ATE552099T1 - Verfahren zur herstellung gekrümmter verbundstofftragelemente - Google Patents

Verfahren zur herstellung gekrümmter verbundstofftragelemente

Info

Publication number
ATE552099T1
ATE552099T1 AT06769909T AT06769909T ATE552099T1 AT E552099 T1 ATE552099 T1 AT E552099T1 AT 06769909 T AT06769909 T AT 06769909T AT 06769909 T AT06769909 T AT 06769909T AT E552099 T1 ATE552099 T1 AT E552099T1
Authority
AT
Austria
Prior art keywords
ply
laying
web surface
composite
tape
Prior art date
Application number
AT06769909T
Other languages
English (en)
Inventor
Todd A Brown
Stephen Douglas Friddell
Christopher G Harris
Andrew E Modin
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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=36809431&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=ATE552099(T1) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Boeing Co filed Critical Boeing Co
Application granted granted Critical
Publication of ATE552099T1 publication Critical patent/ATE552099T1/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
    • B29C70/28—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
    • B29C70/342—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 isostatic pressure
    • 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
    • B32B38/00—Ancillary operations in connection with laminating processes
    • B32B38/18—Handling of layers or the laminate
    • B32B38/1808—Handling of layers or the laminate characterised by the laying up of the layers
    • 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
    • B29C43/00—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
    • B29C43/02—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of definite length, i.e. discrete articles
    • B29C43/10—Isostatic pressing, i.e. using non-rigid pressure-exerting members against rigid parts or dies
    • B29C43/12—Isostatic pressing, i.e. using non-rigid pressure-exerting members against rigid parts or dies using bags surrounding the moulding material or using membranes contacting the moulding material
    • 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
    • B29C70/38—Automated lay-up, e.g. using robots, laying filaments according to predetermined patterns
    • B29C70/382—Automated fiber placement [AFP]
    • 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
    • B29C70/38—Automated lay-up, e.g. using robots, laying filaments according to predetermined patterns
    • B29C70/386—Automated tape laying [ATL]
    • 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
    • B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
    • B29C70/545—Perforating, cutting or machining during or after moulding
    • 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
    • B32B38/00—Ancillary operations in connection with laminating processes
    • B32B38/0004—Cutting, tearing or severing, e.g. bursting; Cutter details
    • 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
    • B32B38/00—Ancillary operations in connection with laminating processes
    • B32B38/04—Punching, slitting or perforating
    • 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
    • B32B38/00—Ancillary operations in connection with laminating processes
    • B32B38/18—Handling of layers or the laminate
    • B32B38/1808—Handling of layers or the laminate characterised by the laying up of the layers
    • B32B38/1816—Cross feeding of one or more of the layers
    • 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
    • B32B38/00—Ancillary operations in connection with laminating processes
    • B32B38/18—Handling of layers or the laminate
    • B32B38/1858—Handling of layers or the laminate using vacuum
    • 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
    • B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/46—Shaping 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
    • B29C70/48—Shaping 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 and impregnating the reinforcements in the closed mould, e.g. resin transfer moulding [RTM], e.g. by vacuum
    • 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
    • B29K2063/00—Use of EP, i.e. epoxy resins 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
    • B29K2067/00—Use of polyesters 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
    • B29K2307/00—Use of elements other than metals as reinforcement
    • 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
    • B29K2309/00—Use of inorganic materials not provided for in groups B29K2303/00 - B29K2307/00, as reinforcement
    • B29K2309/10—Mica
    • 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
    • B29L2031/001—Profiled members, e.g. beams, sections
    • B29L2031/003—Profiled members, e.g. beams, sections having a profiled transverse cross-section
    • 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
    • B29L2031/3082—Fuselages
    • 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
    • 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
    • Y10T156/1051—Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina by folding
    • 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
    • Y10T156/1052—Methods of surface bonding and/or assembly therefor with cutting, punching, tearing or severing
    • Y10T156/1062—Prior to assembly
    • Y10T156/1067—Continuous longitudinal slitting
    • 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
    • Y10T156/1052—Methods of surface bonding and/or assembly therefor with cutting, punching, tearing or severing
    • Y10T156/1062—Prior to assembly
    • Y10T156/1075—Prior to assembly of plural laminae from single stock and assembling to each other or to additional lamina
    • 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
    • Y10T156/1052—Methods of surface bonding and/or assembly therefor with cutting, punching, tearing or severing
    • Y10T156/108—Flash, trim or excess removal

