FR2995344B1 - Procede de fabrication d'un carter d'echappement en materiau composite pour moteur a turbine a gaz et carter d'echappement ainsi obtenu - Google Patents

Procede de fabrication d'un carter d'echappement en materiau composite pour moteur a turbine a gaz et carter d'echappement ainsi obtenu

Info

Publication number
FR2995344B1
FR2995344B1 FR1258449A FR1258449A FR2995344B1 FR 2995344 B1 FR2995344 B1 FR 2995344B1 FR 1258449 A FR1258449 A FR 1258449A FR 1258449 A FR1258449 A FR 1258449A FR 2995344 B1 FR2995344 B1 FR 2995344B1
Authority
FR
France
Prior art keywords
exhaust case
manufacturing
composite material
gas turbine
turbine engine
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
FR1258449A
Other languages
English (en)
Other versions
FR2995344A1 (fr
Inventor
Antoine Jean-Philippe Beaujard
Elric Georges Andre Fremont
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 SAS
Herakles 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 SNECMA SAS, Herakles SA filed Critical SNECMA SAS
Priority to FR1258449A priority Critical patent/FR2995344B1/fr
Priority to PCT/FR2013/052061 priority patent/WO2014037675A1/fr
Priority to GB1504016.5A priority patent/GB2519728B/en
Priority to US14/427,199 priority patent/US9784122B2/en
Publication of FR2995344A1 publication Critical patent/FR2995344A1/fr
Application granted granted Critical
Publication of FR2995344B1 publication Critical patent/FR2995344B1/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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/005—Selecting particular materials
    • 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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • 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
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
    • 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]
    • 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
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49316—Impeller making
    • Y10T29/4932—Turbomachine making
    • Y10T29/49323—Assembling fluid flow directing devices, e.g., stators, diaphragms, nozzles

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • Composite Materials (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR1258449A 2012-09-10 2012-09-10 Procede de fabrication d'un carter d'echappement en materiau composite pour moteur a turbine a gaz et carter d'echappement ainsi obtenu Active FR2995344B1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR1258449A FR2995344B1 (fr) 2012-09-10 2012-09-10 Procede de fabrication d'un carter d'echappement en materiau composite pour moteur a turbine a gaz et carter d'echappement ainsi obtenu
PCT/FR2013/052061 WO2014037675A1 (fr) 2012-09-10 2013-09-06 Procede de fabrication d'un carter en materiau composite pour moteur a turbine a gaz et carter ainsi obtenu
GB1504016.5A GB2519728B (en) 2012-09-10 2013-09-06 A method of fabricating a composite material casing for a gas turbine engine, and a casing obtained thereby
US14/427,199 US9784122B2 (en) 2012-09-10 2013-09-06 Method of fabricating a composite material casing for a gas turbine engine, and a casing obtained thereby

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1258449A FR2995344B1 (fr) 2012-09-10 2012-09-10 Procede de fabrication d'un carter d'echappement en materiau composite pour moteur a turbine a gaz et carter d'echappement ainsi obtenu

Publications (2)

Publication Number Publication Date
FR2995344A1 FR2995344A1 (fr) 2014-03-14
FR2995344B1 true FR2995344B1 (fr) 2014-09-26

Family

ID=47178140

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1258449A Active FR2995344B1 (fr) 2012-09-10 2012-09-10 Procede de fabrication d'un carter d'echappement en materiau composite pour moteur a turbine a gaz et carter d'echappement ainsi obtenu

Country Status (4)

