ATE246590T1 - Zweiachsiges verfahren und vorrichtung zur herstellung von prepregs - Google Patents

Zweiachsiges verfahren und vorrichtung zur herstellung von prepregs

Info

Publication number
ATE246590T1
ATE246590T1 AT00978738T AT00978738T ATE246590T1 AT E246590 T1 ATE246590 T1 AT E246590T1 AT 00978738 T AT00978738 T AT 00978738T AT 00978738 T AT00978738 T AT 00978738T AT E246590 T1 ATE246590 T1 AT E246590T1
Authority
AT
Austria
Prior art keywords
preg
wavy
rollers
fibers
group
Prior art date
Application number
AT00978738T
Other languages
English (en)
Inventor
William F Pratt
Original Assignee
William F Pratt
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 William F Pratt filed Critical William F Pratt
Application granted granted Critical
Publication of ATE246590T1 publication Critical patent/ATE246590T1/de

Links

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
    • 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
    • B29C70/20—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in a single direction, e.g. roofing or other parallel fibres
    • 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
    • B29C70/40—Shaping or impregnating by compression not applied
    • B29C70/50—Shaping or impregnating by compression not applied for producing articles of indefinite length, e.g. prepregs, sheet moulding compounds [SMC] or cross moulding compounds [XMC]
    • B29C70/504—Shaping or impregnating by compression not applied for producing articles of indefinite length, e.g. prepregs, sheet moulding compounds [SMC] or cross moulding compounds [XMC] using rollers or pressure bands
    • 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
    • B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/22—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
    • B32B5/24—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
    • B32B5/26—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/12—Construction or attachment of skin panels
    • 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
    • B29C37/00—Component parts, details, accessories or auxiliary operations, not covered by group B29C33/00 or B29C35/00
    • B29C2037/90—Measuring, controlling or regulating
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C2001/0054—Fuselage structures substantially made from particular materials
    • B64C2001/0072—Fuselage structures substantially made from particular materials from composite materials
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Textile Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
  • Reinforced Plastic Materials (AREA)
AT00978738T 1999-11-18 2000-11-17 Zweiachsiges verfahren und vorrichtung zur herstellung von prepregs ATE246590T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/443,232 US6453962B1 (en) 1997-11-14 1999-11-18 Dual-axis method and machine for producing pre-preg
PCT/US2000/031541 WO2001036183A1 (en) 1999-11-18 2000-11-17 Dual-axis method and machine for producing pre-preg

Publications (1)

Publication Number Publication Date
ATE246590T1 true ATE246590T1 (de) 2003-08-15

Family

ID=23759947

Family Applications (1)

Application Number Title Priority Date Filing Date
AT00978738T ATE246590T1 (de) 1999-11-18 2000-11-17 Zweiachsiges verfahren und vorrichtung zur herstellung von prepregs

Country Status (5)

Country Link
US (2) US6453962B1 (de)
EP (1) EP1233859B1 (de)
AT (1) ATE246590T1 (de)
DE (1) DE60004390D1 (de)
WO (1) WO2001036183A1 (de)

