JP2008514458A - 薄肉プライラミネート - Google Patents
薄肉プライラミネート Download PDFInfo
- Publication number
- JP2008514458A JP2008514458A JP2007533776A JP2007533776A JP2008514458A JP 2008514458 A JP2008514458 A JP 2008514458A JP 2007533776 A JP2007533776 A JP 2007533776A JP 2007533776 A JP2007533776 A JP 2007533776A JP 2008514458 A JP2008514458 A JP 2008514458A
- Authority
- JP
- Japan
- Prior art keywords
- ply
- thin
- thickness
- sublaminate
- plies
- 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.)
- Withdrawn
Links
Images
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
- B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar form; Layered products 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 form; Layered products 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 form; Layered products 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
- 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
- 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 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
- 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
- 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
Abstract
【選択図】 なし
Description
本出願は2004年9月24日に出願された米国仮出願第60/612,740号、および2005年4月4日に出願された米国仮出願第60/668,341号の利益を主張する。
発明の分野
本発明は一般に繊維複合材料、より具体的には薄肉プライを用いて向上した物理特性を達成する複合材料およびこのような材料の製造方法に関する。
通常の複合薄肉プライ(含浸樹脂を含むかまたは含まない)は、少なくとも0.12mmの厚さがある。複合プライのラミネートは、一方向プライを一緒に重ね、続いていくつかの圧着および硬化プロセスによって形成されている。様々な配向をもつプライは、1を超える方向に機械的特性を与えることが要求される。したがって、最小の2プライ配向としてたとえば基準の0°の角度に配向した一方のプライと90°に配向した他方のプライが必要になる。プライ層の配向は、以下において、たとえば0°の一方のプライと90°の最初のプライ上にラミネートされた他方のプライについて、または+45°の一方を-45°の他方にラミネートしたものについて(ある軸に対する相対的な配向を度で示している)、[0/90]または[+45/−45]のような表記を用いて記述される。加えて、反りを避けるために、ラミネートは対称的に積層する必要がある。したがって、先行技術においては、最小限の[0/90/0]のような3プライまたは[0/90/90/0]のような4プライは、0.36、0.48mmの最小総(ゲージ)厚を有する(その厚さが必要であろうとなかろうと)。これは各々の層が少なくとも0.12mmだからである。[0/90/45/−45]の4プライ配向は普通の実施である。これを対称にする場合、8プライが必要になり、少なくとも0.12mmの通常プライを用いると、最小の総ラミネート厚はおよそ8×0.12mmすなわち約1mmとなる。剥離はしばしば、ラミネートの自由端において、または集中的な支持荷重がかかっている点において、または横方向の衝撃もしくはラミネートの硬化の間に発生する応力を受ける点において生じやすい。その起源にかかわらず、剥離は破損モードであり、それはしばしば多方向ラミネートの能力を有する臨界面内荷重の全潜在能力の現実化を制限してしまう。複合材料がますます一次構造物に利用されるようになるにつれ、ボーイング787およびエアバス350および380航空機のように、複合部品は数百パイルの厚さになることもある。剥離は多くの用途にとって複合材の採用に深刻な脅威となる。
簡潔には、本発明の実施形態は、0.08mm以下の厚さの薄肉プライを用いて構築されたラミネートを含む。代替の実施形態は0.08mm未満の薄肉プライと、少なくとも0.12mmのより厚い通常のプライとの組み合わせを含む。これらの組み合わせは、微小なひび割れや剥離への向上した耐性、より薄いラミネートの最小ゲージ、厚肉プライと薄肉プライのハイブリッド化の機会、接着継手の補強、通常の織布よりも高性能の織り交ぜ製品、配管や容器の向上したオンライン強化、より強いシート成形コンパウンドを形成するチョップされた繊維を与える。多プライサブラミネート(以降で「サブラミネートモジュール」と称する)は、複合ラミネートの基本構築ブロックとして形成され、高い剥離耐性を有する一方でアセンブリコストを減らすことができる。オートメーションまたはオートメーションによらずとも、薄肉プライサブラミネートとラミネートからなる製品は、コスト面で通常の厚肉プライラミネートからなる製品に対抗できる。
本発明による複合材料10の断面を図1に示す。複合材料10は、点で示され、第1の方向に配向された第1のプライ12を含む、複数の層(プライ)を有する。第1のプライ12は、第1の方向と異なる第2の方向に配向された第2のプライ14により隔てられている。第2のプライ14は、プライ12と区別する目的で、図1では何も印をつけずに表示されている。本発明によれば、プライ12、14は厚さ「t」が0.08mm未満、好ましくは厚さ0.02〜0.06mmである。図2は、通常/先行技術のラミネートは、16、18のような本発明のものよりも厚い、各々の厚さ「T」が通常0.12mm以上の交互のプライで構築されている、ということを簡単に示すために用いる。
Claims (16)
- 0.08mm未満の厚さを有する薄肉プライを含む複合材料。
