CN102514284B - 薄层层压材料 - Google Patents

薄层层压材料 Download PDF

Info

Publication number
CN102514284B
CN102514284B CN201110428403.2A CN201110428403A CN102514284B CN 102514284 B CN102514284 B CN 102514284B CN 201110428403 A CN201110428403 A CN 201110428403A CN 102514284 B CN102514284 B CN 102514284B
Authority
CN
China
Prior art keywords
layer
thin layer
composite
thickness
thin
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 - Fee Related
Application number
CN201110428403.2A
Other languages
English (en)
Chinese (zh)
Other versions
CN102514284A (zh
Inventor
史蒂芬·W·柴
川边和正
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.)
Mitsuya-Kisako Inc
Itochu Corp
Fukui Prefecture
ILT Corp
Original Assignee
Mitsuya-Kisako Inc
Itochu Corp
Fukui Prefecture
ILT 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 Mitsuya-Kisako Inc, Itochu Corp, Fukui Prefecture, ILT Corp filed Critical Mitsuya-Kisako Inc
Priority claimed from CN 200580032157 external-priority patent/CN101048276A/zh
Publication of CN102514284A publication Critical patent/CN102514284A/zh
Application granted granted Critical
Publication of CN102514284B publication Critical patent/CN102514284B/zh
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B31—MAKING ARTICLES OF PAPER, CARDBOARD OR MATERIAL WORKED IN A MANNER ANALOGOUS TO PAPER; WORKING PAPER, CARDBOARD OR MATERIAL WORKED IN A MANNER ANALOGOUS TO PAPER
    • B31F—MECHANICAL WORKING OR DEFORMATION OF PAPER, CARDBOARD OR MATERIAL WORKED IN A MANNER ANALOGOUS TO PAPER
    • B31F1/00—Mechanical deformation without removing material, e.g. in combination with laminating
    • B31F1/07—Embossing, i.e. producing impressions formed by locally deep-drawing, e.g. using rolls provided with complementary profiles
    • 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
    • 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
    • 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
    • B29C70/08—Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers
    • B29C70/088—Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers and with one or more layers of non-plastics material or non-specified material, e.g. supports
    • 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
    • B29C70/20—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in a single direction, e.g. roofing or other parallel fibres
    • B29C70/202—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in a single direction, e.g. roofing or other parallel fibres arranged in parallel planes or structures of fibres crossing at substantial angles, e.g. cross-moulding compound [XMC]
    • 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 [2D] structure
    • 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
    • B29C70/88—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts characterised primarily by possessing specific properties, e.g. electrically conductive or locally reinforced
    • B29C70/882—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts characterised primarily by possessing specific properties, e.g. electrically conductive or locally reinforced partly or totally electrically conductive, e.g. for EMI shielding
    • B29C70/885—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts characterised primarily by possessing specific properties, e.g. electrically conductive or locally reinforced partly or totally electrically conductive, e.g. for EMI shielding with incorporated metallic wires, nets, films or plates
    • 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
    • B32B15/00—Layered products comprising a layer of metal
    • 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
    • B32B15/00—Layered products comprising a layer of metal
    • B32B15/14—Layered products comprising a layer of metal next to a fibrous or filamentary layer
    • 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
    • B32B15/00—Layered products comprising a layer of metal
    • B32B15/20—Layered products comprising a layer of metal comprising aluminium or copper
    • 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
    • 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
    • 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
    • B32B5/02—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
    • B32B5/10—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 reinforced with filaments
    • 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
    • B32B5/12—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 the relative arrangement of fibres or filaments of different layers, e.g. the fibres or filaments being parallel or perpendicular to each other
    • 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
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
    • B32B7/04—Interconnection of layers
    • B32B7/12—Interconnection of layers using interposed adhesives or interposed materials with bonding properties
    • 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
    • B32B2260/04—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
    • B32B2262/10—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
    • 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
    • B32B2307/582—Tearability
    • B32B2307/5825—Tear resistant
    • 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
    • B32B2307/70—Other properties
    • B32B2307/718—Weight, e.g. weight per square meter
    • 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
    • B32B2419/00—Buildings or parts thereof
    • 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
    • B32B2603/00—Vanes, blades, propellers, rotors with blades
    • 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
    • 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.]
    • Y10T428/24942—Structurally defined web or sheet [e.g., overall dimension, etc.] including components having same physical characteristic in differing degree
    • Y10T428/2495—Thickness [relative or absolute]
    • Y10T428/24967—Absolute thicknesses specified
    • Y10T428/24975—No layer or component greater than 5 mils thick

