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 PDFInfo
- 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
Links
- 238000004519 manufacturing process Methods 0.000 title abstract 3
- 238000000034 method Methods 0.000 title abstract 2
- 239000002184 metal Substances 0.000 title 1
- 239000011248 coating agent Substances 0.000 abstract 2
- 238000000576 coating method Methods 0.000 abstract 2
- 238000012795 verification Methods 0.000 abstract 2
- 238000000151 deposition Methods 0.000 abstract 1
- 239000000463 material Substances 0.000 abstract 1
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)
- Health & Medical Sciences (AREA)
- Life Sciences & Earth Sciences (AREA)
- General Physics & Mathematics (AREA)
- 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.
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)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE112019003125B4 (de) * | 2018-06-19 | 2023-05-11 | Mitsubishi Heavy Industries, Ltd. | Turbinenrotorlaufschaufel, Turbomaschine und Kontaktflächenherstellungsverfahren |
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)
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 |
US4291448A (en) * | 1977-12-12 | 1981-09-29 | Turbine Components Corporation | Method of restoring the shrouds of turbine blades |
US4155152A (en) * | 1977-12-12 | 1979-05-22 | Matthew Bernardo | 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 |
-
2018
- 2018-04-10 FR FR1853135A patent/FR3079847B1/fr active Active
-
2019
- 2019-04-08 US US16/377,708 patent/US11415003B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
FR3079847A1 (fr) | 2019-10-11 |
US11415003B2 (en) | 2022-08-16 |
US20190309638A1 (en) | 2019-10-10 |
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Year of fee payment: 2 |
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Effective date: 20191011 |
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