ATE544580T1 - Verfahren zur minimierung von faserverzerrung während der herstellung einteiliger verbundzylinderteile - Google Patents

Verfahren zur minimierung von faserverzerrung während der herstellung einteiliger verbundzylinderteile

Info

Publication number
ATE544580T1
ATE544580T1 AT07874363T AT07874363T ATE544580T1 AT E544580 T1 ATE544580 T1 AT E544580T1 AT 07874363 T AT07874363 T AT 07874363T AT 07874363 T AT07874363 T AT 07874363T AT E544580 T1 ATE544580 T1 AT E544580T1
Authority
AT
Austria
Prior art keywords
mandrel
fiber distortion
thermal expansion
production
piece composite
Prior art date
Application number
AT07874363T
Other languages
English (en)
Inventor
William H Ingram Jr
Kenneth Dull
Robert Biornstad
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
Application granted granted Critical
Publication of ATE544580T1 publication Critical patent/ATE544580T1/de

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping 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
    • B29C70/32Shaping 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 on a rotating mould, former or core
    • 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
    • B29C53/00Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
    • B29C53/56Winding and joining, e.g. winding spirally
    • B29C53/58Winding and joining, e.g. winding spirally helically
    • B29C53/583Winding and joining, e.g. winding spirally helically for making tubular articles with particular features
    • B29C53/587Winding and joining, e.g. winding spirally helically for making tubular articles with particular features having a non-uniform wall-structure, e.g. with inserts, perforations, locally concentrated reinforcements
    • 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
    • B29C70/38Automated lay-up, e.g. using robots, laying filaments according to predetermined patterns
    • B29C70/382Automated fiber placement [AFP]
    • 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
    • B29C53/00Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
    • B29C53/56Winding and joining, e.g. winding spirally
    • B29C53/58Winding and joining, e.g. winding spirally helically
    • B29C53/60Winding and joining, e.g. winding spirally helically using internal forming surfaces, e.g. mandrels
    • B29C53/62Winding and joining, e.g. winding spirally helically using internal forming surfaces, e.g. mandrels rotatable about the winding axis
    • B29C53/66Winding and joining, e.g. winding spirally helically using internal forming surfaces, e.g. mandrels rotatable about the winding axis with axially movable winding feed member, e.g. lathe type winding
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/40Shaping or impregnating by compression not applied
    • B29C70/42Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/44Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING 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
    • B29K2063/00Use of EP, i.e. epoxy resins or derivatives thereof, as moulding material
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING 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
    • B29K2077/00Use of PA, i.e. polyamides, e.g. polyesteramides or derivatives thereof, as moulding material
    • B29K2077/10Aromatic polyamides [polyaramides] or derivatives thereof
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING 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
    • B29K2079/00Use of polymers having nitrogen, with or without oxygen or carbon only, in the main chain, not provided for in groups B29K2061/00 - B29K2077/00, as moulding material
    • B29K2079/08PI, i.e. polyimides or derivatives thereof
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING 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
    • B29K2105/00Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/24Condition, form or state of moulded material or of the material to be shaped crosslinked or vulcanised
    • B29K2105/243Partially cured
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING 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
    • B29K2105/00Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/24Condition, form or state of moulded material or of the material to be shaped crosslinked or vulcanised
    • B29K2105/246Uncured, e.g. green
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING 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
    • B29K2707/00Use of elements other than metals for preformed parts, e.g. for inserts
    • B29K2707/04Carbon
    • 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
    • B29L2031/3082Fuselages

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Robotics (AREA)
  • Moulding By Coating Moulds (AREA)
  • Golf Clubs (AREA)
  • Yarns And Mechanical Finishing Of Yarns Or Ropes (AREA)
  • Laminated Bodies (AREA)
AT07874363T 2006-12-14 2007-12-13 Verfahren zur minimierung von faserverzerrung während der herstellung einteiliger verbundzylinderteile ATE544580T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US11/638,804 US8691037B2 (en) 2006-12-14 2006-12-14 Method for minimizing fiber distortion during fabrication of one-piece composite barrel section
PCT/US2007/087486 WO2008133748A2 (en) 2006-12-14 2007-12-13 Method and related tool for minimizing fiber distortion during fabrication of one-piece composite barrel section

Publications (1)

