BR112013022019A2 - processo de realização de uma peça metálica tal como um reforço de pá de turbomáquina - Google Patents

processo de realização de uma peça metálica tal como um reforço de pá de turbomáquina

Info

Publication number
BR112013022019A2
BR112013022019A2 BR112013022019A BR112013022019A BR112013022019A2 BR 112013022019 A2 BR112013022019 A2 BR 112013022019A2 BR 112013022019 A BR112013022019 A BR 112013022019A BR 112013022019 A BR112013022019 A BR 112013022019A BR 112013022019 A2 BR112013022019 A2 BR 112013022019A2
Authority
BR
Brazil
Prior art keywords
metal part
metal
reinforcement
turbo
making
Prior art date
Application number
BR112013022019A
Other languages
English (en)
Other versions
BR112013022019B1 (pt
Inventor
Alain Robert Yves Perroux
Bruno Jacques Gérard Dambrine
Thierry Godon
Original Assignee
Snecma
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 claimed from FR1151658A external-priority patent/FR2972126B1/fr
Priority claimed from FR1151661A external-priority patent/FR2972127B1/fr
Priority claimed from FR1151656A external-priority patent/FR2972125B1/fr
Priority claimed from FR1151662A external-priority patent/FR2972128B1/fr
Application filed by Snecma filed Critical Snecma
Publication of BR112013022019A2 publication Critical patent/BR112013022019A2/pt
Publication of BR112013022019B1 publication Critical patent/BR112013022019B1/pt

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21K—MAKING FORGED OR PRESSED METAL PRODUCTS, e.g. HORSE-SHOES, RIVETS, BOLTS OR WHEELS
    • B21K3/00—Making engine or like machine parts not covered by sub-groups of B21K1/00; Making propellers or the like
    • B21K3/04—Making engine or like machine parts not covered by sub-groups of B21K1/00; Making propellers or the like blades, e.g. for turbines; Upsetting of blade roots
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/02—Selection of particular materials
    • F04D29/023—Selection of particular materials especially adapted for elastic fluid pumps
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D22/00—Shaping without cutting, by stamping, spinning, or deep-drawing
    • B21D22/02—Stamping using rigid devices or tools
    • B21D22/022—Stamping using rigid devices or tools by heating the blank or stamping associated with heat treatment
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D53/00—Making other particular articles
    • B21D53/92—Making other particular articles other parts for aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21K—MAKING FORGED OR PRESSED METAL PRODUCTS, e.g. HORSE-SHOES, RIVETS, BOLTS OR WHEELS
    • B21K25/00—Uniting components to form integral members, e.g. turbine wheels and shafts, caulks with inserts, with or without shaping of the components
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/12—Both compacting and sintering
    • B22F3/14—Both compacting and sintering simultaneously
    • B22F3/15—Hot isostatic pressing
    • 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
    • B23K20/00—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating
    • B23K20/02—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating by means of a press ; Diffusion bonding
    • B23K20/021—Isostatic pressure welding
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P15/00—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
    • B23P15/04—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass turbine or like blades from several pieces
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C14/00—Alloys based on titanium
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C29/00—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides
    • C22C29/02—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides based on carbides or carbonitrides
    • C22C29/06—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides based on carbides or carbonitrides based on carbides, but not containing other metal compounds
    • C22C29/065—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides based on carbides or carbonitrides based on carbides, but not containing other metal compounds based on SiC
    • 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
    • F01D5/147—Construction, i.e. structural features, e.g. of weight-saving hollow 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
    • F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/282—Selecting composite materials, e.g. blades with reinforcing filaments
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/26—Rotors specially for elastic fluids
    • F04D29/32—Rotors specially for elastic fluids for axial flow pumps
    • F04D29/321—Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
    • F04D29/324—Blades
    • 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
    • B23K2101/00—Articles made by soldering, welding or cutting
    • B23K2101/001—Turbines
    • 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
    • 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
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/36—Application in turbines specially adapted for the fan of turbofan engines
    • 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
    • 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
    • F05D2240/303—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 leading edge 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
    • 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
    • F05D2240/304—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 trailing edge 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
    • F05D2300/10—Metals, alloys or intermetallic compounds
    • F05D2300/13—Refractory metals, i.e. Ti, V, Cr, Zr, Nb, Mo, Hf, Ta, W
    • F05D2300/133—Titanium
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49316—Impeller making
    • Y10T29/49336—Blade making

