BR112013003189A2 - material composto usinável - Google Patents
material composto usinávelInfo
- Publication number
- BR112013003189A2 BR112013003189A2 BR112013003189A BR112013003189A BR112013003189A2 BR 112013003189 A2 BR112013003189 A2 BR 112013003189A2 BR 112013003189 A BR112013003189 A BR 112013003189A BR 112013003189 A BR112013003189 A BR 112013003189A BR 112013003189 A2 BR112013003189 A2 BR 112013003189A2
- Authority
- BR
- Brazil
- Prior art keywords
- composite material
- fibrous structure
- machinable
- machined
- produce
- Prior art date
Links
- 239000002131 composite material Substances 0.000 title abstract 7
- 239000000835 fiber Substances 0.000 abstract 2
- 239000011159 matrix material Substances 0.000 abstract 1
- 230000035515 penetration Effects 0.000 abstract 1
- 239000011347 resin Substances 0.000 abstract 1
- 229920005989 resin Polymers 0.000 abstract 1
Classifications
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- 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
- B29C70/545—Perforating, cutting or machining during or after 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
- B29C70/68—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks
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- 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
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/28—Layered products comprising a layer of synthetic resin comprising synthetic resins not wholly covered by any one of the sub-groups B32B27/30 - B32B27/42
- B32B27/281—Layered products comprising a layer of synthetic resin comprising synthetic resins not wholly covered by any one of the sub-groups B32B27/30 - B32B27/42 comprising polyimides
-
- 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
- B32B27/28—Layered products comprising a layer of synthetic resin comprising synthetic resins not wholly covered by any one of the sub-groups B32B27/30 - B32B27/42
- B32B27/286—Layered products comprising a layer of synthetic resin comprising synthetic resins not wholly covered by any one of the sub-groups B32B27/30 - B32B27/42 comprising polysulphones; polysulfides
-
- 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
- B32B27/28—Layered products comprising a layer of synthetic resin comprising synthetic resins not wholly covered by any one of the sub-groups B32B27/30 - B32B27/42
- B32B27/288—Layered products comprising a layer of synthetic resin comprising synthetic resins not wholly covered by any one of the sub-groups B32B27/30 - B32B27/42 comprising polyketones
-
- 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
- B32B27/30—Layered products comprising a layer of synthetic resin comprising vinyl (co)polymers; comprising acrylic (co)polymers
-
- 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
- B32B27/36—Layered products comprising a layer of synthetic resin comprising polyesters
-
- 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
- B32B27/38—Layered products comprising a layer of synthetic resin comprising epoxy resins
-
- 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
- B32B27/42—Layered products comprising a layer of synthetic resin comprising condensation resins of aldehydes, e.g. with phenols, ureas or melamines
-
- 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
- B32B5/022—Non-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
- B32B5/024—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
- B32B5/22—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
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- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08J—WORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
- C08J5/00—Manufacture of articles or shaped materials containing macromolecular substances
- C08J5/04—Reinforcing macromolecular compounds with loose or coherent fibrous material
