AU2001287207A1 - Apparatus and method for controlled damage of conformable materials - Google Patents

Apparatus and method for controlled damage of conformable materials

Info

Publication number
AU2001287207A1
AU2001287207A1 AU2001287207A AU8720701A AU2001287207A1 AU 2001287207 A1 AU2001287207 A1 AU 2001287207A1 AU 2001287207 A AU2001287207 A AU 2001287207A AU 8720701 A AU8720701 A AU 8720701A AU 2001287207 A1 AU2001287207 A1 AU 2001287207A1
Authority
AU
Australia
Prior art keywords
conformable materials
controlled damage
damage
controlled
conformable
Prior art date
Legal status (The legal status 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 status listed.)
Abandoned
Application number
AU2001287207A
Other languages
English (en)
Inventor
Elbert Lee McKague Jr.
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Lockheed Martin Corp
Original Assignee
Lockheed Martin Corp
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 Lockheed Martin Corp filed Critical Lockheed Martin Corp
Publication of AU2001287207A1 publication Critical patent/AU2001287207A1/en
Abandoned legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/06Fibrous reinforcements only
    • B29C70/10Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
    • B29C70/12Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of short length, e.g. in the form of a mat
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/40Shaping or impregnating by compression not applied
    • B29C70/42Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/46Shaping 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/54Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
    • B29C70/545Perforating, cutting or machining during or after moulding
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C2793/00Shaping techniques involving a cutting or machining operation
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T156/00Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/10Methods of surface bonding and/or assembly therefor
    • Y10T156/1002Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina
    • Y10T156/1025Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina to form undulated to corrugated sheet and securing to base with parts of shaped areas out of contact
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T156/00Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/10Methods of surface bonding and/or assembly therefor
    • Y10T156/1052Methods of surface bonding and/or assembly therefor with cutting, punching, tearing or severing
    • Y10T156/1062Prior to assembly
    • Y10T156/1075Prior to assembly of plural laminae from single stock and assembling to each other or to additional lamina

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Mechanical Engineering (AREA)
  • Textile Engineering (AREA)
  • Reinforced Plastic Materials (AREA)
  • Laminated Bodies (AREA)
AU2001287207A 2000-08-24 2001-08-23 Apparatus and method for controlled damage of conformable materials Abandoned AU2001287207A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US09645223 2000-08-24
US09/645,223 US6454893B1 (en) 2000-08-24 2000-08-24 Method of shaping continuous fiber lamina to an undulated surface by cutting individual fibers
PCT/US2001/041853 WO2002016116A2 (fr) 2000-08-24 2001-08-23 Dispositif et procede servant a empecher la deterioration de materiaux compatibles

Publications (1)

Publication Number Publication Date
AU2001287207A1 true AU2001287207A1 (en) 2002-03-04

Family

ID=24588139

Family Applications (1)

Application Number Title Priority Date Filing Date
AU2001287207A Abandoned AU2001287207A1 (en) 2000-08-24 2001-08-23 Apparatus and method for controlled damage of conformable materials

Country Status (3)

Country Link
US (1) US6454893B1 (fr)
AU (1) AU2001287207A1 (fr)
WO (1) WO2002016116A2 (fr)

