UA94610C2 - Волоконная армирующая структура для изготовления детали из композитного материала - Google Patents

Волоконная армирующая структура для изготовления детали из композитного материала

Info

Publication number
UA94610C2
UA94610C2 UAA200814658A UAA200814658A UA94610C2 UA 94610 C2 UA94610 C2 UA 94610C2 UA A200814658 A UAA200814658 A UA A200814658A UA A200814658 A UAA200814658 A UA A200814658A UA 94610 C2 UA94610 C2 UA 94610C2
Authority
UA
Ukraine
Prior art keywords
reinforcement structure
production
composite material
fiber reinforcement
part made
Prior art date
Application number
UAA200814658A
Other languages
English (en)
Ukrainian (uk)
Inventor
Эрик БУЙОН
Франсуа Шарль
Каролин Люше-Пуери
Реме Бувье
Доминик Купе
Original Assignee
Снэкма Пропульсён Солид
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 Снэкма Пропульсён Солид filed Critical Снэкма Пропульсён Солид
Publication of UA94610C2 publication Critical patent/UA94610C2/ru

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/02—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
    • B32B5/08—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer the fibres or filaments of a layer being of different substances, e.g. conjugate fibres, mixture of different fibres
    • D—TEXTILES; PAPER
    • D03—WEAVING
    • D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D25/00—Woven fabrics not otherwise provided for
    • D03D25/005—Three-dimensional woven fabrics
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29B—PREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
    • B29B11/00—Making preforms
    • B29B11/14—Making preforms characterised by structure or composition
    • B29B11/16—Making preforms characterised by structure or composition comprising fillers or reinforcement
    • C—CHEMISTRY; METALLURGY
    • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08J—WORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
    • C08J5/00—Manufacture of articles or shaped materials containing macromolecular substances
    • C08J5/04—Reinforcing macromolecular compounds with loose or coherent fibrous material
    • C08J5/047—Reinforcing macromolecular compounds with loose or coherent fibrous material with mixed fibrous material
    • D—TEXTILES; PAPER
    • D03—WEAVING
    • D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D11/00—Double or multi-ply fabrics not otherwise provided for
    • D—TEXTILES; PAPER
    • D03—WEAVING
    • D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D15/00—Woven fabrics characterised by the material, structure or properties of the fibres, filaments, yarns, threads or other warp or weft elements used
    • D03D15/30—Woven fabrics characterised by the material, structure or properties of the fibres, filaments, yarns, threads or other warp or weft elements used characterised by the structure of the fibres or filaments
    • 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
    • Y10T442/00—Fabric [woven, knitted, or nonwoven textile or cloth, etc.]
    • Y10T442/20—Coated or impregnated woven, knit, or nonwoven fabric which is not [a] associated with another preformed layer or fiber layer or, [b] with respect to woven and knit, characterized, respectively, by a particular or differential weave or knit, wherein the coating or impregnation is neither a foamed material nor a free metal or alloy layer
    • Y10T442/2926—Coated or impregnated inorganic fiber fabric
    • Y10T442/2984—Coated or impregnated carbon or carbonaceous fiber fabric
    • 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
    • Y10T442/00—Fabric [woven, knitted, or nonwoven textile or cloth, etc.]
    • Y10T442/30—Woven fabric [i.e., woven strand or strip material]
    • Y10T442/3179—Woven fabric is characterized by a particular or differential weave other than fabric in which the strand denier or warp/weft pick count is specified
    • Y10T442/3195—Three-dimensional weave [e.g., x-y-z planes, multi-planar warps and/or wefts, etc.]
    • 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
    • Y10T442/00—Fabric [woven, knitted, or nonwoven textile or cloth, etc.]
    • Y10T442/30—Woven fabric [i.e., woven strand or strip material]
    • Y10T442/3179—Woven fabric is characterized by a particular or differential weave other than fabric in which the strand denier or warp/weft pick count is specified
    • Y10T442/3195—Three-dimensional weave [e.g., x-y-z planes, multi-planar warps and/or wefts, etc.]
    • Y10T442/3203—Multi-planar warp layers
    • 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
    • Y10T442/00—Fabric [woven, knitted, or nonwoven textile or cloth, etc.]
    • Y10T442/30—Woven fabric [i.e., woven strand or strip material]
    • Y10T442/3179—Woven fabric is characterized by a particular or differential weave other than fabric in which the strand denier or warp/weft pick count is specified
    • Y10T442/3195—Three-dimensional weave [e.g., x-y-z planes, multi-planar warps and/or wefts, etc.]
    • Y10T442/3211—Multi-planar weft layers

