JP6411376B2 - 向上した引張強度を有するベール安定化複合材料 - Google Patents

向上した引張強度を有するベール安定化複合材料 Download PDF

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JP6411376B2
JP6411376B2 JP2015555156A JP2015555156A JP6411376B2 JP 6411376 B2 JP6411376 B2 JP 6411376B2 JP 2015555156 A JP2015555156 A JP 2015555156A JP 2015555156 A JP2015555156 A JP 2015555156A JP 6411376 B2 JP6411376 B2 JP 6411376B2
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reinforcing
composite material
layers
fibers
layer
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JP2016505699A5 (enExample
JP2016505699A (ja
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ケイ・ ツォツィス、トーマス
ケイ・ ツォツィス、トーマス
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Boeing Co
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Boeing Co
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    • 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
    • B32B5/022—Non-woven fabric
    • 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
    • B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B32B37/14—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers
    • 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
    • B32B5/028—Net structure, e.g. spaced apart filaments bonded at the crossing points
    • 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
    • B32B5/06—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 characterised by a fibrous or filamentary layer mechanically connected, e.g. by needling to another layer, e.g. of fibres, of paper
    • 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
    • B32B5/22—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 the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
    • B32B5/24—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 the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
    • B32B5/26—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 the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary
    • 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
    • C08J5/24—Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs
    • C08J5/247—Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs using fibres of at least two types
    • 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
    • B32B2250/00—Layers arrangement
    • B32B2250/20—All layers being fibrous or filamentary
    • 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
    • B32B2250/00—Layers arrangement
    • B32B2250/42—Alternating layers, e.g. ABAB(C), AABBAABB(C)
    • 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
    • B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
    • B32B2260/02—Composition of the impregnated, bonded or embedded layer
    • B32B2260/021—Fibrous or filamentary layer
    • B32B2260/023—Two or more layers
    • 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
    • B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
    • B32B2260/04—Impregnation, embedding, or binder material
    • B32B2260/046—Synthetic resin
    • 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
    • B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/02—Synthetic macromolecular fibres
    • 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
    • B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/10—Inorganic fibres
    • B32B2262/106—Carbon fibres, e.g. graphite fibres
    • 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
    • B32B2305/00—Condition, form or state of the layers or laminate
    • B32B2305/07—Parts immersed or impregnated in a matrix
    • B32B2305/076—Prepregs
    • 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
    • B32B2305/00—Condition, form or state of the layers or laminate
    • B32B2305/10—Fibres of continuous length
    • B32B2305/20—Fibres of continuous length in the form of a non-woven mat
    • 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
    • B32B2305/00—Condition, form or state of the layers or laminate
    • B32B2305/72—Cured, e.g. vulcanised, cross-linked
    • 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
    • B32B2307/00—Properties of the layers or laminate
    • B32B2307/50—Properties of the layers or laminate having particular mechanical properties
    • B32B2307/54—Yield strength; Tensile strength
    • 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
    • B32B2307/00—Properties of the layers or laminate
    • B32B2307/50—Properties of the layers or laminate having particular mechanical properties
    • B32B2307/542—Shear strength
    • 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
    • B32B2605/00—Vehicles
    • B32B2605/18—Aircraft

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Textile Engineering (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Health & Medical Sciences (AREA)
  • Manufacturing & Machinery (AREA)
  • Medicinal Chemistry (AREA)
  • Polymers & Plastics (AREA)
  • Organic Chemistry (AREA)
  • Reinforced Plastic Materials (AREA)
  • Laminated Bodies (AREA)
  • Moulding By Coating Moulds (AREA)
  • Nonwoven Fabrics (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
JP2015555156A 2013-01-30 2013-12-16 向上した引張強度を有するベール安定化複合材料 Active JP6411376B2 (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US13/753,708 2013-01-30
US13/753,708 US20160009051A1 (en) 2013-01-30 2013-01-30 Veil-stabilized Composite with Improved Tensile Strength
PCT/US2013/075255 WO2014120347A1 (en) 2013-01-30 2013-12-16 Veil-stabilized composite with improved tensile strength

Publications (3)

Publication Number Publication Date
JP2016505699A JP2016505699A (ja) 2016-02-25
JP2016505699A5 JP2016505699A5 (enExample) 2017-02-09
JP6411376B2 true JP6411376B2 (ja) 2018-10-24

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JP2015555156A Active JP6411376B2 (ja) 2013-01-30 2013-12-16 向上した引張強度を有するベール安定化複合材料

Country Status (5)

