IN2014DN05637A - - Google Patents

Info

Publication number
IN2014DN05637A
IN2014DN05637A IN5637DEN2014A IN2014DN05637A IN 2014DN05637 A IN2014DN05637 A IN 2014DN05637A IN 5637DEN2014 A IN5637DEN2014 A IN 5637DEN2014A IN 2014DN05637 A IN2014DN05637 A IN 2014DN05637A
Authority
IN
India
Prior art keywords
threads
preform
fibrous
group
rough form
Prior art date
Application number
Inventor
Yann Marchal
Dominique Coupe
Jean Noël MAHIEU
Bruno Jacques Gérard Dambrine
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
Application filed by Snecma filed Critical Snecma
Publication of IN2014DN05637A publication Critical patent/IN2014DN05637A/en

Links

Classifications

    • DTEXTILES; PAPER
    • D03WEAVING
    • D03DWOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D25/00Woven fabrics not otherwise provided for
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/28Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/282Selecting composite materials, e.g. blades with reinforcing filaments
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29BPREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
    • B29B11/00Making preforms
    • B29B11/14Making preforms characterised by structure or composition
    • B29B11/16Making preforms characterised by structure or composition comprising fillers or reinforcement
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/06Fibrous reinforcements only
    • B29C70/10Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
    • B29C70/16Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
    • B29C70/22Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least two directions forming a two dimensional structure
    • B29C70/222Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least two directions forming a two dimensional structure the structure being shaped to form a three dimensional configuration
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/06Fibrous reinforcements only
    • B29C70/10Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
    • B29C70/16Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
    • B29C70/24Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least three directions forming a three dimensional structure
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29DPRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D99/00Subject matter not provided for in other groups of this subclass
    • B29D99/0025Producing blades or the like, e.g. blades for turbines, propellers, or wings
    • DTEXTILES; PAPER
    • D03WEAVING
    • D03DWOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D1/00Woven fabrics designed to make specified articles
    • DTEXTILES; PAPER
    • D03WEAVING
    • D03DWOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D25/00Woven fabrics not otherwise provided for
    • D03D25/005Three-dimensional woven fabrics
    • DTEXTILES; PAPER
    • D03WEAVING
    • D03DWOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D3/00Woven fabrics characterised by their shape
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00Other particular articles
    • B29L2031/08Blades for rotors, stators, fans, turbines or the like, e.g. screw propellers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00Other particular articles
    • B29L2031/08Blades for rotors, stators, fans, turbines or the like, e.g. screw propellers
    • B29L2031/082Blades, e.g. for helicopters
    • 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
    • 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
    • F05D2300/6034Orientation of fibres, weaving, ply angle

Abstract

THE INVENTION RELATES TO A METHOD FOR PRODUCING A FIBROUS PREFORM FOR THE MANUFACTURE OF A TURBOMACHINE BLADE MADE OF COMPOSITE MATERIAL THE METHOD INVOLVING USING THREE DIMENSIONAL WEAVING TO CREATE A FIBROUS ROUGH FORM (100) IN A SINGLE PIECE WITH LAYERS OF LONGITUDINAL THREADS (C TO C) JOINED TOGETHER BY THREADS OF LAYERS OF TRANSVERSE THREADS (T TO T) AND SHAPING THE FIBROUS ROUGH FORM TO OBTAIN A FIBROUS PREFORM IN A SINGLE PIECE HAVING A PART THAT FORMS THE AEROFOIL PREFORM AND AT LEAST A PART THAT FORMS A PLATFORM PREFORM. DURING THE COURSE OF THE WEAVING PROCESS THE THREADS (C TO C) OF A FIRST GROUP OF LONGITUDINAL THREADS ARE LED OUT FROM THE FIBROUS ROUGH FORM ON THE SIDE OF ONE OF THE LATERAL FACES (110A) OF THE ROUGH FORM TO FORM A PART (120) THAT CORRESPONDS TO A PREFORM OF A BLADE PLATFORM AND THREADS (C AND C) OF A SECOND GROUP OF LONGITUDINAL THREADS ARE INJECTED INTO THE FIBROUS ROUGH FORM WITH MUTUAL CRISS CROSSING BETWEEN THE THREADS OF THE FIRST GROUP AND THE THREADS OF THE SECOND GROUP. THE INVENTION ALSO RELATES TO A PREFORM OBTAINED USING THIS METHOD.
IN5637DEN2014 2012-01-09 2013-01-07 IN2014DN05637A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US201261584406P 2012-01-09 2012-01-09
PCT/FR2013/050026 WO2013104852A2 (en) 2012-01-09 2013-01-07 Fibrous preform of a turbomachine blade made of composite material with in-built platform, and method of producing same

