006-03-09 2007-09-13 United Technologies Corporation Segmented component seal
US7534086B2 (en) * 2006-05-05 2009-05-19 Siemens Energy, Inc. Multi-layer ring seal

Also Published As

Publication number Publication date
FR2957969A1 (fr) 2011-09-30

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Legal Events

Date Code Title Description
TQ Partial transmission of property

Owner name: SNECMA, FR

Effective date: 20131121

Owner name: HERAKLES, FR

Effective date: 20131121

Owner name: SNECMA PROPULSION SOLIDE, FR

Effective date: 20131121

PLFP Fee payment

Year of fee payment: 7

PLFP Fee payment

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PLFP Fee payment

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PLFP Fee payment

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CD Change of name or company name

Owner name: HERAKLES, FR

Effective date: 20200303

Owner name: SNECMA PROPULSION SOLIDE, FR

Effective date: 20200303

Owner name: SAFRAN AIRCRAFT ENGINES, FR

Effective date: 20200303

CD Change of name or company name

Owner name: SAFRAN AIRCRAFT ENGINES, FR

Effective date: 20200415

Owner name: SAFRAN CERAMICS, FR

Effective date: 20200415

Owner name: SNECMA PROPULSION SOLIDE, FR

Effective date: 20200415

PLFP Fee payment

Year of fee payment: 12

PLFP Fee payment

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