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Textile Engineering (AREA)
  • Laminated Bodies (AREA)
  • Reinforced Plastic Materials (AREA)
  • Mechanical Treatment Of Semiconductor (AREA)
CN201110428403.2A 2004-09-24 2005-09-23 薄层层压材料 Expired - Fee Related CN102514284B (zh)

Applications Claiming Priority (5)

Application Number Priority Date Filing Date Title
US61274004P 2004-09-24 2004-09-24
US60/612,740 2004-09-24
US66834105P 2005-04-04 2005-04-04
US60/668,341 2005-04-04
CN 200580032157 CN101048276A (zh) 2004-09-24 2005-09-23 薄层层压材料

Related Parent Applications (1)

Application Number Title Priority Date Filing Date
CN 200580032157 Division CN101048276A (zh) 2004-09-24 2005-09-23 薄层层压材料

Publications (2)

Publication Number Publication Date
CN102514284A CN102514284A (zh) 2012-06-27
CN102514284B true CN102514284B (zh) 2015-08-19

Family

ID=36119591

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201110428403.2A Expired - Fee Related CN102514284B (zh) 2004-09-24 2005-09-23 薄层层压材料

Country Status (13)

Country Link
US (1) US20060093802A1 (https=)
EP (1) EP1793989B1 (https=)
JP (3) JP2008514458A (https=)
KR (1) KR101229035B1 (https=)
CN (1) CN102514284B (https=)
AT (1) ATE553917T1 (https=)
AU (1) AU2005289392B2 (https=)
BR (1) BRPI0516061A (https=)
CA (1) CA2581042C (https=)
RU (1) RU2420407C2 (https=)
SG (1) SG155936A1 (https=)
TW (1) TWI401160B (https=)
WO (1) WO2006037083A2 (https=)