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Robotics (AREA)
  • Moulding By Coating Moulds (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
  • Shaping Of Tube Ends By Bending Or Straightening (AREA)
  • Forging (AREA)
AT06769909T 2005-05-03 2006-04-27 Verfahren zur herstellung gekrümmter verbundstofftragelemente ATE552099T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US11/119,756 US8632653B2 (en) 2005-05-03 2005-05-03 Method of manufacturing curved composite structural elements
PCT/US2006/016191 WO2006119002A2 (en) 2005-05-03 2006-04-27 Method of manufacturing curved composite structural elements

Publications (1)

Publication Number Publication Date
ATE552099T1 true ATE552099T1 (de) 2012-04-15

Family

ID=36809431

Family Applications (1)

Application Number Title Priority Date Filing Date
AT06769909T ATE552099T1 (de) 2005-05-03 2006-04-27 Verfahren zur herstellung gekrümmter verbundstofftragelemente

Country Status (6)

Country Link
US (2) US8632653B2 (de)
EP (1) EP1899146B1 (de)
JP (1) JP4986996B2 (de)
AT (1) ATE552099T1 (de)
ES (1) ES2381988T3 (de)
WO (1) WO2006119002A2 (de)

Families Citing this family (97)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7249943B2 (en) 2003-08-01 2007-07-31 Alliant Techsystems Inc. Apparatus for forming composite stiffeners and reinforcing structures
ATE457265T1 (de) * 2004-12-06 2010-02-15 Saab Ab Verfahren zur herstellung eines gekrümmten trägers aus verbundwerkstoff
US8632653B2 (en) 2005-05-03 2014-01-21 The Boeing Company Method of manufacturing curved composite structural elements
US7943076B1 (en) 2005-05-03 2011-05-17 The Boeing Company Method of manufacturing curved composite structural elements
US20070040350A1 (en) * 2005-08-19 2007-02-22 Wiswell John R Recumbent trike
ES2357841T3 (es) * 2005-10-17 2011-05-03 Saab Ab Procedimiento de fabricación para un objeto curvado de material compuesto y objeto curvado así obtenido.
ES2314581T3 (es) * 2005-12-20 2009-03-16 Saab Ab Elemento de rigidizacion y procedimiento de fabricacion de un elemento de rigidizacion.
US9102103B2 (en) * 2006-02-02 2015-08-11 The Boeing Company Thermoplastic composite parts having integrated metal fittings and method of making the same
US10449736B2 (en) 2006-02-02 2019-10-22 The Boeing Company Apparatus for fabricating thermoplastic composite parts
US8691137B2 (en) 2009-03-04 2014-04-08 The Boeing Company Method of molding partus using a tool sleeve for mold die
US8491745B2 (en) * 2007-02-03 2013-07-23 The Boeing Company Method and material efficient tooling for continuous compression molding
US10232532B1 (en) 2006-02-02 2019-03-19 The Boeing Company Method for fabricating tapered thermoplastic composite parts
US8333858B2 (en) 2006-02-02 2012-12-18 The Boeing Company Method for fabricating curved thermoplastic composite parts
US7807005B2 (en) * 2006-02-02 2010-10-05 The Boeing Company Fabrication process for thermoplastic composite parts
KR20090086955A (ko) * 2006-10-23 2009-08-14 꽁스트뤽시옹 엥뒤스뜨리엘 드 라 메디떼라네(쎄.엔.이.엠) 원통부 몰딩을 위한 복합도구
