ATE500056T1 - Vorimprägniertes material mit halbkristalliner matrix und amorpher oberflächenschicht - Google Patents

Vorimprägniertes material mit halbkristalliner matrix und amorpher oberflächenschicht

Info

Publication number
ATE500056T1
ATE500056T1 AT08702561T AT08702561T ATE500056T1 AT E500056 T1 ATE500056 T1 AT E500056T1 AT 08702561 T AT08702561 T AT 08702561T AT 08702561 T AT08702561 T AT 08702561T AT E500056 T1 ATE500056 T1 AT E500056T1
Authority
AT
Austria
Prior art keywords
semi
surface layer
impregnated material
thermoplastic resin
amorphous surface
Prior art date
Application number
AT08702561T
Other languages
English (en)
Inventor
Michele Iannone
Original Assignee
Alenia Aeronautica Spa
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Alenia Aeronautica Spa filed Critical Alenia Aeronautica Spa
Application granted granted Critical
Publication of ATE500056T1 publication Critical patent/ATE500056T1/de

Links

Classifications

    • 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
    • B32B27/00—Layered products comprising a layer of synthetic resin
    • B32B27/04—Layered products comprising a layer of synthetic resin as impregnant, bonding, or embedding substance
    • 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
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/73—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset
    • B29C66/737—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the state of the material of the parts to be joined
    • B29C66/7377—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the state of the material of the parts to be joined amorphous, semi-crystalline or crystalline
    • B29C66/73771—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the state of the material of the parts to be joined amorphous, semi-crystalline or crystalline the to-be-joined area of at least one of the parts to be joined being amorphous
    • 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
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/73—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset
    • B29C66/737—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the state of the material of the parts to be joined
    • B29C66/7377—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the state of the material of the parts to be joined amorphous, semi-crystalline or crystalline
    • B29C66/73773—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the state of the material of the parts to be joined amorphous, semi-crystalline or crystalline the to-be-joined area of at least one of the parts to be joined being semi-crystalline
    • 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
    • B32B27/00—Layered products comprising a layer of synthetic resin
    • B32B27/06—Layered products comprising a layer of synthetic resin as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • B32B27/08—Layered products comprising a layer of synthetic resin as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin
    • C—CHEMISTRY; METALLURGY
    • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08J—WORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
    • C08J5/00—Manufacture of articles or shaped materials containing macromolecular substances
    • C08J5/04—Reinforcing macromolecular compounds with loose or coherent fibrous material
    • C08J5/0405—Reinforcing macromolecular compounds with loose or coherent fibrous material with inorganic fibres
    • C08J5/042—Reinforcing macromolecular compounds with loose or coherent fibrous material with inorganic fibres with carbon fibres
    • C—CHEMISTRY; METALLURGY
    • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08J—WORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
    • C08J5/00—Manufacture of articles or shaped materials containing macromolecular substances
    • C08J5/24—Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs
    • C08J5/241—Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs using inorganic fibres
    • C08J5/243—Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs using inorganic fibres using carbon fibres
    • 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
    • B29K2995/00—Properties of moulding materials, reinforcements, fillers, preformed parts or moulds
    • B29K2995/0037—Other properties
    • B29K2995/0039—Amorphous
    • 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
    • B29K2995/00—Properties of moulding materials, reinforcements, fillers, preformed parts or moulds
    • B29K2995/0037—Other properties
    • B29K2995/004—Semi-crystalline

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Polymers & Plastics (AREA)
  • Manufacturing & Machinery (AREA)
  • Health & Medical Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Medicinal Chemistry (AREA)
  • Inorganic Chemistry (AREA)
  • Organic Chemistry (AREA)
  • Mechanical Engineering (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Laminated Bodies (AREA)
  • Reinforced Plastic Materials (AREA)
  • Lining Or Joining Of Plastics Or The Like (AREA)
  • Light Receiving Elements (AREA)
  • Polishing Bodies And Polishing Tools (AREA)
  • Superconductors And Manufacturing Methods Therefor (AREA)
AT08702561T 2007-02-05 2008-02-04 Vorimprägniertes material mit halbkristalliner matrix und amorpher oberflächenschicht ATE500056T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
IT000079A ITTO20070079A1 (it) 2007-02-05 2007-02-05 Materiale preimpregnato a matrice semicristallina con strato amorfo superficiale
PCT/IB2008/050400 WO2008096312A1 (en) 2007-02-05 2008-02-04 Pre-impregnated material with semi-crystalline matrix and amorphous surface layer

Publications (1)

