PT1995046T - Método para fabricar uma estrutura composta de fibra reforçada possuindo uma superfície gradual e a estrutura obtida por esse meio - Google Patents

Método para fabricar uma estrutura composta de fibra reforçada possuindo uma superfície gradual e a estrutura obtida por esse meio

Info

Publication number
PT1995046T
PT1995046T PT81568545T PT08156854T PT1995046T PT 1995046 T PT1995046 T PT 1995046T PT 81568545 T PT81568545 T PT 81568545T PT 08156854 T PT08156854 T PT 08156854T PT 1995046 T PT1995046 T PT 1995046T
Authority
PT
Portugal
Prior art keywords
fiber reinforced
reinforced composite
stepped surface
fabricating fiber
composite structure
Prior art date
Application number
PT81568545T
Other languages
English (en)
Inventor
Modin Andrew
D Hawkins Robert
A Woods Jack
Original Assignee
Boeing Co
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 Boeing Co filed Critical Boeing Co
Publication of PT1995046T publication Critical patent/PT1995046T/pt

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B38/00Ancillary operations in connection with laminating processes
    • B32B38/0004Cutting, tearing or severing, e.g. bursting; Cutter details
    • 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
    • B29C70/30Shaping 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
    • B29C70/34Shaping 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
    • 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
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00Layered 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
    • B32B5/02Layered 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 structural features of a fibrous or filamentary layer
    • B32B5/12Layered 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 structural features of a fibrous or filamentary layer characterised by the relative arrangement of fibres or filaments of different layers, e.g. the fibres or filaments being parallel or perpendicular to each other
    • 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
    • B29C70/16Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
    • B29C70/20Fibrous 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
    • B29C70/202Fibrous 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 arranged in parallel planes or structures of fibres crossing at substantial angles, e.g. cross-moulding compound [XMC]
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00Other particular articles
    • B29L2031/001Profiled members, e.g. beams, sections
    • B29L2031/003Profiled members, e.g. beams, sections having a profiled transverse cross-section
    • B29L2031/005Profiled members, e.g. beams, sections having a profiled transverse cross-section for making window frames
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00Other particular articles
    • B29L2031/30Vehicles, e.g. ships or aircraft, or body parts thereof
    • B29L2031/3076Aircrafts
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/14Windows; Doors; Hatch covers or access panels; Surrounding frame structures; Canopies; Windscreens accessories therefor, e.g. pressure sensors, water deflectors, hinges, seals, handles, latches, windscreen wipers
    • B64C1/1476Canopies; Windscreens or similar transparent elements
    • B64C1/1492Structure and mounting of the transparent elements in the window or windscreen
    • 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/40Weight reduction
    • 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
    • Y10T156/1026Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina with slitting or removal of material at reshaping area prior to reshaping
    • 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
    • Y10T156/1028Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina by bending, drawing or stretch forming sheet to assume shape of configured lamina while in contact therewith
    • 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
    • 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
    • Y10T156/1056Perforating lamina
    • Y10T156/1057Subsequent to assembly of laminae
    • 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
    • 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
    • Y10T156/1082Partial cutting bonded sandwich [e.g., grooving or incising]
    • 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
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/24Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24058Structurally defined web or sheet [e.g., overall dimension, etc.] including grain, strips, or filamentary elements in respective layers or components in angular relation
    • Y10T428/24124Fibers
    • 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
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/24Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24628Nonplanar uniform thickness material

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Composite Materials (AREA)
  • Mechanical Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
PT81568545T 2007-05-25 2008-05-23 Método para fabricar uma estrutura composta de fibra reforçada possuindo uma superfície gradual e a estrutura obtida por esse meio PT1995046T (pt)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US11/753,849 US8449709B2 (en) 2007-05-25 2007-05-25 Method of fabricating fiber reinforced composite structure having stepped surface

Publications (1)

Publication Number Publication Date
PT1995046T true PT1995046T (pt) 2019-10-18

Family

ID=39764965

Family Applications (1)

Application Number Title Priority Date Filing Date
PT81568545T PT1995046T (pt) 2007-05-25 2008-05-23 Método para fabricar uma estrutura composta de fibra reforçada possuindo uma superfície gradual e a estrutura obtida por esse meio

Country Status (4)

Country Link
US (3) US8449709B2 (pt)
EP (1) EP1995046B1 (pt)
ES (1) ES2757568T3 (pt)
PT (1) PT1995046T (pt)

