BRPI0920231A2 - método de fabricar um painel de geometria complexa em material compósito pré-impregnado - Google Patents
método de fabricar um painel de geometria complexa em material compósito pré-impregnadoInfo
- Publication number
- BRPI0920231A2 BRPI0920231A2 BRPI0920231A BRPI0920231A BRPI0920231A2 BR PI0920231 A2 BRPI0920231 A2 BR PI0920231A2 BR PI0920231 A BRPI0920231 A BR PI0920231A BR PI0920231 A BRPI0920231 A BR PI0920231A BR PI0920231 A2 BRPI0920231 A2 BR PI0920231A2
- Authority
- BR
- Brazil
- Prior art keywords
- fabricating
- composite material
- complex geometry
- prepreg composite
- geometry panel
- Prior art date
Links
- 239000002131 composite material Substances 0.000 title 1
- 238000004519 manufacturing process Methods 0.000 title 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
- B29D99/00—Subject matter not provided for in other groups of this subclass
- B29D99/001—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings
- B29D99/0014—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings provided with ridges or ribs, e.g. joined ribs
-
- 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
- B29C70/34—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 and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation
- B29C70/345—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 and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation using matched moulds
-
- 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
- B29C70/304—In-plane lamination by juxtaposing or interleaving of plies, e.g. scarf joining
-
- 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
-
- 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
- B29C70/461—Rigid movable compressing mould parts acting independently from opening or closing action of the main mould
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
- B32B3/26—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer
- B32B3/30—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer characterised by a layer formed with recesses or projections, e.g. hollows, grooves, protuberances, ribs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/22—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
- B32B5/24—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
- B32B5/26—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
- B32B7/03—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers with respect to the orientation of features
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
- B32B7/04—Interconnection of layers
- B32B7/08—Interconnection of layers by mechanical means
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
- B32B7/04—Interconnection of layers
- B32B7/12—Interconnection of layers using interposed adhesives or interposed materials with bonding properties
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
- B32B2260/02—Composition of the impregnated, bonded or embedded layer
- B32B2260/021—Fibrous or filamentary layer
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- 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
- B32B2307/00—Properties of the layers or laminate
- B32B2307/50—Properties of the layers or laminate having particular mechanical properties
- B32B2307/514—Oriented
-
- 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
- B32B2607/00—Walls, panels
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Architecture (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Moulding By Coating Moulds (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ES200803085A ES2338084B1 (es) | 2008-10-30 | 2008-10-30 | Metodo de fabricacion de un panel de geometria compleja en material compuesto preimpregnado. |
PCT/ES2009/070466 WO2010049566A1 (es) | 2008-10-30 | 2009-10-28 | Método de fabricación de un panel de geometría compleja en material compuesto preimpregnado |
Publications (1)
Publication Number | Publication Date |
---|---|
BRPI0920231A2 true BRPI0920231A2 (pt) | 2018-06-19 |
Family
ID=42105786
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BRPI0920231A BRPI0920231A2 (pt) | 2008-10-30 | 2009-10-28 | método de fabricar um painel de geometria complexa em material compósito pré-impregnado |
Country Status (7)
Country | Link |
---|---|
US (1) | US20100108246A1 (pt) |
EP (1) | EP2357075B1 (pt) |
