ITTO20040198A1 - Procedimento per la fabbricazione di una preforma secca di rinforzo per un elemento strutturale composito di un aeromobile - Google Patents
Procedimento per la fabbricazione di una preforma secca di rinforzo per un elemento strutturale composito di un aeromobileInfo
- Publication number
- ITTO20040198A1 ITTO20040198A1 IT000198A ITTO20040198A ITTO20040198A1 IT TO20040198 A1 ITTO20040198 A1 IT TO20040198A1 IT 000198 A IT000198 A IT 000198A IT TO20040198 A ITTO20040198 A IT TO20040198A IT TO20040198 A1 ITTO20040198 A1 IT TO20040198A1
- Authority
- IT
- Italy
- Prior art keywords
- aircraft
- procedure
- manufacture
- structural element
- composite structural
- 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
- B29C70/40—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
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29B—PREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
- B29B11/00—Making preforms
- B29B11/14—Making preforms characterised by structure or composition
- B29B11/16—Making preforms characterised by structure or composition comprising fillers or reinforcement
-
- 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
- B32B1/00—Layered products having a general shape other than plane
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/02—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
- B32B5/024—Woven fabric
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/02—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
- B32B5/06—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer characterised by a fibrous or filamentary layer mechanically connected, e.g. by needling to another layer, e.g. of fibres, of paper
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/02—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
- B32B5/08—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 the fibres or filaments of a layer being of different substances, e.g. conjugate fibres, mixture of different 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
- 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
-
- D—TEXTILES; PAPER
- D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
- D04H—MAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARY MATERIAL; FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS, NON-WOVEN FABRICS; COTTON-WOOL; WADDING ; NON-WOVEN FABRICS FROM STAPLE FIBRES, FILAMENTS OR YARNS, BONDED WITH AT LEAST ONE WEB-LIKE MATERIAL DURING THEIR CONSOLIDATION
- D04H13/00—Other non-woven fabrics
-
- D—TEXTILES; PAPER
- D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
- D04H—MAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARY MATERIAL; FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS, NON-WOVEN FABRICS; COTTON-WOOL; WADDING ; NON-WOVEN FABRICS FROM STAPLE FIBRES, FILAMENTS OR YARNS, BONDED WITH AT LEAST ONE WEB-LIKE MATERIAL DURING THEIR CONSOLIDATION
- D04H3/00—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length
- D04H3/002—Inorganic yarns or filaments
-
- D—TEXTILES; PAPER
- D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
- D04H—MAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARY MATERIAL; FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS, NON-WOVEN FABRICS; COTTON-WOOL; WADDING ; NON-WOVEN FABRICS FROM STAPLE FIBRES, FILAMENTS OR YARNS, BONDED WITH AT LEAST ONE WEB-LIKE MATERIAL DURING THEIR CONSOLIDATION
- D04H3/00—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length
- D04H3/002—Inorganic yarns or filaments
- D04H3/004—Glass yarns or filaments
-
- D—TEXTILES; PAPER
- D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
- D04H—MAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARY MATERIAL; FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS, NON-WOVEN FABRICS; COTTON-WOOL; WADDING ; NON-WOVEN FABRICS FROM STAPLE FIBRES, FILAMENTS OR YARNS, BONDED WITH AT LEAST ONE WEB-LIKE MATERIAL DURING THEIR CONSOLIDATION
- D04H3/00—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length
- D04H3/02—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of forming fleeces or layers, e.g. reorientation of yarns or filaments
- D04H3/07—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of forming fleeces or layers, e.g. reorientation of yarns or filaments otherwise than in a plane, e.g. in a tubular way
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/001—Profiled members, e.g. beams, sections
- B29L2031/003—Profiled members, e.g. beams, sections having a profiled transverse cross-section
- B29L2031/005—Profiled members, e.g. beams, sections having a profiled transverse cross-section for making window frames
-
- 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
- B32B2605/00—Vehicles
- B32B2605/18—Aircraft
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
IT000198A ITTO20040198A1 (it) | 2004-03-23 | 2004-03-23 | Procedimento per la fabbricazione di una preforma secca di rinforzo per un elemento strutturale composito di un aeromobile |
EP05102235A EP1584462A3 (en) | 2004-03-23 | 2005-03-21 | A method for the manufacture of a dry reinforcing preform for a composite structural member of an aircraft |
US11/084,960 US7503273B2 (en) | 2004-03-23 | 2005-03-21 | Method for the manufacture of a dry reinforcing preform for a composite structural member of an aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
IT000198A ITTO20040198A1 (it) | 2004-03-23 | 2004-03-23 | Procedimento per la fabbricazione di una preforma secca di rinforzo per un elemento strutturale composito di un aeromobile |