Families Citing this family (44)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102006035847B4 (de) 2006-08-01 2009-11-19 Airbus Deutschland Gmbh Strukturanordnung sowie Verfahren zum Herstellen eines Bauteils für die Luft-und Raumfahrt
CA2602319A1 (en) * 2006-09-25 2008-03-25 General Electric Company Blade containment system for a gas turbine engine
JP5590818B2 (ja) * 2009-04-30 2014-09-17 ジャパンマリンユナイテッド株式会社 Ｆｒｐサンドイッチパネル構造体
US8545657B2 (en) * 2009-10-30 2013-10-01 Lawrence Livermore National Security, Llc Methods for tape fabrication of continuous filament composite parts and articles of manufacture thereof
US20110143082A1 (en) * 2010-06-29 2011-06-16 General Electric Company Ply drops modifications for composite laminate materials and related methods
NL2005536C2 (en) * 2010-10-15 2012-04-17 Univ Delft Tech Aircraft wing and fiber metal laminate forming part of such an aircraft wing.
ES2680620T3 (es) 2011-01-12 2018-09-10 Companie Chomarat Estructuras laminadas de material compuesto y métodos de fabricación y uso de las mismas
JP5812439B2 (ja) * 2011-03-29 2015-11-11 東洋紡株式会社 繊維強化熱可塑性樹脂の積層成形品
WO2013015101A1 (ja) * 2011-07-28 2013-01-31 三菱樹脂株式会社 炭素繊維強化炭素複合体およびその製造方法
US9168998B2 (en) * 2011-11-23 2015-10-27 The Boeing Company Composite propeller spar
FR2997144B1 (fr) 2012-10-22 2014-11-21 Hydromecanique & Frottement Ensemble d'articulation autolubrifiant fonctionnant sous fortes charges en regime dynamique
FR2997146B1 (fr) 2012-10-22 2014-11-21 Hydromecanique & Frottement Element d'articulation autolubrifiant fonctionnant sous fortes charges en regime dynamique
US20150030805A1 (en) 2013-07-29 2015-01-29 Compagnie Chomarat Composite bi-angle and thin-ply laminate tapes and methods for manufacturing and using the same
FR3023880B1 (fr) * 2014-07-16 2017-05-26 Hydromecanique & Frottement Piece composite de frottement autolubrifiante
US9950495B2 (en) 2014-07-24 2018-04-24 Nugripmetal S.A.R.L. System and method for additive manufacturing of a three-dimensional object
US9259899B1 (en) * 2015-01-09 2016-02-16 R.A. Investment Management S.A.R.L. Thin layer laminate
WO2016115247A1 (en) * 2015-01-13 2016-07-21 TenCate Advanced Composites USA, Inc. Composite laminates with syntactic cores
US9360067B1 (en) 2015-02-05 2016-06-07 R. A. Investment Management S.A.R.L. Hybrid laminate
CN105552567A (zh) * 2015-12-09 2016-05-04 上海复合材料科技有限公司 天线反射面及其制备方法
RU2620430C1 (ru) * 2015-12-10 2017-05-25 Российская Федерация от имени которой выступает Министерство промышленности и торговли Российской Федерации (Минпромторг России) Силовая решетка из полимерного композиционного материала
US10315382B2 (en) 2016-12-22 2019-06-11 Gripmetal Limited Process for manufacturing textured laminate sheet
US20190389096A1 (en) * 2017-02-22 2019-12-26 Mitsubishi Heavy Industries, Ltd. Composite material and method for manufacturing composite material
WO2018187186A1 (en) 2017-04-04 2018-10-11 The Board Of Trustees Of The Leland Stanford Junior University Double-double composite sub-laminate structures and methods for manufacturing and using the same
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
CN108045016A (zh) * 2017-12-26 2018-05-18 宜兴市天宇世纪高新科技有限公司 一种高强度、高模量碳纤维板
FR3079164B1 (fr) 2018-03-23 2021-10-22 Arkema France Materiau fibreux impregne de polymere thermoplastique d'epaisseur inferieure ou egale a 100μm et son procede de preparation
FR3079163B1 (fr) * 2018-03-23 2021-10-15 Arkema France Nappe de materiau fibreux impregne, son procede de fabrication et son utilisation pour la fabrication de pieces composites en trois dimensions
EP3587477B1 (en) * 2018-06-21 2023-08-23 Tape Weaving Sweden AB Ultra-thin pre-preg sheets and composite materials thereof
EP3983216B1 (en) 2019-06-13 2023-04-19 The Board of Trustees of the Leland Stanford Junior University Composite structures containing finite length tapes and methods for manufacturing and using the same
EP3812137A1 (en) * 2019-10-23 2021-04-28 Airbus Operations, S.L. Composite laminate for an airframe lifting surface and method for manufacturing thereof
US11376812B2 (en) 2020-02-11 2022-07-05 Helicoid Industries Inc. Shock and impact resistant structures
US12275227B2 (en) 2020-02-11 2025-04-15 Helicoid Industries, Inc. Composite materials and structures
CN115052740B (zh) 2020-03-18 2024-08-02 小利兰斯坦福大学理事会 有限尺寸的复合层压插片、由其形成的渐缩复合层压结构及其制造和使用方法
CN115461205A (zh) * 2020-04-28 2022-12-09 日本复合材料株式会社 薄板成型材料及成型品
CN112265288B (zh) * 2020-09-02 2022-09-02 长春长光宇航复合材料有限公司 单面加筋结构碳纤维复合材料板的制备方法
WO2022132228A1 (en) * 2020-12-17 2022-06-23 Helicoid Industries Inc. Composite materials and structures
US11858249B2 (en) 2021-03-16 2024-01-02 The Board Of Trustees Of The Leland Stanford Junior University Stacking sequence combinations for double-double laminate structures
US11752707B2 (en) 2021-05-13 2023-09-12 The Board Of Trustees Of The Leland Stanford Junior University Octogrid constructions and applications utilizing double-double laminate structures
US11346499B1 (en) 2021-06-01 2022-05-31 Helicoid Industries Inc. Containers and methods for protecting pressure vessels
US11852297B2 (en) 2021-06-01 2023-12-26 Helicoid Industries Inc. Containers and methods for protecting pressure vessels
EP4112992B1 (en) * 2021-06-30 2025-01-29 Airbus Operations GmbH Tank for storing fluid media under cryogenic conditions on bord of a vehicle
JP7837704B2 (ja) * 2021-11-25 2026-03-31 株式会社アドテックエンジニアリング 構造体、構造体の製造方法および加工装置
EP4540133A1 (en) 2022-06-27 2025-04-23 Helicoid Industries Inc. High impact-resistant, reinforced fiber for leading edge protection of aerodynamic structures
EP4685048A1 (en) 2024-07-23 2026-01-28 AIRBUS HELICOPTERS DEUTSCHLAND GmbH A structural panel with carbon composite plies

