DE60217488D1 - Dreidimensionale webstruktur - Google Patents

Dreidimensionale webstruktur

Info

Publication number
DE60217488D1
DE60217488D1 DE60217488T DE60217488T DE60217488D1 DE 60217488 D1 DE60217488 D1 DE 60217488D1 DE 60217488 T DE60217488 T DE 60217488T DE 60217488 T DE60217488 T DE 60217488T DE 60217488 D1 DE60217488 D1 DE 60217488D1
Authority
DE
Germany
Prior art keywords
web structure
dimensional web
dimensional
web
Prior art date
Legal status (The legal status 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 status listed.)
Expired - Lifetime
Application number
DE60217488T
Other languages
English (en)
Other versions
DE60217488T2 (de
Inventor
P Schmidt
R Bersuch
A Benson
Amir Islam
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Lockheed Martin Corp
Original Assignee
Lockheed Corp
Lockheed Martin Corp
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 Lockheed Corp, Lockheed Martin Corp filed Critical Lockheed Corp
Application granted granted Critical
Publication of DE60217488D1 publication Critical patent/DE60217488D1/de
Publication of DE60217488T2 publication Critical patent/DE60217488T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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
    • B32B5/22—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
    • 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
    • B29C70/24—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 three directions forming a three dimensional 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
    • B32B1/00—Layered products having a non-planar shape
    • 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
    • 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
    • B32B2262/101—Glass 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
    • 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
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S139/00—Textiles: weaving
    • Y10S139/01—Bias fabric digest
    • 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.]
    • Y10T428/24777—Edge feature
    • 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
    • Y10T428/249921—Web or sheet containing structurally defined element or component
    • Y10T428/249924—Noninterengaged fiber-containing paper-free web or sheet which is not of specified porosity
    • 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
    • Y10T428/249921—Web or sheet containing structurally defined element or component
    • Y10T428/249924—Noninterengaged fiber-containing paper-free web or sheet which is not of specified porosity
    • Y10T428/24994—Fiber embedded in or on the surface of a polymeric matrix
    • Y10T428/249942—Fibers are aligned substantially parallel
    • Y10T428/249945—Carbon or carbonaceous fiber
    • 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)
DE2002617488 2001-06-15 2002-04-26 Dreidimensionale webstruktur Expired - Lifetime DE60217488T2 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US882831 2001-06-15
US09/882,831 US6712099B2 (en) 2001-06-15 2001-06-15 Three-dimensional weave architecture
PCT/US2002/013295 WO2002103098A2 (en) 2001-06-15 2002-04-26 Three-dimensional weave architecture

Publications (2)

Publication Number Publication Date
DE60217488D1 true DE60217488D1 (de) 2007-02-22
DE60217488T2 DE60217488T2 (de) 2007-11-15

Family

ID=25381425

Family Applications (1)

Application Number Title Priority Date Filing Date
DE2002617488 Expired - Lifetime DE60217488T2 (de) 2001-06-15 2002-04-26 Dreidimensionale webstruktur

Country Status (6)

Country Link
US (1) US6712099B2 (de)
EP (1) EP1399610B1 (de)
AU (1) AU2002303509B2 (de)
CA (1) CA2450187C (de)
DE (1) DE60217488T2 (de)
WO (1) WO2002103098A2 (de)

