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FR3034128B1 - Noyau ceramique pour aube de turbine multi-cavites - Google Patents

Noyau ceramique pour aube de turbine multi-cavites

Info

Publication number
FR3034128B1
FR3034128B1 FR1552383A FR1552383A FR3034128B1 FR 3034128 B1 FR3034128 B1 FR 3034128B1 FR 1552383 A FR1552383 A FR 1552383A FR 1552383 A FR1552383 A FR 1552383A FR 3034128 B1 FR3034128 B1 FR 3034128B1
Authority
FR
France
Prior art keywords
turbine blade
ceramic core
cavity turbine
cavity
ceramic
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
FR1552383A
Other languages
English (en)
Other versions
FR3034128A1 (fr
Inventor
Sylvain Paquin
Charlotte Marie Dujol
Patrice Eneau
Hugues Denis Joubert
Adrien Bernard Vincent Rollinger
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
Safran SA
Original Assignee
Safran SA
SNECMA 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
Priority to FR1552383A priority Critical patent/FR3034128B1/fr
Application filed by Safran SA, SNECMA SAS filed Critical Safran SA
Priority to BR112017020233-6A priority patent/BR112017020233A2/pt
Priority to US15/560,234 priority patent/US10961856B2/en
Priority to RU2017134365A priority patent/RU2719410C2/ru
Priority to JP2017549652A priority patent/JP2018515343A/ja
Priority to CN201680018252.4A priority patent/CN107407152A/zh
Priority to PCT/FR2016/050628 priority patent/WO2016151234A1/fr
Priority to CA2981994A priority patent/CA2981994A1/fr
Priority to EP16714492.2A priority patent/EP3274559A1/fr
Publication of FR3034128A1 publication Critical patent/FR3034128A1/fr
Application granted granted Critical
Publication of FR3034128B1 publication Critical patent/FR3034128B1/fr
Priority to JP2021000819A priority patent/JP7455074B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • F01D5/284—Selection of ceramic materials
    • 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
    • B22C9/10—Cores; Manufacture or installation of cores
    • 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
    • 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
    • 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
    • F05D2230/211—Manufacture essentially without removing material by casting by precision casting, e.g. microfusing or investment casting
    • 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
    • F05D2240/00—Components
    • F05D2240/20—Rotors
    • F05D2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
    • F05D2240/305—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor related to the pressure side of a rotor blade
    • 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
    • F05D2300/20—Oxide or non-oxide ceramics

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Ceramic Engineering (AREA)
  • Materials Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Molds, Cores, And Manufacturing Methods Thereof (AREA)
FR1552383A 2015-03-23 2015-03-23 Noyau ceramique pour aube de turbine multi-cavites Active FR3034128B1 (fr)

Priority Applications (10)

Application Number Priority Date Filing Date Title
FR1552383A FR3034128B1 (fr) 2015-03-23 2015-03-23 Noyau ceramique pour aube de turbine multi-cavites
EP16714492.2A EP3274559A1 (fr) 2015-03-23 2016-03-22 Noyau ceramique pour aube de turbine multi-cavites
RU2017134365A RU2719410C2 (ru) 2015-03-23 2016-03-22 Керамичекий сердечник и способ для изготовления полой лопатки турбины, применение керамического сердечника и газотурбинный двигатель с полой лопаткой турбины
JP2017549652A JP2018515343A (ja) 2015-03-23 2016-03-22 多空洞タービン翼用のセラミック中子
CN201680018252.4A CN107407152A (zh) 2015-03-23 2016-03-22 用于多腔涡轮叶片的陶瓷芯
PCT/FR2016/050628 WO2016151234A1 (fr) 2015-03-23 2016-03-22 Noyau ceramique pour aube de turbine multi-cavites
BR112017020233-6A BR112017020233A2 (pt) 2015-03-23 2016-03-22 núcleo cerâmico, uso de um núcleo cerâmico, método de fabricação para fabricar uma pá de turbina oca para um motor de turbina, e, motor de turbina
US15/560,234 US10961856B2 (en) 2015-03-23 2016-03-22 Ceramic core for a multi-cavity turbine blade
CA2981994A CA2981994A1 (fr) 2015-03-23 2016-03-22 Noyau ceramique pour aube de turbine multi-cavites
JP2021000819A JP7455074B2 (ja) 2015-03-23 2021-01-06 多空洞タービン翼用のセラミック中子

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1552383A FR3034128B1 (fr) 2015-03-23 2015-03-23 Noyau ceramique pour aube de turbine multi-cavites

