WO2006119002A3 - Method of manufacturing curved composite structural elements - Google Patents

Method of manufacturing curved composite structural elements Download PDF

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Publication number
WO2006119002A3
WO2006119002A3 PCT/US2006/016191 US2006016191W WO2006119002A3 WO 2006119002 A3 WO2006119002 A3 WO 2006119002A3 US 2006016191 W US2006016191 W US 2006016191W WO 2006119002 A3 WO2006119002 A3 WO 2006119002A3
Authority
WO
WIPO (PCT)
Prior art keywords
structural elements
composite structural
ply
curved composite
manufacturing curved
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.)
Ceased
Application number
PCT/US2006/016191
Other languages
French (fr)
Other versions
WO2006119002A2 (en
Inventor
Todd A Brown
Stephen Douglas Friddell
Christopher G Harris
Andrew E Modin
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.)
Boeing Co
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=WO2006119002(A3) "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
Priority to JP2008510069A priority Critical patent/JP4986996B2/en
Priority to ES06769909T priority patent/ES2381988T3/en
Priority to HK08110115.1A priority patent/HK1115098B/en
Priority to AT06769909T priority patent/ATE552099T1/en
Priority to EP06769909A priority patent/EP1899146B1/en
Publication of WO2006119002A2 publication Critical patent/WO2006119002A2/en
Publication of WO2006119002A3 publication Critical patent/WO2006119002A3/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • 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
    • 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
    • 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)
  • Shaping Of Tube Ends By Bending Or Straightening (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
  • Forging (AREA)

Abstract

A method of manufacturing curved composite structural elements can include fabricating a web ply (310) in a flat curve over a removable substrate and laying up the ply on a curved web surface of a manufacturing tool (200) . Additionally, a cap ply (402) can be laid up on one or both flange surfaces using composite tape. The structural element layup can then be inspected and any excess composite material can be trimmed away.
PCT/US2006/016191 2005-05-03 2006-04-27 Method of manufacturing curved composite structural elements Ceased WO2006119002A2 (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
JP2008510069A JP4986996B2 (en) 2005-05-03 2006-04-27 Method for manufacturing curved composite structural element
ES06769909T ES2381988T3 (en) 2005-05-03 2006-04-27 Manufacturing method of curved composite structural elements
HK08110115.1A HK1115098B (en) 2005-05-03 2006-04-27 Method of manufacturing curved composite structural elements
AT06769909T ATE552099T1 (en) 2005-05-03 2006-04-27 METHOD FOR PRODUCING CURVED COMPOSITE SUPPORT ELEMENTS
EP06769909A EP1899146B1 (en) 2005-05-03 2006-04-27 Method of manufacturing curved composite structural elements

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
US11/119,756 2005-05-03

Publications (2)

Publication Number Publication Date
WO2006119002A2 WO2006119002A2 (en) 2006-11-09
WO2006119002A3 true WO2006119002A3 (en) 2007-04-05

Family

ID=36809431

Family Applications (1)

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

Country Status (6)

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

Families Citing this family (98)

