CN104220212A - 制造用于保护由复合材料制成的前缘并具有嵌件的金属加固件的方法 - Google Patents

制造用于保护由复合材料制成的前缘并具有嵌件的金属加固件的方法 Download PDF

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Publication number
CN104220212A
CN104220212A CN201380019674.XA CN201380019674A CN104220212A CN 104220212 A CN104220212 A CN 104220212A CN 201380019674 A CN201380019674 A CN 201380019674A CN 104220212 A CN104220212 A CN 104220212A
Authority
CN
China
Prior art keywords
insert
reinforcement
alloy
metal
core
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
CN201380019674.XA
Other languages
English (en)
Chinese (zh)
Inventor
吉恩-米歇尔·弗朗切特
吉勒斯·克莱恩
吉尔伯特·勒康特
多米尼克·麦格纳德克斯
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
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
Application filed by SNECMA SAS filed Critical SNECMA SAS
Publication of CN104220212A publication Critical patent/CN104220212A/zh
Pending legal-status Critical Current

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
    • F01D5/005—Repairing methods or devices
    • 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
    • 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
    • F04D29/02—Selection of particular materials
    • F04D29/023—Selection of particular materials especially adapted for elastic fluid pumps
    • 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
    • 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
    • B21D53/78—Making other particular articles propeller blades; turbine 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
    • 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/10—Metals, alloys or intermetallic compounds
    • F05D2300/17—Alloys
    • F05D2300/174—Titanium alloys, e.g. TiAl
    • 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
    • F05D2300/50—Intrinsic material properties or characteristics
    • F05D2300/506—Hardness
    • 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
    • Y10T29/49229—Prime mover or fluid pump making
    • Y10T29/49231—I.C. [internal combustion] engine making
    • Y10T29/49234—Rotary or radial engine making

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • Architecture (AREA)
  • Composite Materials (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
  • Welding Or Cutting Using Electron Beams (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
CN201380019674.XA 2012-04-19 2013-04-11 制造用于保护由复合材料制成的前缘并具有嵌件的金属加固件的方法 Pending CN104220212A (zh)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1253595 2012-04-19
FR1253595A FR2989607B1 (fr) 2012-04-19 2012-04-19 Procede de realisation d'un renfort metallique avec insert pour la protection d'un bord d'attaque en materiau composite
PCT/FR2013/050785 WO2013156711A1 (fr) 2012-04-19 2013-04-11 Procédé de réalisation d'un renfort métallique avec insert pour la protection d'un bord d'attaque en matériau composite

Publications (1)

Publication Number Publication Date
CN104220212A true CN104220212A (zh) 2014-12-17

Family

ID=48289462

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201380019674.XA Pending CN104220212A (zh) 2012-04-19 2013-04-11 制造用于保护由复合材料制成的前缘并具有嵌件的金属加固件的方法

Country Status (9)

Country Link
US (1) US9963971B2 (enExample)
EP (1) EP2838692B1 (enExample)
JP (1) JP6298808B2 (enExample)
CN (1) CN104220212A (enExample)
BR (1) BR112014025383B1 (enExample)
CA (1) CA2870229C (enExample)
FR (1) FR2989607B1 (enExample)
RU (1) RU2643750C2 (enExample)
WO (1) WO2013156711A1 (enExample)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110242358A (zh) * 2018-03-09 2019-09-17 三菱重工业株式会社 复合材料叶片及其制造方法、前缘金属罩形成单元
CN110439627A (zh) * 2019-08-30 2019-11-12 中国航发动力股份有限公司 一种叶片的气膜孔及尾劈缝孔防护方法

Families Citing this family (16)