Publication Number Publication Date
ATE544580T1 true ATE544580T1 (de) 2012-02-15

Family

ID=39864812

Family Applications (1)

Application Number Title Priority Date Filing Date
AT07874363T ATE544580T1 (de) 2006-12-14 2007-12-13 Verfahren zur minimierung von faserverzerrung während der herstellung einteiliger verbundzylinderteile

Country Status (7)

Country Link
US (1) US8691037B2 (de)
EP (2) EP2452807B1 (de)
AT (1) ATE544580T1 (de)
ES (2) ES2549532T3 (de)
HK (1) HK1131767A1 (de)
PT (1) PT2452807E (de)
WO (1) WO2008133748A2 (de)

Families Citing this family (72)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ATE458870T1 (de) * 2005-08-19 2010-03-15 Tb Composites Ltd Verbundwerkstoffkonstruktion und herstellungsverfahren dafür
EP2128017B1 (de) * 2007-01-30 2013-07-24 Airbus Operations S.L. Struktur aus verbundmaterial für flugzeugrümpfe und herstellungsverfahren dafür
GB0712535D0 (en) * 2007-06-28 2007-08-08 Airbus Uk Ltd Method for forming composite components and tool for use therein
US8016970B2 (en) * 2007-08-02 2011-09-13 The Boeing Company Method for applying a pre-cured composite strip to a composite component to minimize inconsistencies appearing on a surface of the composite component
US9238335B2 (en) * 2008-07-10 2016-01-19 The Boeing Company Mandrel for autoclave curing applications
US9327467B2 (en) * 2008-07-10 2016-05-03 The Boeing Company Composite mandrel for autoclave curing applications
US8206526B2 (en) * 2008-08-20 2012-06-26 Claude Baril Process for reducing wrinkles in composite laminated structures
DE102008062477B3 (de) * 2008-12-16 2010-03-25 Airbus Deutschland Gmbh Verfahren, System und Formwerkzeug zum Herstellen von Bauteilen aus Faserverbundwerkstoffen
US8846189B1 (en) * 2009-04-17 2014-09-30 Uab Research Foundation Long fiber thermoplastic thin-walled aeroshells for missile applications and methods of manufacture
US8857128B2 (en) 2009-05-18 2014-10-14 Apple Inc. Reinforced device housing
DE102009040528A1 (de) 2009-09-08 2011-04-07 Premium Aerotec Gmbh Verfahren zur Herstellung eines zumindest ein Hohlprofil aufweisenden Bauteils und Hohlkörper zur Durchführung dieses Verfahrens
DE102009056978A1 (de) * 2009-12-07 2011-06-09 Airbus Operations Gmbh Vorrichtung und Verfahren zur Herstellung einer aus einem Faserverbundwerkstoff bestehenden Rumpfschale für ein Luftfahrzeug
US8408972B2 (en) 2010-01-25 2013-04-02 Apple Inc. Apparatus and method for intricate cuts
US8511498B2 (en) 2010-01-25 2013-08-20 Apple Inc. Method for manufacturing an electronic device enclosure
US8372495B2 (en) 2010-05-26 2013-02-12 Apple Inc. Electronic device enclosure using sandwich construction
KR101188769B1 (ko) * 2010-07-07 2012-10-10 국방과학연구소 고무와 에폭시 수지 함유 복합재료와의 접착력 증진 방법
US9120272B2 (en) * 2010-07-22 2015-09-01 Apple Inc. Smooth composite structure
US8954180B2 (en) 2010-08-06 2015-02-10 Ingersoll Machine Tools, Inc. Manufacturing process and apparatus having an interchangeable machine tool head with integrated control
US8534338B2 (en) 2010-10-15 2013-09-17 Ingersoll Machine Tools, Inc. Fiber delivery apparatus and system having a creel and fiber placement head with polar axis of rotation
GB201101435D0 (en) * 2011-01-27 2011-03-16 Airbus Uk Ltd Stringer for an aircraft wing and method of forming thereof
US9011623B2 (en) 2011-03-03 2015-04-21 Apple Inc. Composite enclosure
WO2012155190A1 (en) * 2011-05-13 2012-11-22 National Ict Australia Ltd Method and apparatus for measurement of neural response
US8887367B2 (en) * 2011-07-12 2014-11-18 The Boeing Company Cell including clean and dirty sections for fabricating composite parts
US9144948B2 (en) * 2012-04-04 2015-09-29 The Boeing Company Hat stiffeners with canted webs
GB201217245D0 (en) * 2012-09-27 2012-11-07 Airbus Operations Ltd A cure tool
US9333713B2 (en) 2012-10-04 2016-05-10 The Boeing Company Method for co-curing composite skins and stiffeners in an autoclave
US10407955B2 (en) 2013-03-13 2019-09-10 Apple Inc. Stiff fabric
EP2796371B1 (de) * 2013-04-23 2019-11-20 Airbus Operations GmbH Flugbegleitersitz mit zusätzlicher Abstützung
US9840041B2 (en) * 2013-12-20 2017-12-12 Saab Ab Stiffening element and reinforced structure
CN104831470B (zh) 2013-12-20 2018-07-27 苹果公司 利用编织纤维增加抗张强度并用于固定附连机制
DE102014102378A1 (de) * 2014-02-24 2015-08-27 Airbus Operations Gmbh Modul für eine Luftfahrzeugkabine mit einem an einer Tür angebrachten Sitz
CN103950209A (zh) * 2014-03-11 2014-07-30 中航复合材料有限责任公司 一种u形复合材料长桁毛坯的成型工装及成型方法
US9724848B2 (en) 2014-07-03 2017-08-08 The Boeing Company Collapsible, coiled mandrel