Families Citing this family (38)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2003023104A1 (en) * 2001-09-12 2003-03-20 Lockheed Martin Corporation Woven preform for structural joints
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
KR20120088843A (ko) 2004-08-31 2012-08-08 오베르메이어 헨리 케이 섬유 보강 복합물에 대한 고강력 결합 시스템
US7713893B2 (en) * 2004-12-08 2010-05-11 Albany Engineered Composites, Inc. Three-dimensional woven integrally stiffened panel
US7247212B2 (en) * 2004-12-21 2007-07-24 General Electric Company Orthogonal weaving for complex shape preforms
US7413999B2 (en) * 2005-11-03 2008-08-19 Albany Engineered Composites, Inc. Corner fitting using fiber transfer
US7655581B2 (en) * 2005-11-17 2010-02-02 Albany Engineered Composites, Inc. Hybrid three-dimensional woven/laminated struts for composite structural applications
US7943535B2 (en) * 2005-11-17 2011-05-17 Albany Engineered Composites, Inc. Hybrid three-dimensional woven/laminated struts for composite structural applications
US7670527B2 (en) * 2006-05-09 2010-03-02 Lockheed Martin Corporation Failsafe injected adhesive joint
FR2907800B1 (fr) * 2006-10-27 2009-03-20 Airbus France Sas Tissage tridimensionnel surfacique
US7964520B2 (en) * 2007-12-21 2011-06-21 Albany Engineered Composites, Inc. Method for weaving substrates with integral sidewalls
US7712488B2 (en) * 2008-03-31 2010-05-11 Albany Engineered Composites, Inc. Fiber architecture for Pi-preforms
FR2932408B1 (fr) * 2008-06-11 2010-05-28 Aircelle Sa Preforme destinee a former une piece mecanique structurante creuse
US8656571B2 (en) 2008-07-18 2014-02-25 The Boeing Company Strong bonded joints for cryogenic applications
US9453293B2 (en) 2008-07-18 2016-09-27 The Boeing Company Method of making a composite tank having joint with softening strip
US10399709B2 (en) * 2008-07-18 2019-09-03 The Boeing Company Method of making a device for controlling stress in joints at cryogenic temperatures
US8127802B2 (en) * 2008-10-29 2012-03-06 Albany Engineered Composites, Inc. Pi-preform with variable width clevis
US8079387B2 (en) * 2008-10-29 2011-12-20 Albany Engineered Composites, Inc. Pi-shaped preform
FR2939153B1 (fr) * 2008-11-28 2011-12-09 Snecma Propulsion Solide Realisation d'une structure fibreuse a epaisseur evolutive par tissage 3d
US8846553B2 (en) * 2008-12-30 2014-09-30 Albany Engineered Composites, Inc. Woven preform with integral off axis stiffeners
US8859083B2 (en) 2008-12-30 2014-10-14 Albany Engineered Composites, Inc. Quasi-isotropic three-dimensional preform and method of making thereof
US20100186893A1 (en) * 2009-01-29 2010-07-29 Lockheed Martin Corporation System, method and apparatus for fabricating composite structures
US7836917B1 (en) * 2009-11-18 2010-11-23 Paradox LLC Weaving connectors for three dimensional textile products
US7841369B1 (en) * 2009-11-18 2010-11-30 vParadox LLC Weaving process for production of a full fashioned woven stretch garment with load carriage capability
US8974135B2 (en) 2010-07-22 2015-03-10 The Boeing Company Fabric preform insert for a composite tank Y-joint
WO2012091695A1 (en) 2010-12-28 2012-07-05 Bell Helicopter Textron Inc. Multi-directional load joint system
US8642151B2 (en) * 2011-01-21 2014-02-04 Albany Engineered Composites, Inc. Preform and method for reinforcing woven fiber nodes
US9150985B2 (en) * 2011-11-03 2015-10-06 Groupe Ctt Inc. Method of manufacturing weaved preform with oriented weft yarns
WO2013088041A2 (fr) * 2011-12-14 2013-06-20 Snecma PREFORME FIBREUSE A SECTION EN π NOTAMMENT POUR PLATE-FORME DE SOUFFLANTE EN MATERIAU COMPOSITE
US9604389B2 (en) 2012-02-17 2017-03-28 Albany Engineered Composites, Inc. Pi-shaped preform with bias fibers
FR2991228B1 (fr) 2012-05-29 2015-03-06 Airbus Operations Sas Procede et dispositif de realisation d'un panneau composite auto-raidi
US9290865B2 (en) 2012-12-26 2016-03-22 Albany Engineered Composites, Inc. Three-dimensional woven corner fitting with lap joint preforms
CA2922198C (en) * 2013-09-04 2021-06-15 Biteam Ab Method and means for weaving a 3d fabric, 3d fabric items thereof and their use
RU2599242C1 (ru) * 2015-07-20 2016-10-10 Открытое акционерное общество "Краснокамский завод металлических сеток" Тканая трехмерная сетка
RU2596122C1 (ru) * 2015-07-20 2016-08-27 Открытое акционерное общество "Краснокамский завод металлических сеток" Тканая трехмерная сетка
RU178542U1 (ru) * 2017-02-20 2018-04-06 Федеральное государственное казенное военное образовательное учреждение высшего образования "ВОЕННАЯ АКАДЕМИЯ МАТЕРИАЛЬНО-ТЕХНИЧЕСКОГО ОБЕСПЕЧЕНИЯ имени генерала армии А.В. Хрулева" Мобильное полимерное дорожное покрытие трехмерная тканая каркасная сетка
US10927710B2 (en) * 2018-09-26 2021-02-23 Raytheon Technologies Corporation Blade outer air seal laminate T-joint
KR102197616B1 (ko) * 2019-02-15 2021-01-05 한국재료연구원 두께 방향 섬유가 연속적으로 보강된 3d 프로파일 빔 프리폼 및 이의 제조 방법

