RU2586033C2 - АРМИРОВАННАЯ ВОЛОКНАМИ ЛОПАТКА КОМПРЕССОРА ИЗ СПЛАВА Al-Li И СПОСОБ ЕЕ ИЗГОТОВЛЕНИЯ - Google Patents

АРМИРОВАННАЯ ВОЛОКНАМИ ЛОПАТКА КОМПРЕССОРА ИЗ СПЛАВА Al-Li И СПОСОБ ЕЕ ИЗГОТОВЛЕНИЯ Download PDF

Info

Publication number
RU2586033C2
RU2586033C2 RU2011154010/06A RU2011154010A RU2586033C2 RU 2586033 C2 RU2586033 C2 RU 2586033C2 RU 2011154010/06 A RU2011154010/06 A RU 2011154010/06A RU 2011154010 A RU2011154010 A RU 2011154010A RU 2586033 C2 RU2586033 C2 RU 2586033C2
Authority
RU
Russia
Prior art keywords
blade
fabric
scapula
mold
bundles
Prior art date
Application number
RU2011154010/06A
Other languages
English (en)
Russian (ru)
Other versions
RU2011154010A (ru
Inventor
Рональд Ральф КАИРО
Цзяньцян ЧЕН
Original Assignee
Дженерал Электрик Компани
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 Дженерал Электрик Компани filed Critical Дженерал Электрик Компани
Publication of RU2011154010A publication Critical patent/RU2011154010A/ru
Application granted granted Critical
Publication of RU2586033C2 publication Critical patent/RU2586033C2/ru

Links

Images

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C47/00Making alloys containing metallic or non-metallic fibres or filaments
    • C22C47/02Pretreatment of the fibres or filaments
    • C22C47/06Pretreatment of the fibres or filaments by forming the fibres or filaments into a preformed structure, e.g. using a temporary binder to form a mat-like element
    • C22C47/062Pretreatment of the fibres or filaments by forming the fibres or filaments into a preformed structure, e.g. using a temporary binder to form a mat-like element from wires or filaments only
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D17/00Pressure die casting or injection die casting, i.e. casting in which the metal is forced into a mould under high pressure
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D19/00Casting in, on, or around objects which form part of the product
    • B22D19/14Casting in, on, or around objects which form part of the product the objects being filamentary or particulate in form
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D21/00Casting non-ferrous metals or metallic compounds so far as their metallurgical properties are of importance for the casting procedure; Selection of compositions therefor
    • B22D21/002Castings of light metals
    • B22D21/007Castings of light metals with low melting point, e.g. Al 659 degrees C, Mg 650 degrees C
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F3/00Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/12Both compacting and sintering
    • B22F3/14Both compacting and sintering simultaneously
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F5/00Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product
    • B22F5/04Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product of turbine blades
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C47/00Making alloys containing metallic or non-metallic fibres or filaments
    • C22C47/08Making alloys containing metallic or non-metallic fibres or filaments by contacting the fibres or filaments with molten metal, e.g. by infiltrating the fibres or filaments placed in a mould
    • C22C47/12Infiltration or casting under mechanical pressure
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C47/00Making alloys containing metallic or non-metallic fibres or filaments
    • C22C47/14Making alloys containing metallic or non-metallic fibres or filaments by powder metallurgy, i.e. by processing mixtures of metal powder and fibres or filaments
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C47/00Making alloys containing metallic or non-metallic fibres or filaments
    • C22C47/20Making alloys containing metallic or non-metallic fibres or filaments by subjecting to pressure and heat an assembly comprising at least one metal layer or sheet and one layer of fibres or filaments
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C49/00Alloys containing metallic or non-metallic fibres or filaments
    • C22C49/02Alloys containing metallic or non-metallic fibres or filaments characterised by the matrix material
    • C22C49/04Light metals
    • C22C49/06Aluminium
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/02Selection of particular materials
    • F04D29/023Selection of particular materials especially adapted for elastic fluid pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/32Rotors specially for elastic fluids for axial flow pumps
    • F04D29/321Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
    • F04D29/324Blades
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00Materials; Properties thereof
    • F05D2300/10Metals, alloys or intermetallic compounds
    • F05D2300/17Alloys
    • F05D2300/173Aluminium alloys, e.g. AlCuMgPb
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00Materials; Properties thereof
    • F05D2300/60Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/603Composites; e.g. fibre-reinforced
    • F05D2300/6032Metal matrix composites [MMC]
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/24Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24058Structurally defined web or sheet [e.g., overall dimension, etc.] including grain, strips, or filamentary elements in respective layers or components in angular relation
    • Y10T428/24074Strand or strand-portions