Publications (2)

Publication Number Publication Date
FR3034128A1 FR3034128A1 (fr) 2016-09-30
FR3034128B1 true FR3034128B1 (fr) 2017-04-14

Family

ID=53514313

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1552383A Active FR3034128B1 (fr) 2015-03-23 2015-03-23 Noyau ceramique pour aube de turbine multi-cavites

Country Status (9)

Country Link
US (1) US10961856B2 (fr)
EP (1) EP3274559A1 (fr)
JP (2) JP2018515343A (fr)
CN (1) CN107407152A (fr)
BR (1) BR112017020233A2 (fr)
CA (1) CA2981994A1 (fr)
FR (1) FR3034128B1 (fr)
RU (1) RU2719410C2 (fr)
WO (1) WO2016151234A1 (fr)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3086893B1 (fr) 2013-12-23 2019-07-24 United Technologies Corporation Cadre structural d'un noyau perdu
FR3037829B1 (fr) * 2015-06-29 2017-07-21 Snecma Noyau pour le moulage d'une aube ayant des cavites superposees et comprenant un trou de depoussierage traversant une cavite de part en part
FR3048718B1 (fr) * 2016-03-10 2020-01-24 Safran Aube de turbomachine a refroidissement optimise
FR3067390B1 (fr) * 2017-04-10 2019-11-29 Safran Aube de turbine presentant une structure amelioree
US11098595B2 (en) * 2017-05-02 2021-08-24 Raytheon Technologies Corporation Airfoil for gas turbine engine
FR3067955B1 (fr) * 2017-06-23 2019-09-06 Safran Aircraft Engines Procede de positionnement d'une piece creuse
US10731474B2 (en) * 2018-03-02 2020-08-04 Raytheon Technologies Corporation Airfoil with varying wall thickness
FR3080051B1 (fr) * 2018-04-13 2022-04-08 Safran Noyau pour la fonderie d'une piece aeronautique
US11040915B2 (en) * 2018-09-11 2021-06-22 General Electric Company Method of forming CMC component cooling cavities
FR3094655B1 (fr) * 2019-04-08 2021-02-26 Safran Procédé de fabrication d’une pluralité de secteurs de distributeur par fonderie
FR3107920B1 (fr) 2020-03-03 2023-11-10 Safran Aircraft Engines Aube creuse de turbomachine et plateforme inter-aubes équipées de saillies perturbatrices de flux de refroidissement
CN111678563A (zh) * 2020-06-20 2020-09-18 贵阳航发精密铸造有限公司 测量多腔涡轮叶片内腔流量夹具
CN112916811B (zh) * 2021-01-22 2023-05-16 成都航宇超合金技术有限公司 带气膜孔的空心涡轮叶片的铸造方法
CN113414355B (zh) * 2021-06-10 2024-04-09 安徽海立精密铸造有限公司 一种复杂型腔汽车铸件全包芯式泥芯结构
CN114393177A (zh) * 2022-01-25 2022-04-26 烟台路通精密科技股份有限公司 一种大型薄壁铝合金增压叶轮的铸造工艺及装置
FR3137316B1 (fr) 2022-06-29 2024-10-25 Safran Aircraft Engines Noyau céramique pour aube de turbine creuse à perçages externes
CN115625286B (zh) * 2022-10-13 2023-06-30 中国航发北京航空材料研究院 单晶空心导向叶片的外型模具及其定位方法
FR3148922A1 (fr) 2023-05-22 2024-11-29 Safran Aircraft Engines Procede de fabrication d’une aube creuse de turbine de turbomachine