Abstract

Волоконная армирующая структура (10), вытканная в виде единой детали, для изготовления детали из композитного материала, имеет внутреннюю часть (12), или сердцевину, выполненную с помощью трехмерного тканья из нитей, образованных волокнами ограниченной длины, и часть, которая граничит с внешней поверхностью, или оболочку, выполненную с помощью тканья из нитей, образованных волокнами неограниченной длины.
UAA200814658A 2006-06-21 2007-06-20 Волоконная армирующая структура для изготовления детали из композитного материала UA94610C2 (ru)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0652572A FR2902802B1 (fr) 2006-06-21 2006-06-21 Structure fibreuse de renfort pour piece en materiau composite et piece la comportant

Publications (1)

Publication Number Publication Date
UA94610C2 true UA94610C2 (ru) 2011-05-25

Family

ID=37459374

Family Applications (1)

Application Number Title Priority Date Filing Date
UAA200814658A UA94610C2 (ru) 2006-06-21 2007-06-20 Волоконная армирующая структура для изготовления детали из композитного материала

Country Status (13)

Country Link
US (2) US8263504B2 (ru)
EP (1) EP2032750B1 (ru)
JP (1) JP5043936B2 (ru)
KR (1) KR101387890B1 (ru)
CN (1) CN101473079B (ru)
BR (1) BRPI0715593B1 (ru)
CA (1) CA2655578C (ru)
DE (1) DE602007005479D1 (ru)
FR (1) FR2902802B1 (ru)
NO (1) NO336887B1 (ru)
RU (1) RU2427675C2 (ru)
UA (1) UA94610C2 (ru)
WO (1) WO2007148018A1 (ru)

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FR2952052B1 (fr) 2009-10-30 2012-06-01 Snecma Propulsion Solide Piece en materiau composite thermostructural de faible epaisseur et procede de fabrication.
FR2968679B1 (fr) * 2010-12-13 2014-02-07 Snecma Structure fibreuse pour piece en materiau composite ayant une ou plusieurs parties en forme d'arche
US8387504B2 (en) * 2011-01-06 2013-03-05 General Electric Company Fiber-reinforced Al-Li compressor airfoil and method of fabricating
FR2972129B1 (fr) * 2011-03-03 2013-04-12 Snecma Piece en materiau composite comportant des elements de bossage
BR112013022506A2 (pt) 2011-03-04 2016-12-06 Michael Ian Brockwell membro estrutural de absorção de energia, estrutura articulada, método de fabricação de um membro estrutural de absorção de energia, kit de peças para montar uma estrutura articulada e método de articular pelo menos dois membros estruturais entre si
RU2612927C2 (ru) * 2011-12-14 2017-03-13 Снекма Волоконная структура, сплетенная в виде единой части путем трехмерного плетения, и ее применение для изготовления детали из композитного материала
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FR3001409B1 (fr) * 2013-01-29 2015-07-03 Herakles Procede de fabrication d'une structure alveolaire de forme courbee en materiau composite
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CN106149168A (zh) * 2016-09-22 2016-11-23 天津工业大学 一种2.5d类缎纹结构织物的织造方法
US11021779B2 (en) 2017-05-01 2021-06-01 Rolls-Royce High Temperature Composites Inc. Sacrificial 3-dimensional weaving method and ceramic matrix composites formed therefrom
FR3066715B1 (fr) 2017-05-24 2021-02-12 Safran Aircraft Engines Texture fibreuse destinee a la fabrication d'un carter de moteur aeronautique
WO2019097147A1 (fr) 2017-11-14 2019-05-23 Safran Ceramics Structure fibreuse et piece en materiau composite incorporant une telle structure
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Also Published As

Publication number Publication date
US8263504B2 (en) 2012-09-11
NO20085296L (no) 2009-03-19
FR2902802A1 (fr) 2007-12-28
US8426326B2 (en) 2013-04-23
CA2655578A1 (en) 2007-12-27
US20120258641A1 (en) 2012-10-11
EP2032750B1 (fr) 2010-03-24
CN101473079B (zh) 2011-06-15
EP2032750A1 (fr) 2009-03-11
WO2007148018A1 (fr) 2007-12-27
CA2655578C (en) 2016-05-24
DE602007005479D1 (de) 2010-05-06
KR101387890B1 (ko) 2014-04-21
US20090280707A1 (en) 2009-11-12
BRPI0715593A2 (pt) 2013-01-22
KR20090021385A (ko) 2009-03-03
RU2009101081A (ru) 2010-07-27
FR2902802B1 (fr) 2008-12-12
JP5043936B2 (ja) 2012-10-10
RU2427675C2 (ru) 2011-08-27
BRPI0715593B1 (pt) 2017-09-26
JP2009541602A (ja) 2009-11-26
CN101473079A (zh) 2009-07-01
NO336887B1 (no) 2015-11-23

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