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FR3080051B1 - Noyau pour la fonderie d'une piece aeronautique - Google Patents

Noyau pour la fonderie d'une piece aeronautique Download PDF

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Publication number
FR3080051B1
FR3080051B1 FR1853268A FR1853268A FR3080051B1 FR 3080051 B1 FR3080051 B1 FR 3080051B1 FR 1853268 A FR1853268 A FR 1853268A FR 1853268 A FR1853268 A FR 1853268A FR 3080051 B1 FR3080051 B1 FR 3080051B1
Authority
FR
France
Prior art keywords
core
foundry
aeronautical part
apex
intended
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
FR1853268A
Other languages
English (en)
Other versions
FR3080051A1 (fr
Inventor
Adrien Bernard Vincent Rollinger
Ramzi Bohli
Ngadia Taha Niane
Hegarat Alain Le
Romain Pierre Cariou
David Grange
Didier Maurice Marceau Guerche
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 SA
Original Assignee
Safran 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
Priority to FR1853268A priority Critical patent/FR3080051B1/fr
Application filed by Safran SA filed Critical Safran SA
Priority to BR112020020820-5A priority patent/BR112020020820B1/pt
Priority to CN201980025474.2A priority patent/CN111971134B/zh
Priority to PCT/FR2019/050874 priority patent/WO2019197791A1/fr
Priority to US17/046,592 priority patent/US11618071B2/en
Priority to CA3097010A priority patent/CA3097010A1/fr
Priority to EP19742818.8A priority patent/EP3774116A1/fr
Priority to JP2020555832A priority patent/JP7522659B2/ja
Publication of FR3080051A1 publication Critical patent/FR3080051A1/fr
Application granted granted Critical
Publication of FR3080051B1 publication Critical patent/FR3080051B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22C—FOUNDRY MOULDING
    • B22C9/00—Moulds or cores; Moulding processes
    • B22C9/10—Cores; Manufacture or installation of cores
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22C—FOUNDRY MOULDING
    • B22C9/00—Moulds or cores; Moulding processes
    • B22C9/10—Cores; Manufacture or installation of cores
    • B22C9/103—Multipart cores
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22C—FOUNDRY MOULDING
    • B22C9/00—Moulds or cores; Moulding processes
    • B22C9/02—Sand moulds or like moulds for shaped castings
    • B22C9/04—Use of lost patterns
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22C—FOUNDRY MOULDING
    • B22C9/00—Moulds or cores; Moulding processes
    • B22C9/22—Moulds for peculiarly-shaped castings
    • B22C9/24—Moulds for peculiarly-shaped castings for hollow articles
    • 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
    • F01D5/14—Form or construction
    • F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • F01D5/187—Convection cooling
    • 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
    • F05D2230/20—Manufacture essentially without removing material
    • F05D2230/21—Manufacture essentially without removing material by casting

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Molds, Cores, And Manufacturing Methods Thereof (AREA)

Abstract

La présente invention concerne un noyau pour la fonderie d'une pièce aéronautique telle qu'une aube de turbine, le noyau étant destiné à être disposé dans un logement interne défini par une moule, le noyau comprenant un corps (13) destiné à former la forme intérieure de l'aube de turbine ; une portion d'impact (15), disposée sur eu moins une portion du pourtour du corps (13) de façon à casser un jet de fluide lors du remplissage du logement interne par le fluide, la portion d'impact (15) comprenant un sommet (17) et au moins une paroi de déflexion (19) convergeant vers le sommet (17).
FR1853268A 2018-04-13 2018-04-13 Noyau pour la fonderie d'une piece aeronautique Active FR3080051B1 (fr)

Priority Applications (8)