US10449734B2 (en) * 2014-09-18 2019-10-22 Alenia Aermacchi S.P.A. Methods for manufacturing elongated structural elements of composite material
US20160176085A1 (en) * 2014-12-19 2016-06-23 Airbus Operations Gmbh Method and system for producing composite structures
US10343355B2 (en) 2015-07-31 2019-07-09 The Boeing Company Systems for additively manufacturing composite parts
US10232570B2 (en) * 2015-07-31 2019-03-19 The Boeing Company Systems for additively manufacturing composite parts
US10201941B2 (en) * 2015-07-31 2019-02-12 The Boeing Company Systems for additively manufacturing composite parts
US10232550B2 (en) * 2015-07-31 2019-03-19 The Boeing Company Systems for additively manufacturing composite parts
US10195784B2 (en) * 2015-07-31 2019-02-05 The Boeing Company Systems for additively manufacturing composite parts
US10166752B2 (en) 2015-07-31 2019-01-01 The Boeing Company Methods for additively manufacturing composite parts
US10343330B2 (en) 2015-07-31 2019-07-09 The Boeing Company Systems for additively manufacturing composite parts
US10173348B2 (en) 2015-09-14 2019-01-08 Bell Helicopter Textron Inc. Modular mandrel for monolithic composite fuselage
US10259586B2 (en) * 2016-05-03 2019-04-16 The Boeing Company Deployable seat assembly, system, and method for an interior cabin of a vehicle
US10457033B2 (en) 2016-11-07 2019-10-29 The Boeing Company Systems and methods for additively manufacturing composite parts
US11440261B2 (en) 2016-11-08 2022-09-13 The Boeing Company Systems and methods for thermal control of additive manufacturing
US10766241B2 (en) 2016-11-18 2020-09-08 The Boeing Company Systems and methods for additive manufacturing
US10843452B2 (en) 2016-12-01 2020-11-24 The Boeing Company Systems and methods for cure control of additive manufacturing
US10576683B2 (en) 2017-01-16 2020-03-03 The Boeing Company Multi-part filaments for additive manufacturing and related systems and methods
US10759159B2 (en) 2017-05-31 2020-09-01 The Boeing Company Feedstock lines for additive manufacturing
US10814550B2 (en) 2017-07-06 2020-10-27 The Boeing Company Methods for additive manufacturing
US10821672B2 (en) 2017-07-06 2020-11-03 The Boeing Company Methods for additive manufacturing
ES2954328T3 (es) * 2017-07-25 2023-11-21 Subaru Corp Plantilla de moldeo de materiales compuestos y método de moldeo de materiales compuestos
US10525635B2 (en) 2017-09-15 2020-01-07 The Boeing Company Systems and methods for creating feedstock lines for additive manufacturing of an object
US10603890B2 (en) 2017-09-15 2020-03-31 The Boeing Company Systems and methods for creating feedstock lines for additive manufacturing of an object
US10543645B2 (en) 2017-09-15 2020-01-28 The Boeing Company Feedstock lines for additive manufacturing of an object
US10105893B1 (en) 2017-09-15 2018-10-23 The Boeing Company Feedstock lines for additive manufacturing of an object, and systems and methods for creating feedstock lines
US10611081B2 (en) 2017-09-15 2020-04-07 The Boeing Company Systems and methods for creating feedstock lines for additive manufacturing of an object
US10618222B2 (en) 2017-09-15 2020-04-14 The Boeing Company Systems and methods for additively manufacturing an object
US10189237B1 (en) 2017-09-15 2019-01-29 The Boeing Company Feedstock lines for additive manufacturing of an object
US10864686B2 (en) 2017-09-25 2020-12-15 Apple Inc. Continuous carbon fiber winding for thin structural ribs
US11090882B2 (en) 2018-09-26 2021-08-17 The Boeing Company Test system and method for creating controlled and repeatable out-of-plane fiber distortion in composite laminates
US11198267B2 (en) * 2018-10-29 2021-12-14 The Boeing Company Bulk factor compensated tool for fabrication of a composite part
US11987389B2 (en) * 2019-12-18 2024-05-21 The Boeing Company Method and apparatus for forming a composite fuselage structure
NL2028114B1 (en) * 2021-04-30 2022-11-09 Boeing Co In-line autoclave adapted to preform geometry
US11718046B2 (en) 2020-11-18 2023-08-08 The Boeing Company In-line autoclave adapted to preform geometry
EP4000841A1 (de) 2020-11-18 2022-05-25 The Boeing Company Verbundanordnung für ungehärtete rumpfkomponenten
EP4000896B1 (de) * 2020-11-18 2024-01-10 The Boeing Company An die vorformgeometrie angepasster inline-autoklav
EP4000898B1 (de) * 2020-11-18 2024-01-10 The Boeing Company Verfahren und system zum abdichten eines autoklaven
JP2022080864A (ja) 2020-11-18 2022-05-30 ザ・ボーイング・カンパニー 未固化の胴体構成要素のための複合組立
NL2027399B1 (en) * 2021-01-26 2022-08-17 Boeing Co Composite assembly for unhardened fuselage components
NL2028117B1 (en) * 2021-04-30 2022-11-09 Boeing Co In-line autoclave adapted to preform geometry