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US20060277843A1 (en) * 2005-05-13 2006-12-14 Tracy Livingston Structural tower
US7435947B2 (en) * 2005-10-31 2008-10-14 The Boeing Company Apparatus and methods for integrating encoding functions in material placement machines
EP1974111A4 (de) * 2005-12-30 2010-01-06 Tracy Livingston Hebesystem und vorrichtung zum bau von windturbinentürmen
US8069634B2 (en) 2006-10-02 2011-12-06 General Electric Company Lifting system and apparatus for constructing and enclosing wind turbine towers
US9511571B2 (en) * 2007-01-23 2016-12-06 The Boeing Company Composite laminate having a damping interlayer and method of making the same
DE102008016989A1 (de) 2007-04-02 2008-10-09 Cetex Institut für Textil- und Verarbeitungsmaschinen gemeinnützige GmbH Verfahren und Vorrichtung zur partiellen Verstärkung einer Warenbahn
ITTO20070557A1 (it) * 2007-07-27 2009-01-28 Alenia Aeronautica Spa Procedimento di fabbricazione di un elemento curvo in materiale composito
US8002744B2 (en) * 2007-08-06 2011-08-23 Bard Peripheral Vascular, Inc Non-compliant medical balloon
US8016268B2 (en) * 2008-05-30 2011-09-13 Wind Tower Systems, Llc Wind tower service lift
EP2301045B1 (de) * 2008-06-27 2013-02-20 Union Carbide Chemicals & Plastics Technology LLC Strangziehverfahren zur herstellung von faserverstärkten verbundstoffen
MX337407B (es) * 2008-12-15 2016-03-03 Ge Wind Energy Llc Forma estructural para miembros de torre de enfriamiento.
DE102009056197A1 (de) * 2009-11-27 2011-06-01 Karl Mayer Malimo Textilmaschinenfabrik Gmbh Verfahren und Vorrichtung zum Erzeugen einer UD-Lage
RU2502600C1 (ru) * 2012-06-19 2013-12-27 Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Московский государственный технологический университет "СТАНКИН" (ФГБОУ ВПО МГТУ "СТАНКИН") Способ изготовления трубчатых изделий из полимерных композиционных материалов
US9091834B2 (en) * 2013-02-01 2015-07-28 Halliburton Energy Services, Inc. Fiber splice housing with temperature compensation
WO2016130721A2 (en) 2015-02-11 2016-08-18 Aerovironment, Inc. Survey migration system for vertical take-off and landing (vtol) unmanned aerial vehicles (uavs)
EP3599069B1 (de) 2018-07-23 2023-04-12 Crompton Technology Group Limited Faserbeschichtungsvorrichtung
CN109822778B (zh) * 2019-02-27 2021-02-12 南京特塑复合材料有限公司 一种连续纤维纵横浸渍制备热塑性复合材料的成型方法
US11371843B2 (en) * 2020-07-02 2022-06-28 Anello Photonics, Inc. Integration of photonics optical gyroscopes with micro-electro-mechanical sensors
KR20260055521A (ko) 2020-09-17 2026-04-23 아이코맷 리미티드 테이프 배치 헤드
CN114248367B (zh) * 2022-01-26 2023-01-20 江苏金纬智能制造有限公司 一种纤维预浸涂覆装置
US12365149B1 (en) 2024-03-18 2025-07-22 General Electric Company Automated fiber placement assembly with pressure roller

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE40360C (de) * 1900-01-01 CH. ROHKRAEMER & SOHN in Erfurt Verfahren zur Darstellung eines stickstoffhaltigen Düngemittels aus thierischen Abfällen
US3361616A (en) * 1963-12-20 1968-01-02 Walter G. Scharf Flecked metallized yarn
IT987956B (it) * 1973-05-23 1975-03-20 Pirelli Mezzo per la trasmissione di se gnali nei cavi di telecomunica zione
JPS5462285A (en) * 1977-10-28 1979-05-19 Bridgestone Corp Reinforcing material for rubber and its preparation
US4481055A (en) * 1981-11-19 1984-11-06 H. B. Fuller Company Method of forming reinforcing network
US4769202A (en) * 1985-11-29 1988-09-06 The B. F. Goodrich Company Process of making a conveyor belt
US4892772A (en) * 1988-11-14 1990-01-09 E. I. Dupont De Nemours And Company Fiber reinforced resin sheets
JPH02173125A (ja) * 1988-12-27 1990-07-04 Sumitomo Chem Co Ltd 繊維強化樹脂複合体プリプレグの製造方法

Also Published As

Publication number Publication date
US6814829B2 (en) 2004-11-09
WO2001036183A1 (en) 2001-05-25
US20030141010A1 (en) 2003-07-31
US6453962B1 (en) 2002-09-24
EP1233859A1 (de) 2002-08-28
EP1233859B1 (de) 2003-08-06
DE60004390D1 (de) 2003-09-11

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