FR3107460B1 - Procédé d’usinage amélioré de rainure pour pièces aéronautiques - Google Patents

Procédé d’usinage amélioré de rainure pour pièces aéronautiques Download PDF

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Publication number
FR3107460B1
FR3107460B1 FR2001694A FR2001694A FR3107460B1 FR 3107460 B1 FR3107460 B1 FR 3107460B1 FR 2001694 A FR2001694 A FR 2001694A FR 2001694 A FR2001694 A FR 2001694A FR 3107460 B1 FR3107460 B1 FR 3107460B1
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FR
France
Prior art keywords
groove
machining
predetermined
final shape
machining process
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
FR2001694A
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English (en)
Other versions
FR3107460A1 (fr
Inventor
Mickael Rancic
Damien Norbert Edgar Hebuterne
Jérôme Salmon
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
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Publication date
Application filed by Safran Aircraft Engines SAS filed Critical Safran Aircraft Engines SAS
Priority to FR2001694A priority Critical patent/FR3107460B1/fr
Publication of FR3107460A1 publication Critical patent/FR3107460A1/fr
Application granted granted Critical
Publication of FR3107460B1 publication Critical patent/FR3107460B1/fr
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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23CMILLING
    • B23C3/00Milling particular work; Special milling operations; Machines therefor
    • B23C3/28Grooving workpieces
    • B23C3/30Milling straight grooves, e.g. keyways
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P15/00Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
    • B23P15/006Making specific metal objects by operations not covered by a single other subclass or a group in this subclass turbine wheels
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02Blade-carrying members, e.g. rotors
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/30Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/3007Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23CMILLING
    • B23C2220/00Details of milling processes
    • B23C2220/36Production of grooves
    • B23C2220/366Turbine blade grooves
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23CMILLING
    • B23C5/00Milling-cutters
    • B23C5/02Milling-cutters characterised by the shape of the cutter
    • B23C5/12Cutters specially designed for producing particular profiles
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00Manufacture
    • F05D2230/10Manufacture by removing material

Abstract

Procédé d’usinage amélioré de rainure pour pièces aéronautiques Procédé d’usinage de pièce aéronautique pour obtenir au moins une rainure s’étendant le long d’une direction longitudinale (X), et présentant une forme finale (F, F’) prédéterminée, le procédé comprenant la formation d’un poinçon sur la pièce et le perçage d’un orifice, l’ébauche de la rainure à partir de l’orifice formé à l’étape précédente, par l’intermédiaire d’un premier outil d’usinage, de manière à obtenir une surépaisseur comprise entre 0,03 et 0,5 mm, la surépaisseur étant la différence entre une profondeur de la rainure lorsqu’elle a atteint la forme finale (F) prédéterminée à la fin de l’usinage, et une profondeur de la rainure à la fin de l’ébauche, et la finition de la rainure par l’intermédiaire d’un deuxième outil d’usinage (6, 60), le deuxième outil présentant une forme complémentaire de la forme finale (F) prédéterminée, et étant configuré pour obtenir les dimensions de la forme finale (F) prédéterminée de la rainure. Figure pour l’abrégé : Fig. 6B.
FR2001694A 2020-02-20 2020-02-20 Procédé d’usinage amélioré de rainure pour pièces aéronautiques Active FR3107460B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR2001694A FR3107460B1 (fr) 2020-02-20 2020-02-20 Procédé d’usinage amélioré de rainure pour pièces aéronautiques

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR2001694 2020-02-20
FR2001694A FR3107460B1 (fr) 2020-02-20 2020-02-20 Procédé d’usinage amélioré de rainure pour pièces aéronautiques

Publications (2)

Publication Number Publication Date
FR3107460A1 FR3107460A1 (fr) 2021-08-27
FR3107460B1 true FR3107460B1 (fr) 2023-03-31

Family

ID=70978107

Family Applications (1)

Application Number Title Priority Date Filing Date
FR2001694A Active FR3107460B1 (fr) 2020-02-20 2020-02-20 Procédé d’usinage amélioré de rainure pour pièces aéronautiques

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FR (1) FR3107460B1 (fr)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113977205A (zh) * 2021-11-22 2022-01-28 富曜半导体(昆山)有限公司 一种深槽加工工艺
FR3139743A1 (fr) * 2022-09-19 2024-03-22 Safran Aircraft Engines Procédé de brossage d’une arête d’au moins une alvéole usinée à la périphérie d’un disque de turbine
FR3140649A1 (fr) * 2022-10-07 2024-04-12 Safran Aircraft Engines Disque pour une turbine de turbomachine d’aeronef

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1020350B (de) * 1955-03-31 1957-12-05 Escher Wyss Gmbh Befestigung einer aus Blech bestehenden Hohlschaufel fuer axial durchstroemte Turbomaschinen
US4885829A (en) * 1989-02-16 1989-12-12 Fatigue Technology, Incorporated Fatigue life enhancement of dovetail connector slots and noncircular openings
JP4989950B2 (ja) * 2005-11-01 2012-08-01 本田技研工業株式会社 ワークの加工方法
US8807885B2 (en) * 2010-10-07 2014-08-19 General Electric Company Method and apparatus for machining a shroud block
GB201121056D0 (en) * 2011-12-08 2012-01-18 Rolls Royce Plc A method of forming a slot in an article

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Publication number Publication date
FR3107460A1 (fr) 2021-08-27

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