JP2010527302A - 複合構造用ナノチューブ強化中間層 - Google Patents
複合構造用ナノチューブ強化中間層 Download PDFInfo
- Publication number
- JP2010527302A JP2010527302A JP2010508491A JP2010508491A JP2010527302A JP 2010527302 A JP2010527302 A JP 2010527302A JP 2010508491 A JP2010508491 A JP 2010508491A JP 2010508491 A JP2010508491 A JP 2010508491A JP 2010527302 A JP2010527302 A JP 2010527302A
- Authority
- JP
- Japan
- Prior art keywords
- fiber layer
- substrate
- carbon nanotubes
- fiber
- flexible substrate
- 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.)
- Granted
Links
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/02—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising combinations of reinforcements, e.g. non-specified reinforcements, fibrous reinforcing inserts and fillers, e.g. particulate fillers, incorporated in matrix material, forming one or more layers and with or without non-reinforced or non-filled layers
- B29C70/021—Combinations of fibrous reinforcement and non-fibrous material
- B29C70/025—Combinations of fibrous reinforcement and non-fibrous material with particular filler
-
- 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
- B29C70/28—Shaping operations therefor
- B29C70/40—Shaping or impregnating by compression not applied
- B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
- B29C70/44—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding
-
- 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
- B29C70/28—Shaping operations therefor
- B29C70/40—Shaping or impregnating by compression not applied
- B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
- B29C70/46—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs
- B29C70/48—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs and impregnating the reinforcements in the closed mould, e.g. resin transfer moulding [RTM], e.g. by vacuum
-
- 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
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/04—Layered products comprising a layer of synthetic resin as impregnant, bonding, or embedding substance
-
- 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
- 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
- B32B5/28—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 impregnated with or embedded in a plastic substance
-
- C—CHEMISTRY; METALLURGY
- C09—DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
- C09D—COATING COMPOSITIONS, e.g. PAINTS, VARNISHES OR LACQUERS; FILLING PASTES; CHEMICAL PAINT OR INK REMOVERS; INKS; CORRECTING FLUIDS; WOODSTAINS; PASTES OR SOLIDS FOR COLOURING OR PRINTING; USE OF MATERIALS THEREFOR
- C09D7/00—Features of coating compositions, not provided for in group C09D5/00; Processes for incorporating ingredients in coating compositions
- C09D7/40—Additives
- C09D7/60—Additives non-macromolecular
- C09D7/61—Additives non-macromolecular inorganic
-
- C—CHEMISTRY; METALLURGY
- C09—DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
- C09D—COATING COMPOSITIONS, e.g. PAINTS, VARNISHES OR LACQUERS; FILLING PASTES; CHEMICAL PAINT OR INK REMOVERS; INKS; CORRECTING FLUIDS; WOODSTAINS; PASTES OR SOLIDS FOR COLOURING OR PRINTING; USE OF MATERIALS THEREFOR
- C09D7/00—Features of coating compositions, not provided for in group C09D5/00; Processes for incorporating ingredients in coating compositions
- C09D7/40—Additives
- C09D7/70—Additives characterised by shape, e.g. fibres, flakes or microspheres
-
- 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
- B29C70/28—Shaping operations therefor
- B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
- B29C70/543—Fixing the position or configuration of fibrous reinforcements before or during moulding
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
- B29K2105/06—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
- B29K2105/16—Fillers
- B29K2105/165—Hollow fillers, e.g. microballoons or expanded particles
- B29K2105/167—Nanotubes
-
- 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
- Y10T428/26—Web or sheet containing structurally defined element or component, the element or component having a specified physical dimension
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Composite Materials (AREA)
- Mechanical Engineering (AREA)
- Life Sciences & Earth Sciences (AREA)
- Materials Engineering (AREA)
- Wood Science & Technology (AREA)
- Organic Chemistry (AREA)
- Inorganic Chemistry (AREA)
- Laminated Bodies (AREA)
- Reinforced Plastic Materials (AREA)
- Carbon And Carbon Compounds (AREA)
Abstract
Description
Claims (23)
- 複合構造を製造する方法であって、
基板上に複数のカーボンナノチューブを作製するステップ、
基板を第1繊維層に付着させるステップ、
第2繊維層を第1繊維層に隣接して配置することにより複数のカーボンナノチューブを第1繊維層及び第2繊維層の間に配置するステップ、
第1及び第2繊維層に樹脂を注入するステップ、及び
樹脂を硬化させて複合構造を硬化させるステップ
を含む方法。 - 基板を第1繊維層に付着させるステップが、第1繊維層に基板を接着するステップを含む、請求項1に記載の方法。
- 基板が接着層を含み、基板を第1繊維層に付着させるステップが、接着層と第1繊維層を加熱して基板を第1繊維層に溶解接着させるステップを含む、請求項1に記載の方法。
- 基板を第1繊維層に付着させるステップが、基板を第1繊維層に機械的に留め付けるステップを含む、請求項1に記載の方法。
- 基板を第1繊維層に付着させるステップが、基板を糸で第1繊維層に縫合するステップを含む、請求項1に記載の方法。
- 基板上に複数のカーボンナノチューブを作製するステップが、柔軟基板上に複数のカーボンナノチューブを生成するステップを含む、請求項1に記載の方法。
- 基板が第1側面及び第2側面を有し、基板上に複数のカーボンナノチューブを作製するステップが、基板の第1側面から少なくともおおむね垂直に延びるカーボンナノチューブの第1部分を作製し、基板の第2側面から少なくともおおむね垂直に延びるカーボンナノチューブの第2部分を作製するステップを含む、請求項1に記載の方法。
- 複数のカーボンナノチューブを第1繊維層及び第2繊維層の間に配置するステップが、複数のカーボンナノチューブを、第1及び第2繊維層に対して少なくともおおむね垂直に延びるように方向付けするステップを含む、請求項1に記載の方法。
- 基板と第1及び第2繊維層に樹脂を注入するステップが、第2繊維層を基板に隣接させて配置する前に、基板と第1繊維層に予め樹脂の第1部分を含浸させ、第2繊維層に予め樹脂の第2部分を含浸させるステップを含む、請求項1に記載の方法。
- 基板上に複数のカーボンナノチューブを作製するステップが、第1柔軟基板上に複数の第1カーボンナノチューブを生成するステップを含み、基板を第1繊維層に付着させるステップが、第1柔軟基板と第1繊維層を加熱して、第1柔軟基板を第1繊維層に溶解接着させるステップを含み、当該方法がさらに、
第2柔軟基板上に複数の第2カーボンナノチューブを生成するステップ、
第2柔軟基板と第2繊維層を加熱して、第2柔軟基板を第2繊維層に溶解接着するステップ、及び
第3繊維層を第2繊維層に隣接して配置することにより、複数の第2カーボンナノチューブを第2繊維層と第3繊維層の間に配置するステップを含み、
第1及び第2繊維層に樹脂を注入するステップが、第1及び第2柔軟基板と、第1、第2、及び第3繊維層に樹脂を注入するステップを含む、請求項1に記載の方法。 - 第3繊維層の上に追加のカーボンナノチューブ強化繊維層を積層させるステップをさらに含む、請求項10に記載の方法。
- 複合構造が航空機の複合構造であり、当該方法がさらに、航空機の一部分に硬化した複合構造を取り付けるステップを含む、請求項1に記載の方法。
- 複合構造用のカーボンナノチューブ強化中間層アセンブリを製造する方法であって、
柔軟基板上に複数のカーボンナノチューブを生成するステップ、及び
柔軟基板を繊維層に付着させるステップ
を含む方法。 - 柔軟基板上に複数のカーボンナノチューブを生成するステップが、化学蒸着法で遷移金属触媒上に複数のカーボンナノチューブを生成するステップを含み、柔軟基板を繊維層に付着させるステップが、基板及び繊維層を加熱することにより、基板の少なくとも一部を溶かしてカーボンナノチューブを繊維層に接着するステップを含む、請求項13に記載の方法。
- 基板が第1側面と第2側面を有し、柔軟基板上に複数のカーボンナノチューブを生成するステップが、基板の第1側面から少なくともおおむね垂直に延びるカーボンナノチューブの第1部分を作製し、基板の第2側面から少なくともおおむね垂直に延びるカーボンナノチューブの第2部分を作製するステップを含む、請求項13に記載の方法。
- 柔軟基板を繊維層に付着させるステップが、繊維層をほぼ垂直なカーボンナノチューブでおおむね均一な配分で覆うステップを含む、請求項13に記載の方法。
- 柔軟基板に接着層を積層するステップをさらに含み、繊維層に柔軟基板を付着させるステップが接着層の少なくとも一部を溶かすステップを含む、請求項13に記載の方法。
- 柔軟基板上に複数のカーボンナノチューブを生成するステップが、柔軟基板の第1側面上に複数の第1カーボンナノチューブを生成し、柔軟基板の第2側面上に複数の第2カーボンナノチューブを生成するステップを含み、柔軟基板を繊維層に付着させるステップが、柔軟基板の少なくとも一部を繊維層に縫合するステップを含む、請求項13に記載の方法。
- 第1繊維層;
第2繊維層;
第1及び第2繊維層の間に配置されて、
基板;及び
基板に付着され且つ基板に対して少なくともおおむね垂直である複数のカーボンナノチューブ;
を含む中間層;ならびに、
第1及び第2繊維層に注入されたマトリクス材
を備える、複合構造。 - 複数のカーボンナノチューブが、基板の第1側面から延びる複数の第1カーボンナノチューブであり、中間層が、基板の第2側面から延びる複数の第2カーボンナノチューブをさらに含む、請求項19に記載の複合構造。
- 基板が第1繊維層に溶解接着されている、請求項19に記載の複合構造。
- 複合構造を製造するシステムであって、
基板上に複数のカーボンナノチューブを作製する手段と、
複数のカーボンナノチューブが第1繊維層から離れて延びるように基板を第1繊維層に付着させる手段と、
基板の上に第2繊維層を配置して、第1繊維層及び第2繊維層の間に複数のカーボンナノチューブを配置する手段と
を備えるシステム。 - 基板と第1及び第2繊維層に樹脂を注入する手段;並びに、
樹脂を硬化させる手段
を更に備える、請求項22に記載のシステム。