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • General Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Architecture (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Composite Materials (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

processo de realização de uma peça metálica tal como um reforço de pá de turbomáquina a presente invenção se refere a um processo de realização de uma peça metálica (30) tal como um reforço metálico de pá de turbomáquina, que compreende sucessivamente uma etapa (230) de posicionamento de uma pluralidade de grampos metálicos (301') dentro de uma ferramenta de forma (400) que apresenta uma matriz (410) e um punção (420,520); e uma etapa (240) de prensagem isostática a quente da dita pluralidade de grampos metálicos (301') que provaca a aglomeração dos ditos grampos metálicos (301') de maneira a obter uma peça maciça (430).
BR112013022019-8A 2011-03-01 2012-02-29 Processo de realização de uma peça metálica tal como um reforço de pá de turbomáquina BR112013022019B1 (pt)

Applications Claiming Priority (9)

Application Number Priority Date Filing Date Title
FR1151658A FR2972126B1 (fr) 2011-03-01 2011-03-01 Procede de realisation d'une piece metallique telle qu'un renfort d'aube de turbomachine
FR1151661A FR2972127B1 (fr) 2011-03-01 2011-03-01 Procede de realisation d'une piece metallique telle qu'un renfort d'aube de turbomachine
FR1151656A FR2972125B1 (fr) 2011-03-01 2011-03-01 Procede de realisation d'une piece metallique telle qu'un renfort d'aube de turbomachine
FR1151656 2011-03-01
FR1151661 2011-03-01
FR1151662A FR2972128B1 (fr) 2011-03-01 2011-03-01 Procede de realisation d'une piece metallique telle qu'un renfort de turbomachine
FR1151658 2011-03-01
FR1151662 2011-03-01
PCT/FR2012/050423 WO2012117201A1 (fr) 2011-03-01 2012-02-29 Procede de realisation d'une piece metallique telle qu'un renfort d'aube de turbomachine

Publications (2)

Publication Number Publication Date
BR112013022019A2 true BR112013022019A2 (pt) 2016-11-29
BR112013022019B1 BR112013022019B1 (pt) 2019-05-21

Family

ID=45930875

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112013022019-8A BR112013022019B1 (pt) 2011-03-01 2012-02-29 Processo de realização de uma peça metálica tal como um reforço de pá de turbomáquina

Country Status (8)

Country Link
US (1) US9364887B2 (pt)
EP (1) EP2681345B1 (pt)
JP (1) JP6026439B2 (pt)
CN (1) CN103429780B (pt)
BR (1) BR112013022019B1 (pt)
CA (1) CA2828385C (pt)
RU (1) RU2570254C2 (pt)
WO (1) WO2012117201A1 (pt)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2957545B1 (fr) * 2010-03-19 2012-07-27 Snecma Procede de realisation d'un insert metallique pour la protection d'un bord d'attaque en materiau composite
FR2970668B1 (fr) * 2011-01-24 2013-01-18 Snecma Procede de realisation d'un renfort metallique
FR2972124B1 (fr) * 2011-03-01 2014-05-16 Snecma Procede de realisation d'une piece metallique telle qu'un renfort d'aube de turbomachine
CA2915299A1 (en) * 2013-07-10 2015-01-15 Howmet Aerospace Inc. Methods for producing forged products and other worked products
EP2845707B1 (fr) * 2013-09-06 2017-06-28 Safran Aero Boosters SA Maintien provisoire de tôle sur moule d'injection par soudure
EP3044419B1 (en) * 2013-09-09 2019-10-02 United Technologies Corporation Airfoil and manufacturing method
EP3044417B1 (en) * 2013-09-09 2019-10-02 United Technologies Corporation Fan blades and manufacture methods
US9713861B2 (en) * 2014-09-29 2017-07-25 General Electric Company Manufacturing system and method for fabricating a component
FR3032898B1 (fr) * 2015-02-19 2017-03-10 Snecma Procede de forgeage a haute temperature d'une piece metallique preformee
CN107848014B (zh) 2015-07-13 2021-06-29 日本精工株式会社 轴承单元的制造方法以及制造装置
FR3042992B1 (fr) * 2015-11-04 2021-09-10 Univ Toulouse 3 Paul Sabatier Mise en œuvre d'une interface mobile pour la fabrication de pieces complexes
CN107052720B (zh) * 2017-04-12 2019-11-08 浙江金固股份有限公司 一种钢制车轮的制造方法及其采用该方法成型的车轮
CN109723671A (zh) * 2017-10-27 2019-05-07 中国航发商用航空发动机有限责任公司 一种复合材料风扇叶片金属加强边的制造方法
US11286782B2 (en) 2018-12-07 2022-03-29 General Electric Company Multi-material leading edge protector
US11123068B2 (en) * 2019-11-08 2021-09-21 Covidien Lp Surgical staple cartridge
CN112548504B (zh) * 2020-12-20 2022-08-09 上海倚胜机电设备有限公司 一种车门焊装工艺
CN113263250B (zh) * 2021-04-20 2022-07-19 上海交通大学 航空发动机风扇叶片金属加强边的复合制造方法
FR3123379B1 (fr) * 2021-05-28 2024-10-11 Safran Aircraft Engines procédé de fabrication d'un bouclier de bord d'attaque et bouclier de bord d'attaque.
CN116618963B (zh) * 2023-05-31 2026-02-17 无锡航亚科技股份有限公司 一种风扇叶片金属包边的加工方法
CN119712235B (zh) * 2024-11-15 2026-06-19 西北工业大学 金属丝网包裹的多孔波浪前缘仿生组合构型叶片设计方法