- 材料は少なくとも0.12mmの厚さを持つ通常のプライと、0.08mm未満の厚さを持つ薄肉プライの組み合わせを含む、請求項1記載の材料。
- 材料は薄肉プライのサブラミネートモジュールの組み合わせを含む、請求項1記載の材料。
- 材料は薄肉プライのサブラミネートモジュールと、通常のプライのサブラミネートモジュールを含む、請求項2記載の材料。
- 材料は薄肉プライと通常のプライからなるサブラミネートモジュールを含む、請求項2記載の材料。
- 薄肉プライを織り交ぜるか、または編み込む、請求項1、請求項2、請求項3、請求項4または請求項5記載の材料。
- 材料を樹脂トランスファー成形を用いて形成する、請求項1、請求項2、請求項3、請求項4または請求項5記載の材料。
- 薄肉プライを接着剤で結合して、複合材および/または金属部品を接着継手で接合するための強化結合材料を与える、請求項1、請求項2、請求項3、請求項4または請求項5記載の材料。
- 薄肉プライを接着剤で結合して、ハニカムまたはサンドイッチ構造を有する複合部品のための強化結合材料を与える、請求項1、請求項2、請求項3、請求項4または請求項5記載の材料。
- 薄肉プライをチョップして成形コンパウンドに再構成する、請求項1、請求項2、請求項3、請求項4または請求項5記載の材料。
- 請求項1、請求項2、請求項3、請求項4または請求項5記載の材料を含む製品であって、薄肉プライまたはサブラミネートモジュールを熱硬化性または熱可塑性テープに組み込み、製品をテーププレースメント法またはテープワインディング法によって成形し、テープを硬化した製品。
- 請求項1、請求項2、請求項3、請求項4または請求項5記載の材料と、金属シートとを含む、繊維−金属複合材料。
- 金属シートを表面層としてのみ敷設した、請求項12記載の複合材料。
- 金属シートを同一の繊維方向を有する薄肉プライの間に敷設した、請求項12記載の複合材料。
- 薄肉プライがグラファイトプライを含む、請求項12、請求項13または請求項14記載のマトリクス複合材料。
- 金属をチタンおよび銅からなる群より選択した、請求項15記載のマトリクス複合材料。
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US61274004P | 2004-09-24 | 2004-09-24 | |
US66834105P | 2005-04-04 | 2005-04-04 | |
PCT/US2005/034961 WO2006037083A2 (en) | 2004-09-24 | 2005-09-23 | Thin ply laminates |
Related Child Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2012108588A Division JP2012196967A (ja) | 2004-09-24 | 2012-05-10 | 薄肉プライラミネート |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2008514458A true JP2008514458A (ja) | 2008-05-08 |
JP2008514458A5 JP2008514458A5 (ja) | 2008-11-13 |
Family
ID=36119591
Family Applications (3)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2007533776A Withdrawn JP2008514458A (ja) | 2004-09-24 | 2005-09-23 | 薄肉プライラミネート |
JP2012108588A Withdrawn JP2012196967A (ja) | 2004-09-24 | 2012-05-10 | 薄肉プライラミネート |
JP2014085608A Active JP5788556B2 (ja) | 2004-09-24 | 2014-04-17 | 薄肉プライラミネート |
Family Applications After (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2012108588A Withdrawn JP2012196967A (ja) | 2004-09-24 | 2012-05-10 | 薄肉プライラミネート |
JP2014085608A Active JP5788556B2 (ja) | 2004-09-24 | 2014-04-17 | 薄肉プライラミネート |
Country Status (13)
Country | Link |
---|---|
US (1) | US20060093802A1 (ja) |
EP (1) | EP1793989B1 (ja) |
JP (3) | JP2008514458A (ja) |
KR (1) | KR101229035B1 (ja) |
CN (1) | CN102514284B (ja) |
AT (1) | ATE553917T1 (ja) |
AU (1) | AU2005289392B2 (ja) |
BR (1) | BRPI0516061A (ja) |
CA (1) | CA2581042C (ja) |
RU (1) | RU2420407C2 (ja) |
SG (1) | SG155936A1 (ja) |
TW (1) | TWI401160B (ja) |
WO (1) | WO2006037083A2 (ja) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2010261472A (ja) * | 2009-04-30 | 2010-11-18 | Universal Shipbuilding Corp | Frpサンドイッチパネル構造体 |
WO2012133013A1 (ja) * | 2011-03-29 | 2012-10-04 | 東洋紡績株式会社 | 繊維強化熱可塑性樹脂の積層成形品 |
WO2018154846A1 (ja) * | 2017-02-22 | 2018-08-30 | 三菱重工業株式会社 | 複合材料及び複合材料の製造方法 |
Families Citing this family (33)
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 |
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. |
US9296174B2 (en) * | 2011-01-12 | 2016-03-29 | Compagnie Chomarat | Composite laminated structures and methods for manufacturing and using the same |