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US8632653B2 (en) 2005-05-03 2014-01-21 The Boeing Company Method of manufacturing curved composite structural elements
EP1731291B1 (fr) * 2005-06-08 2008-09-24 Saab Ab Appareil de positionnement automatique de bandes et procédé utilisant cet appareil
EP1762357B1 (fr) * 2005-09-09 2015-02-25 Saab Ab Procédé et dispositif de moulage par compression d'une ébauche pour élément de construction composé d'une avion
CN101489767B (zh) * 2006-05-22 2015-04-29 尤米柯结构材料(德比)有限公司 模塑材料
ES2901199T3 (es) * 2007-02-02 2022-03-21 Toray Industries Material de base preimpregnado, material de base laminado y plástico reforzado con fibra
US8449709B2 (en) * 2007-05-25 2013-05-28 The Boeing Company Method of fabricating fiber reinforced composite structure having stepped surface
US8932423B2 (en) * 2008-04-17 2015-01-13 The Boeing Company Method for producing contoured composite structures and structures produced thereby
US9278484B2 (en) * 2008-04-17 2016-03-08 The Boeing Company Method and apparatus for producing contoured composite structures and structures produced thereby
US9090028B2 (en) * 2008-04-17 2015-07-28 The Boeing Company Method for producing contoured composite structures and structures produced thereby
US8349105B2 (en) 2008-04-17 2013-01-08 The Boeing Company Curved composite frames and method of making the same
ES2338084B1 (es) * 2008-10-30 2011-03-14 Airbus Operations, S.L. Metodo de fabricacion de un panel de geometria compleja en material compuesto preimpregnado.
US20120073739A1 (en) * 2010-08-23 2012-03-29 Callaway Golf Companyh Advanced unidirectional material compression-molded face component
BR112014020667B1 (pt) 2012-02-28 2020-10-13 Automobili Lamborghini S.P.A. processo de moldagem por comprenssão com calor para a fabricação de artigos de materiais compósitos
BR112015010690B1 (pt) * 2012-11-09 2021-05-11 Dsm Ip Assets B.V partes compósitas flexíveis em formato tridimensional e método de produção dessas partes
US9789662B2 (en) 2013-03-13 2017-10-17 Cubic Tech Corporation Engineered composite systems
EP2969502B1 (fr) 2013-03-13 2021-08-04 DSM IP Assets B.V. Procédé pour produire des articles en trois dimensions à partir de matériaux composites souples
KR102421970B1 (ko) 2013-03-13 2022-07-15 디에스엠 아이피 어셋츠 비.브이. 가요성 복합체 시스템 및 방법
DE102013014902B4 (de) 2013-09-06 2018-08-23 Audi Ag Verfahren zur Modifizierung eines flächigen Endlosfaserhalbzeugs
CN113442466B (zh) 2015-10-27 2023-07-28 东丽株式会社 切口预浸料坯
WO2017221688A1 (fr) * 2016-06-22 2017-12-28 東レ株式会社 Procédé de production de faisceau de fibres séparées, faisceau de fibres séparées, matériau de moulage de résine renforcée par des fibres mettant en oeuvre un faisceau de fibres séparées et procédé de production de matériau de moulage de résine renforcée par des fibres mettant en oeuvre un faisceau de fibres séparées
US10814602B2 (en) * 2016-09-14 2020-10-27 The Boeing Company Method of producing cored composite parts
CN109719969B (zh) * 2018-12-29 2021-08-20 北京航天天美科技有限公司 型面模具上的铺层方法
JP7175820B2 (ja) * 2019-03-26 2022-11-21 三菱重工業株式会社 プリプレグ成形方法
WO2021059421A1 (fr) * 2019-09-26 2021-04-01 三菱重工業株式会社 Procédé de façonnage d'un composant en matériau composite et charge correspondante

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2800423A (en) * 1954-10-18 1957-07-23 Swart Dev Company De Molded article of stretchable glass cloth
US4167130A (en) * 1977-12-22 1979-09-11 Owens-Corning Fiberglas Corporation Method for cutting sheet moulding compound reinforcing strands
US4376749A (en) * 1980-02-06 1983-03-15 Motor Wheel Corporation Fiber-reinforced composite wheel construction
JPS60224530A (ja) * 1984-04-23 1985-11-08 Mazda Motor Corp 強化繊維を含有する複合樹脂シ−ト
GB8512243D0 (en) * 1985-05-15 1985-06-19 Ici Plc Shaped articles
US4990207A (en) * 1987-04-02 1991-02-05 Mitsui Toatsu Chemicals, Inc. Process for preparing fiber-reinforced thermoplastic molded articles
FR2633213B1 (fr) * 1988-06-27 1990-12-28 Europ Propulsion Procede de realisation d'une preforme fibreuse pour la fabrication de pieces en materiau composite ayant une forme complexe
GB9413417D0 (en) * 1994-07-04 1994-08-24 Ford Roger A Improved composite materials and method for making them
US5846356A (en) 1996-03-07 1998-12-08 Board Of Trustees Operating Michigan State University Method and apparatus for aligning discontinuous fibers
DE19944164C2 (de) * 1999-09-15 2001-10-04 Inst Verbundwerkstoffe Gmbh Herstellung von mehreren Bauteilen aus kontinuierlich faserverstärkten Kunststoffplatinen in Formnestern

Also Published As

Publication number Publication date
WO2002016116A2 (fr) 2002-02-28
WO2002016116A3 (fr) 2002-05-02
US6454893B1 (en) 2002-09-24

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