Family Cites Families (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2006A (en) * 1841-03-16 Clamp for crimping leather
GB103888A (en) 1916-02-28 1917-02-15 William Henry Isaac Welch Improvements in or relating to Railway Signals.
US2999272A (en) * 1957-10-09 1961-09-12 Studebaker Packard Corp Machine for forming pre-stressed hollow articles
CH415030A (it) * 1962-10-18 1966-06-15 C I M E M Do F Lli Gadani Procedimento ed impianto per la fabbricazione in continuo di tubi di materia plastica rinforzata
US3265795A (en) * 1964-05-25 1966-08-09 Koppers Co Inc Method of skin molding
US4169749A (en) * 1977-09-21 1979-10-02 The United States Of America As Represented By The Secretary Of The Navy Method of making a hollow airfoil
US4242160A (en) * 1979-02-02 1980-12-30 United Technologies Corporation Method of winding a wind turbine blade using a filament reinforced mandrel
US5173315A (en) * 1989-04-25 1992-12-22 Hercules Incorporated Tool for joining a segmented mandrel for forming composite articles
US5223067A (en) * 1990-02-28 1993-06-29 Fuji Jukogyo Kabushiki Kaisha Method of fabricating aircraft fuselage structure
US5084219A (en) 1990-09-05 1992-01-28 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Method of fabricating composite structures
US5597435A (en) 1992-12-24 1997-01-28 General Electric Company Method using restrained cauls for composite molding
US5853651A (en) 1995-09-07 1998-12-29 Simula, Inc. High pressure hollow process for manufacturing composite structures
US5817269A (en) 1996-10-25 1998-10-06 The Boeing Company Composite fabrication method and tooling to improve part consolidation
US6217000B1 (en) 1996-10-25 2001-04-17 The Boeing Company Composite fabrication method and tooling to improve part consolidation
US5900194A (en) * 1996-12-27 1999-05-04 Wasatch Technologies Corporation Method for removing mandrels from composite tubes of substantial length
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
US6458309B1 (en) * 1998-06-01 2002-10-01 Rohr, Inc. Method for fabricating an advanced composite aerostructure article having an integral co-cured fly away hollow mandrel
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
US7306450B2 (en) * 2004-09-29 2007-12-11 The Boeing Company Apparatuses, systems, and methods for manufacturing composite parts
US7588655B2 (en) 2004-11-24 2009-09-15 The Boeing Company Mandrel with differential in thermal expansion to eliminate wrinkles in ply
US7410352B2 (en) * 2005-04-13 2008-08-12 The Boeing Company Multi-ring system for fuselage barrel formation
US7815160B2 (en) * 2006-04-04 2010-10-19 A & P Technology Composite mandrel

