MX2012004924A - Preforma de fibra, compuesto reforzado con fibra y metodo para fabricar los mismos. - Google Patents

Preforma de fibra, compuesto reforzado con fibra y metodo para fabricar los mismos.

Info

Publication number
MX2012004924A
MX2012004924A MX2012004924A MX2012004924A MX2012004924A MX 2012004924 A MX2012004924 A MX 2012004924A MX 2012004924 A MX2012004924 A MX 2012004924A MX 2012004924 A MX2012004924 A MX 2012004924A MX 2012004924 A MX2012004924 A MX 2012004924A
Authority
MX
Mexico
Prior art keywords
preform
spiral
fiber
making
reinforced composite
Prior art date
Application number
MX2012004924A
Other languages
English (en)
Inventor
Jonathan Goering
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 MX2012004924A publication Critical patent/MX2012004924A/es

Links

Classifications

    • 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
    • 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
    • D—TEXTILES; PAPER
    • D03—WEAVING
    • D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D3/00—Woven fabrics characterised by their shape
    • D—TEXTILES; PAPER
    • D03—WEAVING
    • D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D3/00—Woven fabrics characterised by their shape
    • D03D3/08—Arched, corrugated, or like fabrics
    • 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
    • Y10T428/13—Hollow or container type article [e.g., tube, vase, etc.]
    • Y10T428/1352—Polymer or resin containing [i.e., natural or synthetic]
    • Y10T428/1362—Textile, fabric, cloth, or pile containing [e.g., web, net, woven, knitted, mesh, nonwoven, matted, 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
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24058—Structurally defined web or sheet [e.g., overall dimension, etc.] including grain, strips, or filamentary elements in respective layers or components in angular relation
    • Y10T428/24074—Strand or strand-portions

Landscapes

  • Engineering & Computer Science (AREA)
  • Textile Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Woven Fabrics (AREA)
  • Reinforced Plastic Materials (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
  • Moulding By Coating Moulds (AREA)

Abstract

Se describen una preforma de fibra tejida (100, 200), un compuesto reforzado con fibra que incorpora la preforma (100, 200), y métodos para fabricar los mismos. La preforma tejida (100, 200) incluye una pluralidad de hilos o fibras de urdimbre y de trama entretejidos para formar una tela en espiral continua (50). La tela en espiral (50) puede tomar la forma de una espiral de Arquímedes. Los hilos de trama en la preforma (100, 200) pueden tener una separación de pasada uniforme o variable, o una separación angular uniforme o variable. La tela en espiral (50) de la espiral de Arquímedes puede ensamblarse o enrollarse para formar una estructura de cubierta cónica, la cual puede ser una porción de un huso o un difusor. La tela en espiral (50) puede tejerse sobre un telar equipado con un mecanismo tomador diferencial.
MX2012004924A 2009-10-28 2010-10-26 Preforma de fibra, compuesto reforzado con fibra y metodo para fabricar los mismos. MX2012004924A (es)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US12/607,715 US9186850B2 (en) 2009-10-28 2009-10-28 Fiber preform, fiber reinforced composite, and method of making thereof
PCT/US2010/054117 WO2011056586A1 (en) 2009-10-28 2010-10-26 Fiber preform, fiber reinforced composite, and method of making thereof

Publications (1)

Publication Number Publication Date
MX2012004924A true MX2012004924A (es) 2012-08-15

Family

ID=43646444

Family Applications (1)

Application Number Title Priority Date Filing Date
MX2012004924A MX2012004924A (es) 2009-10-28 2010-10-26 Preforma de fibra, compuesto reforzado con fibra y metodo para fabricar los mismos.