* 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
EP1666353B1 (en) * 2004-12-06 2010-02-10 Saab Ab Method for fabricating a curved beam from composite material
US7943076B1 (en) 2005-05-03 2011-05-17 The Boeing Company Method of manufacturing curved composite structural elements
US8632653B2 (en) 2005-05-03 2014-01-21 The Boeing Company Method of manufacturing curved composite structural elements
US20070040350A1 (en) * 2005-08-19 2007-02-22 Wiswell John R Recumbent trike
DE602005025490D1 (en) * 2005-10-17 2011-02-03 Saab Ab A method of making a curved composite article and article produced by this method
ES2314581T3 (en) * 2005-12-20 2009-03-16 Saab Ab RIGIDIZATION ELEMENT AND MANUFACTURING PROCEDURE OF A RIGIDIZATION ELEMENT.
US10449736B2 (en) 2006-02-02 2019-10-22 The Boeing Company Apparatus for fabricating thermoplastic composite parts
US8491745B2 (en) 2007-02-03 2013-07-23 The Boeing Company Method and material efficient tooling for continuous compression molding
US7807005B2 (en) * 2006-02-02 2010-10-05 The Boeing Company Fabrication process for 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
US8333858B2 (en) * 2006-02-02 2012-12-18 The Boeing Company Method for fabricating curved thermoplastic composite parts
US9102103B2 (en) * 2006-02-02 2015-08-11 The Boeing Company Thermoplastic composite parts having integrated metal fittings and method of making the same
US10232532B1 (en) 2006-02-02 2019-03-19 The Boeing Company Method for fabricating tapered thermoplastic composite parts
MX2009004253A (en) * 2006-10-23 2009-05-14 Mediterranee Const Ind Composite tool for moulding cylindrical parts.
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 (en) * 2006-12-11 2008-06-18 Saab Ab A method and apparatus for manufacturing a curved elongated structural element
US7988094B2 (en) * 2007-01-12 2011-08-02 Scott Ernest Ostrem Aircraft window erosion shield
CA2687830C (en) * 2007-06-12 2015-11-24 Hexcel Reinforcements Method for making composite parts having at least one curved area and resulting parts
ITTO20070557A1 (en) 2007-07-27 2009-01-28 Alenia Aeronautica Spa PROCESS OF MANUFACTURE OF A CURVED ELEMENT IN COMPOSITE MATERIAL
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 (en) * 2007-09-07 2009-12-18 Airbus France STRUCTURAL FRAMEWORK IN COMPOSITE MATERIAL AND AIRCRAFT FUSELAGE COMPRISING SUCH A FRAMEWORK
US8048253B2 (en) * 2007-09-26 2011-11-01 Fiberforge Corporation System and method for the rapid, automated creation of advanced composite tailored blanks
EP2222553B1 (en) * 2007-12-18 2013-09-11 Bell Helicopter Textron Inc. Rotor blade and method of making same
US8152948B2 (en) * 2008-01-09 2012-04-10 The Boeing Company Contoured composite parts
CN101910493B (en) 2008-01-11 2013-07-24 东丽株式会社 Reinforcing fiber base of curved shape, layered product employing the same, preform, fiber-reinforced resin composite material, and processes for producing these
JP5429599B2 (en) * 2008-12-24 2014-02-26 東レ株式会社 Curved reinforced fiber laminate, preform, and method for producing fiber reinforced resin composite material
US8349105B2 (en) * 2008-04-17 2013-01-08 The Boeing Company Curved composite frames and method of making the same
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
US20100116938A1 (en) * 2008-11-13 2010-05-13 Kline William T Method and apparatus for joining composite structural members and structural members made thereby
US9669579B2 (en) 2008-11-13 2017-06-06 The Boeing Company Aircraft skin attachment system
US8282757B2 (en) * 2009-11-10 2012-10-09 Alliant Techsystems Inc. Automated composite annular structure forming
US9662841B2 (en) * 2009-11-10 2017-05-30 Orbital Atk, Inc. Radially extending composite structures
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 (en) * 2010-10-06 2012-10-26 Coriolis Composites Attn Olivier Bouroullec PROCESS FOR MANUFACTURING STIFFENERS OF COMPOSITE MATERIAL
GB2484476B (en) * 2010-10-11 2012-12-12 Gkn Aerospace Services Ltd Composite structure
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
US9387657B2 (en) 2010-11-12 2016-07-12 The Boeing Company Method of fabricating a curved composite structure using composite prepreg tape