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US11/750,207 | 2007-05-17 | ||
US11/750,207 US8388795B2 (en) | 2007-05-17 | 2007-05-17 | Nanotube-enhanced interlayers for composite structures |
PCT/US2008/062386 WO2009014788A2 (en) | 2007-05-17 | 2008-05-02 | Nanotube-enhanced interlayers for composite structures |
Publications (3)
Publication Number | Publication Date |
---|---|
JP2010527302A true JP2010527302A (ja) | 2010-08-12 |
JP2010527302A5 JP2010527302A5 (ja) | 2011-06-16 |
JP5595909B2 JP5595909B2 (ja) | 2014-09-24 |
Family
ID=40027811
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2010508491A Active JP5595909B2 (ja) | 2007-05-17 | 2008-05-02 | 複合構造用ナノチューブ強化中間層 |
Country Status (4)
Country | Link |
---|---|
US (2) | US8388795B2 (ja) |
EP (2) | EP2155471B1 (ja) |
JP (1) | JP5595909B2 (ja) |
WO (1) | WO2009014788A2 (ja) |
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2012018062A1 (ja) * | 2010-08-04 | 2012-02-09 | アイシン精機株式会社 | カーボンナノチューブデバイス、カーボンナノチューブ製造方法およびカーボンナノチューブ製造装置 |
JP2012036022A (ja) * | 2010-08-04 | 2012-02-23 | Aisin Seiki Co Ltd | カーボンナノチューブ製造方法およびカーボンナノチューブ製造装置 |
JP2012035345A (ja) * | 2010-08-04 | 2012-02-23 | Aisin Seiki Co Ltd | カーボンナノチューブデバイス |
JP2013502335A (ja) * | 2009-08-17 | 2013-01-24 | ザ・ボーイング・カンパニー | 積層複合ロッド、その製造方法と複合構造における使用 |
JP2015504799A (ja) * | 2012-01-26 | 2015-02-16 | イー・アイ・デュポン・ドウ・ヌムール・アンド・カンパニーE.I.Du Pont De Nemours And Company | サンドイッチパネルの製造方法 |
JP2015196378A (ja) * | 2014-04-02 | 2015-11-09 | ザ・ボーイング・カンパニーTheBoeing Company | ポリマーナノ粒子ポリマーを用いて製造された不織中間層 |
WO2016159072A1 (ja) * | 2015-03-31 | 2016-10-06 | 国立研究開発法人産業技術総合研究所 | 炭素繊維複合材料の製造方法 |
JP2017507809A (ja) * | 2014-02-04 | 2017-03-23 | エヌ12 テクノロジーズ, インク.N12 Technologies, Inc. | ナノ構造強化コンポジットの物品及び製造方法 |
JP2017525602A (ja) * | 2014-05-28 | 2017-09-07 | ユニヴァーシティ オブ サウス アラバマ | 多孔質媒体中でナノファイバーを一方向に配列する装置及び方法 |
Families Citing this family (85)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7527222B2 (en) | 2004-04-06 | 2009-05-05 | The Boeing Company | Composite barrel sections for aircraft fuselages and other structures, and methods and systems for manufacturing such barrel sections |
US7622066B2 (en) | 2004-07-26 | 2009-11-24 | The Boeing Company | Methods and systems for manufacturing composite parts with female tools |
US7325771B2 (en) | 2004-09-23 | 2008-02-05 | The Boeing Company | Splice joints for composite aircraft fuselages and other structures |
US7306450B2 (en) | 2004-09-29 | 2007-12-11 | The Boeing Company | Apparatuses, systems, and methods for manufacturing composite parts |
US7503368B2 (en) | 2004-11-24 | 2009-03-17 | The Boeing Company | Composite sections for aircraft fuselages and other structures, and methods and systems for manufacturing such sections |
US8557165B2 (en) | 2008-10-25 | 2013-10-15 | The Boeing Company | Forming highly contoured composite parts |
US8601694B2 (en) | 2008-06-13 | 2013-12-10 | The Boeing Company | Method for forming and installing stringers |
US7655168B2 (en) * | 2006-01-31 | 2010-02-02 | The Boeing Company | Tools for manufacturing composite parts and methods for using such tools |
EP2441729B1 (en) | 2006-05-19 | 2017-04-05 | Massachusetts Institute Of Technology | Method of forming a composite article |
US8337979B2 (en) | 2006-05-19 | 2012-12-25 | Massachusetts Institute Of Technology | Nanostructure-reinforced composite articles and methods |
US8158217B2 (en) | 2007-01-03 | 2012-04-17 | Applied Nanostructured Solutions, Llc | CNT-infused fiber and method therefor |
US8951632B2 (en) | 2007-01-03 | 2015-02-10 | Applied Nanostructured Solutions, Llc | CNT-infused carbon fiber materials and process therefor |
US20100279569A1 (en) * | 2007-01-03 | 2010-11-04 | Lockheed Martin Corporation | Cnt-infused glass fiber materials and process therefor |
US8951631B2 (en) | 2007-01-03 | 2015-02-10 | Applied Nanostructured Solutions, Llc | CNT-infused metal fiber materials and process therefor |
US9005755B2 (en) | 2007-01-03 | 2015-04-14 | Applied Nanostructured Solutions, Llc | CNS-infused carbon nanomaterials and process therefor |
EP2125212A2 (en) | 2007-03-23 | 2009-12-02 | Lydall, Inc. | Substrate for carrying catalytic particles |
US8388795B2 (en) | 2007-05-17 | 2013-03-05 | The Boeing Company | Nanotube-enhanced interlayers for composite structures |
US8042767B2 (en) | 2007-09-04 | 2011-10-25 | The Boeing Company | Composite fabric with rigid member structure |
US8919428B2 (en) | 2007-10-17 | 2014-12-30 | Purdue Research Foundation | Methods for attaching carbon nanotubes to a carbon substrate |
US8262835B2 (en) * | 2007-12-19 | 2012-09-11 | Purdue Research Foundation | Method of bonding carbon nanotubes |
DE102008038294B4 (de) | 2008-08-18 | 2013-07-18 | Airbus Sas | Verfahren zur Herstellung eines Faserverbundbauteils sowie textiles Halbzeug hierfür |
US20100136866A1 (en) * | 2008-12-02 | 2010-06-03 | Gm Global Technology Operations, Inc. | Laminated composites and methods of making the same |
US7981501B2 (en) * | 2008-12-02 | 2011-07-19 | GM Global Technology Operations LLC | Laminated composites and methods of making the same |
EP2202336A1 (en) * | 2008-12-12 | 2010-06-30 | Eads Construcciones Aeronauticas S.A. | Method for producing nanofibres of epoxy resin for composite laminates of aeronautical structures to improve their electromagnetic characteristics |
US8404162B2 (en) * | 2008-12-22 | 2013-03-26 | Florida State University Research Foundation | Composite materials and methods for selective placement of nano-particulates within composites |
CA2750484A1 (en) * | 2009-02-17 | 2010-12-16 | Applied Nanostructured Solutions, Llc | Composites comprising carbon nanotubes on fiber |
EP2401416B1 (en) | 2009-02-27 | 2021-03-17 | Applied NanoStructured Solutions, LLC | Low temperature carbon nanotube growth using gas-preheat method |
US20100227134A1 (en) | 2009-03-03 | 2010-09-09 | Lockheed Martin Corporation | Method for the prevention of nanoparticle agglomeration at high temperatures |
WO2010144183A1 (en) | 2009-04-24 | 2010-12-16 | Lockheed Martin Corporation | Cnt-based signature control material |
US9111658B2 (en) | 2009-04-24 | 2015-08-18 | Applied Nanostructured Solutions, Llc | CNS-shielded wires |
KR101696207B1 (ko) | 2009-04-27 | 2017-01-13 | 어플라이드 나노스트럭처드 솔루션스, 엘엘씨. | 복합 구조물 제빙을 위한 cnt계 저항 가열 |
DE102009020452B4 (de) * | 2009-05-08 | 2017-12-28 | Airbus Defence and Space GmbH | Verbundbauteil mit Nanoröhren, Verfahren zu dessen Herstellung, Verwendung des Verbundbauteils in einem Transportmittel und Transportmittel mit diesem Verbundbauteil |
WO2010144009A1 (en) * | 2009-06-11 | 2010-12-16 | Saab Ab | An aircraft structure with structural parts connected by nanostructure and a method for making said aircraft structure |
CA2763259A1 (en) * | 2009-06-11 | 2010-12-16 | Saab Ab | A structural longitudinal composite joint for aircraft structure |
CA2765138A1 (en) * | 2009-06-11 | 2010-12-16 | Saab Ab | Nano-reinforced radius filler for an aircraft structure and a method of producing an aircraft structure comprising such filler |
JP5823393B2 (ja) | 2009-08-03 | 2015-11-25 | アプライド ナノストラクチャード ソリューションズ リミテッド ライアビリティー カンパニーApplied Nanostructuredsolutions, Llc | 複合繊維へのナノ粒子の組み込み |