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4604319A (en) * 1984-06-01 1986-08-05 American Cyanamid Company Thermoplastic interleafed resin matrix composites with improved impact strength and toughness
EP0783960A2 (en) * 1996-01-11 1997-07-16 The Boeing Company Titanium-polymer hybrid laminates
CN1378506A (zh) * 1999-10-18 2002-11-06 斯托克斯克伦斯公司 用于转动筛网印刷的纤维增强的塑料材料制成的印刷印版

Family Cites Families (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3895084A (en) * 1972-03-28 1975-07-15 Ducommun Inc Fiber reinforced composite product
EP0113717B1 (en) * 1982-07-19 1987-12-23 The Boeing Company Method and apparatus for fiber lamination
IT1187392B (it) * 1985-12-03 1987-12-23 Reglass Spa Struttura mulistrato per la realizzazione di elementi tubolari estremamente leggeri e resistenti,in particolare per la costruzione di canne da pesca
JPS6384932A (ja) * 1986-09-22 1988-04-15 旭化成株式会社 積層パネル
EP0312150B1 (en) * 1987-10-14 1992-12-02 Structural Laminates Company Laminate of metal sheets and continuous filaments-reinforced thermoplastic synthetic material, as well as a process for the manufacture of such a laminate
JP2526833B2 (ja) * 1988-06-17 1996-08-21 株式会社ニコン 遮光羽根用板材
JPH0390340A (ja) * 1989-09-01 1991-04-16 Yoshimoto Kasei Kk サンドイッチ構造体及びその製造方法
US5279879A (en) * 1989-12-28 1994-01-18 Tonen Corporation Hybrid prepreg containing carbon fibers and at least one other reinforcing fiber in specific positions within the prepreg
US5171419A (en) * 1990-01-18 1992-12-15 American Cyanamid Company Metal-coated fiber compositions containing alloy barrier layer
US5830548A (en) * 1992-08-11 1998-11-03 E. Khashoggi Industries, Llc Articles of manufacture and methods for manufacturing laminate structures including inorganically filled sheets
US6228453B1 (en) * 1995-06-07 2001-05-08 Lanxide Technology Company, Lp Composite materials comprising two jonal functions and methods for making the same
KR19990007964A (ko) * 1996-02-21 1999-01-25 히라이카쯔히코 섬유강화 복합재료용 에폭시수지조성물, 야안프리프레그 및 그제조방법과 제조장치
JPH09227693A (ja) * 1996-02-21 1997-09-02 Toray Ind Inc エポキシ樹脂組成物、プリプレグ、複合材料およびコンクリート部材
DE69727637T2 (de) * 1996-05-01 2005-01-05 Fukui Prefecture, Fukui Multifilament-spleissgarnfolie und verfahren und vorrichtung zur deren herstellung
MY131797A (en) * 1996-07-15 2007-09-28 Kimberly Clark Co Film-nonwoven laminate containing an adhesively-reinforced stretch-thinned film
KR100189169B1 (ko) * 1996-11-27 1999-06-01 윤덕용 몰폴로지 구배를 갖는 탄소섬유강화 복합재료
JP4116135B2 (ja) * 1997-06-26 2008-07-09 ダイワ精工株式会社 ゴルフクラブ
JPH11319170A (ja) * 1998-03-20 1999-11-24 Fujikura Rubber Ltd ゴルフクラブ用シャフトおよびゴルフクラブ
US6265333B1 (en) * 1998-06-02 2001-07-24 Board Of Regents, University Of Nebraska-Lincoln Delamination resistant composites prepared by small diameter fiber reinforcement at ply interfaces
JP2000110048A (ja) * 1999-08-06 2000-04-18 Fukui Prefecture 開繊糸織物
KR100849289B1 (ko) * 2000-08-22 2008-07-29 사이텍 테크놀러지 코포레이션 경화성 조성물내 가용화제로서 사용하기 위한 가요성 중합체 부재
JP2002225048A (ja) * 2001-02-06 2002-08-14 Toray Ind Inc Ｆｒｐ製成形体およびその製造方法
US6759352B2 (en) * 2001-07-05 2004-07-06 Sony Corporation Composite carbon fiber material and method of making same
NL1022237C2 (nl) * 2002-12-20 2004-07-01 Stork Fokker Aesp Bv Laminaat met stompgelaste metaallagen.

