RU2008106981A - Способ армирования материала основы для композитных конструкций, а также композитные конструкции - Google Patents
Способ армирования материала основы для композитных конструкций, а также композитные конструкции Download PDFInfo
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- RU2008106981A RU2008106981A RU2008106981/12A RU2008106981A RU2008106981A RU 2008106981 A RU2008106981 A RU 2008106981A RU 2008106981/12 A RU2008106981/12 A RU 2008106981/12A RU 2008106981 A RU2008106981 A RU 2008106981A RU 2008106981 A RU2008106981 A RU 2008106981A
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- reinforcing
- composite structures
- base material
- reinforcing structure
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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
- B29C70/06—Fibrous reinforcements only
- B29C70/08—Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers
- B29C70/086—Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers and with one or more layers of pure plastics material, e.g. foam layers
-
- 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
- B29C70/06—Fibrous reinforcements only
- B29C70/08—Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers
-
- 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
- B29C70/06—Fibrous reinforcements only
- B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
- B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
- B29C70/24—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least three directions forming a three dimensional structure
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- 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
- Y10T156/1052—Methods of surface bonding and/or assembly therefor with cutting, punching, tearing or severing
- Y10T156/1062—Prior to assembly
-
- 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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49801—Shaping fiber or fibered material
-
- 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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49826—Assembling or joining
- Y10T29/49833—Punching, piercing or reaming part by surface of second part
-
- 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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49826—Assembling or joining
- Y10T29/49833—Punching, piercing or reaming part by surface of second part
- Y10T29/49835—Punching, piercing or reaming part by surface of second part with shaping
-
- 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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49826—Assembling or joining
- Y10T29/49838—Assembling or joining by stringing
-
- 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.]
- Y10T428/24479—Structurally defined web or sheet [e.g., overall dimension, etc.] including variation in thickness
- Y10T428/24612—Composite web or sheet
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Mechanical Engineering (AREA)
- Textile Engineering (AREA)
- Moulding By Coating Moulds (AREA)
- Laminated Bodies (AREA)
- Lining Or Joining Of Plastics Or The Like (AREA)
- Manufacture Of Alloys Or Alloy Compounds (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
- Woven Fabrics (AREA)
- Panels For Use In Building Construction (AREA)
- Molds, Cores, And Manufacturing Methods Thereof (AREA)
Abstract
1. Способ армирования композитных конструкций, отличающийся тем, что захватная система (1, 2) прокалывает с одной стороны конструкции материал (4) основы или материал (3, 4) основы с нанесенными на него покровными слоями, захватывает на противоположной стороне армирующую структуру (6) и во время обратного движения вводит ее в материал (4) основы или материал (3, 4) основы с нанесенными на него покровными слоями. ! 2. Способ армирования композитных конструкций по п.1, отличающийся тем, что армирующая структура (6) состоит из текстильных усилительных структур или прутковых элементов. ! 3. Способ армирования композитных конструкций по п.1, отличающийся тем, что покровные слои (3) выполнены из текстильных полуфабрикатов, основной слой (4) выполнен из полимерного, природного или структурированного материала основы и покровные слои, основной слой и армирующие элементы заделаны в полимерный матричный материал. ! 4. Способ по одному из пп.1-3, отличающийся тем, что армирующую структуру (6) после введения в материал (4) основы или в материал (3, 4) основы с нанесенными на него покровными слоями (3, 4) не разрезают на мерные длины. ! 5. Способ по одному из пп.1-3, отличающийся тем, что армирующую структуру (6) после введения в материал (4) основы или в материал (3, 4) основы с нанесенными на него покровными слоями разрезают на мерные длины. ! 6. Применение композитных конструкций, получаемых способом по пп.1-5, для изготовления космических, воздушных, морских, сухопутных и рельсовых транспортных средств, спортивных снарядов и строительных элементов для внутреннего, павильонного и наружного строительства.
Claims (6)
1. Способ армирования композитных конструкций, отличающийся тем, что захватная система (1, 2) прокалывает с одной стороны конструкции материал (4) основы или материал (3, 4) основы с нанесенными на него покровными слоями, захватывает на противоположной стороне армирующую структуру (6) и во время обратного движения вводит ее в материал (4) основы или материал (3, 4) основы с нанесенными на него покровными слоями.