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Mechanical Engineering (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Manufacturing & Machinery (AREA)
  • General Engineering & Computer Science (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)
  • Laminated Bodies (AREA)
RU2011154010/06A 2011-01-06 2011-12-29 АРМИРОВАННАЯ ВОЛОКНАМИ ЛОПАТКА КОМПРЕССОРА ИЗ СПЛАВА Al-Li И СПОСОБ ЕЕ ИЗГОТОВЛЕНИЯ RU2586033C2 (ru)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US12/985,825 2011-01-06
US12/985,825 US8387504B2 (en) 2011-01-06 2011-01-06 Fiber-reinforced Al-Li compressor airfoil and method of fabricating

Publications (2)

Publication Number Publication Date
RU2011154010A RU2011154010A (ru) 2013-07-10
RU2586033C2 true RU2586033C2 (ru) 2016-06-10

Family

ID=45442952

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2011154010/06A RU2586033C2 (ru) 2011-01-06 2011-12-29 АРМИРОВАННАЯ ВОЛОКНАМИ ЛОПАТКА КОМПРЕССОРА ИЗ СПЛАВА Al-Li И СПОСОБ ЕЕ ИЗГОТОВЛЕНИЯ

Country Status (5)

Country Link
US (1) US8387504B2 (https=)
EP (1) EP2474638B1 (https=)
JP (1) JP5960988B2 (https=)
CN (1) CN102588333B (https=)
RU (1) RU2586033C2 (https=)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2728306C2 (ru) * 2016-04-25 2020-07-29 Сафран Способ изготовления детали из композиционного материала посредством нагнетания шликера с наполнителем в волокнистую структуру

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FI20105048L (fi) * 2010-01-21 2011-07-22 Runtech Systems Oy Menetelmä radiaalikompressorin juoksupyörän valmistamiseksi
US9650897B2 (en) 2010-02-26 2017-05-16 United Technologies Corporation Hybrid metal fan blade
US9149997B2 (en) 2012-09-14 2015-10-06 United Technologies Composite flange from braided preform
US9797257B2 (en) * 2012-12-10 2017-10-24 General Electric Company Attachment of composite article
US9120144B2 (en) * 2013-02-06 2015-09-01 Siemens Aktiengesellschaft Casting core for twisted gas turbine engine airfoil having a twisted rib
CA2922569C (en) 2013-09-11 2018-02-20 General Electric Company Spring loaded and sealed ceramic matrix composite combustor liner
DE102013226717A1 (de) * 2013-12-19 2015-06-25 Mahle International Gmbh Verfahren zur Herstellung eines Kolbens für einen Verbrennungsmotor
FR3021669B1 (fr) * 2014-06-03 2017-08-25 Sagem Defense Securite Procede de fabrication d'une piece dans un materiau composite a matrice metallique et outillage associe
US10589475B2 (en) * 2014-09-23 2020-03-17 General Electric Company Braided blades and vanes having dovetail roots
CN104314846A (zh) * 2014-10-15 2015-01-28 洛阳北玻台信风机技术有限责任公司 一种具有扇叶保护措施的工业大风扇
US11052458B2 (en) * 2015-02-10 2021-07-06 United States Of America As Represented By The Administrator Of Nasa In-situ selective reinforcement of near-net-shaped formed structures
US10029512B2 (en) * 2015-04-17 2018-07-24 Eve Wheels Llc Composite wheel rim preform and method of fabricating a composite wheel rim preform
JP6210097B2 (ja) * 2015-07-28 2017-10-11 株式会社豊田自動織機 織物積層体、織物積層体の製造方法、及び織物積層体の製造装置
US10400612B2 (en) 2015-12-18 2019-09-03 Rolls-Royce Corporation Fiber reinforced airfoil
FR3062336B1 (fr) * 2017-02-02 2019-04-12 Safran Ceramics Procede de fabrication d'une piece en materiau composite
CN107498886B (zh) * 2017-07-31 2024-03-26 东莞市那宏五金科技有限公司 一种硅胶与金属结合处理工艺
EP3495612B1 (en) * 2017-12-06 2021-05-12 Ansaldo Energia IP UK Limited Method for manufacturing composite component
GB201807150D0 (en) * 2018-05-01 2018-06-13 Composite Metal Tech Ltd Metal matrix composites
EP3586999B1 (de) * 2018-06-28 2022-11-02 GF Casting Solutions AG Metall mit feststoffen
FR3091723B1 (fr) * 2019-01-15 2021-04-02 Safran Aircraft Engines Aube ou Pale d'hélice composite pour aéronef intégrant une pièce de conformation
US11697895B2 (en) * 2019-03-27 2023-07-11 The Boeing Company Metal matrix composite tape fabrication, braiding, and consolidation to form metal matrix composite parts
FR3100741B1 (fr) * 2019-09-13 2021-09-10 Safran Dispositif de fabrication d’une piece creuse
US11549391B2 (en) 2021-03-22 2023-01-10 General Electric Company Component formed from hybrid material
CN119489565B (zh) * 2024-11-06 2025-09-16 湖北三江航天红阳机电有限公司 一种防热层约束件及防热层安装方法