Country Link
US (2) US20160009051A1 (enExample)
EP (1) EP2951012A1 (enExample)
JP (1) JP6411376B2 (enExample)
CN (1) CN104781067B (enExample)
WO (1) WO2014120347A1 (enExample)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10800111B2 (en) 2015-06-16 2020-10-13 The Boeing Company Composite structure fabrication systems and methods
US10060042B2 (en) 2016-04-04 2018-08-28 The Boeing Company Tooling having a durable metallic surface over an additively formed polymer base and method of forming such tooling
CN105953969A (zh) * 2016-06-21 2016-09-21 南京航空航天大学 一种基于正交异性复合材料的腰形管应变式微压传感器
US20180162092A1 (en) * 2016-12-09 2018-06-14 The Boeing Company Fiber-modified interlayer for a composite structure and method of manufacture
TWI633020B (zh) * 2016-12-19 2018-08-21 巨大機械工業股份有限公司 碳纖維輪圈及其製造方法
US10670394B2 (en) * 2017-06-27 2020-06-02 The Boeing Company System and method for determining the direction and spacing of fiber paths for a composite ply
US10710348B2 (en) 2017-07-26 2020-07-14 The Boeing Company Methods and apparatus to increase fire resistance and fracture toughness of a composite structure
US11247413B2 (en) * 2018-12-17 2022-02-15 The Boeing Company Composite parts including hybrid plies, methods of forming the composite parts, and systems for forming the composite parts
DE102020107053A1 (de) 2020-03-13 2021-09-16 Airbus Operations Gmbh Textiler Faserverbundmaterialvorläufer und Verfahren zur Herstellung eines Bauteils aus Faserverbundmaterial
US20210316527A1 (en) * 2020-04-08 2021-10-14 The Boeing Company Interlayer and associated reinforcement structure, composite, and method
US20250282105A1 (en) * 2024-03-07 2025-09-11 United States Of America As Represented By The Administrator Of Nasa Composite parts with stitching

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Publication number Priority date Publication date Assignee Title
JP2955145B2 (ja) * 1992-09-08 1999-10-04 東レ株式会社 扁平糸織物とその製造方法および製造装置
US5905045A (en) * 1996-04-11 1999-05-18 Precision Fabrics Group, Inc. Treated veil for use in the manufacture of a fiber reinforced plastic
AU760808B2 (en) * 1999-03-23 2003-05-22 Toray Industries, Inc. Composite reinforcing fiber base material, preform and production method for fiber reinforced plastic
JP4094231B2 (ja) * 1999-04-08 2008-06-04 三菱レイヨン株式会社 複合材料用プリフォームおよび複合材料
US20040219855A1 (en) * 2003-05-02 2004-11-04 Tsotsis Thomas K. Highly porous interlayers to toughen liquid-molded fabric-based composites
US20080289743A1 (en) * 2003-05-02 2008-11-27 Tsotsis Thomas K Highly porous interlayers to toughen liquid-molded fabric-based composites
US8246882B2 (en) * 2003-05-02 2012-08-21 The Boeing Company Methods and preforms for forming composite members with interlayers formed of nonwoven, continuous materials
JP4774839B2 (ja) * 2004-07-08 2011-09-14 東レ株式会社 繊維強化複合材料の製造方法
WO2006121961A1 (en) * 2005-05-09 2006-11-16 Cytec Technology Corp. Resin-soluble thermoplastic veil for composite materials
JP2007092716A (ja) * 2005-09-30 2007-04-12 Toray Ind Inc 翼構造体およびその製造方法
US7745549B2 (en) * 2005-12-22 2010-06-29 The Boeing Company Distortional matrix of epoxy resin and diamine
GB0717507D0 (en) * 2007-09-07 2007-10-17 Cytec Tech Corp Composite materials and their use
JP5151499B2 (ja) * 2008-01-18 2013-02-27 横浜ゴム株式会社 繊維補強複合材料の成形方法及び繊維補強複合材
CA2736369C (fr) * 2008-10-23 2017-01-24 Hexcel Reinforcements Materiaux de renfort, adaptes a la constitution de pieces composites
US20120149802A1 (en) * 2010-12-14 2012-06-14 The Boeing Company Composites having distortional resin coated fibers

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Publication number Publication date
EP2951012A1 (en) 2015-12-09
US20160009051A1 (en) 2016-01-14
US20170282491A1 (en) 2017-10-05
WO2014120347A1 (en) 2014-08-07
JP2016505699A (ja) 2016-02-25
CN104781067A (zh) 2015-07-15
CN104781067B (zh) 2017-06-23

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