US7854874B2 (en) * 2006-11-20 2010-12-21 The Boeing Company Apparatus and methods for forming hat stiffened composite parts using thermally expansive tooling cauls
US8303757B2 (en) * 2006-12-04 2012-11-06 The Boeing Company Tensioning device for composite structures
EP1932652A1 (de) * 2006-12-11 2008-06-18 Saab Ab Verfahren und Vorrichtung zur Herstellung eines gekrümmten, länglichen Strukturelements
WO2009008903A1 (en) * 2007-01-12 2009-01-15 The Nordam Group, Inc. Aircraft window erosion shield
WO2008155504A2 (fr) * 2007-06-12 2008-12-24 Hexcel Reinforcements Procede de fabrication d ' un materiau composite dans lequel au moins un fil torsade est depose et materiau composite ainsi obtenu
ITTO20070557A1 (it) 2007-07-27 2009-01-28 Alenia Aeronautica Spa Procedimento di fabbricazione di un elemento curvo in materiale composito
US7968169B2 (en) * 2007-08-07 2011-06-28 The Boeing Company Compound contoured composite beams and fabrication methods
GB2452298B (en) * 2007-08-30 2010-01-13 Gkn Aerospace Services Ltd Composite structure
FR2920743B1 (fr) * 2007-09-07 2009-12-18 Airbus France Cadre de structure en materiau composite et fuselage d'aeronef comportant un tel cadre
US8048253B2 (en) * 2007-09-26 2011-11-01 Fiberforge Corporation System and method for the rapid, automated creation of advanced composite tailored blanks
US8632310B2 (en) * 2007-12-18 2014-01-21 Textron Innovations Inc. Rotor blade and method of making same
US8152948B2 (en) * 2008-01-09 2012-04-10 The Boeing Company Contoured composite parts
JP5429599B2 (ja) * 2008-12-24 2014-02-26 東レ株式会社 湾曲形状強化繊維積層体、プリフォーム、繊維強化樹脂複合材料の製造方法
CN101910493B (zh) 2008-01-11 2013-07-24 东丽株式会社 弯曲形状强化纤维基材、及使用其的层合体、预成型体、纤维强化树脂复合材料和它们的制造方法
US8349105B2 (en) * 2008-04-17 2013-01-08 The Boeing Company Curved composite frames and method of making the same
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
US9669579B2 (en) 2008-11-13 2017-06-06 The Boeing Company Aircraft skin attachment system
US20100116938A1 (en) * 2008-11-13 2010-05-13 Kline William T Method and apparatus for joining composite structural members and structural members made thereby
US9662841B2 (en) * 2009-11-10 2017-05-30 Orbital Atk, Inc. Radially extending composite structures
US8282757B2 (en) 2009-11-10 2012-10-09 Alliant Techsystems Inc. Automated composite annular structure forming
US8389424B2 (en) * 2009-11-11 2013-03-05 Albany Engineered Composites, Inc. Reinforcement for darted Pi preforms
US10821653B2 (en) * 2010-02-24 2020-11-03 Alexander M. Rubin Continuous molding of thermoplastic laminates
US9266279B2 (en) 2010-07-08 2016-02-23 Orbital Atk, Inc. Variable material stretch-forming apparatus and methods
US8795567B2 (en) 2010-09-23 2014-08-05 The Boeing Company Method for fabricating highly contoured composite stiffeners with reduced wrinkling
FR2965748B1 (fr) * 2010-10-06 2012-10-26 Coriolis Composites Attn Olivier Bouroullec Procede de fabrication de raidisseurs en materiau composite
GB2484476B (en) * 2010-10-11 2012-12-12 Gkn Aerospace Services Ltd Composite structure
US9387657B2 (en) 2010-11-12 2016-07-12 The Boeing Company Method of fabricating a curved composite structure using composite prepreg tape
