RU2010103130A - Способ производства компонента и термопластический компонент, армированный волокном - Google Patents

Способ производства компонента и термопластический компонент, армированный волокном Download PDF

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Publication number
RU2010103130A
RU2010103130A RU2010103130/05A RU2010103130A RU2010103130A RU 2010103130 A RU2010103130 A RU 2010103130A RU 2010103130/05 A RU2010103130/05 A RU 2010103130/05A RU 2010103130 A RU2010103130 A RU 2010103130A RU 2010103130 A RU2010103130 A RU 2010103130A
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Russia
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preform
component
edge lines
approximately
producing
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RU2010103130/05A
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English (en)
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Клаус ЕДЕЛМАНН (DE)
Клаус ЕДЕЛМАНН
Таня МЕНКЕН (DE)
Таня МЕНКЕН
Тимо ШТОЕФЕН (DE)
Тимо ШТОЕФЕН
Тобиас ВИРТЦ (DE)
Тобиас ВИРТЦ
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Эйрбас Оператионс Гмбх (De)
Эйрбас Оператионс Гмбх
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Publication of RU2010103130A publication Critical patent/RU2010103130A/ru

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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
    • B29C53/00—Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
    • B29C53/02—Bending or folding
    • B29C53/04—Bending or folding of plates or sheets
    • 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
    • B29C70/22—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 two directions forming a two dimensional structure
    • B29C70/222—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 two directions forming a two dimensional structure the structure being shaped to form a three dimensional configuration
    • 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
    • B29C2793/00—Shaping techniques involving a cutting or machining operation
    • B29C2793/0081—Shaping techniques involving a cutting or machining operation before shaping
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2071/00—Use of polyethers, e.g. PEEK, i.e. polyether-etherketone or PEK, i.e. polyetherketone or derivatives thereof, as moulding material
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2081/00—Use of polymers having sulfur, with or without nitrogen, oxygen or carbon only, in the main chain, as moulding material
    • B29K2081/04—Polysulfides, e.g. PPS, i.e. polyphenylene sulfide or derivatives thereof
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2101/00—Use of unspecified macromolecular compounds as moulding material
    • B29K2101/12—Thermoplastic materials
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2277/00—Use of PA, i.e. polyamides, e.g. polyesteramides or derivatives thereof, as reinforcement
    • B29K2277/10—Aromatic polyamides [Polyaramides] or derivatives thereof
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2707/00—Use of elements other than metals for preformed parts, e.g. for inserts
    • B29K2707/04—Carbon
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2709/00—Use of inorganic materials not provided for in groups B29K2703/00 - B29K2707/00, for preformed parts, e.g. for inserts
    • B29K2709/08—Glass
    • 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
    • B29L2009/00—Layered products
    • 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
    • B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
    • B29L2031/3076—Aircrafts
    • 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction
    • 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
    • Y10T156/1036—Bending of one piece blank and joining edges to form article

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Textile Engineering (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
  • Moulding By Coating Moulds (AREA)
  • Multicomponent Fibers (AREA)
  • Processing And Handling Of Plastics And Other Materials For Molding In General (AREA)

Abstract

Способ производства компонента (3), включающий следующие этапы: ! a) подготовка заготовки (1) из термопласта, армированного несколькими слоями волокон, причем заготовка (1) имеет в сущности V-образный вырез (5), вершина которого совпадает с точкой пересечения трех предварительно определенных краевых линий (7, 8, 9, 10) заготовки (1), и имеет приблизительно округлую выемку (6); ! b) формование заготовки (1) по предварительно определенным краевым линиям (7, 8, 9, 10), в большей степени по окончанию сдвига слоев волокон для получения преформы (2) и образования краевых линий (15, 16, 17), которые проходят приблизительно перпендикулярно друг другу; ! c) помещение преформы (2) на пуансон или матрицу (25) пресса, причем преформа имеет форму пирамиды с поверхностью (26) основания и тремя боковыми поверхностями (27, 28, 29), которые вместе образуют вершину (33), так что приблизительно округлая выемка (6) преформы (2) лежит в области вершины (33), при этом поверхности (23, 24) основания преформы (2), относящиеся к V-образной секции (5) преформы (2) по меньшей мере частично лежат на одной из боковых поверхностей (27, 28, 29); ! d) сжатие пресса для формирования конечных краевых линий (15, 16, 17) и уплотнения преформы (2) с соответственными формованием компонента (3).

Claims (1)

  1. Способ производства компонента (3), включающий следующие этапы:
    a) подготовка заготовки (1) из термопласта, армированного несколькими слоями волокон, причем заготовка (1) имеет в сущности V-образный вырез (5), вершина которого совпадает с точкой пересечения трех предварительно определенных краевых линий (7, 8, 9, 10) заготовки (1), и имеет приблизительно округлую выемку (6);
    b) формование заготовки (1) по предварительно определенным краевым линиям (7, 8, 9, 10), в большей степени по окончанию сдвига слоев волокон для получения преформы (2) и образования краевых линий (15, 16, 17), которые проходят приблизительно перпендикулярно друг другу;
    c) помещение преформы (2) на пуансон или матрицу (25) пресса, причем преформа имеет форму пирамиды с поверхностью (26) основания и тремя боковыми поверхностями (27, 28, 29), которые вместе образуют вершину (33), так что приблизительно округлая выемка (6) преформы (2) лежит в области вершины (33), при этом поверхности (23, 24) основания преформы (2), относящиеся к V-образной секции (5) преформы (2) по меньшей мере частично лежат на одной из боковых поверхностей (27, 28, 29);
    d) сжатие пресса для формирования конечных краевых линий (15, 16, 17) и уплотнения преформы (2) с соответственными формованием компонента (3).
RU2010103130/05A 2007-08-09 2008-07-02 Способ производства компонента и термопластический компонент, армированный волокном RU2010103130A (ru)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
US96417007P 2007-08-09 2007-08-09
US60/964,170 2007-08-09
DE102007037649.0 2007-08-09
DE102007037649A DE102007037649A1 (de) 2007-08-09 2007-08-09 Verfahren zur Herstellung eines Bauteils sowie faserverstärktes thermoplastisches Bauteil

Publications (1)

Publication Number Publication Date
RU2010103130A true RU2010103130A (ru) 2011-08-10

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RU2010103130/05A RU2010103130A (ru) 2007-08-09 2008-07-02 Способ производства компонента и термопластический компонент, армированный волокном

Country Status (10)

Country Link
US (1) US7922853B2 (ru)
EP (1) EP2185339B1 (ru)
JP (1) JP2010535650A (ru)
CN (1) CN101815606B (ru)
AT (1) ATE551174T1 (ru)
BR (1) BRPI0814998A2 (ru)
CA (1) CA2695588A1 (ru)
DE (1) DE102007037649A1 (ru)
RU (1) RU2010103130A (ru)
WO (1) WO2009019083A1 (ru)

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Also Published As

Publication number Publication date
WO2009019083A1 (de) 2009-02-12
EP2185339B1 (de) 2012-03-28
ATE551174T1 (de) 2012-04-15
EP2185339A1 (de) 2010-05-19
US20100186882A1 (en) 2010-07-29
CN101815606B (zh) 2013-11-20
BRPI0814998A2 (pt) 2015-02-03
US7922853B2 (en) 2011-04-12
DE102007037649A1 (de) 2009-02-12
CN101815606A (zh) 2010-08-25
CA2695588A1 (en) 2009-02-12
JP2010535650A (ja) 2010-11-25

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