RU93050063A - Способ непрерывного формирования композита на основе смолы, армированной волокном - Google Patents
Способ непрерывного формирования композита на основе смолы, армированной волокномInfo
- Publication number
- RU93050063A RU93050063A RU93050063/26A RU93050063A RU93050063A RU 93050063 A RU93050063 A RU 93050063A RU 93050063/26 A RU93050063/26 A RU 93050063/26A RU 93050063 A RU93050063 A RU 93050063A RU 93050063 A RU93050063 A RU 93050063A
- Authority
- RU
- Russia
- Prior art keywords
- punch
- matrix
- composite
- fiber
- basis
- Prior art date
Links
- 239000002131 composite material Substances 0.000 title claims 2
- 230000015572 biosynthetic process Effects 0.000 title 1
- 238000005755 formation reaction Methods 0.000 title 1
- 239000011159 matrix material Substances 0.000 claims 4
- 239000000463 material Substances 0.000 claims 2
- 239000002184 metal Substances 0.000 claims 2
- 230000023298 conjugation with cellular fusion Effects 0.000 claims 1
- 239000004744 fabric Substances 0.000 claims 1
- 230000013011 mating Effects 0.000 claims 1
- 238000000465 moulding Methods 0.000 claims 1
- 239000011347 resin Substances 0.000 claims 1
- 229920005989 resin Polymers 0.000 claims 1
- 230000021037 unidirectional conjugation Effects 0.000 claims 1
Claims (1)
- Предложен способ непрерывного формования длинных композитных конструкционных профилей, например конфигурации в виде букв "Z", грибовидной конфигурации, или в виде букв "L". Сначала изготавливают пакет из однонаправленной ленты или тканевой ткани, затем материал нагревают для создания размягчения смолы, затем его протягивают через группу валков, а затем через сопряженные металлические матрицу и быстро перемещающийся в возвратно-поступательном направлении пуансон, что позволяет осуществить формование окончательной конфигурации или профиля. По мере того, как материал протягивается через область сопряженных металлических матрицы и пуансона, он охлаждается за счет отвода тепла от матрицы или пуансона или при помощи других устройств так, что когда деталь выходит из области матрицы и пуансона, она достаточно охлаждена, чтобы сохранить желаемую конфигурацию или профиль. Быстро перемещающийся в возвратно-поступательном направлении пуансон позволяет осуществить непрерывное протягивание детали.
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US721.781 | 1991-01-31 | ||
US07/721,781 US5182060A (en) | 1991-01-31 | 1991-01-31 | Continuous forming of composites |
PCT/US1992/000237 WO1992013706A1 (en) | 1991-01-31 | 1992-01-23 | A method for continuously forming a fiber reinforced resin composite |
US721781 | 1996-09-25 |
Publications (2)
Publication Number | Publication Date |
---|---|
RU93050063A true RU93050063A (ru) | 1996-01-27 |
RU2112646C1 RU2112646C1 (ru) | 1998-06-10 |
Family
ID=24899280
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU93050063A RU2112646C1 (ru) | 1991-01-31 | 1992-01-23 | Способ непрерывного формирования композита на основе смолы, армированной волокном (варианты) |
Country Status (11)
Country | Link |
---|---|
US (1) | US5182060A (ru) |
EP (1) | EP0569460B1 (ru) |
JP (1) | JPH06505203A (ru) |
KR (1) | KR100221511B1 (ru) |
AU (1) | AU652419B2 (ru) |
BR (1) | BR9205525A (ru) |
CA (1) | CA2100556A1 (ru) |
DE (1) | DE69205416T2 (ru) |
ES (1) | ES2079853T3 (ru) |
RU (1) | RU2112646C1 (ru) |
WO (1) | WO1992013706A1 (ru) |
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US7249943B2 (en) * | 2003-08-01 | 2007-07-31 | Alliant Techsystems Inc. | Apparatus for forming composite stiffeners and reinforcing structures |
US7521386B2 (en) * | 2004-02-07 | 2009-04-21 | Milliken & Company | Moldable heat shield |
US7696112B2 (en) | 2005-05-17 | 2010-04-13 | Milliken & Company | Non-woven material with barrier skin |
US7428803B2 (en) * | 2005-05-17 | 2008-09-30 | Milliken & Company | Ceiling panel system with non-woven panels having barrier skins |
US7605097B2 (en) * | 2006-05-26 | 2009-10-20 | Milliken & Company | Fiber-containing composite and method for making the same |
US7651964B2 (en) * | 2005-08-17 | 2010-01-26 | Milliken & Company | Fiber-containing composite and method for making the same |
US9102103B2 (en) * | 2006-02-02 | 2015-08-11 | The Boeing Company | Thermoplastic composite parts having integrated metal fittings and method of making the same |
US8691137B2 (en) * | 2009-03-04 | 2014-04-08 | The Boeing Company | Method of molding partus using a tool sleeve for mold die |
US10449736B2 (en) | 2006-02-02 | 2019-10-22 | The Boeing Company | Apparatus for fabricating thermoplastic composite parts |
US8333858B2 (en) | 2006-02-02 | 2012-12-18 | The Boeing Company | Method for fabricating curved thermoplastic composite parts |
US8491745B2 (en) * | 2007-02-03 | 2013-07-23 | The Boeing Company | Method and material efficient tooling for continuous compression molding |