Publication Number Publication Date
ATE500056T1 true ATE500056T1 (de) 2011-03-15

Family

ID=39313211

Family Applications (1)

Application Number Title Priority Date Filing Date
AT08702561T ATE500056T1 (de) 2007-02-05 2008-02-04 Vorimprägniertes material mit halbkristalliner matrix und amorpher oberflächenschicht

Country Status (8)

Country Link
US (1) US20100170637A1 (de)
EP (1) EP2109532B1 (de)
JP (1) JP5113193B2 (de)
AT (1) ATE500056T1 (de)
DE (1) DE602008005264D1 (de)
ES (1) ES2362383T3 (de)
IT (1) ITTO20070079A1 (de)
WO (1) WO2008096312A1 (de)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9126211B2 (en) 2009-07-24 2015-09-08 Durr Systems Gmbh Rotary atomizer comprising an atomizer bell and a retainer
WO2013008720A1 (ja) * 2011-07-11 2013-01-17 東レ株式会社 熱可塑性樹脂プリプレグ、それを用いた予備成形体および複合成形体、ならびにそれらの製造方法
US20150298388A1 (en) * 2012-12-04 2015-10-22 The Boeing Company Joining Composite Components Using Low Temperature Thermoplastic Film Fusion
ES2830825T3 (es) 2014-11-24 2021-06-04 Leonardo Spa Procedimiento para la fabricación de una pieza compuesta a partir de un material preimpregnado con una matriz semicristalina que tiene una capa superficial amorfa
US20160281272A1 (en) * 2015-03-26 2016-09-29 Honeywell International Inc. Ballistic resistant composite material
EP3760666B1 (de) * 2018-02-27 2025-04-02 Mitsubishi Chemical Corporation Faserverstärktes thermoplastisches harz-prepreg und formkörper
FR3112307A1 (fr) 2020-07-10 2022-01-14 Arkema France Procédé d’analyse de semi-produits comprenant une résine thermoplastique
EP4049833B1 (de) 2021-02-24 2025-10-29 The Boeing Company Verfahren zur verbindung eines ersten thermoplastischen substrats mit einem zweiten thermoplastischen substrat
US20230076283A1 (en) * 2021-09-03 2023-03-09 Charles Tobias Mueller Film-bonded infusion
US12227647B2 (en) 2021-11-19 2025-02-18 The Boeing Company Thermoplastic films and methods for coating thermoplastic substrates with thermoset materials
US12577367B2 (en) 2021-11-19 2026-03-17 The Boeing Company Thermoplastic composition, consolidated laminate structure, and method for manufacturing thereof
JP7786940B2 (ja) * 2021-12-24 2025-12-16 旭化成株式会社 連続繊維強化樹脂複合材料及びその製造方法
US12544993B2 (en) 2023-08-01 2026-02-10 The Boeing Company Methods of stamp-forming fiber-reinforced thermoplastic composite assemblies and related systems
WO2026024318A1 (en) * 2024-07-26 2026-01-29 Green Eagle Usa, Llc Polymeric based multi-material multi-layer geometrically enhanced structural compositions and related methods

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB8728887D0 (en) * 1987-12-10 1988-01-27 Ici Plc Fibre reinforced thermoplastic composite structures
JPH04272849A (ja) * 1991-02-27 1992-09-29 Mitsui Toatsu Chem Inc 繊維補強熱可塑性樹脂多層積層板の製造方法及び装置
GB9307231D0 (en) * 1993-04-07 1993-06-02 Courtaulds Aerospace Ltd Composite ballistic armour
JP3250901B2 (ja) * 1994-02-07 2002-01-28 三井化学株式会社 繊維補強樹脂シートの積層体の製造方法
JPH07241920A (ja) * 1994-03-07 1995-09-19 Yokohama Rubber Co Ltd:The 繊維補強熱可塑性樹脂パイプ及びその製造方法
DE19604611A1 (de) * 1996-02-08 1997-08-14 Bayerische Motoren Werke Ag Verfahren zur Herstellung einer Sandwichstruktur aus Kunststoff

Also Published As

Publication number Publication date
EP2109532B1 (de) 2011-03-02
US20100170637A1 (en) 2010-07-08
DE602008005264D1 (de) 2011-04-14
ES2362383T3 (es) 2011-07-04
JP5113193B2 (ja) 2013-01-09
ITTO20070079A1 (it) 2008-08-06
EP2109532A1 (de) 2009-10-21
WO2008096312A1 (en) 2008-08-14
JP2010517823A (ja) 2010-05-27

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