MX376705B - Preforma y metodo para reforzar nodos de fibra tejida. - Google Patents

Preforma y metodo para reforzar nodos de fibra tejida.

Info

Publication number
MX376705B
MX376705B MX2016005377A MX2016005377A MX376705B MX 376705 B MX376705 B MX 376705B MX 2016005377 A MX2016005377 A MX 2016005377A MX 2016005377 A MX2016005377 A MX 2016005377A MX 376705 B MX376705 B MX 376705B
Authority
MX
Mexico
Prior art keywords
preform
preforms
woven fiber
fiber nodes
reinforcing woven
Prior art date
Application number
MX2016005377A
Other languages
English (en)
Inventor
Jonathan Goering
Keith Edward Burgess
Original Assignee
Albany Eng Composites Inc
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 Albany Eng Composites Inc filed Critical Albany Eng Composites Inc
Publication of MX376705B publication Critical patent/MX376705B/es

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23B—TURNING; BORING
    • B23B3/00—General-purpose turning-machines or devices, e.g. centre lathes with feed rod and lead screw; Sets of turning-machines
    • B23B3/08—Turning-machines characterised by the use of faceplates
    • B23B3/12—Turning-machines characterised by the use of faceplates with the faceplate vertical, i.e. face lathes
    • D—TEXTILES; PAPER
    • D03—WEAVING
    • D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D3/00—Woven fabrics characterised by their shape
    • D03D3/06—Fabrics of varying width
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/06—Fibrous reinforcements only
    • B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
    • B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
    • B29C70/22—Fibrous 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
    • B29C70/222—Fibrous 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D99/00—Subject matter not provided for in other groups of this subclass
    • B29D99/0089—Producing honeycomb structures
    • 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
    • B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
    • B32B3/10—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material
    • B32B3/12—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material characterised by a layer of regularly- arranged cells, e.g. a honeycomb structure
    • 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
    • B32B5/024—Woven fabric
    • 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
    • D—TEXTILES; PAPER
    • D03—WEAVING
    • D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D3/00—Woven fabrics characterised by their shape
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00—Other particular articles
    • B29L2031/60—Multitubular or multicompartmented articles, e.g. honeycomb
    • B29L2031/608—Honeycomb structures
    • 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
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/19—Sheets or webs edge spliced or joined
    • 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
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24149—Honeycomb-like
    • Y10T428/24165—Hexagonally shaped cavities
    • 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
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24174—Structurally defined web or sheet [e.g., overall dimension, etc.] including sheet or component perpendicular to plane of web or sheet
    • Y10T428/24182—Inward from edge of web or sheet
    • 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.]

Landscapes

  • Engineering & Computer Science (AREA)
  • Textile Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Woven Fabrics (AREA)
  • Moulding By Coating Moulds (AREA)
  • Reinforced Plastic Materials (AREA)

Abstract

Preformas (20, 30, 40, 50) que incluyen nodos (29, 39, 49, 59) reforzados con fibra para utilizarse en estructuras compuestas reforzadas con fibra y métodos para producir estructuras compuestas reforzadas con fibra. Las preformas con elementos de tela tejida que se extienden radialmente desde un nodo común incluyen al menos una fibra de refuerzo entretejida entre al menos dos elementos y pasa a través del nodo. Un método para ensamblar las estructuras (60, 62) de preforma, utiliza las preformas para proporcionar una estructura con nodos reforzados.
MX2016005377A 2011-01-21 2012-01-20 Preforma y metodo para reforzar nodos de fibra tejida. MX376705B (es)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/011,633 US8642151B2 (en) 2011-01-21 2011-01-21 Preform and method for reinforcing woven fiber nodes
PCT/US2012/022024 WO2012100159A1 (en) 2011-01-21 2012-01-20 Preform and method for reinforcing woven fiber nodes

Publications (1)

Publication Number Publication Date
MX376705B true MX376705B (es) 2025-03-07

Family

ID=45569746

Family Applications (4)

Application Number Title Priority Date Filing Date
MX2016006104A MX376273B (es) 2011-01-21 2012-01-20 Preforma y método para reforzar nodos de fibra tejida.
MX2016005377A MX376705B (es) 2011-01-21 2012-01-20 Preforma y metodo para reforzar nodos de fibra tejida.
MX2016005280A MX376272B (es) 2011-01-21 2012-01-20 Preforma y metodo para reforzar nodos de fibra tejida.
MX2013008491A MX342504B (es) 2011-01-21 2012-01-20 Preforma y metodo para reforzar nodos de fibra tejida.