US8551380B2 (en) 2010-11-12 2013-10-08 The Boeing Company Method of laying up prepreg plies on contoured tools using a deformable carrier film
US9701067B2 (en) 2010-11-12 2017-07-11 The Boeing Company Method of laying up prepreg plies on contoured tools using a deformable carrier film
CN102476455B (zh) * 2010-11-29 2015-07-08 上海杰事杰新材料(集团)股份有限公司 一种热塑性复合材料车门的制造方法
GB2486231B (en) * 2010-12-07 2013-04-03 Gkn Aerospace Services Ltd Composite structure
US10169492B2 (en) * 2011-06-20 2019-01-01 The Boeing Company Fiber placement optimization for steered-fiber plies
US9545757B1 (en) * 2012-02-08 2017-01-17 Textron Innovations, Inc. Composite lay up and method of forming
US8826957B2 (en) * 2012-08-31 2014-09-09 General Electric Company Methods and systems for automated ply layup for composites
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
WO2014082024A1 (en) 2012-11-26 2014-05-30 Ocv Intellectual Capital, Llc Multi-axial fabrics, polymer-fiber laminates, and bodies incorporating same for connecting applications
US9327470B1 (en) * 2012-12-05 2016-05-03 The Boeing Company Variable-radius laminated radius filler and system and method for manufacturing same
CN104903081B (zh) * 2013-01-07 2018-03-13 波音公司 使用复合预浸带制作弯曲复合结构的方法
US10828846B2 (en) 2013-01-07 2020-11-10 The Boeing Company Method and apparatus for fabricating contoured laminate structures
US9314974B2 (en) 2013-01-07 2016-04-19 The Boeing Company Method and apparatus for fabricating contoured laminate structures
DE112014000004A5 (de) 2013-03-12 2014-12-31 Dieffenbacher GmbH Maschinen- und Anlagenbau Verfahren und Systeme zur Herstellung fortschrittlicher Verbundbauteile
CN109940959A (zh) 2013-03-13 2019-06-28 帝斯曼知识产权资产管理有限公司 柔性复合材料体系和方法
CA2906068C (en) 2013-03-13 2021-11-09 Dsm Ip Assets B.V. Systems and method for producing three-dimensional articles from flexible composite materials
US9789662B2 (en) 2013-03-13 2017-10-17 Cubic Tech Corporation Engineered composite systems
DE102013213711A1 (de) 2013-07-12 2015-01-15 Brose Fahrzeugteile Gmbh & Co. Kommanditgesellschaft, Hallstadt Verfahren zur Herstellung eines Strukturbauteils für Kraftfahrzeuge aus einem Organoblech
US9579875B2 (en) 2014-02-04 2017-02-28 The Boeing Company Bonded tab and tooling device
US9782937B1 (en) 2014-05-16 2017-10-10 The Boeing Company Apparatus for forming contoured composite laminates
US10399284B2 (en) 2014-05-16 2019-09-03 The Boeing Company Method and apparatus for forming contoured composite laminates
US9630376B2 (en) * 2014-09-22 2017-04-25 The Boeing Company Composite filler
US9545759B2 (en) * 2015-01-30 2017-01-17 CGTech Automated fiber placement with course trajectory compensation
DE102015110195A1 (de) * 2015-06-24 2016-12-29 Airbus Operations Gmbh Vorrichtung und Verfahren zum Umformen eines Faserhalbzeugs
US10434726B1 (en) 2015-07-13 2019-10-08 The Boeing Company Forming thermoplastic composite parts having steered fiber orientations
US9809297B2 (en) * 2015-08-26 2017-11-07 The Boeing Company Structures containing stiffeners having transition portions