EP2496739A4 (en) * | 2009-11-02 | 2014-07-02 | Applied Nanostructured Sols | CNT-FOUNDED ARAMID FIBER MATERIALS AND METHOD THEREFOR |
KR20120117978A (ko) | 2009-11-23 | 2012-10-25 | 어플라이드 나노스트럭처드 솔루션스, 엘엘씨. | 카본 나노튜브-주입된 섬유 재료를 포함하는 세라믹 복합재료 및 이의 제조방법 |
WO2011126518A2 (en) | 2009-11-23 | 2011-10-13 | Applied Nanostructured Solutions, Llc | Cnt-tailored composite air-based structures |
EP2513250A4 (en) | 2009-12-14 | 2015-05-27 | Applied Nanostructured Sols | FIRE-RESISTANT COMPOSITE MATERIALS AND ARTICLES WITH CARBON NANOTUBES-INFUNDED FIBER MATERIALS |
JP5577089B2 (ja) * | 2009-12-25 | 2014-08-20 | 日東電工株式会社 | カーボンナノチューブ複合構造体および粘着部材 |
US8931740B2 (en) * | 2010-01-14 | 2015-01-13 | Saab Ab | Multifunctional de-icing/anti-icing system |
CA2786839A1 (en) * | 2010-01-14 | 2011-07-21 | Saab Ab | Article with de-icing/anti-icing function |
US9167736B2 (en) | 2010-01-15 | 2015-10-20 | Applied Nanostructured Solutions, Llc | CNT-infused fiber as a self shielding wire for enhanced power transmission line |
CA2785803A1 (en) | 2010-02-02 | 2011-11-24 | Applied Nanostructured Solutions, Llc | Carbon nanotube-infused fiber materials containing parallel-aligned carbon nanotubes, methods for production thereof, and composite materials derived therefrom |
KR101787645B1 (ko) | 2010-03-02 | 2017-10-23 | 어플라이드 나노스트럭처드 솔루션스, 엘엘씨. | 카본 나노튜브-주입된 전극 재료를 포함하는 나선형 권선 전기 장치 및 이의 제조를 위한 방법 및 장치 |
WO2011109485A1 (en) | 2010-03-02 | 2011-09-09 | Applied Nanostructured Solutions,Llc | Electrical devices containing carbon nanotube-infused fibers and methods for production thereof |
FR2960218B1 (fr) * | 2010-05-21 | 2012-08-03 | Thales Sa | Dispositif de dissipation thermique pour equipement spatial, notamment pour satellite |
US8780526B2 (en) | 2010-06-15 | 2014-07-15 | Applied Nanostructured Solutions, Llc | Electrical devices containing carbon nanotube-infused fibers and methods for production thereof |
US9017854B2 (en) | 2010-08-30 | 2015-04-28 | Applied Nanostructured Solutions, Llc | Structural energy storage assemblies and methods for production thereof |
AU2011302314A1 (en) | 2010-09-14 | 2013-02-28 | Applied Nanostructured Solutions, Llc | Glass substrates having carbon nanotubes grown thereon and methods for production thereof |
US8479880B2 (en) | 2010-09-15 | 2013-07-09 | The Boeing Company | Multifunctional nano-skin articles and methods |
WO2012040004A1 (en) | 2010-09-22 | 2012-03-29 | Applied Nanostructured Solutions, Llc | Carbon fiber substrates having carbon nanotubes grown thereon and processes for production thereof |
CA2782976A1 (en) | 2010-09-23 | 2012-03-29 | Applied Nanostructured Solutions, Llc | Cnt-infused fiber as a self shielding wire for enhanced power transmission line |
US9683312B2 (en) | 2011-12-10 | 2017-06-20 | The Boeing Company | Fiber with gradient properties and method of making the same |
US9683310B2 (en) | 2011-12-10 | 2017-06-20 | The Boeing Company | Hollow fiber with gradient properties and method of making the same |
US20130164498A1 (en) * | 2011-12-21 | 2013-06-27 | Adc Acquisition Company | Thermoplastic composite prepreg for automated fiber placement |
US9085464B2 (en) | 2012-03-07 | 2015-07-21 | Applied Nanostructured Solutions, Llc | Resistance measurement system and method of using the same |
US9242415B2 (en) * | 2012-07-06 | 2016-01-26 | Basf Corporation | Transparent and reusable vacuum infusion heating bag and methods of making and using same |
WO2014039509A2 (en) | 2012-09-04 | 2014-03-13 | Ocv Intellectual Capital, Llc | Dispersion of carbon enhanced reinforcement fibers in aqueous or non-aqueous media |
EP2909008B1 (en) * | 2012-10-22 | 2018-04-11 | Saab Ab | Integral attachment of fiber reinforced plastic rib to fiber reinforced plastic skin for aircraft airfoils |
US20140119904A1 (en) * | 2012-11-01 | 2014-05-01 | United Technologies Corporation | In-situ pressure enhanced processing of composite articles |
JP6373284B2 (ja) | 2013-02-28 | 2018-08-15 | エヌ12 テクノロジーズ, インク.N12 Technologies, Inc. | ナノ構造フィルムのカートリッジベース払い出し |
WO2015011549A1 (en) * | 2013-07-24 | 2015-01-29 | Toray Industries, Inc. | Fiber reinforced polymer composition with interlaminar hybridized tougheners |
TWI537984B (zh) * | 2013-10-24 | 2016-06-11 | 國立清華大學 | 可撓式透明電熱膜 |
GB2528080A (en) * | 2014-07-08 | 2016-01-13 | Airbus Operations Ltd | Structure |
US10046539B2 (en) * | 2014-07-22 | 2018-08-14 | United Technologies Corporation | Secondary reinforcement at interface of laminate structure |
US10457017B2 (en) | 2014-12-08 | 2019-10-29 | The Boeing Company | Method of forming a layered composite assembly |
US10024188B2 (en) * | 2015-03-02 | 2018-07-17 | Rohr, Inc. | High temperature composite inner fixed structure |
US10427378B2 (en) * | 2015-10-29 | 2019-10-01 | King Abdulaziz University | Composite epoxy material with embedded silicon carbide and alumina nanoparticles |
US10427382B2 (en) * | 2015-10-29 | 2019-10-01 | King Abdulaziz University | Composite epoxy material with embedded MWCNT fibers and process of manufacturing |
US10093041B2 (en) | 2016-04-11 | 2018-10-09 | The Boeing Company | Conductive pre-impregnated composite sheet and method for making the same |
EP3463826B1 (en) | 2016-05-31 | 2023-07-05 | Massachusetts Institute of Technology | Composite articles comprising non-linear elongated nanostructures and associated methods |
US10570541B2 (en) * | 2016-06-28 | 2020-02-25 | University Of Dayton | Carbon nanotube thread Z-axis multifunctional stitching |
US20180162092A1 (en) * | 2016-12-09 | 2018-06-14 | The Boeing Company | Fiber-modified interlayer for a composite structure and method of manufacture |
US10773467B2 (en) | 2016-12-15 | 2020-09-15 | The Boeing Company | Interlayer-toughened filament-wound composite structure |
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 |
DE102017214334A1 (de) | 2017-08-17 | 2019-02-21 | Technische Universität Dresden | Multi-Material-Verbund und Verfahren zu dessen Herstellung |
US20190065021A1 (en) * | 2017-08-30 | 2019-02-28 | Google Inc. | Hybrid scrolling of user interfaces |
WO2019055155A1 (en) | 2017-09-15 | 2019-03-21 | Massachusetts Institute Of Technology | LOW-RATE MANUFACTURE OF COMPOSITE MATERIAL DEFECTS |
EP3718157A4 (en) | 2017-11-28 | 2021-09-29 | Massachusetts Institute of Technology | SEPARATORS INCLUDING ELONGATED NANOSTRUCTURES AND ASSOCIATED DEVICES AND PROCESSES FOR STORING AND / OR USING ENERGY |
US11180238B2 (en) * | 2018-11-19 | 2021-11-23 | The Boeing Company | Shear ties for aircraft wing |
FR3092592B1 (fr) * | 2019-02-13 | 2021-02-19 | Safran | Procédé de fabrication d’une pièce en matériau composite à matrice renforcée et dispositif de mise en œuvre |
TWI732619B (zh) * | 2020-07-02 | 2021-07-01 | 和成欣業股份有限公司 | 複合材料結構及其成型方法 |
CN112590252A (zh) * | 2020-11-27 | 2021-04-02 | 哈尔滨工业大学 | 一种增强热塑性自动铺放构件层间性能的方法 |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS63286327A (ja) * | 1987-05-19 | 1988-11-24 | Asahi Chem Ind Co Ltd | 長繊維、炭素質ウィスカ−含有複合材 |
JP2005022141A (ja) * | 2003-06-30 | 2005-01-27 | Shinshu Univ | 複合材料およびその製造方法 |
JP2005538026A (ja) * | 2002-09-12 | 2005-12-15 | スネクマ・プロピュルシオン・ソリド | 耐火繊維の3次元繊維構造体、これを調製する方法、および耐熱構造複合材料への適用 |