Family Applications Before (1)

Application Number Title Priority Date Filing Date
MX2016006104A MX376273B (es) 2011-01-21 2012-01-20 Preforma y método para reforzar nodos de fibra tejida.

Family Applications After (2)

Application Number Title Priority Date Filing Date
MX2016005280A MX376272B (es) 2011-01-21 2012-01-20 Preforma y metodo para reforzar nodos de fibra tejida.
MX2013008491A MX342504B (es) 2011-01-21 2012-01-20 Preforma y metodo para reforzar nodos de fibra tejida.

Country Status (15)

Country Link
US (4) US8642151B2 (es)
EP (1) EP2665599B1 (es)
JP (1) JP6073249B2 (es)
KR (1) KR101931660B1 (es)
CN (3) CN110039677B (es)
AU (2) AU2012207177B2 (es)
BR (2) BR112013017524B1 (es)
CA (1) CA2823717C (es)
DK (1) DK2665599T3 (es)
ES (1) ES2837723T3 (es)
MX (4) MX376273B (es)
RU (1) RU2598941C2 (es)
TW (1) TWI599690B (es)
WO (1) WO2012100159A1 (es)
ZA (1) ZA201304931B (es)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102011084441A1 (de) 2011-10-13 2013-04-18 Airbus Operations Gmbh Verfahren zum Herstellen einer Komponente zur Verbindung von Strukturen, Komponente sowie Strukturanordnung
DE102011084472B3 (de) * 2011-10-13 2013-01-03 Airbus Operations Gmbh Strukturanordnung, Luft- oder Raumfahrzeug sowie Verfahren zum Herstellen einer Strukturanordnung
DE102011084438B3 (de) 2011-10-13 2012-11-29 Airbus Operations Gmbh Verfahren zum Herstellen einer Komponente zur Verbindung von Strukturen, Verfahren zum Herstellen einer Strukturanordnung sowie Vorrichtung zum Herstellen einer Komponente zur Verbindung von Strukturen
DE102011084433A1 (de) 2011-10-13 2013-04-18 Airbus Operations Gmbh Komponente, Verstärkungsbauteil, Strukturanordnung, Luft- oder Raumfahrzeug sowie Verfahren
EP2783838B1 (en) * 2013-03-27 2015-11-18 Airbus Operations GmbH Composite reinforcement component, structural element, aircraft or spacecraft and method for producing a composite reinforcement component
US9895840B2 (en) * 2014-05-15 2018-02-20 The Boeing Company Thermoformed cascades for jet engine thrust reversers
US9527238B2 (en) 2015-03-13 2016-12-27 Rohr, Inc. Method of manufacturing thrust reverser cascades
US10830176B2 (en) 2015-08-26 2020-11-10 Rohr, Inc. Additive manufacturing fiber-reinforced, thrust reverser cascade
US11511847B2 (en) 2017-03-28 2022-11-29 The Boeing Company Skin panel of composite material having an internal grid
US10823112B2 (en) 2017-05-25 2020-11-03 The Boeing Company Method for manufacturing and assembly of a thrust reverser cascade
US11035059B2 (en) 2018-08-01 2021-06-15 Albany Engineered Composites, Inc. Curved preform and method of making thereof
US11123916B2 (en) 2019-05-06 2021-09-21 Rohr, Inc. Forming a thrust reverser cascade using corrugated bodies
US11491686B2 (en) 2019-07-22 2022-11-08 The Boeing Company Compression molded cascades with two piece mold
US11046420B2 (en) 2019-10-23 2021-06-29 The Boeing Company Trailing edge flap having a waffle grid interior structure
USD1009455S1 (en) * 2020-01-02 2024-01-02 Marmot Mountain, Llc Cube pattern