Family Cites Families (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR858098A (fr) 1938-08-02 1940-11-16 Tube de pitot chauffé électriquement
US2799919A (en) * 1951-11-01 1957-07-23 Gen Motors Corp Sheet metal blade and manufacture
FR1058237A (fr) 1952-06-11 1954-03-15 Andre Auge & Cie Ets Ressort pour mouvement d'horlogerie
US4301584A (en) * 1980-01-31 1981-11-24 United Technologies Corporation Method of forming fiber and metal matrix composite
US4772450A (en) * 1984-07-25 1988-09-20 Trw Inc. Methods of forming powdered metal articles
US4782992A (en) * 1986-11-21 1988-11-08 Textron Inc. Method of forming articles
US4789770A (en) * 1987-07-15 1988-12-06 Westinghouse Electric Corp. Controlled depth laser drilling system
JPH0819497B2 (ja) * 1987-08-27 1996-02-28 株式会社東芝 タービン羽根の製造方法
JP2532514B2 (ja) * 1987-10-05 1996-09-11 株式会社神戸製鋼所 磁気異方体の製造方法
JPH0741338B2 (ja) * 1992-04-30 1995-05-10 株式会社アサヒエムアンドイー 斜流ファン用ブレードの成形方法
JPH07157374A (ja) * 1993-12-09 1995-06-20 Mitsubishi Heavy Ind Ltd 金属系複合材料成形品の製造方法
DE10005250B4 (de) * 1999-02-09 2004-10-28 Mtu Aero Engines Gmbh Verfahren zur Herstellung von faserverstärkten metallischen Bauteilen
JPWO2004111303A1 (ja) * 2003-06-11 2006-07-20 石川島播磨重工業株式会社 金属製品の製造方法、金属製品、金属部品の接続方法、及び接続構造体
JP4322062B2 (ja) * 2003-07-23 2009-08-26 日本発條株式会社 エンジンブロックおよびその製造方法
FR2867096B1 (fr) * 2004-03-08 2007-04-20 Snecma Moteurs Procede de fabrication d'un bord d'attaque ou de fuite de renforcement pour une aube de soufflante
FR2884550B1 (fr) * 2005-04-15 2010-09-17 Snecma Moteurs Piece pour proteger le bord d'attaque d'une pale
RU2297538C2 (ru) * 2005-04-28 2007-04-20 Открытое акционерное общество "Теплоэнергосервис" Способ упрочнения поверхности верхней части пера турбинной лопатки
US7753643B2 (en) * 2006-09-22 2010-07-13 Siemens Energy, Inc. Stacked laminate bolted ring segment
FR2906320B1 (fr) 2006-09-26 2008-12-26 Snecma Sa Aube composite de turbomachine a renfort metallique
RU2340437C2 (ru) * 2006-12-07 2008-12-10 Федеральное государственное унитарное предприятие "Московское машиностроительное производственное предприятие "САЛЮТ" (ФГУП "ММПП "САЛЮТ") Способ изготовления заготовки пустотелой лопатки турбины газотурбинного двигателя
CA2699952C (en) * 2007-09-19 2013-07-09 Barnes Group Inc. Diffusion bonding
US7805839B2 (en) * 2007-12-31 2010-10-05 Turbine Engine Components Technologies Corporation Method of manufacturing a turbine fan blade
US8256661B2 (en) 2008-09-18 2012-09-04 Barnes Group Inc. Diffusion bonding
FR2939130B1 (fr) * 2008-11-28 2011-09-16 Snecma Propulsion Solide Procede de fabrication de piece de forme de forme complexe en materiau composite.
US8678771B2 (en) * 2009-12-14 2014-03-25 Siemens Energy, Inc. Process for manufacturing a component
FR2965824B1 (fr) * 2010-10-11 2013-11-15 Snecma Procede de fabrication d'une structure fibreuse metallique par tissage
FR2970891B1 (fr) * 2011-02-01 2013-02-15 Snecma Procede de realisation d'une piece metallique renforcee, telle qu'un renfort d'aube de turbomachine

