FR3049305B1 - Procede de fabrication d'une aube de turbomachine et aube obtenue par un tel procede - Google Patents

Procede de fabrication d'une aube de turbomachine et aube obtenue par un tel procede Download PDF

Info

Publication number
FR3049305B1
FR3049305B1 FR1652547A FR1652547A FR3049305B1 FR 3049305 B1 FR3049305 B1 FR 3049305B1 FR 1652547 A FR1652547 A FR 1652547A FR 1652547 A FR1652547 A FR 1652547A FR 3049305 B1 FR3049305 B1 FR 3049305B1
Authority
FR
France
Prior art keywords
aube
turbomachine
manufacturing
dark obtained
dark
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
FR1652547A
Other languages
English (en)
Other versions
FR3049305A1 (fr
Inventor
Vincent Le Cloarec Damien
Michel Serge Magnaudeix Dominique
Claire Rousseau
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
Safran Aircraft Engines SAS
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 Safran Aircraft Engines SAS, SNECMA SAS filed Critical Safran Aircraft Engines SAS
Priority to FR1652547A priority Critical patent/FR3049305B1/fr
Publication of FR3049305A1 publication Critical patent/FR3049305A1/fr
Application granted granted Critical
Publication of FR3049305B1 publication Critical patent/FR3049305B1/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
    • F01D5/28—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
    • F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/3007—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
    • 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
    • F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/3092—Protective layers between blade root and rotor disc surfaces, e.g. anti-friction layers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29B—PREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
    • B29B11/00—Making preforms
    • B29B11/14—Making preforms characterised by structure or composition
    • B29B11/16—Making preforms characterised by structure or composition comprising fillers or reinforcement
    • 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
    • F05D2230/00—Manufacture
    • F05D2230/10—Manufacture by removing material
    • 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
    • F05D2300/601—Fabrics
    • 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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • Composite Materials (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR1652547A 2016-03-24 2016-03-24 Procede de fabrication d'une aube de turbomachine et aube obtenue par un tel procede Active FR3049305B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1652547A FR3049305B1 (fr) 2016-03-24 2016-03-24 Procede de fabrication d'une aube de turbomachine et aube obtenue par un tel procede

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1652547A FR3049305B1 (fr) 2016-03-24 2016-03-24 Procede de fabrication d'une aube de turbomachine et aube obtenue par un tel procede
FR1652547 2016-03-24

Publications (2)

Publication Number Publication Date
FR3049305A1 FR3049305A1 (fr) 2017-09-29
FR3049305B1 true FR3049305B1 (fr) 2018-03-16

Family

ID=56101648

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1652547A Active FR3049305B1 (fr) 2016-03-24 2016-03-24 Procede de fabrication d'une aube de turbomachine et aube obtenue par un tel procede

Country Status (1)

Country Link
FR (1) FR3049305B1 (fr)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3108940B1 (fr) * 2020-04-02 2023-03-17 Safran Aircraft Engines Aube composite de turbomachine et son procede de fabrication
FR3115071B1 (fr) * 2020-10-08 2023-12-22 Safran Aircraft Engines Aube composite et attache de pied d’aube anti-rotation
FR3127522A1 (fr) * 2021-09-24 2023-03-31 Safran Aircraft Engines Procede de preparation d’un pied d’une aube de turbomachine
FR3135487A1 (fr) * 2022-05-16 2023-11-17 Safran Aircraft Engines Aube pour une turbomachine comprenant une protection anti-usure
FR3139493A1 (fr) * 2022-09-14 2024-03-15 Safran Aircraft Engines Texture fibreuse de pied d’aube ou d’helice

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5573377A (en) * 1995-04-21 1996-11-12 General Electric Company Assembly of a composite blade root and a rotor
US5935360A (en) * 1997-09-24 1999-08-10 General Electric Company Method for repairing a strip bonded to an article surface
US7329101B2 (en) * 2004-12-29 2008-02-12 General Electric Company Ceramic composite with integrated compliance/wear layer
US9527777B2 (en) * 2013-03-11 2016-12-27 Rolls-Royce Corporation Compliant layer for ceramic components and methods of forming the same
WO2014143364A2 (fr) * 2013-03-14 2014-09-18 United Technologies Corporation Elément formé conjointement avec couche à faible conductivité

Also Published As

Publication number Publication date
FR3049305A1 (fr) 2017-09-29

Similar Documents

Publication Publication Date Title
FR3049305B1 (fr) Procede de fabrication d'une aube de turbomachine et aube obtenue par un tel procede
FR3022829B1 (fr) Ensemble de compactage et procede de fabrication d'une aube composite de turbomachine
FR3036640B1 (fr) Procede de fabrication d'une aube de turbomachine en tial
FR3027550B1 (fr) Procede de fabrication d'une piece de transfert d'effort ayant une chape en materiau composite et piece obtenue par un tel procede
FR3025056B1 (fr) Dispositif laser et procede de fabrication d'un tel dispositif laser
FR3023317B1 (fr) Procede de fabrication d'une aube bi-composant pour moteur a turbine a gaz et aube obtenue par un tel procede
FR3039706B1 (fr) Procede de fabrication d'un module photovoltaique ayant des pertes resistives faibles
FR3033479B1 (fr) Procede de fabrication d'un masque de beaute a support bio-cellulosique et masque associe
FR3018525B1 (fr) Alliage a base nickel a durcissement structural, piece en cet alliage et son procede de fabrication.
FR3004972B1 (fr) Procede de fabrication d'une piece dotee d'un revetement de surface lubrifiant, piece dotee d'un tel revetement et turbomachine
FR3051828B1 (fr) Procede de fabrication d'un carter a revetement abradable de turbomachine
FR3052595B1 (fr) Procede de fabrication d'un module photovoltaique
FR3048629B1 (fr) Procede de fabrication d'un anneau de turbine pour turbomachine
FR3022811B1 (fr) Procede de fabrication d'un assemblage de noyaux pour la fabrication d'une aube
FR3020987B1 (fr) Procede de fabrication d'un element de securite.
FR3050391B1 (fr) Procede de fabrication additive et piece obtenue par un tel procede
FR3038538B1 (fr) Procede de fabrication d'une piece metallique
FR3046613B1 (fr) Procede de fabrication d'une structure textile a epaisseur variable
FR3043376B1 (fr) Volant et procede de fabrication d'un tel volant.
FR3024591B1 (fr) Procede de fabrication d’un panneau photovoltaique
FR3057586B1 (fr) Procede de fabrication d'un balcon et balcon obtenu
FR3051829B1 (fr) Procede de fabrication d'un carter annulaire equipe de turbomachine
FR3050670B1 (fr) Virole et procede de fabrication d'un carter comprenant une virole
FR3043253B1 (fr) Procede de fabrication d'un module photovoltaique
FR3032636B1 (fr) Procede pour la fabrication d'une piece creuse raidie et vrillee de grande dimension et piece obtenue par un tel procede

Legal Events

Date Code Title Description
PLFP Fee payment

Year of fee payment: 2

PLSC Publication of the preliminary search report

Effective date: 20170929

PLFP Fee payment

Year of fee payment: 3

CD Change of name or company name

Owner name: SAFRAN AIRCRAFT ENGINES, FR

Effective date: 20180809

PLFP Fee payment

Year of fee payment: 5

PLFP Fee payment

Year of fee payment: 6

PLFP Fee payment

Year of fee payment: 7

PLFP Fee payment

Year of fee payment: 8

PLFP Fee payment

Year of fee payment: 9