JP2006527786A (ja) * | 2003-06-16 | 2006-12-07 | ウィリアム・マーシュ・ライス・ユニバーシティ | 官能基化カーボンナノチューブを使用するカーボンナノチューブ強化エポキシポリマー複合体の製造 |
JP2009517531A (ja) * | 2005-11-28 | 2009-04-30 | ユニバーシティ オブ ハワイ | 三次元強化多機能性ナノ複合体 |
JP2009537339A (ja) * | 2006-05-19 | 2009-10-29 | マサチューセッツ・インスティテュート・オブ・テクノロジー | ナノ構造強化された複合体およびナノ構造強化方法 |
Family Cites Families (233)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2004A (en) * | 1841-03-12 | Improvement in the manner of constructing and propelling steam-vessels | ||
US1504547A (en) | 1919-04-16 | 1924-08-12 | Henry C Egerton | Process of molding hollow articles |
US1976257A (en) | 1930-03-12 | 1934-10-09 | Super Marine Systems Inc | Laminated body and method of making same |
US2367750A (en) * | 1941-01-17 | 1945-01-23 | Central Aircraft Corp | Aircraft construction |
US2292372A (en) | 1941-07-28 | 1942-08-11 | Vultee Aircraft Inc | Structural element |
US2387219A (en) | 1941-08-08 | 1945-10-16 | Vickers Armstrongs Ltd | Aircraft structure |
US2750629A (en) * | 1951-05-21 | 1956-06-19 | Baudou Antoine Joseph Georges | Device for the manufacture of molded rubber boots and similar articles |
US3271917A (en) | 1959-06-12 | 1966-09-13 | Rubenstein David | Reinforced plastic constructions |
US2992711A (en) * | 1959-11-16 | 1961-07-18 | Ryan Aeronautical Co | Reinforcing means for attaching structural members to lightweight corrugated panels |
US3071217A (en) * | 1960-01-15 | 1963-01-01 | Avro Aircraft Ltd | Vibration damping in sheet metal structures |
US3306797A (en) * | 1963-08-02 | 1967-02-28 | Universal Moulded Fiber Glass | Method and apparatus for making elongated articles of fiber reinforced resin material |
US3490983A (en) * | 1965-05-17 | 1970-01-20 | Hitco | Fiber reinforced structures and methods of making the same |
US3376184A (en) * | 1965-06-11 | 1968-04-02 | Lawrence H Egland | Pressure bonding system for spanwise reinforced airfoils |
US3507634A (en) * | 1965-10-22 | 1970-04-21 | United Aircraft Corp | Composite metal structure |
US3452501A (en) * | 1966-05-02 | 1969-07-01 | Ernest C Zimmer | Snap locking structural device |
US3526558A (en) | 1966-06-27 | 1970-09-01 | Mill Polishing Corp | Process for making a decorative thermosetting plastic panel |
US3603096A (en) | 1969-12-10 | 1971-09-07 | Atomic Energy Commission | Apparatus for installing a reinforced vessel in an underground cavity |
US3879245A (en) * | 1972-06-27 | 1975-04-22 | Composite Structures Corp | Method of making composite cored structures |
US3975363A (en) | 1973-10-31 | 1976-08-17 | Trw Inc. | Poly(diels-alder) polymer |
US3974313A (en) | 1974-08-22 | 1976-08-10 | The Boeing Company | Projectile energy absorbing protective barrier |
US3995080A (en) | 1974-10-07 | 1976-11-30 | General Dynamics Corporation | Filament reinforced structural shapes |
US3976269A (en) | 1974-12-19 | 1976-08-24 | The Boeing Company | Intrinsically tuned structural panel |
US4086378A (en) * | 1975-02-20 | 1978-04-25 | Mcdonnell Douglas Corporation | Stiffened composite structural member and method of fabrication |
US4064534A (en) | 1976-04-20 | 1977-12-20 | Leone International Sales Corporation | System for monitoring the production of items which are initially difficult to physically inspect |
US4186535A (en) * | 1977-06-10 | 1980-02-05 | Verco Manufacturing, Inc. | Shear load resistant structure |
US4132755A (en) * | 1977-07-22 | 1979-01-02 | Jay Johnson | Process for manufacturing resin-impregnated, reinforced articles without the presence of resin fumes |
US4331495A (en) | 1978-01-19 | 1982-05-25 | Rockwell International Corporation | Method of fabricating a reinforced composite structure |
US4256790A (en) * | 1978-01-19 | 1981-03-17 | Rockwell International Corporation | Reinforced composite structure and method of fabrication thereof |
US4310132A (en) * | 1978-02-16 | 1982-01-12 | Nasa | Fuselage structure using advanced technology fiber reinforced composites |
US4828202A (en) * | 1979-09-27 | 1989-05-09 | The Boeing Company | Method and apparatus for wideband vibration damping of reinforced skin structures |
US4490958A (en) * | 1979-12-12 | 1985-01-01 | Lowe Colin F | Sheet metal beam |
IT1126638B (it) * | 1979-12-20 | 1986-05-21 | Pier Luigi Nava | Procedimento e relativo utensile per stampare manufatti in resina armata |
US4311661A (en) | 1980-05-05 | 1982-01-19 | Mcdonnell Douglas Corporation | Resin impregnation process |
DE3040838C2 (de) | 1980-10-30 | 1984-10-25 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Verfahren und Vorrichtung zum Herstellen von flächigen Bauteilen aus faserverstärkten Werkstoffen |
US4331723A (en) | 1980-11-05 | 1982-05-25 | The Boeing Company | Advanced composite |
FR2497726A1 (fr) | 1981-01-12 | 1982-07-16 | Brochier Fils J | Article textile multicouches pour le renforcement de materiaux stratifies et procede pour son obtention |
US4416170A (en) | 1981-07-30 | 1983-11-22 | Champion International Corporation | Method of producing a steel caul |
US4448838A (en) * | 1981-09-04 | 1984-05-15 | Lear Fan Corp. | Graphite fiber reinforced laminate structure capable of withstanding lightning strikes |
US4463044A (en) * | 1981-09-28 | 1984-07-31 | The Boeing Company | Composite panel of varied thickness |
US4443401A (en) * | 1981-12-17 | 1984-04-17 | The Continental Group, Inc. | Apparatus for and method of thermoforming plastic cans |
WO1984000351A1 (en) | 1982-07-19 | 1984-02-02 | Boeing Co | Method and apparatus for fiber lamination |
US4492607A (en) | 1983-02-22 | 1985-01-08 | Rockwell International Corporation | Method for producing integrally stiffened fiber reinforced plastic panels |
US4715560A (en) | 1983-03-14 | 1987-12-29 | Lear Fan Limited | Composite cruciform structure for joining intersecting structural members of an airframe and the like |
DE3331494A1 (de) | 1983-09-01 | 1985-03-21 | Rudolf 8900 Augsburg Güthler | Mehrband-legemaschine |
US4542055A (en) | 1983-10-19 | 1985-09-17 | Conceptual Arts, Ltd. | Three-dimensional fabric painting surfaces |
US4736566A (en) * | 1984-01-17 | 1988-04-12 | Krotsch Harold V | Modular fabrication panel system |
US4548017A (en) | 1984-01-23 | 1985-10-22 | Liverpool Industries, Inc. | Building panel |
IT1173394B (it) | 1984-02-28 | 1987-06-24 | Rockwell Rimoldi Spa | Dispositivo di trasporto del lavoro in macchina per cucire a trasporto differenziale |
DE3412846A1 (de) | 1984-04-05 | 1985-10-17 | Hoechst Ag, 6230 Frankfurt | Flaechenfoermiger sandwichformkoerper |
US4574029A (en) | 1984-04-27 | 1986-03-04 | Ltv Aerospace And Defense Company | Apparatus for forming concave tape wrapped composite structures |
US4877471A (en) | 1984-08-24 | 1989-10-31 | The Boeing Company | Method and apparatus for delivering a resin-impregnated, multifilament band |
US4548859A (en) | 1984-10-12 | 1985-10-22 | The Boeing Company | Breather material and method of coating fabric with silicone rubber |
US4571355A (en) | 1984-11-28 | 1986-02-18 | The Boeing Company | Fiber reinforced resin composites formed of basic ply blankets |
US4622091A (en) | 1984-11-29 | 1986-11-11 | The Boeing Company | Resin film infusion process and apparatus |
US4608220A (en) | 1984-12-20 | 1986-08-26 | The Boeing Company | Method of forming composite material articles |