Also Published As

Publication number Publication date
CN103429780A (zh) 2013-12-04
JP6026439B2 (ja) 2016-11-16
CN103429780B (zh) 2017-05-17
EP2681345A1 (fr) 2014-01-08
CA2828385C (fr) 2019-03-12
WO2012117201A1 (fr) 2012-09-07
RU2013143969A (ru) 2015-04-10
US9364887B2 (en) 2016-06-14
CA2828385A1 (fr) 2012-09-07
RU2570254C2 (ru) 2015-12-10
US20130333214A1 (en) 2013-12-19
JP2014508888A (ja) 2014-04-10
BR112013022019B1 (pt) 2019-05-21
EP2681345B1 (fr) 2019-01-16

Similar Documents

Publication Publication Date Title
BR112013022129A2 (pt) processo para produzir uma peça de metal tal como um reforço de pá de turbormáquina
ATE544548T1 (de) Verfahren zum massenherstellen dreidimensionale gegenstände aus intermetallische verbindungen
TW200801214A (en) Methods of producing deformed metal articles
EA201391631A1 (ru) Способ изготовления стального профиля
MX2013011153A (es) Metodo para el analisis de conformacion por presion.
PH12016501194B1 (en) Lipid comprising long chain polyunsaturated fatty acids
IN2015DN03008A (pt)
SG169943A1 (en) A die former
PL2782702T3 (pl) Sposób wytwarzania części z blachy łączonej, z obszarem metalowymi oraz odpowiedni tłocznik
BRPI0908592A2 (pt) processo de fabricação de uma pá oca para turbomáquina e turbomáquina tal como um turbopropulsor ou turborreator de avião
RU2013143969A (ru) Способ изготовления металлической части, такой как усиление лопатки турбинного двигателя
MX2010005939A (es) Procedimiento para la preparacion de esteres alquilicos de acidos grasos.
MY179142A (en) Organic waste processing
EP2536862A4 (en) PRE-ALLOY FOR THE PRODUCTION OF SINTERIZED STEEL PARTS AND METHOD FOR THE PRODUCTION OF SINTERED CERTAIN PARTS
FR2965498B1 (fr) Procede de realisation d?un renfort metallique d?aube de turbomachine.
WO2013156572A8 (de) Verfahren zum herstellen eines künstlichen gebisses
FR2965497B1 (fr) Procede de realisation d'une piece metallique
FR2975734B1 (fr) Procede de renforcement d'une piece mecanique de turbomachine
WO2014057222A3 (fr) Procédé de fabrication d'au moins une pièce métallique de turbomachine
WO2013184188A3 (en) Manufacturing system and process using a laser assisted stamping die
EA201290801A1 (ru) Способ получения сциллоинозита
EP3085472A4 (en) Manufacture of metal core by using rapid prototyping method and method for manufacturing precision parts through hot isostatic pressing using same, and turbine blisk for driving liquid rocket turbo pump using same
GB201200360D0 (en) Component production method
EP2358866A4 (en) CORYNEBACTERIA STRUCTURE WITH REINFORCED 5'-XANTHOSINE MONOPHOSPHATE PRODUCTIVITY AND METHOD FOR THE PRODUCTION OF 5'-GUANOSINE-XANTHOSINE THEREWITH
EP2358865A4 (en) CORYNEBACTERIA STRUCTURE FOR REINFORCED 5'-GUANOSINE MONOPHOSPHATE PRODUCTIVITY AND METHOD FOR THE PREPARATION OF 5'-GUANOSINE MONOPHOSPHATE THEREWITH

Legal Events

Date Code Title Description
B07A Application suspended after technical examination (opinion) [chapter 7.1 patent gazette]
B09A Decision: intention to grant [chapter 9.1 patent gazette]
B16A Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]

Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 29/02/2012, OBSERVADAS AS CONDICOES LEGAIS. (CO) 20 (VINTE) ANOS CONTADOS A PARTIR DE 29/02/2012, OBSERVADAS AS CONDICOES LEGAIS

B21F Lapse acc. art. 78, item iv - on non-payment of the annual fees in time

Free format text: REFERENTE A 9A ANUIDADE.

B21H Decision of lapse of a patent or of a certificate of addition of invention cancelled [chapter 21.8 patent gazette]

Free format text: ANULADA A PUBLICACAO CODIGO 21.6 NA RPI NO 2620 DE 23/03/2021 POR TER SIDO INDEVIDA. UMA QUE A 9A ANUIDADE FOI RECOLHIDA CORRETAMENTE EM 29 DE FEVEREIRO.