US10005267B1 (en) 2015-09-22 2018-06-26 Textron Innovations, Inc. Formation of complex composite structures using laminate templates
US10183735B2 (en) * 2016-02-01 2019-01-22 The Boeing Company Window frame assembly for aircraft
US11273622B2 (en) 2016-12-14 2022-03-15 The Boeing Company Stiffening elements that comprise integral current flowpaths
US11077644B2 (en) 2016-12-14 2021-08-03 The Boeing Company Material systems and methods of manufacturing material systems
US11014337B2 (en) 2016-12-14 2021-05-25 The Boeing Company Laminate structures comprising fiber-reinforced thermoplastic prepreg plies
US11254048B2 (en) * 2017-02-21 2022-02-22 Kansas State University Research Foundation Additive manufacturing of continuous fiber thermoplastic composites
EP3597412B1 (de) * 2017-03-17 2022-10-05 Subaru Corporation Formvorrichtung für fasermaterial und formverfahren für fasermaterial
US10746640B2 (en) 2017-03-21 2020-08-18 Textron Innovations Inc. Methods of making a tubular specimen with a predetermined wrinkle defect
US10744727B2 (en) 2017-03-21 2020-08-18 Textron Innovations Inc. Methods of making a specimen with a predetermined wrinkle defect
FR3081369B1 (fr) 2018-05-28 2020-05-08 Stelia Aerospace Dispositif et procede de mise en forme d'une piece d'ebauche pour la formation d'une piece thermoplastique structurelle
US10618210B2 (en) 2018-05-30 2020-04-14 Corning Incorporated High capacity print station, method of making a polymer composite part, and polymer composite part
US10933596B2 (en) * 2018-06-22 2021-03-02 Spirit Aerosystems, Inc. System and method for splicing plies in stringer sheets
US11014314B2 (en) 2018-06-28 2021-05-25 The Boeing Company End effector for forming prepreg plies on highly contoured surfaces
US20200086970A1 (en) * 2018-09-18 2020-03-19 The Boeing Company Composite fabric wing spar with interleaved tape cap plies
US11305498B2 (en) 2018-12-21 2022-04-19 The Boeing Company System and method for fabricating a composite ply layup
US11318689B2 (en) 2018-12-21 2022-05-03 The Boeing Company Ply transporting and compacting apparatus and method therefor
US11220074B2 (en) 2019-01-07 2022-01-11 Goodrich Corporation Reduced wrinkles in multi-section composite tank
US11511502B2 (en) * 2019-08-27 2022-11-29 Spirit Aerosystems, Inc. Method for securing core to tool during machining
EP3822068B1 (de) * 2019-11-13 2023-07-19 Airbus Operations, S.L.U. Vorrichtung und verfahren zur ausbildung eines verbundlaminats zur herstellung eines z-förmigen profils
WO2021171529A1 (ja) * 2020-02-28 2021-09-02 三菱重工業株式会社 積層体および積層方法
CN111483156B (zh) * 2020-04-08 2021-02-02 北京航天新风机械设备有限责任公司 一种复合材料大型薄壁含筋半罩铺层方法
US20220016856A1 (en) * 2020-07-16 2022-01-20 Honeywell Federal Manufacturing & Technologies, Llc Customized composite debulking caul
CN111844809B (zh) * 2020-08-17 2024-06-18 沈阳飞机工业（集团）有限公司 复合材料c型框辅助铺叠工具及其使用方法
CN112078148B (zh) * 2020-08-18 2022-03-04 武汉大学 一种应用于曲面的复合材料自动铺放装置
CN113478868B (zh) * 2021-05-25 2023-05-05 贵州石鑫玄武岩科技有限公司 一种层切式复合材料板簧生产装置
CN115107299B (zh) * 2022-07-05 2024-02-09 江西昌兴航空装备股份有限公司 一种垂尾整体梁铺贴方法
CN116782439B (zh) * 2023-08-23 2023-11-17 哈尔滨远驰航空装备有限公司 电加热复合材料结构及其成型方法