* Cited by examiner, † Cited by third party
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FR2970668B1 (fr) * 2011-01-24 2013-01-18 Snecma Procede de realisation d'un renfort metallique
US9969654B2 (en) * 2014-01-24 2018-05-15 United Technologies Corporation Method of bonding a metallic component to a non-metallic component using a compliant material
FR3026033B1 (fr) * 2014-09-19 2017-03-24 Snecma Procede de fabrication de bouclier de bord d'attaque
DE102016108527B4 (de) * 2016-05-09 2018-01-04 LEISTRITZ Turbinentechnik GmbH Verfahren zur Herstellung einer Kantenabdeckung für ein Schaufelbauteil eines Flugtriebwerks oder einer Gasturbine sowie Kantenabdeckung für ein Schaufelbauteil
CN106181250B (zh) * 2016-08-05 2018-07-03 航天材料及工艺研究所 异种复合构件热等静压扩散连接制备方法
FR3084400B1 (fr) * 2018-07-24 2021-05-07 Safran Aircraft Engines Aube de turbomachine comportant un renfort structurel a adherence renforcee
US11454121B2 (en) 2018-09-28 2022-09-27 General Electric Company Airfoil with leading edge guard
US11156100B2 (en) 2018-12-04 2021-10-26 Raytheon Technologies Corporation Composite fan blade
US11286782B2 (en) 2018-12-07 2022-03-29 General Electric Company Multi-material leading edge protector
FR3092267B1 (fr) * 2019-02-04 2021-04-09 Safran Aircraft Engines Procédé de désolidarisation d'une première pièce mécanique d'une deuxième pièce mécanique
FR3094253B1 (fr) 2019-03-29 2023-06-16 Safran Aircraft Engines Procede de collage d’une piece metallique sur un element en materiau composite d’une turbomachine d’aeronef
US11725524B2 (en) 2021-03-26 2023-08-15 General Electric Company Engine airfoil metal edge
FR3124217B1 (fr) * 2021-06-21 2023-06-30 Safran Aircraft Engines Procede de fabrication d’une aube composite de turbomachine avec controle du poids moment
US11655828B2 (en) 2021-10-27 2023-05-23 General Electric Company Anti-icing systems and airfoils for a fan section of a turbine engine
US11988103B2 (en) 2021-10-27 2024-05-21 General Electric Company Airfoils for a fan section of a turbine engine
US11767607B1 (en) 2022-07-13 2023-09-26 General Electric Company Method of depositing a metal layer on a component

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EP1643011A1 (en) * 2004-09-30 2006-04-05 General Electric Company Erosion and wear resistant protective structures for turbine components
CN101646865A (zh) * 2006-12-15 2010-02-10 丹麦技术大学 加强的空气动力学型材
EP2281645A1 (en) * 2009-07-28 2011-02-09 Rolls-Royce plc A method of manufacturing a reinforcing edge for a turbo machine aerofoil
WO2011104192A1 (fr) * 2010-02-25 2011-09-01 Snecma Procede de realisation d'un renfort metallique d'aube de turbomachine
FR2957545A1 (fr) * 2010-03-19 2011-09-23 Snecma Procede de realisation d'un insert metallique pour la protection d'un bord d'attaque en materiau composite

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EP0574290B1 (fr) * 1992-06-05 1996-04-17 Gec Alsthom Electromecanique Sa Procédé de pose d'un insert servant de revêtement protecteur sur une pièce en acier martensitique ou en alliage de titane
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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
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FR2965202B1 (fr) * 2010-09-28 2012-10-12 Snecma Procede de fabrication d'une piece et piece massive composite obtenue par ce procede

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1643011A1 (en) * 2004-09-30 2006-04-05 General Electric Company Erosion and wear resistant protective structures for turbine components
CN101646865A (zh) * 2006-12-15 2010-02-10 丹麦技术大学 加强的空气动力学型材
EP2281645A1 (en) * 2009-07-28 2011-02-09 Rolls-Royce plc A method of manufacturing a reinforcing edge for a turbo machine aerofoil
WO2011104192A1 (fr) * 2010-02-25 2011-09-01 Snecma Procede de realisation d'un renfort metallique d'aube de turbomachine
FR2957545A1 (fr) * 2010-03-19 2011-09-23 Snecma Procede de realisation d'un insert metallique pour la protection d'un bord d'attaque en materiau composite

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110242358A (zh) * 2018-03-09 2019-09-17 三菱重工业株式会社 复合材料叶片及其制造方法、前缘金属罩形成单元
CN110242358B (zh) * 2018-03-09 2021-11-19 三菱重工业株式会社 复合材料叶片及其制造方法、前缘金属罩形成单元
CN110439627A (zh) * 2019-08-30 2019-11-12 中国航发动力股份有限公司 一种叶片的气膜孔及尾劈缝孔防护方法

Also Published As

Publication number Publication date
FR2989607B1 (fr) 2014-05-09
BR112014025383B1 (pt) 2021-11-23
RU2014141065A (ru) 2016-06-10
JP6298808B2 (ja) 2018-03-20
CA2870229C (fr) 2020-08-25
EP2838692A1 (fr) 2015-02-25
CA2870229A1 (fr) 2013-10-24
EP2838692B1 (fr) 2019-07-03
BR112014025383A2 (pt) 2017-06-20
FR2989607A1 (fr) 2013-10-25
US9963971B2 (en) 2018-05-08
US20150104323A1 (en) 2015-04-16
WO2013156711A1 (fr) 2013-10-24
JP2015520033A (ja) 2015-07-16
RU2643750C2 (ru) 2018-02-05

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Application publication date: 20141217

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