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 (en) * 2010-11-29 2015-07-08 上海杰事杰新材料(集团)股份有限公司 Manufacturing method of thermoplastic composite vehicle door
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
CN105102213B (en) * 2012-11-09 2018-08-10 帝斯曼知识产权资产管理有限公司 The system and method that three-dimensional article is prepared by flexible composite
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
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
RU2631296C2 (en) * 2013-01-07 2017-09-20 Зе Боинг Компани Method of manufacturing curvilinear composite construction using composite preliminary impregnated tape
WO2014140146A1 (en) 2013-03-12 2014-09-18 Dieffenbacher GmbH Maschinen- und Anlagenbau Method and systems for producing advanced composite components
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
KR20220021018A (en) 2013-03-13 2022-02-21 디에스엠 아이피 어셋츠 비.브이. Flexible composite systems and methods
US9789662B2 (en) 2013-03-13 2017-10-17 Cubic Tech Corporation Engineered composite systems
DE102013213711A1 (en) * 2013-07-12 2015-01-15 Brose Fahrzeugteile Gmbh & Co. Kommanditgesellschaft, Hallstadt Method for producing a structural component for motor vehicles from an organic sheet
US9579875B2 (en) 2014-02-04 2017-02-28 The Boeing Company Bonded tab and tooling device
US10399284B2 (en) 2014-05-16 2019-09-03 The Boeing Company Method and apparatus for forming contoured composite laminates
US9782937B1 (en) 2014-05-16 2017-10-10 The Boeing Company 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 (en) * 2015-06-24 2016-12-29 Airbus Operations Gmbh Apparatus and method for forming a semi-finished fiber product
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
US11077644B2 (en) 2016-12-14 2021-08-03 The Boeing Company Material systems and methods of manufacturing material systems
US11273622B2 (en) 2016-12-14 2022-03-15 The Boeing Company Stiffening elements that comprise integral current flowpaths
US11014337B2 (en) 2016-12-14 2021-05-25 The Boeing Company Laminate structures comprising fiber-reinforced thermoplastic prepreg plies
WO2018156511A1 (en) * 2017-02-21 2018-08-30 Kansas State University Research Foundation Additive manufacturing of continuous fiber thermoplastic composites
WO2018168202A1 (en) * 2017-03-17 2018-09-20 株式会社Subaru Shaping device for fiber material and shaping method for fiber material
US10744727B2 (en) 2017-03-21 2020-08-18 Textron Innovations Inc. Methods of making a specimen with a predetermined wrinkle defect
US10746640B2 (en) 2017-03-21 2020-08-18 Textron Innovations Inc. Methods of making a tubular specimen with a predetermined wrinkle defect
FR3081369B1 (en) 2018-05-28 2020-05-08 Stelia Aerospace DEVICE AND METHOD FOR SHAPING A BLANK PART FOR FORMING A STRUCTURAL THERMOPLASTIC PART
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
ES2958761T3 (en) * 2019-11-13 2024-02-14 Airbus Operations Slu Device and method of forming a composite laminate to obtain a Z-shaped profile
JP7404499B2 (en) 2020-02-28 2023-12-25 三菱重工業株式会社 Laminate and composite manufacturing method
CN111483156B (en) * 2020-04-08 2021-02-02 北京航天新风机械设备有限责任公司 Large thin-wall reinforced half-cover layering method for composite material
US20220016856A1 (en) * 2020-07-16 2022-01-20 Honeywell Federal Manufacturing & Technologies, Llc Customized composite debulking caul
CN111844809B (en) * 2020-08-17 2024-06-18 沈阳飞机工业(集团)有限公司 Composite material C-shaped frame auxiliary laying tool and application method thereof
CN112078148B (en) * 2020-08-18 2022-03-04 武汉大学 A composite material automatic laying device applied to curved surfaces
CN113478868B (en) * 2021-05-25 2023-05-05 贵州石鑫玄武岩科技有限公司 Layer-cutting type composite plate spring production device
CN115107299B (en) * 2022-07-05 2024-02-09 江西昌兴航空装备股份有限公司 Vertical-tail integral beam paving method
US12617162B2 (en) 2022-11-14 2026-05-05 Rohr, Inc. Forming thermoplastic structure stamping blank using automated fiber placement device
CN116782439B (en) * 2023-08-23 2023-11-17 哈尔滨远驰航空装备有限公司 Electric heating composite material structure and forming method thereof