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20020062561A1 (en) * 2000-11-30 2002-05-30 Verter Battistini Method for production of a rotor for centrifugal compressors
RU2206798C2 (ru) * 2001-09-20 2003-06-20 Открытое акционерное общество "Сибэнергомаш" Лопатка рабочего колеса радиального вентилятора
UA68628A (en) * 2003-08-29 2004-08-16 Mykola Ilarionovych Tregub Blade of windmill

Family Cites Families (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3594288A (en) 1968-07-31 1971-07-20 Boeing Co Process for electroplating nickel onto metal surfaces
GB1268202A (en) 1968-08-01 1972-03-22 Rolls Royce Composite blade for an elastic fluid flow machine
US3572971A (en) 1969-09-29 1971-03-30 Gen Electric Lightweight turbo-machinery blading
US3694104A (en) 1970-10-07 1972-09-26 Garrett Corp Turbomachinery blade
US3762835A (en) 1971-07-02 1973-10-02 Gen Electric Foreign object damage protection for compressor blades and other structures and related methods
US3895922A (en) 1972-08-02 1975-07-22 Mc Donnell Douglas Corp Ring pad stress coined structure
US4108572A (en) 1976-12-23 1978-08-22 United Technologies Corporation Composite rotor blade
JPS5966966A (ja) * 1982-10-09 1984-04-16 Toyota Motor Corp 耐熱性軽合金部材およびその製造方法
EP0206647B1 (en) * 1985-06-21 1992-07-29 Imperial Chemical Industries Plc Fibre-reinforced metal matrix composites
GB8804860D0 (en) * 1988-03-01 1988-03-30 Ici Plc Solid electrolyte devices
US4930983A (en) * 1988-09-26 1990-06-05 United Technologies Corporation Hybrid helicopter rotor hub retention plate
GB2253185A (en) * 1991-03-01 1992-09-02 Secr Defence Reinforced alloy laminates
US5375978A (en) 1992-05-01 1994-12-27 General Electric Company Foreign object damage resistant composite blade and manufacture
GB2293631B (en) 1994-09-30 1998-09-09 Gen Electric Composite fan blade trailing edge reinforcement
US5881775A (en) * 1994-10-24 1999-03-16 Hexcel Corporation Heat exchanger tube and method for making
US5921754A (en) * 1996-08-26 1999-07-13 Foster-Miller, Inc. Composite turbine rotor
US6074716A (en) * 1997-06-10 2000-06-13 Mcdonnell Douglas Corporation Weavable metal matrix impregnated tow composite material
US6451416B1 (en) * 1999-11-19 2002-09-17 United Technologies Corporation Hybrid monolithic ceramic and ceramic matrix composite airfoil and method for making the same
DE10101650C1 (de) * 2001-01-16 2002-08-29 Daimler Chrysler Ag Verstärktes Strukturelement
US7575417B2 (en) * 2003-09-05 2009-08-18 General Electric Company Reinforced fan blade
US7758892B1 (en) * 2004-05-20 2010-07-20 Boston Scientific Scimed, Inc. Medical devices having multiple layers
US8157205B2 (en) * 2006-03-04 2012-04-17 Mcwhirk Bruce Kimberly Multibody aircrane
FR2902802B1 (fr) * 2006-06-21 2008-12-12 Snecma Propulsion Solide Sa Structure fibreuse de renfort pour piece en materiau composite et piece la comportant
US8808726B2 (en) * 2006-09-15 2014-08-19 Boston Scientific Scimed. Inc. Bioerodible endoprostheses and methods of making the same
WO2008034066A1 (en) * 2006-09-15 2008-03-20 Boston Scientific Limited Bioerodible endoprostheses and methods of making the same
US20090077802A1 (en) * 2007-09-20 2009-03-26 General Electric Company Method for making a composite airfoil
FR2939129B1 (fr) * 2008-11-28 2014-08-22 Snecma Propulsion Solide Aube de turbomachine en materiau composite et procede pour sa fabrication.

