RU2643750C2 - Способ осуществления металлического усилительного элемента со вставкой для защиты передней кромки из композитного материала - Google Patents

Способ осуществления металлического усилительного элемента со вставкой для защиты передней кромки из композитного материала Download PDF

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Publication number
RU2643750C2
RU2643750C2 RU2014141065A RU2014141065A RU2643750C2 RU 2643750 C2 RU2643750 C2 RU 2643750C2 RU 2014141065 A RU2014141065 A RU 2014141065A RU 2014141065 A RU2014141065 A RU 2014141065A RU 2643750 C2 RU2643750 C2 RU 2643750C2
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RU
Russia
Prior art keywords
insert
alloy
reinforcing element
core
titanium alloy
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RU2014141065A
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English (en)
Russian (ru)
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RU2014141065A (ru
Inventor
Жан-Мишель ФРАНШЕ
Жилль КЛЕЙН
Жильбер ЛЕКОНТ
Доминик МАНЬОДЕКС
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Снекма
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Publication of RU2014141065A publication Critical patent/RU2014141065A/ru
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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
    • 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
    • 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
    • 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)
RU2014141065A 2012-04-19 2013-04-11 Способ осуществления металлического усилительного элемента со вставкой для защиты передней кромки из композитного материала RU2643750C2 (ru)

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 (2)

Publication Number Publication Date
RU2014141065A RU2014141065A (ru) 2016-06-10
RU2643750C2 true RU2643750C2 (ru) 2018-02-05

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
RU2014141065A RU2643750C2 (ru) 2012-04-19 2013-04-11 Способ осуществления металлического усилительного элемента со вставкой для защиты передней кромки из композитного материала

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)

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
JP6735299B2 (ja) * 2018-03-09 2020-08-05 三菱重工業株式会社 複合材翼、前縁金属カバー形成ユニット、複合材翼の製造方法
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
CN110439627B (zh) * 2019-08-30 2022-02-11 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
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

Citations (5)

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US4010530A (en) * 1975-07-24 1977-03-08 United Technologies Corporation Method for making blade protective sheaths
SU1483049A1 (ru) * 1987-09-17 1989-05-30 Ленинградский Политехнический Институт Им.М.И.Калинина Рабоча лопатка влажно-паровой турбины
RU2118462C1 (ru) * 1995-07-20 1998-08-27 Акционерное общество "К.Т.С." Рабочая лопатка турбомашины
EP2281645A1 (en) * 2009-07-28 2011-02-09 Rolls-Royce plc A method of manufacturing a reinforcing edge for a turbo machine aerofoil
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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US4738594A (en) * 1986-02-05 1988-04-19 Ishikawajima-Harima Jukogyo Kabushiki Kaisha Blades for axial fans
DE69302219T2 (de) * 1992-06-05 1996-09-19 Gec Alsthom Electromec Verfahren zum Anbringen von Schutzüberzügen bildenden Einsätzen auf Gegenständen aus martensitischens Stahl oder aus Titanlegierungen
DE69529178T2 (de) 1995-09-13 2003-10-02 Boehler Schmiedetechnik Ges.M.B.H. & Co. Kg, Kapfenberg Verfahren zum herstellen einer turbinenschaufel aus titanlegierung und titanlegierungsturbinenschaufel
DE10305912B4 (de) 2003-02-13 2014-01-30 Alstom Technology Ltd. Hybrid- Schaufel für thermische Turbomaschinen
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
US7575418B2 (en) * 2004-09-30 2009-08-18 General Electric Company Erosion and wear resistant protective structures for turbine components
CN101646865B (zh) * 2006-12-15 2013-01-09 布拉德纳公司 加强的空气动力学型材
US7866605B2 (en) * 2007-04-24 2011-01-11 The Boeing Company Energy absorbing impact band and method
WO2010084941A1 (ja) 2009-01-22 2010-07-29 株式会社Ihi ファンブレードの前縁強化部材の製造方法
FR2956602B1 (fr) * 2010-02-25 2012-05-25 Snecma Procede de realisation d'un renfort metallique d'aube de turbomachine
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
US4010530A (en) * 1975-07-24 1977-03-08 United Technologies Corporation Method for making blade protective sheaths
SU1483049A1 (ru) * 1987-09-17 1989-05-30 Ленинградский Политехнический Институт Им.М.И.Калинина Рабоча лопатка влажно-паровой турбины
RU2118462C1 (ru) * 1995-07-20 1998-08-27 Акционерное общество "К.Т.С." Рабочая лопатка турбомашины
EP2281645A1 (en) * 2009-07-28 2011-02-09 Rolls-Royce plc A method of manufacturing a reinforcing edge for a turbo machine aerofoil
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

Also Published As

Publication number Publication date
CN104220212A (zh) 2014-12-17
WO2013156711A1 (fr) 2013-10-24
EP2838692A1 (fr) 2015-02-25
CA2870229A1 (fr) 2013-10-24
FR2989607B1 (fr) 2014-05-09
CA2870229C (fr) 2020-08-25
US20150104323A1 (en) 2015-04-16
FR2989607A1 (fr) 2013-10-25
US9963971B2 (en) 2018-05-08
RU2014141065A (ru) 2016-06-10
JP6298808B2 (ja) 2018-03-20
BR112014025383B1 (pt) 2021-11-23
BR112014025383A2 (pt) 2017-06-20
JP2015520033A (ja) 2015-07-16
EP2838692B1 (fr) 2019-07-03

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