CN (1) | CN102282006B (pt) |
BR (1) | BRPI0920231A2 (pt) |
CA (1) | CA2741486C (pt) |
ES (1) | ES2338084B1 (pt) |
WO (1) | WO2010049566A1 (pt) |
Families Citing this family (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8747098B1 (en) | 2008-03-24 | 2014-06-10 | Ebert Composites Corporation | Thermoplastic pultrusion die system and method |
US8123510B1 (en) * | 2008-03-24 | 2012-02-28 | Ebert Composite Corporation | Thermoplastic pultrusion die system and method |
US10723047B2 (en) | 2011-09-08 | 2020-07-28 | Tovi Llc | Hockey stick |
US8608597B2 (en) | 2011-09-08 | 2013-12-17 | Tzvi Avnery | Hockey stick |
WO2013078647A1 (en) * | 2011-11-30 | 2013-06-06 | Airbus S.A.S. | Panel,component for an airplane airfoil comprising the panel,and method for producing the panel |
GB201120994D0 (en) * | 2011-12-07 | 2012-01-18 | Airbus Uk Ltd | Integral stiffener |
ES2413189B1 (es) * | 2012-01-10 | 2015-02-11 | Manuel Torres Martínez | Instalacion para fabricar larguerillos de fibra para estructuras aeroespaciales |
DE102012210043A1 (de) * | 2012-06-14 | 2013-12-19 | Airbus Operations Gmbh | Verfahren und Vorrichtung zur Herstellung einer Leichtbaustruktur sowie Leichtbaustruktur |
CN105984153A (zh) * | 2015-02-13 | 2016-10-05 | 全耐塑料公司 | 预成型预浸渍复合材料片时的铺设方法 |
GB201504498D0 (en) * | 2015-03-17 | 2015-04-29 | Penso Holdings Ltd | Method and apparatus for production of carbon fibre components |
US9969419B2 (en) * | 2016-04-01 | 2018-05-15 | Tk Holdings Inc. | Preimpregnated carbon fiber steering wheel |
FI127614B (en) * | 2017-04-07 | 2018-10-15 | Patria Aerostructures Oy | COMPOSITE ELEMENT AND METHOD FOR MANUFACTURING IT |
FR3071765B1 (fr) * | 2017-10-03 | 2020-11-20 | Safran Ceram | Realisation en materiau composite d'une structure a lobes de melangeur de flux |
CN112004660B (zh) * | 2018-10-05 | 2023-06-06 | 福井县 | 薄层带自动层叠方法和装置 |
CN109551659B (zh) * | 2018-12-19 | 2021-03-23 | 航天特种材料及工艺技术研究所 | 一种复合浸渍工装及其应用 |
WO2021042059A1 (en) * | 2019-08-30 | 2021-03-04 | Arris Composites Inc. | Compression molding method and compression mold |
Family Cites Families (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4525228A (en) * | 1982-08-13 | 1985-06-25 | United Kingdom Atomic Energy Authority | Method of winding on foam mandrel |
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 |
JPS6143540A (ja) * | 1984-08-06 | 1986-03-03 | Mazda Motor Corp | Frp部品の製造方法 |
US5747179A (en) * | 1991-04-05 | 1998-05-05 | The Boeing Company | Pack for inductively consolidating an organic matrix composite |
GB9413417D0 (en) * | 1994-07-04 | 1994-08-24 | Ford Roger A | Improved composite materials and method for making them |
US6692681B1 (en) * | 1997-01-29 | 2004-02-17 | Raytheon Aircraft Company | Method and apparatus for manufacturing composite structures |
US6406580B1 (en) * | 2000-06-09 | 2002-06-18 | Lockheed Martin Corporation | Method for manufacturing composite parts |
US6553734B1 (en) * | 2000-08-24 | 2003-04-29 | Lockheed Martin Corporation | Composite structural panel with undulated body |
US6454893B1 (en) * | 2000-08-24 | 2002-09-24 | Lockheed Martin Corporation | Method of shaping continuous fiber lamina to an undulated surface by cutting individual fibers |
US6649006B2 (en) * | 2001-10-09 | 2003-11-18 | Lockheed Martin Corporation | Method of making a waffle stiffener |
DE10210517B3 (de) * | 2002-03-09 | 2004-01-29 | Airbus Deutschland Gmbh | Verfahren zur Herstellung eines Bauteiles in Faserverbundbauweise |
EP1547756A1 (en) * | 2003-12-24 | 2005-06-29 | Airbus UK Limited | Method of manufacturing aircraft components |
ES2315580T3 (es) * | 2004-02-13 | 2009-04-01 | Saab Ab | Procedimiento para la fabricacion de un articulo de material compuesto. |
US7134629B2 (en) * | 2004-04-06 | 2006-11-14 | The Boeing Company | Structural panels for use in aircraft fuselages and other structures |
US7410352B2 (en) * | 2005-04-13 | 2008-08-12 | The Boeing Company | Multi-ring system for fuselage barrel formation |
US7824171B2 (en) * | 2005-10-31 | 2010-11-02 | The Boeing Company | Corner-consolidating inflatable apparatus and method for manufacturing composite structures |
US7867352B2 (en) * | 2006-02-13 | 2011-01-11 | The Boeing Company | Composite material placement method and system |
DE102006031335B4 (de) * | 2006-07-06 | 2011-01-27 | Airbus Operations Gmbh | Verfahren zur Herstellung eines Faserverbundbauteils für die Luft- und Raumfahrt |