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4696707A (en) * 1987-08-18 1987-09-29 The Ingersoll Milling Machine Company Composite tape placement apparatus with natural path generation means
US4720255A (en) * 1984-06-28 1988-01-19 The Boeing Company Apparatus for planar forming of zero degree composite tape
FR2635484A1 (en) * 1988-08-18 1990-02-23 Aerospatiale Method and devices for manufacturing curved plane components made of composite material
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
US20030173019A1 (en) * 2002-03-08 2003-09-18 Ulrich Eberth Method of producing textile preforms for fiber reinforced composite products from textile semi-finished articles
WO2003099545A1 (en) * 2002-05-29 2003-12-04 Societe De Technologie Michelin Device and method for applying a strip to a rotary surface
US20050067731A1 (en) * 2003-04-17 2005-03-31 Alain Bruyere Process and system for fabricating a reinforcing preform

Family Cites Families (83)

* 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
US4208238A (en) * 1977-07-11 1980-06-17 Grumman Aerospace Corporation Gantry for use in the manufacture of laminar structures
US4133711A (en) * 1977-07-11 1979-01-09 Grumman Aerospace Corporation Automated integrated composite lamination system
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
DE3249987C2 (en) 1981-06-22 1995-08-17 Vought Aircraft Co Appts. for mfg. composite by laying fibre resin tape on mould
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
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
US4726924A (en) 1984-06-28 1988-02-23 The Boeing Company Method of planar forming of zero degree composite tape
JPS61290038A (en) * 1985-06-19 1986-12-20 Agency Of Ind Science & Technol Automatic sticking method for for tape and its device
FR2590069B1 (en) 1985-11-14 1987-12-11 Alsthom WRAPPER FOR HOT WRAPPING OF AN ELECTRIC CONDUCTOR
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
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 (en) * 1992-03-18 1995-02-02 Peguform Werke Gmbh Process for the production of supports made of fiber-reinforced plastics for motor vehicle bumpers and such supports
US5242523A (en) 1992-05-14 1993-09-07 The Boeing Company Caul and method for bonding and curing intricate composite structures
US5538589A (en) * 1994-08-31 1996-07-23 The Boeing Company Composite stringer assembly machine
JPH08187788A (en) * 1995-01-10 1996-07-23 Toray Ind Inc Method and apparatus for manufacturing arc-shaped FRP body
US5648109A (en) * 1995-05-03 1997-07-15 Massachusetts Institute Of Technology Apparatus for diaphragm forming
FR2766407B1 (en) 1997-07-22 1999-10-15 Aerospatiale PROCESS FOR MANUFACTURING LARGE-DIMENSIONAL PARTS IN COMPOSITE MATERIAL WITH A THERMOPLASTIC MATRIX, SUCH AS FUSELAGE TRUNKS OF AIRCRAFT
WO1999022932A1 (en) 1997-11-05 1999-05-14 Sikorsky Aircraft Corporation Feed control system for fiber placement machines
GB9828368D0 (en) 1998-12-22 1999-02-17 British Aerospace Forming reinforcing components
DE19909869C2 (en) 1999-03-08 2001-05-10 Daimler Chrysler Ag Method of manufacturing a trim part
JP2001038752A (en) * 1999-07-30 2001-02-13 Fuji Heavy Ind Ltd Apparatus and method for forming composite curved panel
FR2808472B1 (en) 2000-05-05 2003-02-28 Aerospatiale Matra Airbus METHOD FOR MANUFACTURING A PANEL OF COMPOSITE MATERIAL WITH STRAINER BANDS AND A PANEL THUS OBTAINED
US6451152B1 (en) 2000-05-24 2002-09-17 The Boeing Company Method for heating and controlling temperature of composite material during automated placement
DE10031510A1 (en) 2000-06-28 2002-01-17 Airbus Gmbh Structural component for an aircraft
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
US7056402B2 (en) 2000-11-21 2006-06-06 Eads Deutschland Gmbh Technical production method, tension module and sewing material holder for creating textile preforms for the production of fibre-reinforced plastic components
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
EP1342553B1 (en) 2002-03-08 2016-05-18 Airbus Operations GmbH Process for producing a fiber reinforced composite windowframe for airplanes and apparatus to implement the method