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08J—WORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
- C08J5/00—Manufacture of articles or shaped materials containing macromolecular substances
- C08J5/24—Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs
- C08J5/241—Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs using inorganic fibres
- C08J5/243—Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs using inorganic fibres using carbon fibres
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/02—Synthetic macromolecular fibres
- B32B2262/0253—Polyolefin fibres
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/02—Synthetic macromolecular fibres
- B32B2262/0261—Polyamide fibres
- B32B2262/0269—Aromatic polyamide fibres
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/10—Inorganic fibres
- B32B2262/101—Glass fibres
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/10—Inorganic fibres
- B32B2262/106—Carbon fibres, e.g. graphite fibres
-
- 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
- B32B2307/72—Density
-
- 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
- B32B2307/732—Dimensional 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
- B32B2605/00—Vehicles
- B32B2605/18—Aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/10—Manufacturing or assembling aircraft, e.g. jigs therefor
-
- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/249921—Web or sheet containing structurally defined element or component
- Y10T428/249923—Including interlaminar mechanical fastener
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/249921—Web or sheet containing structurally defined element or component
- Y10T428/249924—Noninterengaged fiber-containing paper-free web or sheet which is not of specified porosity
- Y10T428/249933—Fiber embedded in or on the surface of a natural or synthetic rubber matrix
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/249921—Web or sheet containing structurally defined element or component
- Y10T428/249924—Noninterengaged fiber-containing paper-free web or sheet which is not of specified porosity
- Y10T428/249933—Fiber embedded in or on the surface of a natural or synthetic rubber matrix
- Y10T428/249939—Two or more layers
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/249921—Web or sheet containing structurally defined element or component
- Y10T428/249924—Noninterengaged fiber-containing paper-free web or sheet which is not of specified porosity
- Y10T428/24994—Fiber embedded in or on the surface of a polymeric matrix
- Y10T428/249942—Fibers are aligned substantially parallel
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/249921—Web or sheet containing structurally defined element or component
- Y10T428/249924—Noninterengaged fiber-containing paper-free web or sheet which is not of specified porosity
- Y10T428/24994—Fiber embedded in or on the surface of a polymeric matrix
- Y10T428/24995—Two or more layers
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Polymers & Plastics (AREA)
- Composite Materials (AREA)
- Health & Medical Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Medicinal Chemistry (AREA)
- Textile Engineering (AREA)
- Organic Chemistry (AREA)
- Manufacturing & Machinery (AREA)
- Mechanical Engineering (AREA)
- Inorganic Chemistry (AREA)
- Moulding By Coating Moulds (AREA)
- Reinforced Plastic Materials (AREA)
- Laminated Bodies (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
Abstract
material composto usinável.um material composto que pode ser usinado para produzir uma peça composta para aplicações estruturais que tem pelo menos uma superfície usinada. o material composto inclui uma estrutura fibrosa contendo fibras e uma matriz de resina. a estrutura fibrosa tem pelo menos uma superfície. uma camada usinável de material composto de fibra descontínua fica localizada na(s) superfície(s) da estrutura fibrosa. uma porção da(s) camada(s) usinável(is) é removida para produzir uma peça composta tendo a dimensão usinada final desejada sem a penetração na estrutura fibrosa.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US85621010A | 2010-08-13 | 2010-08-13 | |