Family Cites Families (39)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4715560A (en) * 1983-03-14 1987-12-29 Lear Fan Limited Composite cruciform structure for joining intersecting structural members of an airframe and the like
JPS61179731A (ja) * 1984-12-29 1986-08-12 日本マイヤー株式会社 三次元構造材料
JPS62231073A (ja) 1986-03-31 1987-10-09 石川県 炭素繊維複合材の製造方法
GB8609865D0 (en) 1986-04-23 1986-05-29 Courtaulds Plc Composite articles
FR2637838B1 (fr) 1988-10-14 1991-01-25 Europ Propulsion Procede de fabrication de pieces composites constituees d'un voile et d'un renfort
US5026595A (en) 1989-11-09 1991-06-25 Techniweave, Inc. Woven gap filler for use in the lay-up of composite plastic structural units
US5304339A (en) 1990-05-23 1994-04-19 Le Comte Adolf Method for manufacturing a large-sized object of fiber reinforced synthetic resin
US6854388B2 (en) 1990-09-06 2005-02-15 Hunter Douglas Inc. Pearlescent honeycomb material and method for fabricating same
WO1992020503A1 (en) 1991-05-24 1992-11-26 Dow-United Technologies Composite Products, Inc. Braided complex composite parts and methods of forming same
US5277854A (en) 1991-06-06 1994-01-11 Hunt John F Methods and apparatus for making grids from fibers
US5508085A (en) 1991-10-03 1996-04-16 Tolo, Inc. Structural elements made with cores of fiber-reinforced plastic
GB9314311D0 (en) 1993-07-10 1993-08-25 3 D Composites Ltd Composite article
US5843354A (en) 1995-11-21 1998-12-01 General Electric Company Method for compression molding a fan blade
CN1042754C (zh) * 1997-06-27 1999-03-31 天津纺织工学院 多层机织物
US6179943B1 (en) 1997-07-30 2001-01-30 The Boeing Company Method for forming a composite acoustic panel
CA2253037C (en) 1997-11-12 2004-11-02 Sakura Rubber Co., Ltd. Method of manufacturing structure by using biodegradable mold
US6245274B1 (en) 1998-03-02 2001-06-12 The United States Of America As Represented By The Secretary Of The Air Force Method for making advanced grid-stiffened structures
US6149851A (en) 1998-04-30 2000-11-21 Alliant Techsystems Inc. Tooling apparatus and method for producing grid stiffened fiber reinforced structures
US6103337A (en) 1998-07-09 2000-08-15 Albany International Techniweave, Inc. Fiber-reinforced composite materials structures and methods of making same
US6630093B1 (en) 1999-08-21 2003-10-07 Ronald D. Jones Method for making freeform-fabricated core composite articles
JP2001206778A (ja) 2000-01-24 2001-07-31 Ishikawajima Harima Heavy Ind Co Ltd 繊維強化複合部材の製造方法およびその装置
US6986940B1 (en) 2000-07-27 2006-01-17 General Electric Company Fiber reinforced composite article, fiber member, and method for making
US6374570B1 (en) * 2000-08-25 2002-04-23 Lockheed Martin Corporation Apparatus and method for joining dissimilar materials to form a structural support member
US6520706B1 (en) * 2000-08-25 2003-02-18 Lockheed Martin Corporation Composite material support structures with sinusoidal webs and method of fabricating same
WO2002081210A1 (en) 2001-04-06 2002-10-17 Marion Composites, A Division Of Advanced Technical Products, Inc. Method of manufacturing a hollow section, grid stiffened panel
US6712099B2 (en) 2001-06-15 2004-03-30 Lockheed Martin Corporation Three-dimensional weave architecture
US6446675B1 (en) * 2001-07-05 2002-09-10 Albany International Techniweave, Inc. Minimum distortion 3D woven preforms
US6630095B2 (en) 2001-08-01 2003-10-07 Lockheed Martin Corporation Method for making composite structures
US6627142B2 (en) 2001-08-01 2003-09-30 Lockheed Martin Corporation Apparatus for making composite structures and method for making same
US20040213953A1 (en) * 2003-04-24 2004-10-28 Lockheed Martin Corporation Apparatus, system, and method of joining structural components with a tapered tension bond joint
US7244487B2 (en) * 2003-04-24 2007-07-17 Lockheed Martin Corporation Apparatus, system, and method of joining structural components with a tapered tension bond joint
US7713893B2 (en) * 2004-12-08 2010-05-11 Albany Engineered Composites, Inc. Three-dimensional woven integrally stiffened panel
US7625510B2 (en) 2005-11-29 2009-12-01 Lockheed Martin Corporation System, method, and apparatus for production-worthy, low cost composite tool fabrication
US20080060755A1 (en) 2006-09-13 2008-03-13 General Electric Corporation composite corner and method for making composite corner
US7960298B2 (en) * 2007-12-07 2011-06-14 Albany Engineered Composites, Inc. Method for weaving closed structures with intersecting walls
US8152948B2 (en) * 2008-01-09 2012-04-10 The Boeing Company Contoured composite parts
US7712488B2 (en) 2008-03-31 2010-05-11 Albany Engineered Composites, Inc. Fiber architecture for Pi-preforms
US8079387B2 (en) * 2008-10-29 2011-12-20 Albany Engineered Composites, Inc. Pi-shaped preform
US8846553B2 (en) * 2008-12-30 2014-09-30 Albany Engineered Composites, Inc. Woven preform with integral off axis stiffeners