Also Published As

Publication number Publication date
HK1131767A1 (en) 2010-02-05
ES2382219T3 (es) 2012-06-06
EP2452807A1 (de) 2012-05-16
US20100024964A1 (en) 2010-02-04
PT2452807E (pt) 2015-09-03
WO2008133748A2 (en) 2008-11-06
EP2452807B1 (de) 2015-07-08
US8691037B2 (en) 2014-04-08
EP2121288A2 (de) 2009-11-25
WO2008133748A3 (en) 2008-12-18
EP2121288B1 (de) 2012-02-08
ES2549532T3 (es) 2015-10-29

Similar Documents

Publication Publication Date Title
ATE544580T1 (de) Verfahren zur minimierung von faserverzerrung während der herstellung einteiliger verbundzylinderteile
RU2009103204A (ru) Способ изготовления конструктивного компонента из армированного волокнами композиционного материала, предназначенного для авиакосмической отрасли, формовочный стержень для изготовления такого компонента и конструктивный компонент, полученный этим способом и/или посредством этого стержня
ATE554913T1 (de) Verfahren zur herstellung von mehreren faserverbundbauteilen
US7815160B2 (en) Composite mandrel
RU2686894C2 (ru) Изготовление пропитанной смолой цельной композитной фермовой конструкции
ATE523322T1 (de) Verfahren zur herstellung von rumpfzellensektionen für ein flugzeug mit verbundstofffasermaterialien sowie vorrichtung
ATE509757T1 (de) Verfahren zur herstellung von faserverstärkten verbundteilen
EP2038100B1 (de) Verfahren und formkern zur herstellung einer faserverbundkomponente für luft- und raumfahrt
ATE432812T1 (de) Verfahren zur herstellung einer verbindungsstange aus einem verbundwerkstoff
RU2010151431A (ru) Единая конструкция летательного аппарата из композитного материала
JP2009542460A (ja) 折り畳み可能な成形コアを用いた複合ファイバ構成要素を作製する方法および上記成形コア
ATE555011T1 (de) Verfahren zur herstellung einer produktfamilie von flugzeugflügeln
ATE540799T1 (de) Verfahren zur herstellung einer innenverkleidung für eine heckklappe unter verwendung eines verstärkten kunststoffmaterials und innenverkleidung für eine heckklappe
ATE477914T1 (de) Vakuumiervorgang zur verwendung bei einem verfahren zur herstellung einer verbundstruktur
WO2010000990A3 (fr) Procédé de fabrication d'une pièce à corps creux en matériau composite
ATE500957T1 (de) Verfahren und vorrichtung zur herstellung eines luftreifens
ATE409567T1 (de) Verfahren zur herstellung eines integralen formteils aus faserverstärktem verbundwerkstoff und werkzeugsystem zur herstellung desselben
RU2543872C2 (ru) Приспособление для формования заготовки
DE60303348D1 (de) Verfahren zur Herstellung eines monolithischen, doppelwandigen und hitzbeständigen Verbundwerkstoffteiles und danach hergestelltes Verbundwerkstoffteil
ATE508863T1 (de) Verstärkter schlauch
CA2659448A1 (en) Wing panel structure
US20170232693A1 (en) Method of repairing a perforated skin of a panel using a doubler
US20140086678A1 (en) Assembly for an aircraft nacelle
US8409387B2 (en) Process for producing components
ATE530334T1 (de) Verfahren zur herstellung einer reifenwulst und eines reifens und vorrichtung dafür