Publications (1)
Publication Number | Publication Date |
---|---|
ITTO20040198A1 true ITTO20040198A1 (it) | 2004-06-23 |
Family
ID=34897826
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IT000198A ITTO20040198A1 (it) | 2004-03-23 | 2004-03-23 | Procedimento per la fabbricazione di una preforma secca di rinforzo per un elemento strutturale composito di un aeromobile |
Country Status (3)
Country | Link |
---|---|
US (1) | US7503273B2 (it) |
EP (1) | EP1584462A3 (it) |
IT (1) | ITTO20040198A1 (it) |
Families Citing this family (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20070125032A1 (en) * | 2005-11-22 | 2007-06-07 | Ramiro Guerrero | Structural assembly and a method for its manufacture |
FR2900420B1 (fr) * | 2006-04-26 | 2008-07-25 | Snecma Propulsion Solide Sa | Procede de realisation de strate fibreuse pour la fabrication d'une preforme de piece composite |
EP1977882B1 (de) * | 2007-04-02 | 2020-06-24 | Cetex Institut gGmbH | Verfahren und Vorrichtung zur partiellen Verstärkung einer Warenbahn |
DE102007032904B3 (de) * | 2007-07-14 | 2008-11-27 | Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. | Verfahren zur Strukturfixierung von textilen Flächengebilden für Hochleistungs-Faserverbundbauteile und ein nach diesem Verfahren hergestelltes textiles Flächengebilde |
ITTO20070557A1 (it) | 2007-07-27 | 2009-01-28 | Alenia Aeronautica Spa | Procedimento di fabbricazione di un elemento curvo in materiale composito |
ITTO20070796A1 (it) | 2007-11-08 | 2009-05-09 | Alenia Aeronautica Spa | Attrezzatura per infusione di resina in una preforma in stampo chiuso. |
WO2010056164A1 (en) * | 2008-11-13 | 2010-05-20 | Saab Ab | Method of forming a composite article |
BR112012021917B1 (pt) * | 2010-03-18 | 2020-09-29 | Toho Tenax Europe Gmbh | Tecido não plissado multiaxial |
FR2957845B1 (fr) * | 2010-03-26 | 2012-08-10 | Messier Dowty Sa | Procede de fabrication d'un bras en materiau composite comportant un palier transversal destine a recevoir un axe fixe ou rotatif |
DE102010015199B9 (de) | 2010-04-16 | 2013-08-01 | Compositence Gmbh | Faserführungsvorrichtung und Vorrichtung zum Aufbau eines dreidimensionalen Vorformlings |
DE102010050079A1 (de) | 2010-10-29 | 2012-05-03 | Premium Aerotec Gmbh | Partiell fixiertes textiles Halbzeug |
DE102011100640A1 (de) | 2011-05-05 | 2012-11-08 | Compositence Gmbh | Verfahren und Vorrichtung zum Herstellen von Fasergelegen und Bauteilvorformlingen aus Fasern |
DE102011075374B9 (de) * | 2011-05-05 | 2020-03-19 | J. Finck Gmbh & Co. Kg | Wärmedämmstoffmatte, insbesondere für den Gebäudebau |
MX2014011486A (es) * | 2012-04-02 | 2015-04-13 | William Anton Trondl | Metodo para hacer un objeto tridimensional de material compuesto. |
DE102012007439A1 (de) | 2012-04-13 | 2013-10-17 | Compositence Gmbh | Legekopf und Vorrichtung und Verfahren zum Aufbau eines dreidimensionalen Vorformlings für ein Bauteil aus einem Faserverbundwerkstoff |
EP2938478B1 (de) | 2012-12-28 | 2020-08-19 | Compositence GmbH | Verfahren und vorrichtung zum herstellen von dreidimensionalen fasergelegen und bauteilvorformlingen aus fasern in zwei stufen |
DE102014201278A1 (de) * | 2014-01-24 | 2015-07-30 | Bayerische Motoren Werke Aktiengesellschaft | Vorrichtung zum Fügen einer Verstärkungslage mit einer Trägerlage |
US9309613B1 (en) * | 2014-11-03 | 2016-04-12 | Goodrich Corporation | System and method to fabricate helical fabric |
EP3399085B1 (en) | 2017-05-05 | 2022-07-13 | Ratier-Figeac SAS | Multi-layer braided article, a method of making same, an aircraft component comprising the braided article and a method of making a propeller blade |
US10787757B2 (en) * | 2018-08-27 | 2020-09-29 | Arevo, Inc. | Tailored fiber placement utilizing functional thread |
FR3109551B1 (fr) | 2020-04-28 | 2022-04-29 | Inst De Rech Tech Jules Verne | Procédé de fabrication d’une préforme tridimensionnelle |
CN112831906B (zh) * | 2021-01-07 | 2022-04-12 | 泰山玻璃纤维有限公司 | 连续玻璃纤维缝编毡生产装置及生产方法 |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4867086A (en) | 1988-07-21 | 1989-09-19 | Xerkon, Inc. | Method of making a dry fiber form and composites prepared therefrom |
FR2687174B1 (fr) * | 1992-02-11 | 1995-09-22 | Aerospatiale | Procede pour la realisation d'une armature de fibres pour piece de matiere composite a parois non coplanaires, et piece composite comportant une telle armature. |
FR2687173B1 (fr) * | 1992-02-11 | 1995-09-08 | Aerospatiale | Procede pour la realisation d'une armature de fibres pour piece de matiere composite, et piece composite comportant une telle armature. |
FR2718758B1 (fr) * | 1994-04-18 | 1996-06-14 | Aerospatiale | Procédé et machine pour la réalisation d'une armature pour une pièce de matière composite. |
FR2779749B1 (fr) * | 1998-06-10 | 2000-08-11 | Aerospatiale | Armature fibreuse pour piece de matiere composite, ainsi que procede et dispositif pour sa realisation |
US6645333B2 (en) * | 2001-04-06 | 2003-11-11 | Ebert Composites Corporation | Method of inserting z-axis reinforcing fibers into a composite laminate |
-
2004
- 2004-03-23 IT IT000198A patent/ITTO20040198A1/it unknown
-
2005
- 2005-03-21 US US11/084,960 patent/US7503273B2/en active Active
- 2005-03-21 EP EP05102235A patent/EP1584462A3/en not_active Withdrawn
Also Published As
Publication number | Publication date |
---|---|
EP1584462A3 (en) | 2009-01-07 |
US7503273B2 (en) | 2009-03-17 |
EP1584462A2 (en) | 2005-10-12 |
US20050268832A1 (en) | 2005-12-08 |
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