2. Способ армирования композитных конструкций по п.1, отличающийся тем, что армирующая структура (6) состоит из текстильных усилительных структур или прутковых элементов.
3. Способ армирования композитных конструкций по п.1, отличающийся тем, что покровные слои (3) выполнены из текстильных полуфабрикатов, основной слой (4) выполнен из полимерного, природного или структурированного материала основы и покровные слои, основной слой и армирующие элементы заделаны в полимерный матричный материал.
4. Способ по одному из пп.1-3, отличающийся тем, что армирующую структуру (6) после введения в материал (4) основы или в материал (3, 4) основы с нанесенными на него покровными слоями (3, 4) не разрезают на мерные длины.
5. Способ по одному из пп.1-3, отличающийся тем, что армирующую структуру (6) после введения в материал (4) основы или в материал (3, 4) основы с нанесенными на него покровными слоями разрезают на мерные длины.
6. Применение композитных конструкций, получаемых способом по пп.1-5, для изготовления космических, воздушных, морских, сухопутных и рельсовых транспортных средств, спортивных снарядов и строительных элементов для внутреннего, павильонного и наружного строительства.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102005035681.8 | 2005-07-27 | ||
DE102005035681A DE102005035681A1 (de) | 2005-07-27 | 2005-07-27 | Fertigungsverfahren zur Armierung von Kernmaterialien für Kernverbunde sowie von Kernverbund-Strukturen |
Publications (2)
Publication Number | Publication Date |
---|---|
RU2008106981A true RU2008106981A (ru) | 2009-09-10 |
RU2419543C2 RU2419543C2 (ru) | 2011-05-27 |
Family
ID=36609036
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU2008106981/12A RU2419543C2 (ru) | 2005-07-27 | 2006-04-05 | Способ армирования материала основы для композитных конструкций |
Country Status (20)
Country | Link |
---|---|
US (1) | US20080226876A1 (ru) |
EP (1) | EP1907193B8 (ru) |
JP (1) | JP4751448B2 (ru) |
KR (1) | KR101319703B1 (ru) |
CN (1) | CN101198459B (ru) |
AT (1) | ATE500049T1 (ru) |
AU (1) | AU2006274270B2 (ru) |
BR (1) | BRPI0613882A2 (ru) |
CA (1) | CA2616655C (ru) |
DE (2) | DE102005035681A1 (ru) |
DK (1) | DK1907193T3 (ru) |
ES (1) | ES2361617T3 (ru) |
HK (1) | HK1120768A1 (ru) |
IL (1) | IL186761A (ru) |
NZ (1) | NZ563572A (ru) |
PL (1) | PL1907193T3 (ru) |
RU (1) | RU2419543C2 (ru) |
TW (1) | TWI388429B (ru) |
WO (1) | WO2007012353A1 (ru) |
ZA (1) | ZA200800782B (ru) |
Families Citing this family (27)
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US7861969B2 (en) | 2007-05-24 | 2011-01-04 | The Boeing Company | Shaped composite stringers and methods of making |
DE102007033120A1 (de) * | 2007-07-13 | 2009-01-15 | Evonik Röhm Gmbh | Verbesserte Stumpfstoßverbindungen für Kernwerkstoffe |
DE102007051422A1 (de) * | 2007-10-25 | 2009-04-30 | Evonik Röhm Gmbh | Zweiseiten-Einnadel-Unterfaden-Nähtechnik |
US7879276B2 (en) | 2007-11-08 | 2011-02-01 | The Boeing Company | Foam stiffened hollow composite stringer |
DE102007055684A1 (de) * | 2007-11-21 | 2009-06-10 | Airbus Deutschland Gmbh | Vorrichtung zur Herstellung eines verstärkten Schaumwerkstoffes |
US8127450B2 (en) * | 2008-01-31 | 2012-03-06 | Airbus Operations Gmbh | Method for producing a sandwich construction, in particular a sandwich construction for the aeronautical and aerospace fields |
