EP4698348A1 - Verfahren zur modellierung der verbindung einer schaufel mit einem turbinenmotorrotorstutzen durch orbitalschweissen - Google Patents

Verfahren zur modellierung der verbindung einer schaufel mit einem turbinenmotorrotorstutzen durch orbitalschweissen

Info

Publication number
EP4698348A1
EP4698348A1 EP24719563.9A EP24719563A EP4698348A1 EP 4698348 A1 EP4698348 A1 EP 4698348A1 EP 24719563 A EP24719563 A EP 24719563A EP 4698348 A1 EP4698348 A1 EP 4698348A1
Authority
EP
European Patent Office
Prior art keywords
junction
max
section
maximum thickness
blade
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.)
Pending
Application number
EP24719563.9A
Other languages
English (en)
French (fr)
Inventor
Johann PANCRACE
Jeremy Jean-Claude Jacques Louis ESCAFFRE
Yann Jean-Pierre LEFAUX
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 Aero Boosters SA
Original Assignee
Safran Aero Boosters 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 Safran Aero Boosters SA filed Critical Safran Aero Boosters SA
Publication of EP4698348A1 publication Critical patent/EP4698348A1/de
Pending legal-status Critical Current

Links

Classifications

    • 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K20/00Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating
    • B23K20/12Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating the heat being generated by friction; Friction welding
    • B23K20/1205Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating the heat being generated by friction; Friction welding using translation movement
    • 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
    • F01D5/3061Fixing blades to rotors; Blade roots ; Blade spacers by welding, brazing
    • 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
    • F01D5/34Rotor-blade aggregates of unitary construction, e.g. formed of sheet laminae
    • 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
    • F05D2230/20Manufacture essentially without removing material
    • F05D2230/23Manufacture essentially without removing material by permanently joining parts together
    • F05D2230/232Manufacture essentially without removing material by permanently joining parts together by welding
    • 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
    • F05D2230/20Manufacture essentially without removing material
    • F05D2230/23Manufacture essentially without removing material by permanently joining parts together
    • F05D2230/232Manufacture essentially without removing material by permanently joining parts together by welding
    • F05D2230/239Inertia or friction welding

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Ceramic Engineering (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
EP24719563.9A 2023-04-21 2024-04-19 Verfahren zur modellierung der verbindung einer schaufel mit einem turbinenmotorrotorstutzen durch orbitalschweissen Pending EP4698348A1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
BE20235298A BE1031524B1 (fr) 2023-04-21 2023-04-21 Procédé de modélisation d'une jonction d'aube à un moignon de rotor de turbomachine par soudage orbital
PCT/EP2024/060674 WO2024218277A1 (fr) 2023-04-21 2024-04-19 Procédé de modélisation d'une jonction d'aube à un moignon de rotor de turbomachine par soudage orbital

Publications (1)

Publication Number Publication Date
EP4698348A1 true EP4698348A1 (de) 2026-02-25

Family

ID=86142639

Family Applications (1)

Application Number Title Priority Date Filing Date
EP24719563.9A Pending EP4698348A1 (de) 2023-04-21 2024-04-19 Verfahren zur modellierung der verbindung einer schaufel mit einem turbinenmotorrotorstutzen durch orbitalschweissen

Country Status (4)

Country Link
EP (1) EP4698348A1 (de)
CN (1) CN121079177A (de)
BE (1) BE1031524B1 (de)
WO (1) WO2024218277A1 (de)

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB201012140D0 (en) 2010-07-20 2010-09-01 Rolls Royce Plc Linear friction welding of an aerofoil blisk
EP2535516B1 (de) * 2011-06-17 2014-02-26 Techspace Aero S.A. Reibschweißverfahren von Laufradschaufeln für die Rotortrommel eines Axialkompressors, und entsprechende Vorrichtung
GB2560001B (en) * 2017-02-24 2019-07-17 Rolls Royce Plc A weld stub arrangement and a method of using the arrangement to make an article

Also Published As

Publication number Publication date
BE1031524B1 (fr) 2024-11-18
WO2024218277A1 (fr) 2024-10-24
CN121079177A (zh) 2025-12-05
BE1031524A1 (fr) 2024-11-14

Similar Documents

Publication Publication Date Title
EP1747840B1 (de) Verfahren zum Reparieren einer Schaufel einer integral beschaufelten Turbinenrotorscheibe und Prüfkörper zur Durchführung des Verfahrens
CA2537427A1 (fr) Procede de reparation de disque aubage monobloc, eprouvette de debut et de fin campagne
FR2993359A1 (fr) Procede de realisation d'un essai en fatigue vibratoire d'une piece mecanique
EP2788143B1 (de) Verfahren zum umformen durch kugelstrahlen einer turbomaschinenschaufel mit mindestens einer verformten zone
BE1031524B1 (fr) Procédé de modélisation d'une jonction d'aube à un moignon de rotor de turbomachine par soudage orbital
FR3008185A1 (fr) Insert comprenant une surface externe faisant partie d'au moins un profil aerodynamique d'une aube de test de turbomachine
WO2024218270A1 (fr) Procédé de fabrication d'un disque aubagé pour turbomachine avec des aubes soudées par friction orbitale
BE1031525B1 (fr) Procédé de soudage par friction orbitale d'aubes sur un rotor de turbomachine avec des paramètres optimisés
WO2017017343A1 (fr) Procédé de détermination d'une contrainte alternée maximale admissible pour une pièce soumise a des sollicitations cycliques; unité de détermination d'une telle contrainte
BE1031532B1 (fr) Procédé de dimensionnement de moignons optimisés pour le soudage orbital d'aubes sur un rotor de turbomachine
EP4450766A1 (de) Verfahren zur dimensionierung von stumpfen einer beschaufelten rotorscheibe einer strömungsmaschine zum orbitalschweissen
EP4634630A1 (de) Überwachung des kriechens einer turbomaschinenschaufel eines flugzeugs
BE1031526B1 (fr) Procédé de soudage par friction orbitale d'une aube à un moignon sur un disque rotorique de turbomachine
EP3963282B1 (de) Verfahren zur dimensionskontrolle einer turbomaschinenkomponente
EP3084131B1 (de) Schaufel, laufrad und turbomaschine sowie verfahren zur herstellung der schaufel
FR3132858A1 (fr) Procede d’usinage d’alveole(s) dans une piece metallique
BE1031527B1 (fr) Procédé de soudage par friction sur support renforcé
EP1672170A1 (de) Verfahren zur Reparatur von beschaufelten Rotorscheiben
BE1031528B1 (fr) Procédé de soudage par friction sur support renforcé
FR3071428A1 (fr) Dispositif de mise en position de jauge de contrainte
WO2017220916A1 (fr) Disque aubage monobloc amélioré d'un compresseur, et turbomachine associée
BE1027711A1 (fr) Etage de compresseur de turbomachine
FR3071542A1 (fr) Organe de turbomachine configure pour controler la direction de propagation d'une crique

Legal Events

Date Code Title Description
STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: UNKNOWN

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE INTERNATIONAL PUBLICATION HAS BEEN MADE

PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE

17P Request for examination filed

Effective date: 20251020

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC ME MK MT NL NO PL PT RO RS SE SI SK SM TR