JPS61169394A (ja) | 1985-01-21 | 1986-07-31 | 日立造船株式会社 | 飛行機の胴体成形方法 |
FR2579130B1 (fr) | 1985-03-25 | 1987-10-09 | Aerospatiale | Procede et dispositif pour realiser une piece creuse de forme complexe par enroulement filamentaire au contact |
US4615935A (en) | 1985-04-29 | 1986-10-07 | The Boeing Company | Glass fiber reinforced ceramic preform and method of casting it |
US4966802A (en) | 1985-05-10 | 1990-10-30 | The Boeing Company | Composites made of fiber reinforced resin elements joined by adhesive |
US4780262A (en) | 1986-01-15 | 1988-10-25 | The Boeing Company | Method for making composite structures |
US4693678A (en) | 1986-01-15 | 1987-09-15 | The Boeing Company | Male layup-female molding system for fabricating reinforced composite structures |
US4699683A (en) | 1986-02-07 | 1987-10-13 | The Boeing Company | Multiroving fiber laminator |
DE3614618A1 (de) | 1986-04-30 | 1987-11-05 | Messerschmitt Boelkow Blohm | Schalenstruktur aus faserverstaerktem kunststoff |
US4830298A (en) * | 1986-09-30 | 1989-05-16 | The Boeing Company | Self-centering sheave for filaments |
US4933232A (en) * | 1986-11-28 | 1990-06-12 | Jim Walter Research Corp. | Isocyanate-carboxyl group-containing fatty compounds for manufacture of lignocellulosic composites |
US4760444A (en) * | 1987-07-22 | 1988-07-26 | Csd International, Inc. | Machine visual inspection device and method |
US4941182A (en) * | 1987-07-29 | 1990-07-10 | Phoenix Software Development Co. | Vision system and method for automated painting equipment |
JP2604607B2 (ja) | 1987-12-09 | 1997-04-30 | 三井金属鉱業株式会社 | 欠陥分布測定法および装置 |
US4959110A (en) | 1988-05-11 | 1990-09-25 | Morton Thiokol Inc. | Method for lining the inner surface of a cylindrical or domed cylindrical member with an elastomeric material |
FR2632604B1 (fr) * | 1988-06-08 | 1991-07-12 | Aerospatiale | Cadre en materiau composite notamment pour fuselage d'aeronef, et son procede de fabrication |
US4902215A (en) * | 1988-06-08 | 1990-02-20 | Seemann Iii William H | Plastic transfer molding techniques for the production of fiber reinforced plastic structures |
US4922232A (en) * | 1988-10-21 | 1990-05-01 | Bosich Joseph F | Leakage containment and detection systems |
GB2224000B (en) | 1988-11-10 | 1992-05-27 | Genrikh Vasilievich Novozhilov | Aircraft fuselage or other pressure vessel. |
US4942013A (en) | 1989-03-27 | 1990-07-17 | Mcdonnell Douglas Corporation | Vacuum resin impregnation process |
US5251849A (en) | 1989-12-26 | 1993-10-12 | Florida International University For Board Of Regents | Strain reduced airplane skin |
US5223067A (en) * | 1990-02-28 | 1993-06-29 | Fuji Jukogyo Kabushiki Kaisha | Method of fabricating aircraft fuselage structure |
US5086997A (en) * | 1990-04-02 | 1992-02-11 | The Boeing Company | Structural joint and a method for joining in reinforced thermoplastic fabrication |
FR2661872B1 (fr) | 1990-05-11 | 1992-09-04 | Rockwell Automotive Body Syst | Procede de fabrication d'un pare-soleil recouvert de tissu. |
FR2667013B1 (fr) | 1990-09-20 | 1994-06-03 | Snecma | Outillage pour le moulage d'une piece realisee en materiau composite. |
US5178812A (en) * | 1990-11-28 | 1993-01-12 | E. I. Du Pont De Nemours And Company | Method of making composites having improved surface properties |
US5058497A (en) | 1990-12-17 | 1991-10-22 | Mcdonnell Douglas Corporation | Compliant pressure roller |
CA2056330C (en) * | 1990-12-19 | 2003-06-10 | Alexander C. Dublinski | Method of fabricating a complex part made of composite material |
US5152949A (en) | 1990-12-19 | 1992-10-06 | United Technologies Corporation | Tooling method for resin transfer molding |
US5129813A (en) * | 1991-02-11 | 1992-07-14 | Shepherd G Maury | Embossed vacuum bag, methods for producing and using said bag |
US5464337A (en) | 1991-03-27 | 1995-11-07 | The Charles Stark Draper Laboratories | Resin transfer molding system |
US5262220A (en) | 1991-06-18 | 1993-11-16 | Chem-Tronics, Inc. | High strength structure assembly and method of making the same |
US5240376A (en) | 1991-07-31 | 1993-08-31 | Mcdonnell Douglas Corporation | SPF/DB hollow core fan blade |
US5292475A (en) * | 1992-03-06 | 1994-03-08 | Northrop Corporation | Tooling and process for variability reduction of composite structures |
US5337647A (en) | 1992-03-13 | 1994-08-16 | The Boeing Company | 3 dimensional braiding apparatus |
US5281388A (en) | 1992-03-20 | 1994-01-25 | Mcdonnell Douglas Corporation | Resin impregnation process for producing a resin-fiber composite |
US5242523A (en) | 1992-05-14 | 1993-09-07 | The Boeing Company | Caul and method for bonding and curing intricate composite structures |
US5429326A (en) * | 1992-07-09 | 1995-07-04 | Structural Laminates Company | Spliced laminate for aircraft fuselage |
US5830305A (en) | 1992-08-11 | 1998-11-03 | E. Khashoggi Industries, Llc | Methods of molding articles having an inorganically filled organic polymer matrix |
US5297760A (en) * | 1992-08-21 | 1994-03-29 | Mcdonnell Douglas Corporation | Aircraft skin lap splice |
US5651600A (en) | 1992-09-28 | 1997-07-29 | The Boeing Company | Method for controlling projection of optical layup template utilizing cooperative targets |
US5450147A (en) | 1992-09-28 | 1995-09-12 | The Boeing Company | Method for controlling projection of optical layup template utilizing cooperative targets |
US5560102A (en) | 1992-10-13 | 1996-10-01 | The Boeing Company | Panel and fuselage assembly |
US5951800A (en) | 1992-11-18 | 1999-09-14 | Mcdonnell Douglas Corp. | Fiber/metal laminate splice |
US5366684A (en) | 1992-12-31 | 1994-11-22 | Grumman Aerospace Corporation | Molding composite method using an inflatable bladder pressurized in an autoclave |
JPH06226889A (ja) * | 1993-02-05 | 1994-08-16 | Sky Alum Co Ltd | パネル材およびこれを用いた複合パネル |
US5765329A (en) * | 1993-06-28 | 1998-06-16 | Huang; Chihshu | Roof construction of corrugated sheets |
US6045651A (en) * | 1993-09-07 | 2000-04-04 | The Boeing Company | Hand assisted lamination system |
FR2713979B1 (fr) | 1993-12-21 | 1996-03-15 | Aerospatiale | Procédé et dispositif de fabrication de pièces stratifiées injectées basse pression, notamment à emboutis profonds. |
US5518208A (en) * | 1993-12-28 | 1996-05-21 | The Boeing Company | Optimum aircraft body frame to body skin shear tie installation pattern for body skin/stringer circumferential splices |
US5439549A (en) | 1993-12-28 | 1995-08-08 | The Boeing Company | Double edged pressure sensitive folded tape application apparatus |
RU2083371C1 (ru) * | 1994-04-28 | 1997-07-10 | Акционерное общество "Центр перспективных разработок" Акционерного общества "Центральный научно-исследовательский институт специального машиностроения | Несущая труба-оболочка из композиционных материалов, способ и оправка для ее изготовления |
US5540126A (en) | 1994-05-26 | 1996-07-30 | Piramoon Technologies | Automatic lay-up machine for composite fiber tape |
US5850107A (en) | 1994-06-10 | 1998-12-15 | Johnson & Johnson Vision Products, Inc. | Mold separation method and apparatus |
US5772950A (en) * | 1994-08-31 | 1998-06-30 | The Boeing Company | Method of vacuum forming a composite |