Also Published As

Publication number Publication date
MX376272B (es) 2025-03-07
JP6073249B2 (ja) 2017-02-01
CA2823717A1 (en) 2012-07-26
TWI599690B (zh) 2017-09-21
CN107097366A (zh) 2017-08-29
EP2665599B1 (en) 2020-12-09
RU2013130165A (ru) 2015-02-27
MX342504B (es) 2016-10-03
BR112013017524B1 (pt) 2020-12-29
US9757803B2 (en) 2017-09-12
MX376273B (es) 2025-03-07
AU2012207177A1 (en) 2013-07-25
MX2013008491A (es) 2013-08-12
US8642151B2 (en) 2014-02-04
WO2012100159A1 (en) 2012-07-26
CN103328194A (zh) 2013-09-25
CN103328194B (zh) 2016-12-21
AU2012207177B2 (en) 2017-05-11
ZA201304931B (en) 2014-09-25
US20120189798A1 (en) 2012-07-26
AU2017204140A1 (en) 2017-07-06
BR122019026067B1 (pt) 2021-03-16
AU2017204140B2 (en) 2019-04-04
JP2014504671A (ja) 2014-02-24
CA2823717C (en) 2019-01-08
CN110039677B (zh) 2021-08-24
CN110039677A (zh) 2019-07-23
BR112013017524A2 (pt) 2016-10-04
KR101931660B1 (ko) 2018-12-21
US20140120296A1 (en) 2014-05-01
CN107097366B (zh) 2019-08-13
US9132603B2 (en) 2015-09-15
KR20140007371A (ko) 2014-01-17
TW201241257A (en) 2012-10-16
US20150284884A1 (en) 2015-10-08
EP2665599A1 (en) 2013-11-27
US20140220295A1 (en) 2014-08-07
RU2598941C2 (ru) 2016-10-10
US9205494B2 (en) 2015-12-08
ES2837723T3 (es) 2021-07-01
DK2665599T3 (da) 2021-01-04