KR102008540B1 (ko) * | 2011-07-28 | 2019-08-07 | 미쯔비시 케미컬 주식회사 | 탄소 섬유 강화 탄소 복합체 및 그의 제조 방법 |
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 |
US20160200070A1 (en) * | 2015-01-13 | 2016-07-14 | 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 |
US11446897B2 (en) | 2017-04-04 | 2022-09-20 | 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 |
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 |
US11376812B2 (en) | 2020-02-11 | 2022-07-05 | Helicoid Industries Inc. | Shock and impact resistant structures |
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 |
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 |
EP4112992A1 (en) * | 2021-06-30 | 2023-01-04 | Airbus Operations GmbH | Tank for storing fluid media under cryogenic conditions on bord of a vehicle |
WO2024006078A1 (en) | 2022-06-27 | 2024-01-04 | Helicoid Industries Inc. | High impact-resistant, reinforced fiber for leading edge protection of aerodynamic structures |
Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS6384932A (ja) * | 1986-09-22 | 1988-04-15 | 旭化成株式会社 | 積層パネル |
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 |
JPH09193296A (ja) * | 1996-01-11 | 1997-07-29 | Boeing Co:The | ハイブリッド積層、航空機の外板パネル、および胴体部分 |
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 |
JPH1170197A (ja) * | 1997-06-26 | 1999-03-16 | Daiwa Seiko Inc | 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 |
JP2000110048A (ja) * | 1999-08-06 | 2000-04-18 | Fukui Prefecture | 開繊糸織物 |
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 |
Family Cites Families (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3895084A (en) * | 1972-03-28 | 1975-07-15 | Ducommun Inc | Fiber reinforced composite product |
WO1984000351A1 (en) * | 1982-07-19 | 1984-02-02 | Boeing Co | Method and apparatus for fiber lamination |
US4604319B1 (en) * | 1984-06-01 | 1995-07-04 | American Cyanamid Co | Thermoplastic interleafed resin matrix composites with improved impact strength and toughness |
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 |
ATE82903T1 (de) * | 1987-10-14 | 1992-12-15 | Structural Laminates Co | Schichtstoff aus metallschichten und aus durchgehendem,faserverstaerkten,synthetischen,th rmoplastischen material und verfahren zu seiner herstellung. |
JP2526833B2 (ja) * | 1988-06-17 | 1996-08-21 | 株式会社ニコン | 遮光羽根用板材 |
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 |
ATE296851T1 (de) * | 1996-02-21 | 2005-06-15 | Toray Industries | Verbundfaden und daraus hergestellte faserverstärkte verbundwerkstoffe |
WO1997041285A1 (fr) * | 1996-05-01 | 1997-11-06 | Fukui Prefecture | Bande a base de fils clives multifilamentaire, procede et dispositif pour la fabrication de celle-ci |
KR100189169B1 (ko) * | 1996-11-27 | 1999-06-01 | 윤덕용 | 몰폴로지 구배를 갖는 탄소섬유강화 복합재료 |
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 |
MY133638A (en) * | 1999-10-18 | 2007-11-30 | Stork Screens B V A Dutch Company | Printing forme for rotary screen printing made from fibre-reinforced plastics material |