US7014806B2 (en) * 2002-03-08 2006-03-21 Airbus Deutschland Gmbh Method for producing a three-dimensional fiber reinforced ring frame component
JP3999031B2 (en) 2002-04-26 2007-10-31 東京特殊電線株式会社 Manufacturing method of square cross-section magnet wire
WO2004016844A1 (en) * 2002-08-12 2004-02-26 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
US7384585B2 (en) * 2003-01-14 2008-06-10 Shikibo Ltd. Method for producing dry preform for composite material
JP4286563B2 (en) 2003-03-14 2009-07-01 シキボウ株式会社 Dry preform for composite material, its manufacturing method and manufacturing apparatus
US7249943B2 (en) 2003-08-01 2007-07-31 Alliant Techsystems Inc. Apparatus for forming composite stiffeners and reinforcing structures
JP3742082B2 (en) * 2003-08-08 2006-02-01 株式会社ジャムコ Method and apparatus for continuously forming fiber-reinforced plastic member having curvature
US7134629B2 (en) * 2004-04-06 2006-11-14 The Boeing Company Structural panels for use in aircraft fuselages and other structures
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
JP2006056022A (en) * 2004-08-17 2006-03-02 Murata Mach Ltd Manufacturing method of reinforcing fiber preform for curved FRP girders
US7842145B2 (en) 2004-10-05 2010-11-30 The Boeing Company Method for laying composite tape
EP1666353B1 (en) 2004-12-06 2010-02-10 Saab Ab Method for fabricating a curved beam from composite material
ES2267367B1 (en) 2004-12-30 2009-05-01 Airbus España S.L. PROCEDURE AND USEFUL FOR THE WRAPPING OF CURVED PARTS MOLDS.
DE602005027434D1 (en) 2005-02-01 2011-05-26 Honda Motor Co Ltd Process for producing fiber-reinforced composite materials
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 (en) 2005-06-22 2016-01-21 Airbus Operations Gmbh Method for producing a reinforcing profile
US7469735B2 (en) 2005-08-03 2008-12-30 The Boeing Corporation Composite structural element fabricating device and method
ES2314581T3 (en) 2005-12-20 2009-03-16 Saab Ab RIGIDIZATION ELEMENT AND MANUFACTURING PROCEDURE OF A RIGIDIZATION ELEMENT.
ES2311937T3 (en) * 2005-12-20 2009-02-16 Saab Ab RIGIDIZATION ELEMENT AND PROCEDURE FOR THE MANUFACTURE OF RIGIDIZATION ELEMENT.
US7747421B2 (en) 2005-12-23 2010-06-29 The Boeing Company Head assignment modeling and simulation
ES2560660T3 (en) 2005-12-29 2016-02-22 Airbus Operations S.L. Procedure and tools for the manufacture of composite frames
US8333858B2 (en) 2006-02-02 2012-12-18 The Boeing Company Method for fabricating curved thermoplastic composite parts
WO2007102573A1 (en) 2006-03-08 2007-09-13 Toray Industries, Inc. Process, and apparatus, 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
CN101910493B (en) 2008-01-11 2013-07-24 东丽株式会社 Reinforcing fiber base of curved shape, layered product employing the same, preform, fiber-reinforced resin composite material, and processes for producing these
JP5429599B2 (en) 2008-12-24 2014-02-26 東レ株式会社 Curved reinforced fiber laminate, preform, and method for producing fiber reinforced resin composite material
JP5278790B2 (en) 2008-01-11 2013-09-04 東レ株式会社 Manufacturing method and manufacturing apparatus for fiber reinforced resin composite material
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
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

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4720255A (en) * 1984-06-28 1988-01-19 The Boeing Company Apparatus for planar forming of zero degree composite tape
US4696707A (en) * 1987-08-18 1987-09-29 The Ingersoll Milling Machine Company Composite tape placement apparatus with natural path generation means
FR2635484A1 (en) * 1988-08-18 1990-02-23 Aerospatiale Method and devices for manufacturing curved plane components made of composite material
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
US20030173019A1 (en) * 2002-03-08 2003-09-18 Ulrich Eberth Method of producing textile preforms for fiber reinforced composite products from textile semi-finished articles
WO2003099545A1 (en) * 2002-05-29 2003-12-04 Societe De Technologie Michelin Device and method for applying a strip to a rotary surface
US20050067731A1 (en) * 2003-04-17 2005-03-31 Alain Bruyere Process and system for fabricating a reinforcing preform

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