Similar Documents

Publication Publication Date Title
MX376272B (es) Preforma y metodo para reforzar nodos de fibra tejida.
PE20142423A1 (es) Barra de refuerzo y metodo para la fabricacion de la misma
MX2014009840A (es) Preforma en pi con fibras sesgadas.
BRPI0923609A2 (pt) pré-formas integralmente tecida com endurecedores em duas ou mais direções, compósitos reforçados de fibra e métodos de formação de pré-forma integralmente tecida e de compósito reforçado de fibra
MX2010005051A (es) Postes laminados/tejidos tridimensionales hibridos para aplicaciones estructurales compuestos.
BR132020021868E2 (pt) peneira para uma máquina de filtração vibratória; peneira vibratória e método para fabricação de uma peneira para uma máquina de filtração vibratória
TW200728550A (en) Hybrid three-dimensional woven/laminated struts for composite structural applications
EP3075785A4 (en) HEAT-CURABLE RESIN COMPOSITION, PREPREG AND METHOD FOR PRODUCING A FIBER-REINFORCED COMPOSITE MATERIAL USING THE SAME
PL2630282T3 (pl) Tkane preformy rurowe, kompozyty wzmocnione włóknami i sposoby ich wytwarzania
BR112014015754A8 (pt) fibras de carbono revestidas com agente de colagem, processo de produção das fibras de carbono, pré-impregnado e material compósito reforçado com fibras de carbono
EP2794272A4 (en) PREPREG, FIBER-REINFORCED COMPOSITE MATERIAL AND MANUFACTURING METHOD FOR THE FIBER-REINFORCED COMPOSITE MATERIAL
MX2015012227A (es) Resorte de láminas compuesto de alta resistencia, de peso ligero y método de producción.
EP2796325A4 (en) BUMPER RAILBARS WITH A FIBER-REFORMING MATERIAL WITH AN INSIDE HOLLOW SECTION AND BUMPER ACCORDING TO THIS
BRPI0909269A2 (pt) Pré-impregnado para fabricar um material compósito reforçado com fibra, método para fabricar um membro estrutural alongado de material compósito reforçado com fibra, e, uso de um pré-impregnado
BRPI0920714A2 (pt) dispositivo para a deposição e o drapeamento de seções de uma estrutura de fibra reforçada para a fabricação de um produto semiacabado, bem como, processo
BR112014013260A2 (pt) fibra de carbono com um acabamento condutor, método para produzir fibras de carbono para materiais compósitos tendo melhorada condutividade, e, material compósito reforçado por fibra
FR2970715B1 (fr) Structure fibreuse tissee multicouches ayant une partie tubulaire creuse, procede de fabrication et piece composite la comportant
BR112015013093A2 (pt) processo para produzir um material compósito reforçado com fibra, com uma matriz de poliamida e material compósito reforçado com fibra.
BR112016029528A2 (pt) ?método de produção de uma camada de reforço de fibra contínua a partir de mantas de fibras individuais?
EP2811054A4 (en) COMPOSITE FIBER, METHOD FOR PRODUCING A POLYURETHANELASTOMER TISSUE AND POLYURETHANEELASTOMER TISSUE
EP2484711A4 (en) METHOD FOR PRODUCING A FIBER-REINFORCED COMPOSITE, HEAT-RESISTANT MATERIAL USING THIS COMPOSITE AND HEAT-RESISTANT TREE MATERIAL USING THIS COMPOSITE
BR112014017253A2 (pt) processo para a fabricação de um tecido tecido de reforço, de um artigo compósito e de uma pluralidade de peças em bruto, tecido tecido de reforço, material pré-formado, material compósito reforçado com fibra, e, conjunto de peça em bruto
PH12016500622B1 (en) A modular structure and said modular structure`s structural members made of composite material
EP3434823A4 (en) METHOD FOR PRODUCING A COMPOSITE TISSUE, COMPOSITE TISSUE AND CARBON FIBER REINFORCED SHAPING
MX383576B (es) Elemento de construccion para suelos sobreelevados y similares y metodo de fabricacion.