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4604319A (en) * 1984-06-01 1986-08-05 American Cyanamid Company Thermoplastic interleafed resin matrix composites with improved impact strength and toughness
US4604319B1 (en) * 1984-06-01 1995-07-04 American Cyanamid Co Thermoplastic interleafed resin matrix composites with improved impact strength and toughness
EP0783960A2 (en) * 1996-01-11 1997-07-16 The Boeing Company Titanium-polymer hybrid laminates
CN1378506A (zh) * 1999-10-18 2002-11-06 斯托克斯克伦斯公司 用于转动筛网印刷的纤维增强的塑料材料制成的印刷印版

Also Published As

Publication number Publication date
AU2005289392B2 (en) 2011-08-25
JP2012196967A (ja) 2012-10-18
RU2007115401A (ru) 2008-10-27
JP5788556B2 (ja) 2015-09-30
TW200624260A (en) 2006-07-16
SG155936A1 (en) 2009-10-29
JP2008514458A (ja) 2008-05-08
CN102514284A (zh) 2012-06-27
CA2581042A1 (en) 2006-04-06
WO2006037083A2 (en) 2006-04-06
EP1793989A2 (en) 2007-06-13
BRPI0516061A (pt) 2008-08-19
JP2014177125A (ja) 2014-09-25
EP1793989A4 (en) 2010-08-11
US20060093802A1 (en) 2006-05-04
EP1793989B1 (en) 2012-04-18
ATE553917T1 (de) 2012-05-15
CA2581042C (en) 2013-11-19
AU2005289392A1 (en) 2006-04-06
RU2420407C2 (ru) 2011-06-10
WO2006037083A3 (en) 2006-12-21
TWI401160B (zh) 2013-07-11
KR101229035B1 (ko) 2013-02-01
KR20070083765A (ko) 2007-08-24

Similar Documents

Publication Publication Date Title
CN102514284B (zh) 薄层层压材料
US11407199B2 (en) Metal-coated fabrics for fiber-metal laminates
US5866272A (en) Titanium-polymer hybrid laminates
CN102892572B (zh) 加强板之间的复合梁弦杆及相关的制造方法
EP2763849B1 (en) Improved fiber-metal laminate
US5227216A (en) Fiber/metal laminate
US20130316148A1 (en) Metal sheet-fiber reinforced composite laminate
US20150240396A1 (en) Fiber-reinforced composite material and method for manufacturing the same
US20040242095A1 (en) Composites reinforced by wire net or mesh for lightweight, strength and stiffness
WO2010104741A1 (en) Composite structures employing quasi-isotropic laminates
EP2006464B1 (en) Sandwich panel
CA2473346A1 (en) Lightweight structure particularly for aircraft
US10035333B2 (en) Fibre reinforced composite
CN101048276A (zh) 薄层层压材料
US7255916B2 (en) Metallic layer material, reinforced with basalt fibers, as well as products made thereof
CN104448877A (zh) 包括分散的纤维丝的复合织物
EP3388215B1 (en) Sandwich panel, method for producing unidirectional prepreg, and method for producing sandwich panel
JP2002307364A (ja) ロボットハンド部材及びその製造方法
JP6900594B2 (ja) 金属／樹脂繊維テープ材織物及びその製造方法、並びに金属／樹脂繊維テープ材織物積層材
EP1520895B1 (en) A method for securing a component
JP2026064336A (ja) 積層成形体
CRADDOCK Strength of hybrid laminates under bending and extension
JP2008302541A (ja) 炭素繊維強化プラスチック製部材

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C53 Correction of patent of invention or patent application
CB02 Change of applicant information

Address after: Osaka

Applicant after: Itochu Corp.

Applicant after: Ilt Corp

Applicant after: Mitsuya-kisako, Inc.

Applicant after: Fukui Prefecture Government

Address before: Tokyo, Japan

Applicant before: Itochu Corp.

Applicant before: Ilt Corp

Applicant before: Mitsuya-kisako, Inc.

Applicant before: Fukui Prefecture Government

C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20150819

Termination date: 20180923