Application Number Priority Date Filing Date Title
FR1853268A FR3080051B1 (fr) 2018-04-13 2018-04-13 Noyau pour la fonderie d'une piece aeronautique
CN201980025474.2A CN111971134B (zh) 2018-04-13 2019-04-12 用于金属铸造航空部件的型芯
PCT/FR2019/050874 WO2019197791A1 (fr) 2018-04-13 2019-04-12 Noyau pour la fonderie d'une pièce aéronautique
US17/046,592 US11618071B2 (en) 2018-04-13 2019-04-12 Core for metal casting an aeronautical part
BR112020020820-5A BR112020020820B1 (pt) 2018-04-13 2019-04-12 Macho para a fundição de uma peça aeronáutica, dispositivo de fundição para uma pá de turbina, e, método para produzir um macho
CA3097010A CA3097010A1 (fr) 2018-04-13 2019-04-12 Noyau pour la fonderie d'une piece aeronautique
EP19742818.8A EP3774116A1 (fr) 2018-04-13 2019-04-12 Noyau pour la fonderie d'une pièce aéronautique
JP2020555832A JP7522659B2 (ja) 2018-04-13 2019-04-12 航空機部品の鋳造用のコア

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1853268 2018-04-13
FR1853268A FR3080051B1 (fr) 2018-04-13 2018-04-13 Noyau pour la fonderie d'une piece aeronautique

Publications (2)

Publication Number Publication Date
FR3080051A1 FR3080051A1 (fr) 2019-10-18
FR3080051B1 true FR3080051B1 (fr) 2022-04-08

Family

ID=63490541

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1853268A Active FR3080051B1 (fr) 2018-04-13 2018-04-13 Noyau pour la fonderie d'une piece aeronautique

Country Status (8)

Country Link
US (1) US11618071B2 (fr)
EP (1) EP3774116A1 (fr)
JP (1) JP7522659B2 (fr)
CN (1) CN111971134B (fr)
BR (1) BR112020020820B1 (fr)
CA (1) CA3097010A1 (fr)
FR (1) FR3080051B1 (fr)
WO (1) WO2019197791A1 (fr)

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5296308A (en) * 1992-08-10 1994-03-22 Howmet Corporation Investment casting using core with integral wall thickness control means
JPH0970642A (ja) * 1995-09-05 1997-03-18 Mitsubishi Materials Corp 鋳型の製造方法及びこの鋳型を用いた精密鋳造品の製造方法
RU2094163C1 (ru) 1995-12-28 1997-10-27 Всероссийский научно-исследовательский институт авиационных материалов Составной керамический стержень
US6637500B2 (en) 2001-10-24 2003-10-28 United Technologies Corporation Cores for use in precision investment casting
DE102005010838B4 (de) * 2005-03-07 2007-06-06 Hydro Aluminium Alucast Gmbh Gießform, Vorrichtung und Verfahren zum Vergießen von Metallschmelze
US7610946B2 (en) * 2007-01-05 2009-11-03 Honeywell International Inc. Cooled turbine blade cast tip recess
FR2914871B1 (fr) 2007-04-11 2009-07-10 Snecma Sa Outillage pour la fabrication de noyaux ceramiques de fonderie pour aubes de turbomachines
EP2003291B1 (fr) * 2007-06-15 2017-08-09 Ansaldo Energia Switzerland AG Aube de turbine à gaz moulée et procédé de production
US9422817B2 (en) * 2012-05-31 2016-08-23 United Technologies Corporation Turbine blade root with microcircuit cooling passages
GB201415726D0 (en) * 2014-09-05 2014-10-22 Rolls Royce Plc Casting of engine parts
FR3034128B1 (fr) * 2015-03-23 2017-04-14 Snecma Noyau ceramique pour aube de turbine multi-cavites
US11193386B2 (en) * 2016-05-18 2021-12-07 Raytheon Technologies Corporation Shaped cooling passages for turbine blade outer air seal
US20180161866A1 (en) 2016-12-13 2018-06-14 General Electric Company Multi-piece integrated core-shell structure for making cast component

Also Published As

Publication number Publication date
EP3774116A1 (fr) 2021-02-17
BR112020020820B1 (pt) 2024-01-30
WO2019197791A1 (fr) 2019-10-17
US11618071B2 (en) 2023-04-04
JP7522659B2 (ja) 2024-07-25
BR112020020820A2 (pt) 2021-01-19
FR3080051A1 (fr) 2019-10-18
CN111971134B (zh) 2023-05-12
JP2021521011A (ja) 2021-08-26
US20210138533A1 (en) 2021-05-13
CN111971134A (zh) 2020-11-20
CA3097010A1 (fr) 2019-10-17

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