Families Citing this family (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9586699B1 (en) 1999-08-16 2017-03-07 Smart Drilling And Completion, Inc. Methods and apparatus for monitoring and fixing holes in composite aircraft
US9625361B1 (en) 2001-08-19 2017-04-18 Smart Drilling And Completion, Inc. Methods and apparatus to prevent failures of fiber-reinforced composite materials under compressive stresses caused by fluids and gases invading microfractures in the materials
US8632653B2 (en) 2005-05-03 2014-01-21 The Boeing Company Method of manufacturing curved composite structural elements
US8449709B2 (en) 2007-05-25 2013-05-28 The Boeing Company Method of fabricating fiber reinforced composite structure having stepped surface
US9278484B2 (en) 2008-04-17 2016-03-08 The Boeing Company Method and apparatus for producing contoured composite structures and structures produced thereby
US8932423B2 (en) 2008-04-17 2015-01-13 The Boeing Company Method 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
EP2349686B1 (en) * 2008-11-13 2018-08-08 Saab AB Method of forming a composite article
US9662841B2 (en) * 2009-11-10 2017-05-30 Orbital Atk, Inc. Radially extending composite structures
US10357901B2 (en) * 2010-07-08 2019-07-23 Acushnet Company Golf club head having multi-material face and method of manufacture
US10143898B2 (en) 2010-07-08 2018-12-04 Acushnet Company Golf club head having a multi-material face
US11186016B2 (en) 2010-07-08 2021-11-30 Acushnet Company Golf club head having multi-material face and method of manufacture
DE102010048365B4 (de) * 2010-10-13 2012-08-23 Airbus Operations Gmbh Flächengebilde und Flugzeugrumpf mit einem derartigen Flächengebilde
CA2825057A1 (en) * 2011-01-21 2012-07-26 Saab Ab A composite article and a method of forming a composite article
US8616500B2 (en) * 2011-03-04 2013-12-31 The Boeing Company Diamond shaped window for composite and/or metallic airframe
US8944381B2 (en) 2011-03-25 2015-02-03 The Boeing Company Aircraft window and installation method
US9221533B1 (en) * 2011-10-24 2015-12-29 The Boeing Company Removable window system for space vehicles
US20130231902A1 (en) * 2012-03-05 2013-09-05 Siemens Product Lifecycle Management Software Inc. Spine-based rosette and simulation in fiber-composite materials
US9162396B2 (en) * 2012-10-12 2015-10-20 The Boeing Company Method for forming fuselage stringers
DE102014100630B4 (de) * 2014-01-21 2017-05-04 Deutsches Zentrum für Luft- und Raumfahrt e.V. Herstellung eines Faserverbundbauteils
US9895848B2 (en) * 2015-04-22 2018-02-20 The Boeing Company Systems and tooling for manufacturing composite parts and related methods
US10183735B2 (en) * 2016-02-01 2019-01-22 The Boeing Company Window frame assembly for aircraft
FR3080323B1 (fr) * 2018-04-19 2021-05-14 Airbus Operations Sas Procede de fabrication d'une piece en materiau composite comprenant au moins une decoupe et piece en materiau composite ainsi obtenue
CN109533272A (zh) * 2018-11-23 2019-03-29 江苏恒神股份有限公司 一种碳纤维复合材料飞机窗框及其制造方法
CN109866912A (zh) * 2019-03-22 2019-06-11 宁波慈星股份有限公司 一种复合纤维飞机窗框及其成型方法
US11952099B2 (en) * 2021-07-07 2024-04-09 The Boeing Company Aircraft window assemblies and related methods
US11491377B1 (en) 2021-12-28 2022-11-08 Acushnet Company Golf club head having multi-layered striking face
US11850461B2 (en) 2022-03-11 2023-12-26 Acushnet Company Golf club head having supported striking face
FR3143542A1 (fr) * 2022-12-15 2024-06-21 Airbus Operations (S.A.S.) Procédé de fabrication d’un cadre de hublot d’aéronef comportant une couche barrière, cadre de hublot obtenu à partir de ce procédé et aéronef comprenant au moins un tel cadre de hublot

