FR3098542B1 - Turbomachine parts set - Google Patents

Turbomachine parts set Download PDF

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Publication number
FR3098542B1
FR3098542B1 FR1907718A FR1907718A FR3098542B1 FR 3098542 B1 FR3098542 B1 FR 3098542B1 FR 1907718 A FR1907718 A FR 1907718A FR 1907718 A FR1907718 A FR 1907718A FR 3098542 B1 FR3098542 B1 FR 3098542B1
Authority
FR
France
Prior art keywords
turbomachine
parts set
turbomachine parts
assembly
abstract
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
FR1907718A
Other languages
French (fr)
Other versions
FR3098542A1 (en
Inventor
Jean-François Henne
Maxime François Roger Carlin
Lisa Pin
Thierry Guy Xavier Tesson
Fabrice Crabos
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 Ceramics SA
Original Assignee
Safran Ceramics SA
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 Ceramics SA filed Critical Safran Ceramics SA
Priority to FR1907718A priority Critical patent/FR3098542B1/en
Publication of FR3098542A1 publication Critical patent/FR3098542A1/en
Application granted granted Critical
Publication of FR3098542B1 publication Critical patent/FR3098542B1/en
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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/007—Preventing corrosion
    • 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
    • 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
    • F05D2240/10—Stators
    • F05D2240/11—Shroud seal segments
    • 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
    • F05D2240/57—Leaf 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/10—Metals, alloys or intermetallic compounds
    • F05D2300/11—Iron
    • 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
    • F05D2300/10—Metals, alloys or intermetallic compounds
    • F05D2300/13—Refractory metals, i.e. Ti, V, Cr, Zr, Nb, Mo, Hf, Ta, W
    • F05D2300/132—Chromium
    • 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
    • F05D2300/10—Metals, alloys or intermetallic compounds
    • F05D2300/17—Alloys
    • F05D2300/173—Aluminium alloys, e.g. AlCuMgPb
    • 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)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

Ensemble de pièces de turbomachine La présente invention concerne un ensemble comprenant au moins une première pièce (1) de turbomachine en matériau composite à matrice céramique et une deuxième pièce (18) de turbomachine en alliage FeCrAl en contact avec la première pièce. Figure pour l’abrégé : Fig. 2.Assembly of turbomachine parts The present invention relates to an assembly comprising at least a first turbomachine part (1) made of ceramic matrix composite material and a second turbomachine part (18) of FeCrAl alloy in contact with the first part. Figure for abstract: Fig. 2.

FR1907718A 2019-07-10 2019-07-10 Turbomachine parts set Active FR3098542B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1907718A FR3098542B1 (en) 2019-07-10 2019-07-10 Turbomachine parts set

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1907718 2019-07-10
FR1907718A FR3098542B1 (en) 2019-07-10 2019-07-10 Turbomachine parts set

Publications (2)

Publication Number Publication Date
FR3098542A1 FR3098542A1 (en) 2021-01-15
FR3098542B1 true FR3098542B1 (en) 2023-11-24

Family

ID=68733212

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1907718A Active FR3098542B1 (en) 2019-07-10 2019-07-10 Turbomachine parts set

Country Status (1)

Country Link
FR (1) FR3098542B1 (en)

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7316539B2 (en) * 2005-04-07 2008-01-08 Siemens Power Generation, Inc. Vane assembly with metal trailing edge segment
FR2887601B1 (en) 2005-06-24 2007-10-05 Snecma Moteurs Sa MECHANICAL PIECE AND METHOD FOR MANUFACTURING SUCH A PART
US7625170B2 (en) * 2006-09-25 2009-12-01 General Electric Company CMC vane insulator and method of use
US8047773B2 (en) * 2007-08-23 2011-11-01 General Electric Company Gas turbine shroud support apparatus
US9175571B2 (en) * 2012-03-19 2015-11-03 General Electric Company Connecting system for metal components and CMC components, a turbine blade retaining system and a rotating component retaining system

Also Published As

Publication number Publication date
FR3098542A1 (en) 2021-01-15

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