FR3079847B1 - Procede de fabrication d'un element aubage metallique d'une turbomachine d'aeronef - Google Patents

Procede de fabrication d'un element aubage metallique d'une turbomachine d'aeronef Download PDF

Info

Publication number
FR3079847B1
FR3079847B1 FR1853135A FR1853135A FR3079847B1 FR 3079847 B1 FR3079847 B1 FR 3079847B1 FR 1853135 A FR1853135 A FR 1853135A FR 1853135 A FR1853135 A FR 1853135A FR 3079847 B1 FR3079847 B1 FR 3079847B1
Authority
FR
France
Prior art keywords
manufacturing
conformity
blade element
metal blade
bladed
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
FR1853135A
Other languages
English (en)
Other versions
FR3079847A1 (fr
Inventor
Bruno Marc-Etienne Loisel
Guillaume Sylvain Frederic Evrard
Alexandre Thanh Nhan Nguyen
Carine Thuy-Huong Pragassam
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
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 filed Critical Safran Aircraft Engines SAS
Priority to FR1853135A priority Critical patent/FR3079847B1/fr
Priority to US16/377,708 priority patent/US11415003B2/en
Publication of FR3079847A1 publication Critical patent/FR3079847A1/fr
Application granted granted Critical
Publication of FR3079847B1 publication Critical patent/FR3079847B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K35/00—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
    • 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
    • F01D5/288—Protective coatings for blades
    • 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
    • F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
    • F01D21/003—Arrangements for testing or measuring
    • 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
    • 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
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B3/00—Measuring instruments characterised by the use of mechanical techniques
    • G01B3/30—Bars, blocks, or strips in which the distance between a pair of faces is fixed, although it may be preadjustable, e.g. end measure, feeler strip
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N33/00—Investigating or analysing materials by specific methods not covered by groups G01N1/00 - G01N31/00
    • G01N33/20—Metals
    • G01N33/208—Coatings, e.g. platings
    • 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
    • F05D2230/90—Coating; Surface treatment
    • 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
    • F05D2250/00—Geometry
    • F05D2250/20—Three-dimensional
    • 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
    • F05D2260/80—Diagnostics
    • 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
    • F05D2260/83—Testing, e.g. methods, components or tools therefor
    • 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
    • F05D2300/611—Coating
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B21/00—Measuring arrangements or details thereof, where the measuring technique is not covered by the other groups of this subclass, unspecified or not relevant
    • G01B21/16—Measuring arrangements or details thereof, where the measuring technique is not covered by the other groups of this subclass, unspecified or not relevant for measuring distance of clearance between spaced objects

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Health & Medical Sciences (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Materials Engineering (AREA)
  • Food Science & Technology (AREA)
  • Medicinal Chemistry (AREA)
  • Analytical Chemistry (AREA)
  • Biochemistry (AREA)
  • General Health & Medical Sciences (AREA)
  • Immunology (AREA)
  • Pathology (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Powder Metallurgy (AREA)

Abstract

Procédé de fabrication d'un élément aubagé (10, 10') métallique d'une turbomachine, en particulier d'aéronef, comportant les étapes consistant à : a) fabriquer l'élément aubagé, b) déposer un revêtement (36) en matériau anti-usure sur au moins une portion de l'élément aubagé, e) vérifier, de préférence visuellement, la conformité de l'élément aubagé, caractérisé en ce que l'étape e) comprend une étape de mise en place d'un élément de vérification (50) sur l'élément aubagé, cet élément de vérification étant configuré selon une valeur seuil de conformité (S) pour cacher une non-conformité du revêtement si cette non-conformité a au moins une dimension (R) inférieure à cette valeur seuil, et pour laisser visible au moins une partie de cette non-conformité si ladite au moins une dimension est supérieure à cette valeur seuil.
FR1853135A 2018-04-10 2018-04-10 Procede de fabrication d'un element aubage metallique d'une turbomachine d'aeronef Active FR3079847B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1853135A FR3079847B1 (fr) 2018-04-10 2018-04-10 Procede de fabrication d'un element aubage metallique d'une turbomachine d'aeronef
US16/377,708 US11415003B2 (en) 2018-04-10 2019-04-08 Method for producing a metal bladed element of an aircraft turbine engine