Country Link
US (1) US9784122B2 (fr)
FR (1) FR2995344B1 (fr)
GB (1) GB2519728B (fr)
WO (1) WO2014037675A1 (fr)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB201306123D0 (en) * 2013-04-05 2013-05-22 Rolls Royce Plc Vane assembly and method of making the same
JP6616402B2 (ja) * 2014-08-26 2019-12-04 サフラン エアークラフト エンジンズ ガスタービンエンジン用の千鳥状取付フランジを具備する複合材料製案内翼
CA2924855A1 (fr) * 2015-04-29 2016-10-29 Rolls-Royce Corporation Sillage de pale a distorsion trapezoidale
US10385868B2 (en) * 2016-07-05 2019-08-20 General Electric Company Strut assembly for an aircraft engine
FR3063313B1 (fr) * 2017-02-28 2022-10-28 Safran Aircraft Engines Agencement d'entree de moteur d'aeronef comprenant un decoupleur mecanique

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4108562A (en) * 1977-11-09 1978-08-22 Kraft, Inc. Releasable coupling
US4643636A (en) * 1985-07-22 1987-02-17 Avco Corporation Ceramic nozzle assembly for gas turbine engine
US4993918A (en) * 1989-05-19 1991-02-19 United Technologies Corporation Replaceable fairing for a turbine exhaust case
US5474419A (en) * 1992-12-30 1995-12-12 Reluzco; George Flowpath assembly for a turbine diaphragm and methods of manufacture
US5494404A (en) * 1993-12-22 1996-02-27 Alliedsignal Inc. Insertable stator vane assembly
US5586864A (en) * 1994-07-27 1996-12-24 General Electric Company Turbine nozzle diaphragm and method of assembly
US6547518B1 (en) * 2001-04-06 2003-04-15 General Electric Company Low hoop stress turbine frame support
US7093359B2 (en) * 2002-09-17 2006-08-22 Siemens Westinghouse Power Corporation Composite structure formed by CMC-on-insulation process
FR2871847B1 (fr) * 2004-06-17 2006-09-29 Snecma Moteurs Sa Montage d'un distributeur de turbine sur une chambre de combustion a parois en cmc dans une turbine a gaz
US7329087B2 (en) * 2005-09-19 2008-02-12 General Electric Company Seal-less CMC vane to platform interfaces
US7648336B2 (en) * 2006-01-03 2010-01-19 General Electric Company Apparatus and method for assembling a gas turbine stator
GB0703827D0 (en) * 2007-02-28 2007-04-11 Rolls Royce Plc Rotor seal segment
US8206087B2 (en) * 2008-04-11 2012-06-26 Siemens Energy, Inc. Sealing arrangement for turbine engine having ceramic components
FR2940350B1 (fr) * 2008-12-23 2011-03-18 Snecma Roue mobile de turbomachine a aubes en materiau composite munie d'un anneau ressort.
EP2204547B1 (fr) * 2008-12-29 2013-12-11 Techspace Aero Virole extérieure et procédé de montage par soudage entre cette virole et une aube fixe
JP5321186B2 (ja) * 2009-03-26 2013-10-23 株式会社Ｉｈｉ Ｃｍｃタービン静翼
US20110206522A1 (en) * 2010-02-24 2011-08-25 Ioannis Alvanos Rotating airfoil fabrication utilizing cmc
FR2981602B1 (fr) 2011-10-25 2017-02-17 Snecma Propulsion Solide Procede de fabrication d'un secteur de distributeur de turbine ou redresseur de compresseur en materiau composite pour turbomachine et turbine ou compresseur incorporant un distributeur ou un redresseur forme de tels secteurs
FR2983519B1 (fr) 2011-12-01 2015-07-24 Snecma Propulsion Solide Aube de turbine a pale creuse en materiau composite, turbine ou compresseur ayant un distributeur ou redresseur forme de telles aubes et turbomachine les comprenant

Also Published As

Publication number Publication date
GB2519728A (en) 2015-04-29
US20150226084A1 (en) 2015-08-13
FR2995344A1 (fr) 2014-03-14
US9784122B2 (en) 2017-10-10
WO2014037675A1 (fr) 2014-03-13
GB2519728B (en) 2019-10-30
GB201504016D0 (en) 2015-04-22

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