US5562788A (en) | 1994-09-20 | 1996-10-08 | The Boeing Company | Composite material laser flaw detection |
US5622733A (en) * | 1994-10-04 | 1997-04-22 | Rockwell International Corporation | Tooling for the fabrication of composite hollow crown-stiffened skins and panels |
US5529480A (en) | 1994-10-28 | 1996-06-25 | The Boeing Company | Honeycomb core forming restricter |
US5683646A (en) | 1995-05-10 | 1997-11-04 | Mcdonnell Douglas Corporation | Fabrication of large hollow composite structure with precisely defined outer surface |
MX9708842A (es) * | 1995-05-25 | 1998-03-31 | Minnesota Mining & Mfg | Filamentos de componentes multiples que se pueden fusionar y secar de modo durable, resistentes, no estirados. |
US5904972A (en) | 1995-06-07 | 1999-05-18 | Tpi Technology Inc. | Large composite core structures formed by vacuum assisted resin transfer molding |
US5619837A (en) * | 1995-07-26 | 1997-04-15 | Disanto; Fabricio N. | Corrugated panel structure |
DE19536675C1 (de) | 1995-09-30 | 1997-02-20 | Deutsche Forsch Luft Raumfahrt | Vorrichtung und Verfahren zur Herstellung von großflächigen Bauelementen nach dem RTM-Verfahren |
RU2099194C1 (ru) | 1995-12-01 | 1997-12-20 | Акционерное общество "Центр перспективных разработок" Акционерного общества "Центральный научно-исследовательский институт специального машиностроения" | Несущая труба-оболочка в виде тела вращения из композиционных материалов, способ и оправка для ее изготовления |
US5893534A (en) * | 1995-12-22 | 1999-04-13 | The Boeing Company | Structural apparatus and design to prevent oil can movement of webs in aircraft pressure bulkheads |
US5866272A (en) | 1996-01-11 | 1999-02-02 | The Boeing Company | Titanium-polymer hybrid laminates |
US5700337A (en) | 1996-03-01 | 1997-12-23 | Mcdonnell Douglas Corporation | Fabrication method for composite structure adapted for controlled structural deformation |
US5746553A (en) * | 1996-04-08 | 1998-05-05 | The Boeing Company | Dual purpose lay-up tool |
US6205239B1 (en) * | 1996-05-31 | 2001-03-20 | Texas Instruments Incorporated | System and method for circuit repair |
US6013341A (en) * | 1996-08-19 | 2000-01-11 | Mcdonnell Douglas Corporation | Carrying (bearing) pipe-casing made of composite materials, the method and the setting (straightening device) for its manufacturing |
US5809805A (en) | 1996-09-03 | 1998-09-22 | Mcdonnell Douglas Corporation | Warp/knit reinforced structural fabric |
US5963660A (en) | 1996-09-26 | 1999-10-05 | The Boeing Company | Method and apparatus for detecting and measuring laps and gaps in composite materials |
US6187411B1 (en) * | 1996-10-04 | 2001-02-13 | The Boeing Company | Stitch-reinforced sandwich panel and method of making same |
RU2103200C1 (ru) | 1996-10-29 | 1998-01-27 | Акционерное общество "Центр перспективных разработок" Акционерного общества "Центральный научно-исследовательский институт специального машиностроения" | Несущая труба-оболочка из композиционных материалов |
US6692681B1 (en) * | 1997-01-29 | 2004-02-17 | Raytheon Aircraft Company | Method and apparatus for manufacturing composite structures |
DE59806899D1 (de) * | 1997-02-05 | 2003-02-20 | Anatoli J Vassiliev | Flugzeug für Personen- und/oder Frachttransport |
US6051089A (en) | 1997-02-07 | 2000-04-18 | Mcdonnell Douglas Corporation | Reinforcing member for composite workpieces and associated methods |
JPH10258463A (ja) | 1997-03-19 | 1998-09-29 | Fuji Heavy Ind Ltd | 複合材の小骨およびその成形方法 |
WO1998050180A1 (en) * | 1997-05-06 | 1998-11-12 | The Boeing Company | Hybrid lay-up tool |
US5954917A (en) | 1997-06-02 | 1999-09-21 | Boeing North American, Inc. | Automated material delivery system |
US6074716A (en) * | 1997-06-10 | 2000-06-13 | Mcdonnell Douglas Corporation | Weavable metal matrix impregnated tow composite material |
FR2766407B1 (fr) | 1997-07-22 | 1999-10-15 | Aerospatiale | Procede de fabrication de pieces de grandes dimensions en materiau composite a matrice thermoplastique, telles que des troncons de fuselage d'aeronefs |
US5902535A (en) | 1997-07-30 | 1999-05-11 | Mcdonnell Douglas Corporation | Resin film infusion mold tooling and molding method |
US5979531A (en) | 1997-10-01 | 1999-11-09 | Mcdonnell Douglas Corporation | Bi-directional fiber placement head |
US6229819B1 (en) * | 1997-10-21 | 2001-05-08 | Mci Communications Corporation | Advanced intelligent network gateway |
FR2771332B1 (fr) | 1997-11-26 | 2000-01-07 | Jean Marie Finot | Procede pour la realisation de pieces de grandes dimensions, notamment de coques de bateaux en stratifie |
US5915317A (en) | 1997-12-22 | 1999-06-29 | Thrash; Patrick J. | Automated gantry-type stitching system |
US5953231A (en) | 1997-12-22 | 1999-09-14 | Mcdonnell Douglas Corporation | Automated quality control for stitching of textile articles |
US5931107A (en) | 1997-12-22 | 1999-08-03 | Mcdonnell Douglas Corporation | Advanced stitching head for making stitches in a textile article having variable thickness |
US6198983B1 (en) | 1997-12-22 | 2001-03-06 | Mcdonnell Douglas Corporation | Table-driven software architecture for a stitching system |
US6128545A (en) | 1997-12-22 | 2000-10-03 | Mcdonnell Douglas Corporation | Automated apparatus and method of generating native code for a stitching machine |
US6099906A (en) | 1998-06-22 | 2000-08-08 | Mcdonnell Douglas Corporation | Immersion process for impregnation of resin into preforms |
US6231941B1 (en) | 1998-07-14 | 2001-05-15 | The Boeing Company | Radius fillers for a resin transfer molding process |
US6766984B1 (en) | 1998-07-16 | 2004-07-27 | Icom Engineering Corporation | Stiffeners for aircraft structural panels |
US6086696A (en) | 1998-07-21 | 2000-07-11 | The Boeing Company | Method of forming a seamless, cylindrical, thermoplastic structure with a multiple compaction roller winder |
DE19844035C1 (de) * | 1998-09-25 | 1999-11-25 | Daimler Chrysler Aerospace | Schalenbauteil für ein Flugzeug und Verfahren zur Herstellung |
FI982095A (fi) * | 1998-09-29 | 2000-03-30 | Nokia Networks Oy | Menetelmä muistin toteuttamiseksi ja muistijärjestely |
US6112792A (en) | 1998-11-19 | 2000-09-05 | The Boeing Company | Fiber placement mid-span redirect |
US6190484B1 (en) * | 1999-02-19 | 2001-02-20 | Kari Appa | Monolithic composite wing manufacturing process |
US6558590B1 (en) * | 1999-03-18 | 2003-05-06 | David H. Stewart | Method and machine for manufacturing molded structures using zoned pressure molding |
US6261675B1 (en) | 1999-03-23 | 2001-07-17 | Hexcel Corporation | Core-crush resistant fabric and prepreg for fiber reinforced composite sandwich structures |
US6319447B1 (en) | 1999-04-09 | 2001-11-20 | The Boeing Company | Resin transfer molding process |
US6136237A (en) | 1999-04-13 | 2000-10-24 | The Boeing Company | Method of fabricating a fiber-reinforced ceramic matrix composite part |
US6510961B1 (en) * | 1999-04-14 | 2003-01-28 | A&P Technology | Integrally-reinforced braided tubular structure and method of producing the same |
US6245275B1 (en) * | 1999-05-13 | 2001-06-12 | Vought Aircraft Industries, Inc. | Method for fabricating composite structures |
US6431837B1 (en) | 1999-06-01 | 2002-08-13 | Alexander Velicki | Stitched composite fan blade |