JP2008273176A (ja) * | 2007-04-03 | 2008-11-13 | Toray Ind Inc | 繊維強化プラスチックの製造方法 |
DE102008008386A1 (de) * | 2008-02-09 | 2009-08-13 | Airbus Deutschland Gmbh | Verfahren zur Herstellung eines FVW-Bauteils |
-
2008
- 2008-10-30 ES ES200803085A patent/ES2338084B1/es not_active Expired - Fee Related
-
2009
- 2009-01-08 US US12/318,792 patent/US20100108246A1/en not_active Abandoned
- 2009-10-28 EP EP09823120.2A patent/EP2357075B1/en not_active Not-in-force
- 2009-10-28 CN CN200980153362.1A patent/CN102282006B/zh not_active Expired - Fee Related
- 2009-10-28 BR BRPI0920231A patent/BRPI0920231A2/pt not_active IP Right Cessation
- 2009-10-28 CA CA2741486A patent/CA2741486C/en not_active Expired - Fee Related
- 2009-10-28 WO PCT/ES2009/070466 patent/WO2010049566A1/es active Application Filing
Also Published As
Publication number | Publication date |
---|---|
CN102282006B (zh) | 2015-02-18 |
EP2357075B1 (en) | 2015-07-08 |
WO2010049566A1 (es) | 2010-05-06 |
CN102282006A (zh) | 2011-12-14 |
CA2741486A1 (en) | 2010-05-06 |
US20100108246A1 (en) | 2010-05-06 |
ES2338084B1 (es) | 2011-03-14 |
EP2357075A4 (en) | 2012-08-15 |
ES2338084A1 (es) | 2010-05-03 |
EP2357075A1 (en) | 2011-08-17 |
CA2741486C (en) | 2016-11-15 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
BRPI0920231A2 (pt) | método de fabricar um painel de geometria complexa em material compósito pré-impregnado | |
HRP20181609T1 (hr) | Postupak za proizvodnju ploče i preprega | |
EP2691199A4 (en) | PREPREG, FIBER-REINFORCED COMPOSITE MATERIAL AND MANUFACTURING METHOD FOR THE FIBER-REINFORCED COMPOSITE MATERIAL | |
BRPI0922077A2 (pt) | processo de fabricação de uma peça de forma complexa de material compósito. | |
GB0820800D0 (en) | Method of designing a composite laminate | |
PT2285670T (pt) | Método para produzir estruturas compósitas com contornos e estruturas produzidas pelo mesmo | |
PL2583815T3 (pl) | Stabilizator z kompozytu z tworzywa sztucznego wzmocnionego włóknami i metoda jego wytwarzania | |
EP2794272A4 (en) | PREPREG, FIBER REINFORCED COMPOSITE MATERIAL, AND METHOD FOR MANUFACTURING FIBER REINFORCED COMPOSITE MATERIAL | |
IL195474A (en) | A method for making the carbon fiber composite parts | |
EP2612889A4 (en) | RESIN COMPOSITE MATERIAL AND METHOD FOR PRODUCING A RESIN COMPOSITE MATERIAL | |
HK1133232A1 (en) | Method for fabricating curved thermoplastic composite parts | |
EP2762520A4 (en) | FIBER REINFORCED RESIN COMPOSITE MATERIAL AND MANUFACTURING METHOD THEREFOR | |
EP2190933A4 (en) | AGGREGATE CHUCKS FOR THE PRODUCTION OF COMPOSITE PARTS AND PROCESSES FOR PRODUCING COMPOSITE PARTS | |
BR112012003657A2 (pt) | método de moldar peças compósitas complexas usando laminado de fibra contínua multidirecional pré-plissado | |
TWI561562B (en) | Fiber reinforced composite material and method for producing fiber reinforced composite material | |
EP2554581A4 (en) | PRE-IMPREGNATED, FIBER REINFORCED COMPOSITE MATERIAL, AND PROCESS FOR PRODUCING THE PRE-IMPREGNATED | |
EP2479014A4 (en) | Jig having thick regions in the cross-section thereof and which is for producing composite material structures | |
ZA201309467B (en) | Meyhod for locally strengthening a composite panel with fibrous reinforcement and panel obtained using such a method | |
EP2380924A4 (en) | COMPOSITE FILM AND METHOD FOR THE PRODUCTION THEREOF | |
BRPI0921988A2 (pt) | método de fabricação e aparelho de fabricação de material composto reforçado com fibra | |
EP2690128A4 (en) | PRE-IMPREGNATED AND FIBER REINFORCED COMPOSITE MATERIAL | |
EP2296858B8 (en) | Method for recycling composite material | |
EP2327469A4 (en) | Semi-transparent composite film and method for its production | |
PL2125947T3 (pl) | Materiały kompozytowe i sposób ich wytwarzania | |
EP2301998A4 (en) | METHOD FOR PRODUCING EVOH-COMPOSITE MATERIAL |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
B08F | Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette] | ||
B08K | Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette] |
Free format text: EM VIRTUDE DO ARQUIVAMENTO PUBLICADO NA RPI 2477 DE 26-06-2018 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDO O ARQUIVAMENTO DO PEDIDO DE PATENTE, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013. |