Family Cites Families (61)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2478166A (en) 1941-08-25 1949-08-02 Mini Of Supply Process for removing carbon monoxide from air and gas mask canister therefor
US2478165A (en) * 1946-05-24 1949-08-02 Owens Corning Fiberglass Corp Low-pressure molding apparatus
US2495640A (en) * 1946-05-31 1950-01-24 Method of molding
US3356781A (en) * 1963-10-03 1967-12-05 Johns Manville Method of transfer molding
EP0089337B1 (en) 1981-09-30 1987-08-12 The Boeing Company Composite structures window belt and method of making
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
US4622091A (en) * 1984-11-29 1986-11-11 The Boeing Company Resin film infusion process and apparatus
US4741943A (en) * 1985-12-30 1988-05-03 The Boeing Company Aerodynamic structures of composite construction
DE3620192A1 (de) 1986-06-16 1987-12-17 Albert Weiss Verfahren und vorrichtung zur herstellung eines rahmens
US5236321A (en) * 1988-04-05 1993-08-17 Newton John R Mold for molding a fiber reinforced article
US4902215A (en) * 1988-06-08 1990-02-20 Seemann Iii William H Plastic transfer molding techniques for the production of fiber reinforced plastic structures
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
US4942013A (en) * 1989-03-27 1990-07-17 Mcdonnell Douglas Corporation Vacuum resin impregnation process
ES2089139T3 (es) 1991-08-01 1996-10-01 Scrimp Systems Llc Metodo y aparato de conformacion al vacio de materiales compuestos de resina reforzados con fibra.
US5281388A (en) * 1992-03-20 1994-01-25 Mcdonnell Douglas Corporation Resin impregnation process for producing a resin-fiber composite
US5322665A (en) * 1992-04-15 1994-06-21 The Charles Stark Draper Laboratories, Inc. Disposable self contained cartridge or resin transfer molding and resin transfer molding method
US5443912A (en) * 1993-11-24 1995-08-22 Sierracin Corporation Laminated environmental protection layer for acrylic aircraft windows
US5441692A (en) * 1994-02-14 1995-08-15 Thermal Equipment Corporation Process and apparatus for autoclave resin transfer molding
US5518385A (en) * 1994-11-09 1996-05-21 United Technologies Corporation Apparatus for resin transfer molding
US5728755A (en) * 1995-09-22 1998-03-17 Minnesota Mining And Manufacturing Company Curable epoxy resin compositions with 9,9'-bis(4-aminophenyl)fluorenes as curatives
US5576030A (en) * 1995-10-02 1996-11-19 Lockheed Corporation Apparatus for fabricating composite parts
DE19650416B4 (de) * 1996-12-05 2004-10-07 Airbus Deutschland Gmbh Fenster für ein Flugzeug mit einer Druckkabine
DE19813104A1 (de) 1998-03-25 1999-09-30 Daimler Chrysler Ag Verfahren zur Herstellung von Faserverbundbauteilen
US6482497B1 (en) * 1998-11-30 2002-11-19 Rocky Mountain Composites Inc. Pressure-cycled, packet-transfer infusion of resin-stitched preforms
DE19915083C1 (de) * 1999-04-01 2000-04-13 Daimler Chrysler Ag Verfahren zur Herstellung faserverstärkter Kunststoffbauteile mit nicht-vollständig abwickelbarer Geometrie
DE19944164C2 (de) * 1999-09-15 2001-10-04 Inst Verbundwerkstoffe Gmbh Herstellung von mehreren Bauteilen aus kontinuierlich faserverstärkten Kunststoffplatinen in Formnestern
DE60018455T3 (de) * 1999-12-07 2009-02-19 The Boeing Company, Seattle Doppelfolien vakuuminjektionsverfahren zur herstellung eines verbundwerkstoffes und damit hergestellter verbundwerkstoff
DE10013409C1 (de) * 2000-03-17 2000-11-23 Daimler Chrysler Ag Verfahren und Vorrichtung zur Herstellung von faserverstärkten Bauteilen mittels eines Injektionsverfahrens
US6454893B1 (en) * 2000-08-24 2002-09-24 Lockheed Martin Corporation Method of shaping continuous fiber lamina to an undulated surface by cutting individual fibers
US7060156B2 (en) * 2001-07-23 2006-06-13 Vrac, Llc Three-dimensional spacer fabric resin interlaminar infusion media process and vacuum-induced reinforcing composite laminate structures
WO2003047830A1 (fr) * 2001-12-06 2003-06-12 Toray Industries, Inc. Materiau composite a fibres et son procede de production