| PCT/US2011/045130 WO2012021283A1 (en) | 2010-08-13 | 2011-07-23 | Machinable composite material |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| BR112013003189A2 true BR112013003189A2 (pt) | 2016-05-17 |
| BR112013003189B1 BR112013003189B1 (pt) | 2019-12-31 |
Family
ID=45565040
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BR112013003189A BR112013003189B1 (pt) | 2010-08-13 | 2011-07-23 | aeronave |
Country Status (8)
| Country | Link |
|---|---|
| US (1) | US8864070B2 (pt) |
| EP (1) | EP2603380A1 (pt) |
| JP (1) | JP6218323B2 (pt) |
| CN (1) | CN103068568B (pt) |
| AU (1) | AU2011289779B2 (pt) |
| BR (1) | BR112013003189B1 (pt) |
| CA (1) | CA2806330C (pt) |
| WO (1) | WO2012021283A1 (pt) |
Families Citing this family (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CA2806330C (en) * | 2010-08-13 | 2017-01-03 | Hexcel Corporation | Machinable composite material |
| US9393745B2 (en) * | 2012-05-15 | 2016-07-19 | Hexcel Corporation | Over-molding of load-bearing composite structures |
| US10239289B2 (en) * | 2013-04-12 | 2019-03-26 | Hexcel Corporation | Multi-component composite structures |
| EP3058199B1 (en) * | 2013-10-15 | 2021-06-30 | Raytheon Technologies Corporation | Compression molded fiber reinforced fan case ice panel |
| US20150355111A1 (en) | 2014-06-09 | 2015-12-10 | Hexcel Corporation | Tracers for use in compression molding of unidirectional discontinuous fiber composite molding compound |
| US9399510B2 (en) * | 2014-08-20 | 2016-07-26 | The Boeing Company | Hat stringer closeout fitting and method of making same |
| US9857789B2 (en) * | 2015-05-04 | 2018-01-02 | The Boeing Company | Model-based definition for machining aircraft parts |
| US9724854B2 (en) | 2015-05-13 | 2017-08-08 | Hexcel Composites Limited | Preforms made directly from thermosetting composite chips |
| US20180162019A1 (en) * | 2015-06-23 | 2018-06-14 | Hexcel Reinforcements SASU | Improvements in or relating to three dimensional mouldings |
| DE102016003109A1 (de) * | 2016-03-15 | 2017-09-21 | Premium Aerotec Gmbh | Verfahren zur Herstellung eines thermoplastischen Faserverbundbauteils und thermoplastisches Faserverbundbauteil |
| GB2550605B (en) * | 2016-05-23 | 2022-05-11 | Chambers David | A joint comprising an interface enabling structural continuity between joining intersecting members manufactured using composite materials |
| WO2018163411A1 (ja) * | 2017-03-10 | 2018-09-13 | 日産自動車株式会社 | 複合材料部材、複合材料部材の製造方法及びその成形用型 |
| US11192595B2 (en) * | 2018-01-09 | 2021-12-07 | Faurecia Emissions Control Technologies, Usa, Llc | Overmolded brackets for composite shock tower |
Family Cites Families (28)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4136846A (en) | 1976-12-20 | 1979-01-30 | Boeing Commercial Airplane Company | Composite structure |
| JPH01281930A (ja) * | 1988-05-07 | 1989-11-13 | Mitsubishi Electric Corp | アラミド繊維強化プラスチック積層体 |
| DE19716057A1 (de) * | 1997-04-17 | 1998-10-22 | Dynamit Nobel Ag | Formteile aus Aramid-Hochleistungsfaser-verstärktem Kunststoff |
| FR2763882B1 (fr) | 1997-05-29 | 1999-08-20 | Aerospatiale | Outillage de reparation sur site d'une structure composite presentant une zone endommagee et procede correspondant |
| FR2770802B1 (fr) | 1997-11-13 | 2000-02-11 | Duqueine | Procede de moulage d'une piece composite, structure composite employee dans ce procede et manivelle obtenue selon ce procede |
| EP1125728B1 (en) * | 1999-03-23 | 2011-10-05 | Toray Industries, Inc. | Composite reinforcing fiber base material, preform and production method for fiber reinforced plastic |