DE102008006981B3 (de) * | 2008-01-31 | 2009-06-10 | Airbus Deutschland Gmbh | Verfahren zum Herstellen eines Kernverbundes, insbesondere eines Kernverbundes im Luft- und Raumfahrtbereich |
DE102008001826B3 (de) * | 2008-05-16 | 2009-09-17 | Airbus Deutschland Gmbh | Ausschnittverstärkung für Kernverbunde sowie ein Verfahren zum Herstellen einer Ausschnittverstärkung für Kernverbunde |
DE102008041788A1 (de) | 2008-09-03 | 2010-03-11 | Airbus Deutschland Gmbh | Sandwichplatte mit integrierter Verstärkungsstruktur sowie Verfahren zu deren Herstellung |
US8540921B2 (en) | 2008-11-25 | 2013-09-24 | The Boeing Company | Method of forming a reinforced foam-filled composite stringer |
US8500066B2 (en) | 2009-06-12 | 2013-08-06 | The Boeing Company | Method and apparatus for wireless aircraft communications and power system using fuselage stringers |
US8570152B2 (en) | 2009-07-23 | 2013-10-29 | The Boeing Company | Method and apparatus for wireless sensing with power harvesting of a wireless signal |
US8617687B2 (en) | 2009-08-03 | 2013-12-31 | The Boeing Company | Multi-functional aircraft structures |
DE102010054935B4 (de) * | 2010-12-17 | 2013-11-28 | Daimler Ag | Karosseriemodulbauteil |
CN108453993B (zh) | 2012-07-24 | 2021-07-02 | 赢创运营有限公司 | Pmi泡沫材料的新成型方法和/或由其制备的复合组件 |
GB2510133B (en) * | 2013-01-24 | 2017-08-30 | Bae Systems Plc | Conductive bonded composites |
DE102013223347A1 (de) | 2013-11-15 | 2015-05-21 | Evonik Industries Ag | Mit Poly(meth)acrylimid-Schaum gefüllte Wabenstrukturen |
DE102013018158A1 (de) | 2013-12-05 | 2015-06-11 | Airbus Defence and Space GmbH | Verfahren zur Herstellung von verstärkten Materialien und Material erhältlich aus diesem Verfahren |
DE102014014961A1 (de) * | 2014-10-14 | 2016-04-14 | Airbus Defence and Space GmbH | Vorrichtung sowie Verfahren |
CA2971793A1 (en) * | 2014-12-22 | 2016-06-30 | Basf Se | Fiber reinforcment of foams made from mutually bonded segments |
DE102015202035A1 (de) * | 2015-02-05 | 2016-08-11 | Bayerische Motoren Werke Aktiengesellschaft | Verfahren zur Herstellung eines Faser-Kunststoff-Verbund-Bauteils |
DE102015110855B4 (de) | 2015-07-06 | 2019-12-05 | Technische Universität Chemnitz | Verfahren zur Fertigung von komplexen 3D-Preformen |
EP3263321B1 (de) | 2016-06-29 | 2021-07-28 | Airbus Defence and Space GmbH | Verfahren zur herstellung eines sandwich-paneels mit einem verstärkten schaumstoffkern |
RU2678021C1 (ru) * | 2017-09-11 | 2019-01-22 | Государственное бюджетное образовательное учреждение высшего образования Московской области "Технологический университет" | Способ изготовления объемно армированного композиционного материала |
GB201903190D0 (en) * | 2019-03-09 | 2019-04-24 | Rolls Royce Plc | An apparatus for gripping a plurality of reinforcement rods |
DE102019114433A1 (de) * | 2019-05-29 | 2020-12-03 | Airbus Operations Gmbh | Verfahren und ein System zum Herstellen eines Bauteils oder Halbzeugs mit einem faserverstärkten Schaumkern |
FR3098444B1 (fr) * | 2019-07-08 | 2021-10-01 | Soc Internationale Pour Le Commerce Et Lindustrie | Procédé de renforcement d’un panneau et un procédé de fabrication de panneau composite mettant en œuvre un tel procédé |