Family Cites Families (90)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB763972A (en) 1953-09-30 1956-12-19 Andre Rubber Co Improvements in or relating to flexible couplings for pipes
US3042562A (en) 1959-05-04 1962-07-03 Dow Chemical Co Product and method for production of articles having compound curves
US3259021A (en) 1961-05-05 1966-07-05 North American Aviation Inc Multiple purpose fabrication apparatus and method
US3556922A (en) * 1968-08-27 1971-01-19 Du Pont Fiber-resin composite of polyamide and inorganic fibers
US3775219A (en) * 1971-04-05 1973-11-27 Goldsworthy Eng Inc Composite-tape placement head
US4133711A (en) * 1977-07-11 1979-01-09 Grumman Aerospace Corporation Automated integrated composite lamination system
US4208238A (en) * 1977-07-11 1980-06-17 Grumman Aerospace Corporation Gantry for use in the manufacture of laminar structures
US4249704A (en) 1978-04-25 1981-02-10 Mitsubishi Denki Kabushiki Kaisha Automatic taping apparatus
US4305903A (en) * 1980-02-25 1981-12-15 Norris Industries, Inc. Composite fiber reinforced member and method
US4591402A (en) 1981-06-22 1986-05-27 Ltv Aerospace And Defense Company Apparatus and method for manufacturing composite structures
GB2101519B (en) 1981-06-22 1986-03-19 Vought Corp Apparatus for tape laying and manufacture of composite structures
DE3249987C2 (de) 1981-06-22 1995-08-17 Vought Aircraft Co Vorrichtung für die Herstellung eines Formteils
GB8305749D0 (en) * 1983-03-02 1983-04-07 British Aerospace Tape laying apparatus
US4588466A (en) * 1983-04-08 1986-05-13 Vektronics Manufacturing, Inc. Tape laying method and apparatus
US4576849A (en) 1983-06-06 1986-03-18 Hercules Incorporated Curved composite beam
US4461669A (en) * 1983-09-30 1984-07-24 The Boeing Company Pivotal mount for laminating head
US4475976A (en) * 1983-12-23 1984-10-09 The Boeing Company Method and apparatus for forming composite material articles
US4720255A (en) * 1984-06-28 1988-01-19 The Boeing Company Apparatus for planar forming of zero degree composite tape
US4726924A (en) 1984-06-28 1988-02-23 The Boeing Company Method of planar forming of zero degree composite tape
JPS61290038A (ja) * 1985-06-19 1986-12-20 Agency Of Ind Science & Technol Ｆｒｐテ−プの自動貼着方法および装置
US4696707A (en) * 1987-08-18 1987-09-29 The Ingersoll Milling Machine Company Composite tape placement apparatus with natural path generation means
FR2590069B1 (fr) 1985-11-14 1987-12-11 Alsthom Enrubanneuse pour l'enrubannage a chaud d'un conducteur electrique
US4955803A (en) * 1986-02-03 1990-09-11 The Board Of Trustees Of The Leland Stanford Junior University Apparatus for forming fiber composite materials
US4750965A (en) * 1986-03-28 1988-06-14 The Ingersoll Milling Machine Company Adaptive control for tape laying head having natural path generation
US4867834A (en) 1986-04-07 1989-09-19 Hercules Filament winding system
US4847063A (en) 1987-12-02 1989-07-11 Fiber Materials, Inc. Hollow composite body having an axis of symmetry
FR2635484B1 (fr) 1988-08-18 1991-04-05 Aerospatiale Procede et dispositifs de fabrication de pieces planes incurvees en materiau composite
US5358583A (en) * 1988-10-19 1994-10-25 E. I. Du Pont De Nemours And Company Apparatus and method for shaping fiber reinforced resin matrix materials and product thereof
US5038291A (en) * 1989-04-03 1991-08-06 General Electric Company Computerized ply pattern generation
US5338806A (en) * 1989-11-02 1994-08-16 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Tough, processable simultaneous semi-interpenetrating polyimides
US5431984A (en) 1990-12-11 1995-07-11 Avco Corporation Composite preforms with groves for fibers and groves for off-gassing