| FR2806425B1 (fr) | 2000-03-16 | 2002-07-12 | Hexcel Composites | Produit intermediaire composite, procede de production d'un tel produit et utilisation a titre de materiau de moulage |
| US6924021B1 (en) | 2002-07-03 | 2005-08-02 | Trek Bicycle Corporation | Complex-shaped carbon fiber structural member and its method of manufacture |
| JP4177041B2 (ja) * | 2002-07-18 | 2008-11-05 | 三菱レイヨン株式会社 | 繊維強化複合材料の製造方法 |
| US7141191B2 (en) | 2003-05-02 | 2006-11-28 | The Boeing Company | Triple purpose lay-up tool |
| JP4260039B2 (ja) * | 2004-02-20 | 2009-04-30 | 鹿島建設株式会社 | 切削可能部材およびその製造方法 |
| US20060115320A1 (en) | 2004-11-30 | 2006-06-01 | The Boeing Company | Determinant assembly features for vehicle structures |
| US8212194B2 (en) * | 2006-06-27 | 2012-07-03 | Hexcel Corporation | Aerospace articles made from quasi-isotropic chopped prepreg |
| US7960674B2 (en) * | 2005-06-28 | 2011-06-14 | Hexcel Corporation | Aerospace articles made from quasi-isotropic chopped prepreg |
| US7510390B2 (en) | 2005-07-13 | 2009-03-31 | Hexcel Corporation | Machinable composite mold |
| JP2007203723A (ja) * | 2006-02-06 | 2007-08-16 | Nippon Steel Composite Co Ltd | 繊維強化プラスチック製管体及びその製造方法 |
| JP2007229344A (ja) * | 2006-03-03 | 2007-09-13 | Brother Ind Ltd | ミシンの加工布位置決めガイド装置 |
| DE102006026170B4 (de) * | 2006-06-06 | 2012-06-21 | Airbus Operations Gmbh | Flugzeugrumpfstruktur und Verfahren zu deren Herstellung |
| GB0619401D0 (en) | 2006-10-02 | 2006-11-08 | Hexcel Composites Ltd | Composite materials with improved performance |
| WO2009008903A1 (en) | 2007-01-12 | 2009-01-15 | The Nordam Group, Inc. | Aircraft window erosion shield |
| JP5045285B2 (ja) * | 2007-07-18 | 2012-10-10 | トヨタ自動車株式会社 | 繊維強化樹脂面材の製作方法 |
| US7854204B2 (en) * | 2007-10-12 | 2010-12-21 | Walter Dacus | Ultralight unit load device |
| FR2926118B1 (fr) * | 2008-01-04 | 2010-01-29 | Snecma | Bride en composite avec partie d'usinage. |
| US20110247958A1 (en) * | 2008-10-16 | 2011-10-13 | Composite Transport Technologies ,Inc. | Lightweight unit load device |
| IN2012DN02746A (pt) * | 2009-10-13 | 2015-09-18 | Bell Helicopter Textron Inc | |
| US8585451B2 (en) * | 2010-08-05 | 2013-11-19 | Eric Bleicken | Circumferential ring propulsors and control assemblies for manned or unmanned underwater vehicles |
| CA2806330C (en) * | 2010-08-13 | 2017-01-03 | Hexcel Corporation | Machinable composite material |
| US9187636B2 (en) * | 2012-08-26 | 2015-11-17 | Hexcel Corporation | Composite material with polyamide particle mixtures |
-
2011
- 2011-07-23 CA CA2806330A patent/CA2806330C/en not_active Expired - Fee Related
- 2011-07-23 JP JP2013524089A patent/JP6218323B2/ja not_active Expired - Fee Related
- 2011-07-23 WO PCT/US2011/045130 patent/WO2012021283A1/en not_active Ceased
- 2011-07-23 AU AU2011289779A patent/AU2011289779B2/en not_active Ceased
- 2011-07-23 EP EP11748516.9A patent/EP2603380A1/en not_active Withdrawn
- 2011-07-23 CN CN201180039148.0A patent/CN103068568B/zh not_active Expired - Fee Related
- 2011-07-23 BR BR112013003189A patent/BR112013003189B1/pt not_active IP Right Cessation
- 2011-08-31 US US13/222,261 patent/US8864070B2/en active Active
Also Published As
| Publication number | Publication date |
|---|---|
| EP2603380A1 (en) | 2013-06-19 |
| CA2806330A1 (en) | 2012-02-16 |
| CA2806330C (en) | 2017-01-03 |
| BR112013003189B1 (pt) | 2019-12-31 |
| CN103068568A (zh) | 2013-04-24 |
| AU2011289779A1 (en) | 2013-01-31 |
| AU2011289779B2 (en) | 2014-01-30 |
| US20120040169A1 (en) | 2012-02-16 |
| CN103068568B (zh) | 2015-08-12 |
| US8864070B2 (en) | 2014-10-21 |
| JP2013540608A (ja) | 2013-11-07 |
| WO2012021283A1 (en) | 2012-02-16 |
| JP6218323B2 (ja) | 2017-10-25 |
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