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US7563497B2 (en) * | 2004-12-27 | 2009-07-21 | Mkp Structural Design Associates, Inc. | Lightweight, rigid composite structures |
DE102005024408A1 (de) * | 2005-05-27 | 2006-11-30 | Airbus Deutschland Gmbh | Verstärkung von Schaumwerkstoffen |
DE102007055684A1 (de) * | 2007-11-21 | 2009-06-10 | Airbus Deutschland Gmbh | Vorrichtung zur Herstellung eines verstärkten Schaumwerkstoffes |
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2005
- 2005-07-27 DE DE102005035681A patent/DE102005035681A1/de not_active Withdrawn
-
2006
- 2006-04-05 PL PL06724058T patent/PL1907193T3/pl unknown
- 2006-04-05 CA CA2616655A patent/CA2616655C/en not_active Expired - Fee Related
- 2006-04-05 JP JP2008523137A patent/JP4751448B2/ja not_active Expired - Fee Related
- 2006-04-05 NZ NZ563572A patent/NZ563572A/en not_active IP Right Cessation
- 2006-04-05 KR KR1020087002100A patent/KR101319703B1/ko not_active IP Right Cessation
- 2006-04-05 AU AU2006274270A patent/AU2006274270B2/en not_active Ceased
- 2006-04-05 DE DE502006009011T patent/DE502006009011D1/de active Active
- 2006-04-05 ES ES06724058T patent/ES2361617T3/es active Active
- 2006-04-05 WO PCT/EP2006/003110 patent/WO2007012353A1/de active Application Filing
- 2006-04-05 RU RU2008106981/12A patent/RU2419543C2/ru not_active IP Right Cessation
- 2006-04-05 DK DK06724058.0T patent/DK1907193T3/da active
- 2006-04-05 CN CN2006800185389A patent/CN101198459B/zh not_active Expired - Fee Related
- 2006-04-05 AT AT06724058T patent/ATE500049T1/de active
- 2006-04-05 US US11/914,064 patent/US20080226876A1/en not_active Abandoned
- 2006-04-05 BR BRPI0613882-9A patent/BRPI0613882A2/pt not_active IP Right Cessation
- 2006-04-05 EP EP06724058A patent/EP1907193B8/de not_active Not-in-force
- 2006-04-19 TW TW095113987A patent/TWI388429B/zh not_active IP Right Cessation
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2007
- 2007-10-18 IL IL186761A patent/IL186761A/en not_active IP Right Cessation
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2008
- 2008-01-25 ZA ZA200800782A patent/ZA200800782B/xx unknown
- 2008-11-13 HK HK08112447.6A patent/HK1120768A1/xx not_active IP Right Cessation
Also Published As
Publication number | Publication date |
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BRPI0613882A2 (pt) | 2011-02-15 |
ZA200800782B (en) | 2008-12-31 |
AU2006274270A1 (en) | 2007-02-01 |
NZ563572A (en) | 2010-08-27 |
HK1120768A1 (en) | 2009-04-09 |
WO2007012353A1 (de) | 2007-02-01 |
JP4751448B2 (ja) | 2011-08-17 |
CA2616655C (en) | 2014-01-07 |
RU2419543C2 (ru) | 2011-05-27 |
KR20080031908A (ko) | 2008-04-11 |
IL186761A0 (en) | 2008-02-09 |
KR101319703B1 (ko) | 2013-10-17 |
EP1907193B1 (de) | 2011-03-02 |
DK1907193T3 (da) | 2011-06-14 |
PL1907193T3 (pl) | 2011-08-31 |
EP1907193B8 (de) | 2011-10-12 |
CA2616655A1 (en) | 2007-02-01 |
CN101198459B (zh) | 2012-02-22 |
CN101198459A (zh) | 2008-06-11 |
ES2361617T3 (es) | 2011-06-20 |
TW200709929A (en) | 2007-03-16 |
JP2009502562A (ja) | 2009-01-29 |
IL186761A (en) | 2011-01-31 |
DE502006009011D1 (de) | 2011-04-14 |
DE102005035681A1 (de) | 2007-02-08 |
ATE500049T1 (de) | 2011-03-15 |
EP1907193A1 (de) | 2008-04-09 |
US20080226876A1 (en) | 2008-09-18 |
TWI388429B (zh) | 2013-03-11 |
AU2006274270B2 (en) | 2011-06-16 |
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