CA2057201C (en) * 1990-12-19 1998-05-19 Vernon M. Benson Multiple axes fiber placement machine
EP0496695A3 (en) 1991-01-15 1993-04-21 United Technologies Corporation A unitary, multi-legged helicopter rotor flexbeam made solely of composite materials and the method of manufacturing same
US5292475A (en) * 1992-03-06 1994-03-08 Northrop Corporation Tooling and process for variability reduction of composite structures
DE4208670C2 (de) * 1992-03-18 1995-02-02 Peguform Werke Gmbh Verfahren zur Herstellung von Trägern aus faserverstärkten Kunststoffen für Kraftfahrzeug-Stoßfänger sowie derartige Träger
US5242523A (en) 1992-05-14 1993-09-07 The Boeing Company Caul and method for bonding and curing intricate composite structures
US5431749A (en) * 1993-09-30 1995-07-11 The Ingersoll Milling Machine Company Tape laying head with curved tape laying capability and improved adaptive steering
US5538589A (en) * 1994-08-31 1996-07-23 The Boeing Company Composite stringer assembly machine
JPH08187788A (ja) * 1995-01-10 1996-07-23 Toray Ind Inc 円弧状ｆｒｐ体の製造方法および装置
US5648109A (en) * 1995-05-03 1997-07-15 Massachusetts Institute Of Technology Apparatus for diaphragm forming
FR2766407B1 (fr) 1997-07-22 1999-10-15 Aerospatiale Procede de fabrication de pieces de grandes dimensions en materiau composite a matrice thermoplastique, telles que des troncons de fuselage d'aeronefs
JP2001521839A (ja) 1997-11-05 2001-11-13 シコルスキー エアクラフト コーポレイション 繊維配置装置の供給制御システム
GB9828368D0 (en) 1998-12-22 1999-02-17 British Aerospace Forming reinforcing components
DE19909869C2 (de) 1999-03-08 2001-05-10 Daimler Chrysler Ag Verfahren zur Herstellung eines Verkleidungsteils
JP2001038752A (ja) * 1999-07-30 2001-02-13 Fuji Heavy Ind Ltd 複合材曲面パネルの成形装置及び成形方法
FR2808472B1 (fr) 2000-05-05 2003-02-28 Aerospatiale Matra Airbus Procede de fabrication d'un panneau en materiau composite a bandes raidisseurs et panneau ainsi obtenu
US6451152B1 (en) 2000-05-24 2002-09-17 The Boeing Company Method for heating and controlling temperature of composite material during automated placement
DE10031510A1 (de) 2000-06-28 2002-01-17 Airbus Gmbh Strukturbauteil für ein Flugzeug
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
WO2002042044A1 (de) 2000-11-21 2002-05-30 Eads Deutschland Gmbh Konfektionstechnisches verfahren, ein spannmodul und ein nähguthalter zur gestaltung von textilen vorformlingen zur herstellung von faserverstärkten kunststoff-bauteilen
US6723271B2 (en) 2001-04-16 2004-04-20 W. Scott Hemphill Method and apparatus for making composite parts
US6648273B2 (en) 2001-10-30 2003-11-18 The Boeing Company Light weight and high strength fuselage
EP1342554B1 (de) 2002-03-08 2010-02-03 Airbus Deutschland GmbH Verfahren zum Herstellen textiler Vorformlinge aus textilen Halbzeugen
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
US7014806B2 (en) * 2002-03-08 2006-03-21 Airbus Deutschland Gmbh Method for producing a three-dimensional fiber reinforced ring frame component
JP3999031B2 (ja) 2002-04-26 2007-10-31 東京特殊電線株式会社 角形断面マグネットワイヤの製造方法
ATE324249T1 (de) 2002-05-29 2006-05-15 Michelin Soc Tech Vorrichtung und verfahren zum aufbringen eines streifens auf eine rotierende oberfläche
US7138167B2 (en) * 2002-08-12 2006-11-21 Shikibo Ltd. Preform precursor for fiber-reinforced composite material, preform for fiber-reinforced composite material, and method of manufacturing the precursor and the preform
US7137182B2 (en) 2002-11-22 2006-11-21 The Boeing Company Parallel configuration composite material fabricator
JP4286563B2 (ja) 2003-03-14 2009-07-01 シキボウ株式会社 複合材料用ドライプリフォームとその製造方法および製造装置