US7132161B2 (en) * | 1999-06-14 | 2006-11-07 | Energy Science Laboratories, Inc. | Fiber adhesive material |
EP1224052A1 (en) | 1999-09-03 | 2002-07-24 | Lockheed Martin Corp. | Friction stir welding as a rivet replacement technology |
US6374750B1 (en) * | 1999-11-16 | 2002-04-23 | Aero Transportation Products, Inc. | Structural panel system |
US6129031A (en) | 1999-11-16 | 2000-10-10 | The Boeing Company | Robotic stitching apparatus and end effector therefor |
US6390169B1 (en) * | 2000-02-23 | 2002-05-21 | The Boeing Company | Conformable compaction apparatus for use with a fiber placement machine |
EP1261787A2 (en) | 2000-02-25 | 2002-12-04 | The Boeing Company | Laminated composite radius filler |
ES2185443B1 (es) * | 2000-03-07 | 2004-09-01 | Airbus España S.L. | Procedimiento de fabricacion de piezas precuradas en material compuesto con rigidizadores aplicados en estado fresco. |
DE10013409C1 (de) * | 2000-03-17 | 2000-11-23 | Daimler Chrysler Ag | Verfahren und Vorrichtung zur Herstellung von faserverstärkten Bauteilen mittels eines Injektionsverfahrens |
FR2806349B1 (fr) * | 2000-03-20 | 2002-12-06 | Plastic Omnium Cie | Procede de fabrication d'une piece en matiere plastique renforcee |
JP4425422B2 (ja) | 2000-04-14 | 2010-03-03 | 本田技研工業株式会社 | 複合材製構造体の製造方法、及びそれにより製造される複合材製構造体 |
JP4318381B2 (ja) | 2000-04-27 | 2009-08-19 | 本田技研工業株式会社 | 繊維強化複合材からなる胴体構造体の製造方法、及びそれにより製造される胴体構造体 |
JP4425424B2 (ja) * | 2000-05-01 | 2010-03-03 | 本田技研工業株式会社 | 繊維強化複合材からなるジョグル付き半硬化物品の製造方法、及びそれを用いた予備成形構造体の製造方法 |
US6451152B1 (en) | 2000-05-24 | 2002-09-17 | The Boeing Company | Method for heating and controlling temperature of composite material during automated placement |
US6620484B1 (en) | 2000-06-06 | 2003-09-16 | The Boeing Company | Variable density stitched-composite structural elements for energy absorption |
US6415581B1 (en) | 2000-07-17 | 2002-07-09 | Deck West, Incorporated | Corrugated stiffening member |
DE10037307B4 (de) | 2000-07-28 | 2004-02-05 | Honsel Gmbh & Co Kg | Strukturelement für ein Flugzeug, insbesondere Flugzeugtür |
WO2002040254A2 (en) | 2000-11-15 | 2002-05-23 | Toyota Motor Sales, U.S.A., Inc. | One-piece closed-shape structure and method of forming same |
JP4526698B2 (ja) * | 2000-12-22 | 2010-08-18 | 富士重工業株式会社 | 複合材成形品及びその製造方法 |
US6480271B1 (en) | 2001-01-08 | 2002-11-12 | The Boeing Company | Traversing laser locating system |
US6743504B1 (en) | 2001-03-01 | 2004-06-01 | Rohr, Inc. | Co-cured composite structures and method of making them |
US7171033B2 (en) * | 2001-03-28 | 2007-01-30 | The Boeing Company | System and method for identifying defects in a composite structure |
SE519185C2 (sv) * | 2001-06-07 | 2003-01-28 | Saab Ab | Flygplanspanel |
US6840750B2 (en) | 2001-06-11 | 2005-01-11 | The Boeing Company | Resin infusion mold tool system and vacuum assisted resin transfer molding with subsequent pressure bleed |
US6862989B2 (en) * | 2001-09-19 | 2005-03-08 | Goss International Americas, Inc. | Blanket cylinder with integrated compressible layer |
US6648273B2 (en) | 2001-10-30 | 2003-11-18 | The Boeing Company | Light weight and high strength fuselage |
US6799619B2 (en) | 2002-02-06 | 2004-10-05 | The Boeing Company | Composite material collation machine and associated method for high rate collation of composite materials |
US20030190455A1 (en) | 2002-04-05 | 2003-10-09 | The Boeing Company | Textile joint reinforcement and associated method |
JP2005527410A (ja) * | 2002-05-29 | 2005-09-15 | ザ・ボーイング・カンパニー | 制御された大気圧樹脂注入プロセス |
US6860957B2 (en) * | 2002-06-13 | 2005-03-01 | Kawasaki Jukogyo Kabushiki Kaisha | Automatic prepreg laminating method and apparatus for carrying out the same |
JP2004074271A (ja) | 2002-06-20 | 2004-03-11 | Sumitomo Heavy Ind Ltd | プレス装置 |
JP2004025946A (ja) | 2002-06-24 | 2004-01-29 | Honda Motor Co Ltd | 航空機の翼構造 |
US6871684B2 (en) * | 2002-08-13 | 2005-03-29 | The Boeing Company | System for identifying defects in a composite structure |
US6622974B1 (en) | 2002-08-14 | 2003-09-23 | The Boeing Company | Geometric morphing wing with expandable spars |
US20040035979A1 (en) * | 2002-08-23 | 2004-02-26 | Mccoskey William Robert | Integrally stiffened axial load carrying skin panels for primary aircraft structure and closed loop manufacturing methods for making the same |
US20040086341A1 (en) * | 2002-11-05 | 2004-05-06 | Conoco Inc. | Metal lined composite risers in offshore applications |
US7137182B2 (en) | 2002-11-22 | 2006-11-21 | The Boeing Company | Parallel configuration composite material fabricator |
US20040222080A1 (en) * | 2002-12-17 | 2004-11-11 | William Marsh Rice University | Use of microwaves to crosslink carbon nanotubes to facilitate modification |
US20040145092A1 (en) | 2003-01-24 | 2004-07-29 | Mccollum Robert P. | Method of making a composite molded article |
FR2844472B1 (fr) | 2003-02-14 | 2006-03-31 | Saint Gobain Vetrotex | Procede de fabrication de produits composites par rotomoulage et produits obtenus |
US6896841B2 (en) | 2003-03-20 | 2005-05-24 | The Boeing Company | Molding process and apparatus for producing unified composite structures |
TWI221554B (en) | 2003-03-21 | 2004-10-01 | Micro Star Int Co Ltd | Method in BIOS for shadow memory assignment |
US20040219855A1 (en) * | 2003-05-02 | 2004-11-04 | Tsotsis Thomas K. | Highly porous interlayers to toughen liquid-molded fabric-based composites |
US8246882B2 (en) * | 2003-05-02 | 2012-08-21 | The Boeing Company | Methods and preforms for forming composite members with interlayers formed of nonwoven, continuous materials |
JP3782072B2 (ja) | 2003-05-30 | 2006-06-07 | 川崎重工業株式会社 | 複合材型材の成形方法及び装置 |
US7236625B2 (en) * | 2003-07-28 | 2007-06-26 | The Boeing Company | Systems and method for identifying foreign objects and debris (FOD) and defects during fabrication of a composite structure |
US7080441B2 (en) | 2003-07-28 | 2006-07-25 | The Boeing Company | Composite fuselage machine and method of automated composite lay up |
US7048024B2 (en) * | 2003-08-22 | 2006-05-23 | The Boeing Company | Unidirectional, multi-head fiber placement |
US7083698B2 (en) | 2003-08-22 | 2006-08-01 | The Boeing Company | Automated composite lay-up to an internal fuselage mandrel |
US7282107B2 (en) | 2003-08-22 | 2007-10-16 | The Boeing Company | Multiple head automated composite laminating machine for the fabrication of large barrel section components |
US7228611B2 (en) * | 2003-11-18 | 2007-06-12 | The Boeing Company | Method of transferring large uncured composite laminates |
US7289656B2 (en) | 2003-12-02 | 2007-10-30 | The Boeing Company | Systems and methods for determining inconsistency characteristics of a composite structure |
FR2865739B1 (fr) * | 2004-01-30 | 2006-06-02 | Centre Nat Rech Scient | Procede d'obtention de nanotubes de carbone sur des supports et composites les renfermant |
US7039485B2 (en) * | 2004-03-12 | 2006-05-02 | The Boeing Company | Systems and methods enabling automated return to and/or repair of defects with a material placement machine |
US7093797B2 (en) | 2004-03-29 | 2006-08-22 | The Boeing Company | Adaptable payload apparatus and methods |
US7195201B2 (en) * | 2004-03-29 | 2007-03-27 | The Boeing Company | Adaptable payload enabling architecture |