Family Cites Families (32)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB860126A (en) * 1956-06-20 1961-02-01 Wiggin & Co Ltd Henry Improvements relating to the production of hollow metal articles
FR2569225A1 (fr) * 1977-06-11 1986-02-21 Rolls Royce Aube creuse refroidie, pour moteur a turbine a gaz
GB2121483B (en) * 1982-06-08 1985-02-13 Rolls Royce Cooled turbine blade for a gas turbine engine
US4596281A (en) * 1982-09-02 1986-06-24 Trw Inc. Mold core and method of forming internal passages in an airfoil
US4627480A (en) * 1983-11-07 1986-12-09 General Electric Company Angled turbulence promoter
US5667359A (en) 1988-08-24 1997-09-16 United Technologies Corp. Clearance control for the turbine of a gas turbine engine
US5720431A (en) 1988-08-24 1998-02-24 United Technologies Corporation Cooled blades for a gas turbine engine
US5296308A (en) * 1992-08-10 1994-03-22 Howmet Corporation Investment casting using core with integral wall thickness control means
US5599166A (en) * 1994-11-01 1997-02-04 United Technologies Corporation Core for fabrication of gas turbine engine airfoils
US5702232A (en) * 1994-12-13 1997-12-30 United Technologies Corporation Cooled airfoils for a gas turbine engine
US5947181A (en) * 1996-07-10 1999-09-07 General Electric Co. Composite, internal reinforced ceramic cores and related methods
US5820774A (en) * 1996-10-28 1998-10-13 United Technologies Corporation Ceramic core for casting a turbine blade
US6511293B2 (en) * 2001-05-29 2003-01-28 Siemens Westinghouse Power Corporation Closed loop steam cooled airfoil
GB0114503D0 (en) * 2001-06-14 2001-08-08 Rolls Royce Plc Air cooled aerofoil
US6637500B2 (en) * 2001-10-24 2003-10-28 United Technologies Corporation Cores for use in precision investment casting
US6915840B2 (en) * 2002-12-17 2005-07-12 General Electric Company Methods and apparatus for fabricating turbine engine airfoils
US6929054B2 (en) * 2003-12-19 2005-08-16 United Technologies Corporation Investment casting cores
US6966756B2 (en) * 2004-01-09 2005-11-22 General Electric Company Turbine bucket cooling passages and internal core for producing the passages
US20050258577A1 (en) * 2004-05-20 2005-11-24 Holowczak John E Method of producing unitary multi-element ceramic casting cores and integral core/shell system
FR2875425B1 (fr) * 2004-09-21 2007-03-30 Snecma Moteurs Sa Procede de fabrication d'une aube de turbomachine, assemblage de noyaux pour la mise en oeuvre du procede.
US7377746B2 (en) * 2005-02-21 2008-05-27 General Electric Company Airfoil cooling circuits and method
US7413403B2 (en) * 2005-12-22 2008-08-19 United Technologies Corporation Turbine blade tip cooling
US7625178B2 (en) * 2006-08-30 2009-12-01 Honeywell International Inc. High effectiveness cooled turbine blade
US7722324B2 (en) * 2006-09-05 2010-05-25 United Technologies Corporation Multi-peripheral serpentine microcircuits for high aspect ratio blades
US7674093B2 (en) * 2006-12-19 2010-03-09 General Electric Company Cluster bridged casting core
US20100034662A1 (en) * 2006-12-26 2010-02-11 General Electric Company Cooled airfoil and method for making an airfoil having reduced trail edge slot flow
FR2914871B1 (fr) 2007-04-11 2009-07-10 Snecma Sa Outillage pour la fabrication de noyaux ceramiques de fonderie pour aubes de turbomachines
FR2961552B1 (fr) 2010-06-21 2014-01-31 Snecma Aube de turbine a cavite de bord d'attaque refroidie par impact
FR2986982B1 (fr) * 2012-02-22 2024-07-05 Snecma Ensemble de noyau de fonderie pour la fabrication d'une aube de turbomachine, procede de fabrication d'une aube et aube associes
US9765630B2 (en) 2013-01-09 2017-09-19 General Electric Company Interior cooling circuits in turbine blades
FR3021698B1 (fr) * 2014-05-28 2021-07-02 Snecma Aube de turbine, comprenant un conduit central de refroidissement isole thermiquement de parois de l'aube par deux cavites laterales jointives en aval du conduit central
FR3021697B1 (fr) * 2014-05-28 2021-09-17 Snecma Aube de turbine a refroidissement optimise

Also Published As

Publication number Publication date
JP7455074B2 (ja) 2024-03-25
CN107407152A8 (zh) 2018-01-12
CA2981994A1 (fr) 2016-09-29
CN107407152A (zh) 2017-11-28
RU2017134365A3 (fr) 2019-09-12
RU2719410C2 (ru) 2020-04-17
EP3274559A1 (fr) 2018-01-31
JP2021062408A (ja) 2021-04-22
US20180073373A1 (en) 2018-03-15
BR112017020233A2 (pt) 2018-05-22
US10961856B2 (en) 2021-03-30
JP2018515343A (ja) 2018-06-14
RU2017134365A (ru) 2019-04-03
WO2016151234A1 (fr) 2016-09-29
FR3034128A1 (fr) 2016-09-30

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