FR2834726B1 (fr) * 2002-01-16 2004-06-04 Saint Gobain Vetrotex Structure fibreuse pour la realisation de materiaux composites
US7014806B2 (en) * 2002-03-08 2006-03-21 Airbus Deutschland Gmbh Method for producing a three-dimensional fiber reinforced ring frame component
EP1342553B1 (de) * 2002-03-08 2016-05-18 Airbus Operations GmbH Verfahren zum Herstellen eines Fensterrahmens für Flugzeuge aus faserverstärktem Kunststoff und Vorrichtung zur Durchführung des Verfahrens
EP1507647B1 (en) 2002-05-29 2012-09-12 The Boeing Company Controlled atmospheric pressure resin infusion process
WO2004016844A1 (ja) * 2002-08-12 2004-02-26 Shikibo Ltd. 繊維強化複合材料用プリフォーム前駆体、繊維強化複合材料用プリフォームおよびその製造方法
GB0229094D0 (en) * 2002-12-13 2003-01-15 Hexcel Composites Ltd Improvements in or relating to the preparation of fibre-reinforced composites
US6915988B2 (en) * 2003-01-27 2005-07-12 Msa Aircraft Products, Ltd. Matrix window
WO2004076216A2 (en) * 2003-02-27 2004-09-10 Sierracin/Sylmar Corporation Window frame/seal assembly and method of forming the same
KR20050106493A (ko) 2003-03-13 2005-11-09 도호 테낙구스 가부시키가이샤 수지 트랜스퍼 성형법
EP1473131A3 (de) * 2003-04-30 2007-01-03 Airbus Deutschland GmbH Verfahren zum herstellen textiler vorformlinge aus textilen halbzeugen
US20040219855A1 (en) * 2003-05-02 2004-11-04 Tsotsis Thomas K. Highly porous interlayers to toughen liquid-molded fabric-based composites
US7008555B2 (en) * 2003-05-22 2006-03-07 Applied Poleramic Inc. Epoxy resin curing agents and epoxy resin compositions
PT1646813E (pt) * 2003-07-23 2013-07-09 Ppg Ind Ohio Inc Vedante compósito e conjunto de janela
US7300693B2 (en) * 2003-09-04 2007-11-27 The Boeing Company Resin infused transparent skin panel and method of making same
US7028950B2 (en) * 2004-05-10 2006-04-18 The Boeing Company Load bearing window
DE102004025381B4 (de) 2004-05-24 2014-01-23 Airbus Operations Gmbh Fensterrahmen für Flugzeuge
DE102004025377B4 (de) * 2004-05-24 2013-02-14 Airbus Operations Gmbh Fensterrahmen für Flugzeuge
DE102004025378B4 (de) * 2004-05-24 2011-01-13 Airbus Operations Gmbh Fensterrahmen für Flugzeuge
US7802413B2 (en) * 2004-10-04 2010-09-28 The Boeing Company Apparatus and methods for reinforcing a structural panel
US7469735B2 (en) * 2005-08-03 2008-12-30 The Boeing Corporation Composite structural element fabricating device and method
ATE492392T1 (de) * 2005-10-17 2011-01-15 Saab Ab Verfahren zur herstellung eines gekrümmten gegenstands aus verbundwerkstoff sowie durch dieses verfahren hergestellter gegenstand
US8066503B2 (en) * 2005-10-25 2011-11-29 The Boeing Company Controlled delta pressure bulk resin infusion system
US7281686B2 (en) * 2005-11-02 2007-10-16 The Boeing Company Window assembly for aircraft fuselage
US20070100565A1 (en) * 2005-11-03 2007-05-03 The Boeing Company System and Computer Program Product for Analyzing and Manufacturing a Structural Member Having a Predetermined Load Capacity
US7633040B2 (en) * 2005-11-14 2009-12-15 The Boeing Company Bulk resin infusion system apparatus and method
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
US20080078876A1 (en) 2006-08-15 2008-04-03 Baggette Phillip D Composite resin window frame constructions for airplanes
US8123168B2 (en) * 2006-08-24 2012-02-28 The Boeing Company Window assembly and method for a mobile platform
US7988094B2 (en) * 2007-01-12 2011-08-02 Scott Ernest Ostrem Aircraft window erosion shield
US8449709B2 (en) 2007-05-25 2013-05-28 The Boeing Company Method of fabricating fiber reinforced composite structure having stepped surface

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US20130236685A1 (en) 2013-09-12
US20150231834A1 (en) 2015-08-20
EP1995046B1 (en) 2019-08-21
EP1995046A3 (en) 2016-01-27
EP1995046A2 (en) 2008-11-26
US9770872B2 (en) 2017-09-26
ES2757568T3 (es) 2020-04-29
US8449709B2 (en) 2013-05-28
US9056448B2 (en) 2015-06-16
US20080289747A1 (en) 2008-11-27

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