US10232532B1 (en) | 2006-02-02 | 2019-03-19 | The Boeing Company | Method for fabricating tapered thermoplastic composite parts |
US7807005B2 (en) * | 2006-02-02 | 2010-10-05 | The Boeing Company | Fabrication process for thermoplastic composite parts |
DE102006031436B4 (de) | 2006-07-07 | 2012-12-06 | Airbus Operations Gmbh | Strukturelement, Verfahren zur Herstellung eines derartigen Strukturelements und Flugzeug mit einem derartigen Strukturelement |
US7825050B2 (en) * | 2006-12-22 | 2010-11-02 | Milliken & Company | VOC-absorbing nonwoven composites |
GB0712549D0 (en) * | 2007-06-29 | 2007-08-08 | Airbus Uk Ltd | Improvements in elongate composite structural members |
GB0712552D0 (en) * | 2007-06-29 | 2007-08-08 | Airbus Uk Ltd | Elongate composite structural members and improvements therein |
GB0712553D0 (en) * | 2007-06-29 | 2007-08-08 | Airbus Uk Ltd | Composite panel stiffener |
WO2009059012A2 (en) * | 2007-10-30 | 2009-05-07 | Paul Kermit D | Improved fiber reinforced plastic composites and method and apparatus for making |
US8052823B2 (en) | 2008-01-31 | 2011-11-08 | Alliant Techsystems Inc. | Stiffener tool positioning apparatus |
DE102008010228A1 (de) | 2008-02-21 | 2009-09-03 | Airbus Deutschland Gmbh | Verfahren und Vorrichtung zur Herstellung faserverstärkter Kunststoffprofilteile |
GB0813161D0 (en) | 2008-07-18 | 2008-08-27 | Airbus Uk Ltd | Ramped stiffener and apparatus and method for forming the same |
GB0813146D0 (en) * | 2008-07-18 | 2008-08-27 | Airbus Uk Ltd | Ramped stiffener and apparatus and method for forming the same |
GB0813149D0 (en) * | 2008-07-18 | 2008-08-27 | Airbus Uk Ltd | Ramped stiffener and apparatus and method for forming the same |
US20100112881A1 (en) * | 2008-11-03 | 2010-05-06 | Pradip Bahukudumbi | Composite material and method for manufacturing composite material |
US9662841B2 (en) | 2009-11-10 | 2017-05-30 | Orbital Atk, Inc. | Radially extending composite structures |
US8282757B2 (en) | 2009-11-10 | 2012-10-09 | Alliant Techsystems Inc. | Automated composite annular structure forming |
US10821653B2 (en) * | 2010-02-24 | 2020-11-03 | Alexander M. Rubin | Continuous molding of thermoplastic laminates |
ES2413189B1 (es) * | 2012-01-10 | 2015-02-11 | Manuel Torres Martínez | Instalacion para fabricar larguerillos de fibra para estructuras aeroespaciales |
US9498915B2 (en) * | 2013-01-02 | 2016-11-22 | The Boeing Company | Fabrication of reinforced thermoplastic composite parts |
DE102015206917B4 (de) * | 2015-04-16 | 2022-03-17 | Bayerische Motoren Werke Aktiengesellschaft | Pultrusion von Endlosprofilen mit diskontinuierlichem Querschnittsverlauf |
DE102016103484A1 (de) * | 2016-02-26 | 2017-08-31 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Faserlegekopf zum Legen von Faserhalbzeugprofilen, Faserlegeanlage sowie Verfahren hierzu |
JP6667391B2 (ja) * | 2016-07-06 | 2020-03-18 | 三菱重工業株式会社 | 複合材、引抜成形装置及び引抜成形方法 |
DE102016120197A1 (de) * | 2016-10-24 | 2018-04-26 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Anlage und Verfahren zur Herstellung einer Faserpreform |
EP3354433A1 (de) * | 2017-01-31 | 2018-08-01 | Covestro Deutschland AG | Vorrichtung mit freilaufenden kühlwalzen zur herstellung eines faserverbundwerkstoffs in form eines mit polymer imprägnierten faserbands, verfahren zur herstellung dieses faserbands, ein imprägniertes faserband und ein aus dem imprägnierten faserband hergestellter mehrschichtverbund |
FR3081369B1 (fr) | 2018-05-28 | 2020-05-08 | Stelia Aerospace | Dispositif et procede de mise en forme d'une piece d'ebauche pour la formation d'une piece thermoplastique structurelle |
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CN117341183A (zh) * | 2023-11-30 | 2024-01-05 | 广东包庄科技有限公司 | Pet塑钢带成品打包校直方法及装置 |
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-
1991
- 1991-01-31 US US07/721,781 patent/US5182060A/en not_active Expired - Lifetime
-
1992
- 1992-01-23 BR BR9205525A patent/BR9205525A/pt active Search and Examination
- 1992-01-23 DE DE69205416T patent/DE69205416T2/de not_active Expired - Fee Related
- 1992-01-23 CA CA002100556A patent/CA2100556A1/en not_active Abandoned
- 1992-01-23 KR KR1019930702260A patent/KR100221511B1/ko not_active IP Right Cessation
- 1992-01-23 EP EP92904366A patent/EP0569460B1/en not_active Expired - Lifetime
- 1992-01-23 JP JP4504523A patent/JPH06505203A/ja active Pending
- 1992-01-23 RU RU93050063A patent/RU2112646C1/ru active
- 1992-01-23 ES ES92904366T patent/ES2079853T3/es not_active Expired - Lifetime
- 1992-01-23 WO PCT/US1992/000237 patent/WO1992013706A1/en active IP Right Grant
- 1992-01-23 AU AU12004/92A patent/AU652419B2/en not_active Ceased
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