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FR2497839A1 (fr) * 1981-01-12 1982-07-16 Brochier Fils J Tissu tridimensionnel pour le renforcement de materiaux stratifies et elements en forme obtenus a partir d'un tel tissu
US4725485A (en) * 1984-03-13 1988-02-16 Shikishima Canvas Kabushiki Kaisha Textile structure for reinforced composite material
US4782864A (en) * 1984-12-31 1988-11-08 Edo Corporation Three dimensional woven fabric connector
US4671470A (en) 1985-07-15 1987-06-09 Beech Aircraft Corporation Method for fastening aircraft frame elements to sandwich skin panels covering same using woven fiber connectors
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DE68907742T2 (de) * 1988-02-19 1993-11-11 Mitsubishi Heavy Ind Ltd Textile Struktur für das Verstärken von Bauelementen, wie Balken, aus Verbundwerkstoffen und Verfahren zur Herstellung derselben.
JPH0791725B2 (ja) * 1988-02-29 1995-10-04 三菱重工業株式会社 異形断面の三次元織物
FR2653141B1 (fr) * 1989-10-16 1992-04-17 Chaignaud Ind Materiau composite et son procede de realisation.
US5026595A (en) 1989-11-09 1991-06-25 Techniweave, Inc. Woven gap filler for use in the lay-up of composite plastic structural units
DE4100738A1 (de) * 1991-01-12 1992-07-16 Vorwerk Co Interholding Bauteil auf basis eines abstandsgewebes
GB9117863D0 (en) * 1991-08-19 1991-10-09 Cambridge Consultants Fibre preforms for structural composite components
US5451448A (en) * 1993-07-01 1995-09-19 The United States Of America As Represented By The United States National Aeronautics And Space Administration Flexible ceramic thermal protection system resistant to high aeroacoustic noise comprising a three-dimensional woven-fiber structure having a multilayer top fabric layer, a bottom fabric layer and an intermediate rib fabric layer
DE4342575A1 (de) * 1993-10-12 1995-04-13 Textilma Ag Textileinlage zur Herstellung eines Faserverbundwerkstoffes sowie Faserverbundwerkstoff
US5465760A (en) * 1993-10-25 1995-11-14 North Carolina State University Multi-layer three-dimensional fabric and method for producing
US6019138A (en) * 1997-03-21 2000-02-01 Northrop Grumman Corporation Automated three-dimensional method for making integrally stiffened skin panels
US6446675B1 (en) * 2001-07-05 2002-09-10 Albany International Techniweave, Inc. Minimum distortion 3D woven preforms

Also Published As

Publication number Publication date
CA2450187A1 (en) 2002-12-27
AU2002303509B2 (en) 2007-08-02
EP1399610B1 (de) 2007-01-10
US6712099B2 (en) 2004-03-30
US20020192450A1 (en) 2002-12-19
EP1399610A2 (de) 2004-03-24
DE60217488T2 (de) 2007-11-15
WO2002103098A3 (en) 2003-12-18
WO2002103098A2 (en) 2002-12-27
CA2450187C (en) 2009-09-22

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