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20020062561A1 (en) * 2000-11-30 2002-05-30 Verter Battistini Method for production of a rotor for centrifugal compressors
RU2206798C2 (ru) * 2001-09-20 2003-06-20 Открытое акционерное общество "Сибэнергомаш" Лопатка рабочего колеса радиального вентилятора
UA68628A (en) * 2003-08-29 2004-08-16 Mykola Ilarionovych Tregub Blade of windmill

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2728306C2 (ru) * 2016-04-25 2020-07-29 Сафран Способ изготовления детали из композиционного материала посредством нагнетания шликера с наполнителем в волокнистую структуру
US11285638B2 (en) 2016-04-25 2022-03-29 Safran Method of fabricating a composite material part by injecting a filled slurry into a fiber texture

Also Published As

Publication number Publication date
US8387504B2 (en) 2013-03-05
EP2474638A2 (en) 2012-07-11
EP2474638B1 (en) 2019-07-17
CN102588333A (zh) 2012-07-18
CN102588333B (zh) 2017-03-01
RU2011154010A (ru) 2013-07-10
JP5960988B2 (ja) 2016-08-02
US20120177501A1 (en) 2012-07-12
EP2474638A3 (en) 2017-05-17
JP2012144806A (ja) 2012-08-02

Similar Documents

Publication Publication Date Title
RU2586033C2 (ru) АРМИРОВАННАЯ ВОЛОКНАМИ ЛОПАТКА КОМПРЕССОРА ИЗ СПЛАВА Al-Li И СПОСОБ ЕЕ ИЗГОТОВЛЕНИЯ
RU2533384C2 (ru) Лопасть винта летательного аппарата
CA2867913C (en) Process for producing ceramic composite components
US9579861B2 (en) Laminate pre-form for a wind turbine blade
EP2354455A2 (en) Composite fan blade
US11739649B2 (en) Woven fibrous preform for manufacturing a fan blade made of composite material
JP5503481B2 (ja) 繊維強化複合材料を用いた翼状構造体およびその製造方法
JP2012144806A5 (https=)
CN103261499A (zh) 用于具有一个或多个拱形部分的由复合材料制成的零件的纤维结构
CN106457696A (zh) 以两个步骤制造的风力涡轮机叶片部件
CN111051585B (zh) 用于形成壳体预制件的编织纤维结构
CN116134212A (zh) 具有三维编织的纤维增强和二维编织的表层的复合材料制成的叶片及其制造方法
RU2770493C2 (ru) Способ получения полой детали из композиционного материала с керамической матрицей
CN108839398B (zh) 一种具有碳纤维-多孔尼龙复合结构的螺旋桨及其制备方法
CN112513352A (zh) 用于由复合材料制备的抗剪强度提高的壳体的纤维织构
CN108081636A (zh) 复合材料弹簧的生产方法
CN116964261A (zh) 用于纤维结构的三维或多层编织的方法和具有三维或多层编织的纤维结构
JP2005205902A (ja) 向上した層強度を有するセラミックマトリックス複合材及びそのための方法
RU2661429C1 (ru) Способ изготовления направляющего лопаточного аппарата компрессора авиационного двигателя
CN101629272B (zh) 一种制备连续纤维局部增强铝合金零件的方法
RU86186U1 (ru) Лопатка вентилятора
DE60318814T2 (de) Hybride Mehrkomponententurbinenschaufel
CN119704716B (zh) 复合材料叶片制备方法
CN118159413A (zh) 用于制造包括增强型空腔的叶片的方法
CN121224168A (zh) 碳纤维与芳纶纤维复合编织的螺旋桨叶片及其制备工艺

Legal Events

Date Code Title Description
MM4A The patent is invalid due to non-payment of fees

Effective date: 20201230