Country Status (17)

Country Link
US (1) US9186850B2 (es)
EP (1) EP2493677B1 (es)
JP (1) JP5793502B2 (es)
KR (1) KR101910417B1 (es)
CN (1) CN102666075B (es)
AU (1) AU2010315543B2 (es)
BR (1) BR112012009798B1 (es)
CA (1) CA2778982C (es)
ES (1) ES2532475T3 (es)
HU (1) HUE024567T2 (es)
MX (1) MX2012004924A (es)
PL (1) PL2493677T3 (es)
PT (1) PT2493677E (es)
RU (1) RU2542976C2 (es)
TW (1) TWI535905B (es)
WO (1) WO2011056586A1 (es)
ZA (1) ZA201203044B (es)

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EP2444535B1 (en) * 2010-10-19 2013-09-04 Tape Weaving Sweden AB Method and means for measured control of tape-like warps for shedding and taking-up operations
US10648106B2 (en) 2012-03-05 2020-05-12 Goodrich Corporation Systems and methods for reduced crimp carbon fiber helical fabric
FR3048435B1 (fr) * 2016-03-02 2018-04-06 Safran Aircraft Engines Installation et procede pour la fabrication d'une texture fibreuse en forme de bande presentant en section transversale un profil evolutif
CN106747533B (zh) * 2016-06-13 2017-12-19 北京航空航天大学 一种提高发动机热端构件用陶瓷基复合材料力学性能的纤维排布方式
CN106435956B (zh) * 2016-10-12 2018-04-20 中材科技股份有限公司 一种锥形中空夹芯回转体织物及其应用
FR3062659B1 (fr) * 2017-02-03 2019-03-22 Safran Aircraft Engines Appel de preforme dans un metier a tisser du type jacquard
EP3750798B1 (en) * 2017-07-13 2022-02-09 Ratier-Figeac SAS Protection of propeller components
FR3070402B1 (fr) * 2017-08-30 2020-08-28 Safran Aircraft Engines Texture fibreuse tissee pour la formation d'une preforme de carter
CN108656690B (zh) * 2018-07-23 2024-05-28 沈阳丰禾包装有限公司 一种高强纤维复合板结构
MX2021001250A (es) * 2018-08-01 2021-05-27 Albany Eng Composites Inc Preformas curvas y metodos de fabricacion de las mismas.
CN109518340A (zh) * 2019-01-11 2019-03-26 深圳市奔雷材料制品有限公司 一种纤维多角度编织复合毡及其制造方法以及制造装置
GB2585036B (en) * 2019-06-25 2021-08-11 North Thin Ply Tech Sarl Fibre-reinforced composite tubular shafts and manufacture thereof
CN111890701A (zh) * 2020-07-31 2020-11-06 杭州紫麟科技有限公司 一种2.5d纤维机织增强树脂基复合材料及其制备方法
CN114086294B (zh) * 2021-11-19 2023-11-21 北京方硕复合材料技术有限公司 一种变形易于调控的纤维织物及模具组件
CN115369542B (zh) * 2022-08-29 2023-05-23 华南理工大学 一种带螺纹的机织纤维增强筋及织造方法
TWI821018B (zh) * 2022-11-14 2023-11-01 天下長榮科技有限公司 交織纖維複合材料

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Also Published As

Publication number Publication date
KR101910417B1 (ko) 2018-12-28
JP2013509505A (ja) 2013-03-14
AU2010315543B2 (en) 2016-10-27
ES2532475T3 (es) 2015-03-27
TW201120264A (en) 2011-06-16
HUE024567T2 (hu) 2016-02-29
CN102666075B (zh) 2014-11-26
EP2493677A1 (en) 2012-09-05
CA2778982C (en) 2017-10-24
CA2778982A1 (en) 2011-05-12
JP5793502B2 (ja) 2015-10-14
BR112012009798A2 (pt) 2016-10-18
RU2012118069A (ru) 2013-12-10
PL2493677T3 (pl) 2015-06-30
RU2542976C2 (ru) 2015-02-27
BR112012009798B1 (pt) 2020-03-10
US20110097526A1 (en) 2011-04-28
US9186850B2 (en) 2015-11-17
ZA201203044B (en) 2013-06-26
EP2493677B1 (en) 2014-12-17
WO2011056586A1 (en) 2011-05-12
PT2493677E (pt) 2015-03-24
AU2010315543A1 (en) 2012-05-24
TWI535905B (zh) 2016-06-01
KR20120112431A (ko) 2012-10-11
CN102666075A (zh) 2012-09-12

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