US7384585B2 (en) * 2003-01-14 2008-06-10 Shikibo Ltd. Method for producing dry preform for composite material
FR2853914B1 (fr) 2003-04-17 2005-11-25 Hexcel Fabrics Procede et installation de fabrication d'une preforme de renfort
US7249943B2 (en) 2003-08-01 2007-07-31 Alliant Techsystems Inc. Apparatus for forming composite stiffeners and reinforcing structures
JP3742082B2 (ja) * 2003-08-08 2006-02-01 株式会社ジャムコ 曲率を有した繊維強化プラスチック部材の連続成形方法及び装置
US7527222B2 (en) * 2004-04-06 2009-05-05 The Boeing Company Composite barrel sections for aircraft fuselages and other structures, and methods and systems for manufacturing such barrel sections
US7134629B2 (en) * 2004-04-06 2006-11-14 The Boeing Company Structural panels for use in aircraft fuselages and other structures
JP2006056022A (ja) * 2004-08-17 2006-03-02 Murata Mach Ltd 湾曲したｆｒｐ桁材用の強化繊維プリフォームの製作方法
US7842145B2 (en) 2004-10-05 2010-11-30 The Boeing Company Method for laying composite tape
ATE457265T1 (de) 2004-12-06 2010-02-15 Saab Ab Verfahren zur herstellung eines gekrümmten trägers aus verbundwerkstoff
ES2267367B1 (es) 2004-12-30 2009-05-01 Airbus España S.L. Procedimiento y util para el encintado de moldes de piezas curvas.
EP1685947B1 (de) 2005-02-01 2011-04-13 Honda Motor Co., Ltd. Verfahren zur Herstellung faserverstärkter Verbundwerkstoffen
US8632653B2 (en) 2005-05-03 2014-01-21 The Boeing Company Method of manufacturing curved composite structural elements
US7943076B1 (en) 2005-05-03 2011-05-17 The Boeing Company Method of manufacturing curved composite structural elements
DE102005028765B4 (de) 2005-06-22 2016-01-21 Airbus Operations Gmbh Verfahren zur Herstellung eines Verstärkungsprofils
US7469735B2 (en) 2005-08-03 2008-12-30 The Boeing Corporation Composite structural element fabricating device and method
ATE405413T1 (de) * 2005-12-20 2008-09-15 Saab Ab Versteifungselement und verfahren zu dessen herstellung
ES2314581T3 (es) 2005-12-20 2009-03-16 Saab Ab Elemento de rigidizacion y procedimiento de fabricacion de un elemento de rigidizacion.
US7747421B2 (en) 2005-12-23 2010-06-29 The Boeing Company Head assignment modeling and simulation
WO2007074179A1 (es) 2005-12-29 2007-07-05 Airbus España, S.L. Procedimiento y útiles para la fabricación de cuadernas de material compuesto
US8333858B2 (en) 2006-02-02 2012-12-18 The Boeing Company Method for fabricating curved thermoplastic composite parts
US8163221B2 (en) 2006-03-08 2012-04-24 Toray Industries, Inc. Process for producing reinforcing fiber molding
US8449709B2 (en) 2007-05-25 2013-05-28 The Boeing Company Method of fabricating fiber reinforced composite structure having stepped surface
JP5278790B2 (ja) 2008-01-11 2013-09-04 東レ株式会社 繊維強化樹脂複合材料の製造方法および製造装置
JP5429599B2 (ja) 2008-12-24 2014-02-26 東レ株式会社 湾曲形状強化繊維積層体、プリフォーム、繊維強化樹脂複合材料の製造方法
CN101910493B (zh) 2008-01-11 2013-07-24 东丽株式会社 弯曲形状强化纤维基材、及使用其的层合体、预成型体、纤维强化树脂复合材料和它们的制造方法
US8932423B2 (en) 2008-04-17 2015-01-13 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
US9090028B2 (en) 2008-04-17 2015-07-28 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
US8709576B2 (en) 2008-11-21 2014-04-29 Airbus Operations (Sas) Curved structural part made of composite material and a process for manufacturing such a part

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US20140069576A1 (en) 2014-03-13
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WO2006119002A2 (en) 2006-11-09
US9630390B2 (en) 2017-04-25
EP1899146B1 (de) 2012-04-04
EP1899146A2 (de) 2008-03-19
US8632653B2 (en) 2014-01-21
HK1115098A1 (en) 2008-11-21
US20060249868A1 (en) 2006-11-09
JP2008540168A (ja) 2008-11-20
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