US6759352B2 (en) * | 2001-07-05 | 2004-07-06 | Sony Corporation | Composite carbon fiber material and method of making same |
-
2005
- 2005-09-23 CA CA2581042A patent/CA2581042C/en not_active Expired - Fee Related
- 2005-09-23 SG SG200906236-5A patent/SG155936A1/en unknown
- 2005-09-23 EP EP05810521A patent/EP1793989B1/en not_active Not-in-force
- 2005-09-23 KR KR1020077009176A patent/KR101229035B1/ko not_active IP Right Cessation
- 2005-09-23 CN CN201110428403.2A patent/CN102514284B/zh not_active Expired - Fee Related
- 2005-09-23 US US11/233,716 patent/US20060093802A1/en not_active Abandoned
- 2005-09-23 JP JP2007533776A patent/JP2008514458A/ja not_active Withdrawn
- 2005-09-23 AU AU2005289392A patent/AU2005289392B2/en not_active Ceased
- 2005-09-23 RU RU2007115401/02A patent/RU2420407C2/ru not_active IP Right Cessation
- 2005-09-23 TW TW094132998A patent/TWI401160B/zh not_active IP Right Cessation
- 2005-09-23 WO PCT/US2005/034961 patent/WO2006037083A2/en active Application Filing
- 2005-09-23 AT AT05810521T patent/ATE553917T1/de active
- 2005-09-23 BR BRPI0516061-8A patent/BRPI0516061A/pt not_active IP Right Cessation
-
2012
- 2012-05-10 JP JP2012108588A patent/JP2012196967A/ja not_active Withdrawn
-
2014
- 2014-04-17 JP JP2014085608A patent/JP5788556B2/ja active Active
Patent Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS6384932A (ja) * | 1986-09-22 | 1988-04-15 | 旭化成株式会社 | 積層パネル |
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 |
JPH09193296A (ja) * | 1996-01-11 | 1997-07-29 | Boeing Co:The | ハイブリッド積層、航空機の外板パネル、および胴体部分 |
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 |
JPH1170197A (ja) * | 1997-06-26 | 1999-03-16 | Daiwa Seiko Inc | 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 |
JP2000110048A (ja) * | 1999-08-06 | 2000-04-18 | Fukui Prefecture | 開繊糸織物 |
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 |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2010261472A (ja) * | 2009-04-30 | 2010-11-18 | Universal Shipbuilding Corp | Frpサンドイッチパネル構造体 |
WO2012133013A1 (ja) * | 2011-03-29 | 2012-10-04 | 東洋紡績株式会社 | 繊維強化熱可塑性樹脂の積層成形品 |
WO2018154846A1 (ja) * | 2017-02-22 | 2018-08-30 | 三菱重工業株式会社 | 複合材料及び複合材料の製造方法 |
JPWO2018154846A1 (ja) * | 2017-02-22 | 2019-06-27 | 三菱重工業株式会社 | 複合材料及び複合材料の製造方法 |
Also Published As
Publication number | Publication date |
---|---|
RU2007115401A (ru) | 2008-10-27 |
RU2420407C2 (ru) | 2011-06-10 |
WO2006037083A3 (en) | 2006-12-21 |
TW200624260A (en) | 2006-07-16 |
TWI401160B (zh) | 2013-07-11 |
CA2581042A1 (en) | 2006-04-06 |
CA2581042C (en) | 2013-11-19 |
CN102514284B (zh) | 2015-08-19 |
EP1793989B1 (en) | 2012-04-18 |
JP2014177125A (ja) | 2014-09-25 |
AU2005289392B2 (en) | 2011-08-25 |
JP2012196967A (ja) | 2012-10-18 |
BRPI0516061A (pt) | 2008-08-19 |
JP5788556B2 (ja) | 2015-09-30 |
KR101229035B1 (ko) | 2013-02-01 |
EP1793989A4 (en) | 2010-08-11 |
SG155936A1 (en) | 2009-10-29 |
US20060093802A1 (en) | 2006-05-04 |
KR20070083765A (ko) | 2007-08-24 |
WO2006037083A2 (en) | 2006-04-06 |