EP1729949B1 (de) | 2004-03-30 | 2011-07-13 | Esoro Ag | Verfahren zur herstellung von formkörpern aus thermoplastischem material |
US7159822B2 (en) * | 2004-04-06 | 2007-01-09 | The Boeing Company | Structural panels for use in aircraft fuselages and other structures |
US7527222B2 (en) * | 2004-04-06 | 2009-05-05 | The Boeing Company | Composite barrel sections for aircraft fuselages and other structures, and methods and systems for manufacturing such barrel sections |
US7134629B2 (en) | 2004-04-06 | 2006-11-14 | The Boeing Company | Structural panels for use in aircraft fuselages and other structures |
US7193696B2 (en) * | 2004-04-12 | 2007-03-20 | United Technologies Corporation | Systems and methods for using light to indicate defect locations on a composite structure |
EP1755997B1 (en) | 2004-04-21 | 2014-11-26 | Ingersoll Machine Tools, Inc. | Automated fiber placement using multiple placement heads, replaceable creels, and replaceable placement heads |
US7080805B2 (en) | 2004-05-05 | 2006-07-25 | The Boeing Company | Stiffened structures and associated methods |
US7622066B2 (en) * | 2004-07-26 | 2009-11-24 | The Boeing Company | Methods and systems for manufacturing composite parts with female tools |
US7325771B2 (en) * | 2004-09-23 | 2008-02-05 | The Boeing Company | Splice joints for composite aircraft fuselages and other structures |
US7306450B2 (en) * | 2004-09-29 | 2007-12-11 | The Boeing Company | Apparatuses, systems, and methods for manufacturing composite parts |
US7126496B2 (en) * | 2004-09-30 | 2006-10-24 | Safe Flight Instrument Corporation | Tactile cueing system and method for aiding a helicopter pilot in making landings |
US7503368B2 (en) * | 2004-11-24 | 2009-03-17 | The Boeing Company | Composite sections for aircraft fuselages and other structures, and methods and systems for manufacturing such sections |
US20060118244A1 (en) * | 2004-12-02 | 2006-06-08 | The Boeing Company | Device for laying tape materials for aerospace applications |
US7624488B2 (en) | 2004-12-07 | 2009-12-01 | The Boeing Company | One-piece barrel assembly cart |
US7278198B2 (en) | 2005-02-01 | 2007-10-09 | The Boeing Company | Mandrel segment loader |
US7655168B2 (en) | 2006-01-31 | 2010-02-02 | The Boeing Company | Tools for manufacturing composite parts and methods for using such tools |
US8388795B2 (en) | 2007-05-17 | 2013-03-05 | The Boeing Company | Nanotube-enhanced interlayers for composite structures |
US8042767B2 (en) | 2007-09-04 | 2011-10-25 | The Boeing Company | Composite fabric with rigid member structure |
-
2007
- 2007-05-17 US US11/750,207 patent/US8388795B2/en active Active
-
2008
- 2008-05-02 EP EP08826563.2A patent/EP2155471B1/en active Active
- 2008-05-02 EP EP13165426.1A patent/EP2623296B1/en active Active
- 2008-05-02 WO PCT/US2008/062386 patent/WO2009014788A2/en active Application Filing
- 2008-05-02 JP JP2010508491A patent/JP5595909B2/ja active Active
-
2012
- 2012-08-16 US US13/587,567 patent/US8657990B2/en active Active
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS63286327A (ja) * | 1987-05-19 | 1988-11-24 | Asahi Chem Ind Co Ltd | 長繊維、炭素質ウィスカ−含有複合材 |
JP2005538026A (ja) * | 2002-09-12 | 2005-12-15 | スネクマ・プロピュルシオン・ソリド | 耐火繊維の3次元繊維構造体、これを調製する方法、および耐熱構造複合材料への適用 |
JP2006527786A (ja) * | 2003-06-16 | 2006-12-07 | ウィリアム・マーシュ・ライス・ユニバーシティ | 官能基化カーボンナノチューブを使用するカーボンナノチューブ強化エポキシポリマー複合体の製造 |
JP2005022141A (ja) * | 2003-06-30 | 2005-01-27 | Shinshu Univ | 複合材料およびその製造方法 |
JP2009517531A (ja) * | 2005-11-28 | 2009-04-30 | ユニバーシティ オブ ハワイ | 三次元強化多機能性ナノ複合体 |
JP2009537339A (ja) * | 2006-05-19 | 2009-10-29 | マサチューセッツ・インスティテュート・オブ・テクノロジー | ナノ構造強化された複合体およびナノ構造強化方法 |
Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2013502335A (ja) * | 2009-08-17 | 2013-01-24 | ザ・ボーイング・カンパニー | 積層複合ロッド、その製造方法と複合構造における使用 |
WO2012018062A1 (ja) * | 2010-08-04 | 2012-02-09 | アイシン精機株式会社 | カーボンナノチューブデバイス、カーボンナノチューブ製造方法およびカーボンナノチューブ製造装置 |
JP2012036022A (ja) * | 2010-08-04 | 2012-02-23 | Aisin Seiki Co Ltd | カーボンナノチューブ製造方法およびカーボンナノチューブ製造装置 |
JP2012035345A (ja) * | 2010-08-04 | 2012-02-23 | Aisin Seiki Co Ltd | カーボンナノチューブデバイス |
JP2015504799A (ja) * | 2012-01-26 | 2015-02-16 | イー・アイ・デュポン・ドウ・ヌムール・アンド・カンパニーE.I.Du Pont De Nemours And Company | サンドイッチパネルの製造方法 |
JP2017507809A (ja) * | 2014-02-04 | 2017-03-23 | エヌ12 テクノロジーズ, インク.N12 Technologies, Inc. | ナノ構造強化コンポジットの物品及び製造方法 |
JP2015196378A (ja) * | 2014-04-02 | 2015-11-09 | ザ・ボーイング・カンパニーTheBoeing Company | ポリマーナノ粒子ポリマーを用いて製造された不織中間層 |
JP7053131B2 (ja) | 2014-04-02 | 2022-04-12 | ザ・ボーイング・カンパニー | ポリマーナノ粒子ポリマーを用いて製造された不織中間層 |
JP2017525602A (ja) * | 2014-05-28 | 2017-09-07 | ユニヴァーシティ オブ サウス アラバマ | 多孔質媒体中でナノファイバーを一方向に配列する装置及び方法 |
US10556390B2 (en) | 2014-05-28 | 2020-02-11 | University Of South Alabama | Apparatus and method for directional alignment of nanofibers in a porous medium |
WO2016159072A1 (ja) * | 2015-03-31 | 2016-10-06 | 国立研究開発法人産業技術総合研究所 | 炭素繊維複合材料の製造方法 |
JPWO2016159072A1 (ja) * | 2015-03-31 | 2018-03-08 | 国立研究開発法人産業技術総合研究所 | 炭素繊維複合材料の製造方法 |
Also Published As
Publication number | Publication date |
---|---|
US20140020825A1 (en) | 2014-01-23 |
US20080286564A1 (en) | 2008-11-20 |
EP2623296B1 (en) | 2018-10-17 |
EP2155471A2 (en) | 2010-02-24 |
EP2623296A1 (en) | 2013-08-07 |
WO2009014788A3 (en) | 2009-12-30 |
US8388795B2 (en) | 2013-03-05 |
JP5595909B2 (ja) | 2014-09-24 |
US8657990B2 (en) | 2014-02-25 |
WO2009014788A2 (en) | 2009-01-29 |
EP2155471B1 (en) | 2019-01-02 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
JP5595909B2 (ja) | 複合構造用ナノチューブ強化中間層 | |
AU2020201610B2 (en) | Fabrication of composite laminates using temporarily stitched preforms | |
US10427330B2 (en) | Hybrid lay-up mold | |
EP1827813B1 (en) | Method and preforms for forming composite members with interlayers formed of nonwoven continuous materials | |
JP2010527302A5 (ja) | ||
EP3854924B1 (en) | Method of manufacturing a composite structure | |
US10035333B2 (en) | Fibre reinforced composite | |
CN110573312A (zh) | 具有局部增强物的预制件 | |
JP2021169686A (ja) | 中間層、並びにこれに関連する補強構造体、複合材及び方法 |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
A521 | Request for written amendment filed |
Free format text: JAPANESE INTERMEDIATE CODE: A523 Effective date: 20110425 |
|
A621 | Written request for application examination |
Free format text: JAPANESE INTERMEDIATE CODE: A621 Effective date: 20110425 |
|
A977 | Report on retrieval |
Free format text: JAPANESE INTERMEDIATE CODE: A971007 Effective date: 20130724 |
|
A131 | Notification of reasons for refusal |
Free format text: JAPANESE INTERMEDIATE CODE: A131 Effective date: 20130820 |
|
TRDD | Decision of grant or rejection written | ||
A01 | Written decision to grant a patent or to grant a registration (utility model) |
Free format text: JAPANESE INTERMEDIATE CODE: A01 Effective date: 20140708 |
|
A61 | First payment of annual fees (during grant procedure) |
Free format text: JAPANESE INTERMEDIATE CODE: A61 Effective date: 20140806 |
|
R150 | Certificate of patent or registration of utility model |
Ref document number: 5595909 Country of ref document: JP Free format text: JAPANESE INTERMEDIATE CODE: R150 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |