BR112014026869A2 - método de formação de artigo compósito e artigo compósito. - Google Patents
método de formação de artigo compósito e artigo compósito.Info
- Publication number
- BR112014026869A2 BR112014026869A2 BR112014026869A BR112014026869A BR112014026869A2 BR 112014026869 A2 BR112014026869 A2 BR 112014026869A2 BR 112014026869 A BR112014026869 A BR 112014026869A BR 112014026869 A BR112014026869 A BR 112014026869A BR 112014026869 A2 BR112014026869 A2 BR 112014026869A2
- Authority
- BR
- Brazil
- Prior art keywords
- composite article
- forming
- forming composite
- article
- composite
- Prior art date
Links
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
- B29C70/04—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
- B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
- B29C70/302—Details of the edges of fibre composites, e.g. edge finishing or means to avoid delamination
-
- 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
- B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
-
- 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
- B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
- B32B37/14—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/02—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
- B32B5/12—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer characterised by the relative arrangement of fibres or filaments of different layers, e.g. the fibres or filaments being parallel or perpendicular to each other
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
- B32B2260/04—Impregnation, embedding, or binder material
- B32B2260/046—Synthetic resin
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2305/00—Condition, form or state of the layers or laminate
- B32B2305/08—Reinforcements
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2305/00—Condition, form or state of the layers or laminate
- B32B2305/10—Fibres of continuous length
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2220/00—Application
- F05D2220/30—Application in turbines
- F05D2220/32—Application in turbines in gas turbines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2230/00—Manufacture
- F05D2230/30—Manufacture with deposition of material
- F05D2230/31—Layer deposition
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2300/00—Materials; Properties thereof
- F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
- F05D2300/603—Composites; e.g. fibre-reinforced
-
- 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
- Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
- Y10T156/10—Methods of surface bonding and/or assembly therefor
- Y10T156/1002—Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina
- Y10T156/1007—Running or continuous length work
- Y10T156/1023—Surface deformation only [e.g., embossing]
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24058—Structurally defined web or sheet [e.g., overall dimension, etc.] including grain, strips, or filamentary elements in respective layers or components in angular relation
- Y10T428/24124—Fibers
Applications Claiming Priority (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US201261639900P | 2012-04-28 | 2012-04-28 | |
US61/639,900 | 2012-04-28 | ||
US13/687,117 US10654246B2 (en) | 2012-04-28 | 2012-11-28 | Composite article and methods therefor |
US13/687,117 | 2012-11-28 | ||
PCT/US2013/037095 WO2013162989A1 (en) | 2012-04-28 | 2013-04-18 | Composite article and methods therefor |
Publications (3)
Publication Number | Publication Date |
---|---|
BR112014026869A2 true BR112014026869A2 (pt) | 2017-06-27 |
BR112014026869B1 BR112014026869B1 (pt) | 2021-05-11 |
BR112014026869B8 BR112014026869B8 (pt) | 2021-05-25 |
Family
ID=48225132
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR112014026869-0A BR112014026869B1 (pt) | 2012-04-28 | 2013-04-18 | Método de formação de um artigo compósito e artigo compósito |
Country Status (7)
Country | Link |
---|---|
US (1) | US10654246B2 (pt) |
EP (1) | EP2841256B1 (pt) |
JP (1) | JP5970606B2 (pt) |
CN (1) | CN104254439B (pt) |
BR (1) | BR112014026869B1 (pt) |
CA (1) | CA2870731C (pt) |
WO (1) | WO2013162989A1 (pt) |
Families Citing this family (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9327470B1 (en) * | 2012-12-05 | 2016-05-03 | The Boeing Company | Variable-radius laminated radius filler and system and method for manufacturing same |
WO2015187867A1 (en) | 2014-06-04 | 2015-12-10 | Bright Lite Structures Llc | Multicomponent polymer resin, methods for applying the same, and composite laminate structure including the same |
US9442514B1 (en) * | 2014-07-23 | 2016-09-13 | Google Inc. | Graphite layer between carbon layers |
EP3277868B1 (en) | 2015-04-03 | 2021-11-24 | Bright Lite Structures LLC | Apparatus for controllably cutting fibers and related methods |
US9745849B2 (en) * | 2015-06-26 | 2017-08-29 | General Electric Company | Methods for treating field operated components |
WO2017109403A1 (fr) * | 2015-12-22 | 2017-06-29 | Safran Aircraft Engines | Carter allégé en matériau composite et son procédé de fabrication |
US10401030B2 (en) | 2016-07-12 | 2019-09-03 | General Electric Company | Axisymmetric components and methods for forming axisymmetric components |
US11242866B2 (en) | 2018-08-01 | 2022-02-08 | General Electric Company | Casing having a non-axisymmetric composite wall |
US11209166B2 (en) | 2018-12-05 | 2021-12-28 | General Electric Company | Combustor assembly for a turbine engine |
US11047574B2 (en) | 2018-12-05 | 2021-06-29 | General Electric Company | Combustor assembly for a turbine engine |
US10919256B2 (en) * | 2019-05-09 | 2021-02-16 | The Boeing Company | Composite structure having a variable gage and methods for forming a composite structure having a variable gage |
US10913215B2 (en) * | 2019-05-09 | 2021-02-09 | The Boeing Company | Composite structure having a variable gage and methods for forming a composite structure having a variable gage |
US10919260B2 (en) * | 2019-05-09 | 2021-02-16 | The Boeing Company | Composite structure having a variable gage and methods for forming a composite structure having a variable gage |
US11376812B2 (en) | 2020-02-11 | 2022-07-05 | Helicoid Industries Inc. | Shock and impact resistant structures |
CN113147053B (zh) * | 2021-05-21 | 2023-01-24 | 江苏恒神股份有限公司 | 加筋结构件端框及其成型方法 |
US11852297B2 (en) | 2021-06-01 | 2023-12-26 | Helicoid Industries Inc. | Containers and methods for protecting pressure vessels |
WO2022256022A1 (en) | 2021-06-01 | 2022-12-08 | Helicoid Industries Inc. | Containers and methods for protecting pressure vessels |
US11927113B2 (en) | 2021-08-06 | 2024-03-12 | Rtx Corporation | Composite fan blade airfoil, methods of manufacture thereof and articles comprising the same |
US11952103B2 (en) | 2022-06-27 | 2024-04-09 | Helicoid Industries Inc. | High impact-resistant, reinforced fiber for leading edge protection of aerodynamic structures |
Family Cites Families (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4051289A (en) * | 1976-04-12 | 1977-09-27 | General Electric Company | Composite airfoil construction |
DE2622163C3 (de) * | 1976-05-19 | 1983-05-26 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Profilträger aus faserverstärktem Werkstoff |
JPS60224530A (ja) | 1984-04-23 | 1985-11-08 | Mazda Motor Corp | 強化繊維を含有する複合樹脂シ−ト |
ZA864464B (en) | 1985-07-05 | 1987-03-25 | Gen Electric | Brazed composite compact implements |
FR2718074B1 (fr) | 1994-04-01 | 1996-04-26 | Snecma | Procédé de fabrication d'une pièce complexe en matériau composite. |
US5939007A (en) * | 1994-08-31 | 1999-08-17 | Sikorsky Aircraft Corporation | Method for manufacture of a fiber reinforced composite spar for rotary wing aircraft |
US5866272A (en) * | 1996-01-11 | 1999-02-02 | The Boeing Company | Titanium-polymer hybrid laminates |
US7229513B2 (en) | 2003-10-31 | 2007-06-12 | The Boeing Company | Method for an integral composite forward flange in a composite |
US7531058B2 (en) * | 2005-02-24 | 2009-05-12 | The Boeing Company | Reinforced rampdown for composite structural member and method for same |
JP4736906B2 (ja) | 2006-03-31 | 2011-07-27 | 株式会社豊田自動織機 | 複合材成形体及びその製造方法 |
DE102006024329A1 (de) | 2006-05-24 | 2007-11-29 | Bayerische Motoren Werke Ag | Flanschbauteil in Verbundbauweise sowie Verfahren zur Herstellung eines Flanschbauteiles |
US8475895B2 (en) * | 2006-11-21 | 2013-07-02 | General Electric Company | Articles comprising composite structures having mounting flanges |
GB2470087B (en) | 2007-06-07 | 2010-12-29 | Gkn Aerospace Services Ltd | Mandrel for use in a method of making composite flange |
US8181345B2 (en) * | 2007-07-20 | 2012-05-22 | Airbus Operations Sas | Method for optimizing the mass of a composite panel |
FR2926118B1 (fr) | 2008-01-04 | 2010-01-29 | Snecma | Bride en composite avec partie d'usinage. |
US8152948B2 (en) * | 2008-01-09 | 2012-04-10 | The Boeing Company | Contoured composite parts |
US8932423B2 (en) | 2008-04-17 | 2015-01-13 | The Boeing Company | Method for producing contoured composite structures and structures produced thereby |
DE102008028337B4 (de) | 2008-06-13 | 2013-09-26 | Ellergon Antriebstechnik Gmbh | Verfahren zur Herstellung einer Hohlwelle mit mindestens einem integralen Flansch aus Faserverbundwerkstoff |
US8449260B2 (en) * | 2009-10-30 | 2013-05-28 | General Electric Company | Composite load-bearing rotating ring and process therefor |
CA2799105A1 (en) * | 2010-05-11 | 2011-11-17 | Saab Ab | A composite article comprising particles and a method of forming a composite article |
US9248587B2 (en) * | 2012-07-05 | 2016-02-02 | General Electric Company | Apparatus for manufacturing a flanged composite component and methods of manufacturing the same |
-
2012
- 2012-11-28 US US13/687,117 patent/US10654246B2/en active Active
-
2013
- 2013-04-18 CN CN201380022445.3A patent/CN104254439B/zh active Active
- 2013-04-18 JP JP2015509031A patent/JP5970606B2/ja active Active
- 2013-04-18 EP EP13719341.3A patent/EP2841256B1/en active Active
- 2013-04-18 BR BR112014026869-0A patent/BR112014026869B1/pt active IP Right Grant
- 2013-04-18 WO PCT/US2013/037095 patent/WO2013162989A1/en active Application Filing
- 2013-04-18 CA CA2870731A patent/CA2870731C/en active Active
Also Published As
Publication number | Publication date |
---|---|
BR112014026869B1 (pt) | 2021-05-11 |
JP5970606B2 (ja) | 2016-08-17 |
WO2013162989A1 (en) | 2013-10-31 |
BR112014026869B8 (pt) | 2021-05-25 |
EP2841256A1 (en) | 2015-03-04 |
US20150314556A1 (en) | 2015-11-05 |
WO2013162989A8 (en) | 2014-10-23 |
EP2841256B1 (en) | 2020-07-29 |
CA2870731C (en) | 2019-11-26 |
CN104254439A (zh) | 2014-12-31 |
US10654246B2 (en) | 2020-05-19 |
CN104254439B (zh) | 2018-02-09 |
CA2870731A1 (en) | 2013-10-31 |
JP2015529575A (ja) | 2015-10-08 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
B06F | Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette] | ||
B06U | Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette] | ||
B06A | Patent application procedure suspended [chapter 6.1 patent gazette] | ||
B09A | Decision: intention to grant [chapter 9.1 patent gazette] | ||
B16A | Patent or certificate of addition of invention granted [chapter 16.1 patent gazette] |
Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 18/04/2013, OBSERVADAS AS CONDICOES LEGAIS. |
|
B16C | Correction of notification of the grant [chapter 16.3 patent gazette] |
Free format text: REFERENTE AO DESPACHO 16.1 PUBLICADO NA RPI 2627, QUANTO AO NOME DE UM DOS INVENTORES |