Publications (1)

Publication Number Publication Date
IN2014DN05637A true IN2014DN05637A (en) 2015-04-03

Family

ID=47628361

Family Applications (1)

Application Number Title Priority Date Filing Date
IN5637DEN2014 IN2014DN05637A (en) 2012-01-09 2013-01-07

Country Status (9)

Country Link
US (1) US9771810B2 (en)
EP (1) EP2802701B1 (en)
JP (1) JP6038178B2 (en)
CN (1) CN104040056B (en)
BR (1) BR112014016859B1 (en)
CA (1) CA2862685C (en)
IN (1) IN2014DN05637A (en)
RU (1) RU2612628C2 (en)
WO (1) WO2013104852A2 (en)

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FR3021349B1 (en) 2014-05-22 2021-07-02 Herakles METHOD OF MANUFACTURING A TURBOMACHINE VANE FROM COMPOSITE MATERIAL, THUS OBTAINED VANE AND TURBOMACHINE INCORPORATING IT
FR3037097B1 (en) * 2015-06-03 2017-06-23 Snecma COMPOSITE AUBE COMPRISING A PLATFORM WITH A STIFFENER
FR3032462B1 (en) 2015-02-10 2017-03-10 Aircelle Sa METHOD FOR MANUFACTURING A WOVEN REINFORCED FIBER PREFORM COMPRISING AN EVOLUTIVE SECTION
FR3035676B1 (en) * 2015-04-29 2017-05-12 Snecma DAWN WITH PLATFORMS POSSESSING A STIFFENER
FR3035678B1 (en) * 2015-04-29 2017-05-12 Snecma DAWN WITH PLATFORMS HAVING A RESTRAINT LEG
FR3035677B1 (en) * 2015-04-29 2017-05-12 Snecma DAWN HAVING PLATFORMS HAVING HOISTING PORTIONS
FR3035675B1 (en) * 2015-04-29 2017-05-12 Snecma DAWN WITH PLATFORMS COMPRISING INSERTS
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FR3091723B1 (en) * 2019-01-15 2021-04-02 Safran Aircraft Engines Composite blade or propeller blade for aircraft incorporating a shaping part
FR3092034B1 (en) * 2019-01-30 2022-12-02 Safran Aircraft Engines Casing in composite material with local thickness variation
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CN109972271B (en) * 2019-03-27 2023-03-14 南京玻璃纤维研究设计院有限公司 Variable thickness preform, composite component and yarn reducing method of variable thickness preform
US11434177B2 (en) 2019-05-13 2022-09-06 Rolls-Royce Plc Ceramic matrix composite vane with hybrid construction
US20210086471A1 (en) * 2019-09-20 2021-03-25 United Technologies Corporation Composite material marking and identification
FR3102392B1 (en) * 2019-10-29 2021-10-08 Safran Woven fiber preform to make a blower blade in composite material
CN111365079A (en) * 2020-04-01 2020-07-03 南京航空航天大学 Ceramic matrix composite turbine rotor blade disk tenon connecting structure and turbine disk
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Also Published As

Publication number Publication date
EP2802701A2 (en) 2014-11-19
BR112014016859A8 (en) 2017-07-04
RU2612628C2 (en) 2017-03-09
JP2015509159A (en) 2015-03-26
EP2802701B1 (en) 2016-11-16
CA2862685A1 (en) 2013-07-18
CN104040056A (en) 2014-09-10
US20140369848A1 (en) 2014-12-18
CN104040056B (en) 2016-05-04
JP6038178B2 (en) 2016-12-07
CA2862685C (en) 2020-03-10
WO2013104852A2 (en) 2013-07-18
BR112014016859B1 (en) 2021-02-09
US9771810B2 (en) 2017-09-26
WO2013104852A3 (en) 2014-02-20
BR112014016859A2 (en) 2017-06-13
RU2014132876A (en) 2016-02-27

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