MX376273B - Preforma y método para reforzar nodos de fibra tejida. - Google Patents

Preforma y método para reforzar nodos de fibra tejida.

Info

Publication number
MX376273B
MX376273B MX2016006104A MX2016006104A MX376273B MX 376273 B MX376273 B MX 376273B MX 2016006104 A MX2016006104 A MX 2016006104A MX 2016006104 A MX2016006104 A MX 2016006104A MX 376273 B MX376273 B MX 376273B
Authority
MX
Mexico
Prior art keywords
preform
preforms
woven fiber
fiber nodes
reinforcing woven
Prior art date
Application number
MX2016006104A
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 MX376273B publication Critical patent/MX376273B/es

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23BTURNING; BORING
    • B23B3/00General-purpose turning-machines or devices, e.g. centre lathes with feed rod and lead screw; Sets of turning-machines
    • B23B3/08Turning-machines characterised by the use of faceplates
    • B23B3/12Turning-machines characterised by the use of faceplates with the faceplate vertical, i.e. face lathes
    • DTEXTILES; PAPER
    • D03WEAVING
    • D03DWOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D3/00Woven fabrics characterised by their shape
    • D03D3/06Fabrics of varying width
    • 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
    • B29DPRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D99/00Subject matter not provided for in other groups of this subclass
    • B29D99/0089Producing honeycomb structures
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B3/00Layered 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
    • B32B3/10Layered 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
    • B32B3/12Layered 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00Layered 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
    • B32B5/02Layered 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
    • B32B5/024Woven fabric
    • 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
    • B29L2031/60Multitubular or multicompartmented articles, e.g. honeycomb
    • B29L2031/608Honeycomb structures
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/19Sheets or webs edge spliced or joined
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/24Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24149Honeycomb-like
    • Y10T428/24165Hexagonally shaped cavities
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/24Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24174Structurally defined web or sheet [e.g., overall dimension, etc.] including sheet or component perpendicular to plane of web or sheet
    • Y10T428/24182Inward from edge of web or sheet
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T442/00Fabric [woven, knitted, or nonwoven textile or cloth, etc.]
    • Y10T442/30Woven fabric [i.e., woven strand or strip material]
    • Y10T442/3179Woven fabric is characterized by a particular or differential weave other than fabric in which the strand denier or warp/weft pick count is specified
    • Y10T442/3195Three-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.
MX2016006104A 2011-01-21 2012-01-20 Preforma y método para reforzar nodos de fibra tejida. MX376273B (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
MX376273B true MX376273B (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 After (3)

Application Number Title Priority Date Filing Date
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.

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)

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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
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US9527238B2 (en) 2015-03-13 2016-12-27 Rohr, Inc. Method of manufacturing thrust reverser cascades
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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

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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
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
MX376705B (es) 2025-03-07
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

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