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1853135 2018-04-10
FR1853135A FR3079847B1 (fr) 2018-04-10 2018-04-10 Procede de fabrication d'un element aubage metallique d'une turbomachine d'aeronef

Publications (2)

Publication Number Publication Date
FR3079847A1 FR3079847A1 (fr) 2019-10-11
FR3079847B1 true FR3079847B1 (fr) 2023-11-10

Family

ID=63490533

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1853135A Active FR3079847B1 (fr) 2018-04-10 2018-04-10 Procede de fabrication d'un element aubage metallique d'une turbomachine d'aeronef

Country Status (2)

Country Link
US (1) US11415003B2 (fr)
FR (1) FR3079847B1 (fr)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP6986155B2 (ja) * 2018-06-19 2021-12-22 三菱パワー株式会社 タービン動翼、ターボ機械及びコンタクト面製造方法
FR3107079B1 (fr) * 2020-02-07 2022-01-21 Safran Aircraft Engines Aube de turbomachine d’aeronef
FR3107921B1 (fr) 2020-03-04 2022-08-05 Safran Aircraft Engines Procede pour remboiter des talons d’aubes d’une roue de rotor dans une turbomachine d’aeronef
FR3124215A1 (fr) 2021-06-22 2022-12-23 Safran Aircraft Engines Procede pour reengager des clinquants pour aubes de turbomachine et dispositif de reengagement d’un clinquant

Family Cites Families (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US989512A (en) * 1909-04-09 1911-04-11 George H Riehl Typographical gage.
US2607125A (en) * 1948-06-21 1952-08-19 Johansson Ab C E Measuring device
US4090302A (en) * 1977-03-17 1978-05-23 Dayco Corporation Printing blanket holding bar gage
US4155152A (en) * 1977-12-12 1979-05-22 Matthew Bernardo Method of restoring the shrouds of turbine blades
US4291448A (en) * 1977-12-12 1981-09-29 Turbine Components Corporation Method of restoring the shrouds of turbine blades
US4257741A (en) * 1978-11-02 1981-03-24 General Electric Company Turbine engine blade with airfoil projection
DE3135585A1 (de) 1981-09-09 1983-03-24 MTU Motoren- und Turbinen-Union München GmbH, 8000 München "messwerkzeug"
US4957567A (en) 1988-12-13 1990-09-18 General Electric Company Fatigue crack growth resistant nickel-base article and alloy and method for making
FR2746043B1 (fr) * 1996-03-14 1998-04-17 Soc Nat Detude Et De Construction De Moteurs Daviation Snecma Procede de realisation d'un apport sur une zone localisee de piece en superalliage
US6164916A (en) * 1998-11-02 2000-12-26 General Electric Company Method of applying wear-resistant materials to turbine blades, and turbine blades having wear-resistant materials
US20040124231A1 (en) * 1999-06-29 2004-07-01 Hasz Wayne Charles Method for coating a substrate
US6701616B2 (en) * 2002-06-28 2004-03-09 General Electric Company Method of repairing shroud tip overlap on turbine buckets
US7001152B2 (en) * 2003-10-09 2006-02-21 Pratt & Wiley Canada Corp. Shrouded turbine blades with locally increased contact faces
FR2860741B1 (fr) * 2003-10-10 2007-04-13 Snecma Moteurs Procede de reparation de pieces metalliques notamment d'aubes de turbine de moteur a turbine a gaz
US7934315B2 (en) * 2006-08-11 2011-05-03 United Technologies Corporation Method of repairing shrouded turbine blades with cracks in the vicinity of the outer shroud notch
US7771171B2 (en) * 2006-12-14 2010-08-10 General Electric Company Systems for preventing wear on turbine blade tip shrouds
US20080229598A1 (en) * 2007-03-23 2008-09-25 Hsu Hsiu-Kwei Liu Multi-function measuring tool
FR2967714B1 (fr) * 2010-11-22 2012-12-14 Snecma Aube mobile de turbomachine
FR2985759B1 (fr) 2012-01-17 2014-03-07 Snecma Aube mobile de turbomachine
FR3001758B1 (fr) 2013-02-01 2016-07-15 Snecma Aube de rotor de turbomachine
FR3047310B1 (fr) 2016-01-28 2019-04-05 Safran Aircraft Engines Methode de controle d'une piece de machine