CN102514284A (zh) | 2012-06-27 |
EP1793989A2 (en) | 2007-06-13 |
AU2005289392A1 (en) | 2006-04-06 |
ATE553917T1 (de) | 2012-05-15 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
JP5788556B2 (ja) | 薄肉プライラミネート | |
AU2006317054B2 (en) | Hybrid three-dimensional woven/laminated struts for composite structural applications | |
US11407199B2 (en) | Metal-coated fabrics for fiber-metal laminates | |
US20040242095A1 (en) | Composites reinforced by wire net or mesh for lightweight, strength and stiffness | |
US20160101591A1 (en) | Composite article | |
JP3207221U (ja) | 炭素繊維プリプレグ材料の構造 | |
US10035333B2 (en) | Fibre reinforced composite | |
CN101048276A (zh) | 薄层层压材料 | |
WO2000064668A1 (fr) | Materiau composite a base de resine renforcee par des fibres, et possedant un coefficient reduit d'expansion lineaire | |
EP2922696B1 (en) | Multi-axial fabrics, polymer-fiber laminates, and bodies incorporating same for connecting applications | |
JPH04363215A (ja) | 炭素繊維プリプレグ及び炭素繊維強化樹脂 | |
JP4402477B2 (ja) | 不織布を備える管状積層体及びその製造方法 | |
JP3632846B2 (ja) | ロボットハンド部材及びその製造方法 | |
EP2189277A1 (en) | Fibre reinforced composite | |
WO2013191232A1 (ja) | 強化繊維複合材料及び強化繊維複合材料の製造方法 | |
JPH0743501U (ja) | 軸継手 |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
A521 | Request for written amendment filed |
Free format text: JAPANESE INTERMEDIATE CODE: A523 Effective date: 20080922 |
|
A621 | Written request for application examination |
Free format text: JAPANESE INTERMEDIATE CODE: A621 Effective date: 20080922 |
|
A977 | Report on retrieval |
Free format text: JAPANESE INTERMEDIATE CODE: A971007 Effective date: 20110106 |
|
A131 | Notification of reasons for refusal |
Free format text: JAPANESE INTERMEDIATE CODE: A131 Effective date: 20110111 |
|
A601 | Written request for extension of time |
Free format text: JAPANESE INTERMEDIATE CODE: A601 Effective date: 20110411 |
|
A602 | Written permission of extension of time |
Free format text: JAPANESE INTERMEDIATE CODE: A602 Effective date: 20110418 |
|
A521 | Request for written amendment filed |
Free format text: JAPANESE INTERMEDIATE CODE: A523 Effective date: 20110711 |
|
RD01 | Notification of change of attorney |
Free format text: JAPANESE INTERMEDIATE CODE: A7426 Effective date: 20111227 |
|
A02 | Decision of refusal |
Free format text: JAPANESE INTERMEDIATE CODE: A02 Effective date: 20120110 |
|
A521 | Request for written amendment filed |
Free format text: JAPANESE INTERMEDIATE CODE: A821 Effective date: 20111228 |
|
A521 | Request for written amendment filed |
Free format text: JAPANESE INTERMEDIATE CODE: A523 Effective date: 20120510 |
|
A911 | Transfer to examiner for re-examination before appeal (zenchi) |
Free format text: JAPANESE INTERMEDIATE CODE: A911 Effective date: 20120702 |
|
A912 | Re-examination (zenchi) completed and case transferred to appeal board |
Free format text: JAPANESE INTERMEDIATE CODE: A912 Effective date: 20120817 |
|
A761 | Written withdrawal of application |
Free format text: JAPANESE INTERMEDIATE CODE: A761 Effective date: 20121116 |