Also Published As

Publication number Publication date
US11415003B2 (en) 2022-08-16
FR3079847A1 (fr) 2019-10-11
US20190309638A1 (en) 2019-10-10

Similar Documents

Publication Publication Date Title
FR3079847B1 (fr) Procede de fabrication d'un element aubage metallique d'une turbomachine d'aeronef
CA2574100C (fr) Garniture rapportee pour ensemble formant duse
US5971086A (en) Pipe gripping die
JP6350771B1 (ja) 圧潰強度予測方法
EP3053702B1 (fr) Réparation d'extrémité de pale de turbine
MX2021003597A (es) Metodo para obtener un material que comprende una hoja de vidrio.
PH12020551232A1 (en) Plant inspection method
FR3096400B1 (fr) Aube de turbomachine à bord d’attaque métallique intégré et procédé pour l’obtenir
FR3090426B1 (fr) Procede de fabrication d’un noyau metallique, et procede de fabrication d’un bouclier de bord d’attaque d’une aube a partir d’un tel noyau metallique
FR3091589B1 (fr) Procédé de contrôle d'une propriété de tolérance aux dommages d'une pièce réalisée en un alliage d'aluminium
US11707808B2 (en) Method for repairing an upstream rail of a turbine engine turbine casing
MX2022001737A (es) Un metodo para calcular el espesor de los bordes trasero y delantero de un perfil de alabe.
PL416283A1 (pl) Wyrób z ulepszonym układem powłok oraz sposoby jego wytwarzania
FR3094253B1 (fr) Procede de collage d’une piece metallique sur un element en materiau composite d’une turbomachine d’aeronef
FR3101562B1 (fr) Procédé de décapage d’au moins une zone d’une aube de turbomachine
BR112021018772A2 (pt) Substrato metálico pré-revestido, substrato de aço pré-revestido, método para a fabricação do substrato metálico pré-revestido, método para a fabricação de um substrato metálico revestido, substrato metálico revestido e uso de um substrato metálico revestido
US2446291A (en) Repairing and repaired cracked metal walls
FR3096727B1 (fr) Aube de turbine dotée d’une cavité de fragilisation d’une section frangible
Barter Investigation of a Boeing 747 wing main landing gear trunnion failure
US10801369B2 (en) Intermediate casing of a turbine engine, provided with a sealing part at the arm/shroud interface
FR3088839B1 (fr) Procede de fabrication d’une piece metallique pour une turbomachine d’aeronef
EP4034753B1 (fr) Aube pour un moteur de turbomachine et moteur à turbomachine associé
Beretta et al. A simple format for the definition of safety factors for LCF
GB201804420D0 (en) A gas turbine engine having a metallic test sample and a method of dertermining the service life of a gas turbine engine component using a metallic sample
JP2018096887A (ja) 管材の応力腐食割れ試験方法

Legal Events

Date Code Title Description
PLFP Fee payment

Year of fee payment: 2

PLSC Publication of the preliminary search report

Effective date: 20191011

PLFP Fee payment

Year of fee payment: 3

PLFP Fee payment

Year of fee payment: 4

PLFP Fee payment

Year of fee payment: 5

PLFP Fee payment

Year of fee payment: 6

PLFP Fee payment

Year of fee payment: 7