JP6357486B2 - 輪郭に合致した積層構造体を製作するための方法及び装置 - Google Patents

輪郭に合致した積層構造体を製作するための方法及び装置 Download PDF

Info

Publication number
JP6357486B2
JP6357486B2 JP2015551676A JP2015551676A JP6357486B2 JP 6357486 B2 JP6357486 B2 JP 6357486B2 JP 2015551676 A JP2015551676 A JP 2015551676A JP 2015551676 A JP2015551676 A JP 2015551676A JP 6357486 B2 JP6357486 B2 JP 6357486B2
Authority
JP
Japan
Prior art keywords
tool
stack
modules
forming
module
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.)
Active
Application number
JP2015551676A
Other languages
English (en)
Japanese (ja)
Other versions
JP2016508900A (ja
JP2016508900A5 (enExample
Inventor
ジェームズ エヌ． バトリック，
ジェームズ エヌ． バトリック，
デーヴィッド ピー． バンクス，
デーヴィッド ピー． バンクス，
デニス ダブリュ． スチュアート，
デニス ダブリュ． スチュアート，
ジーザス サンチェス，
ジーザス サンチェス，
アンドリュー イー． モディン，
アンドリュー イー． モディン，
エドアルド ピー． デパセ，
エドアルド ピー． デパセ，
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
Application filed by Boeing Co filed Critical Boeing Co
Publication of JP2016508900A publication Critical patent/JP2016508900A/ja
Publication of JP2016508900A5 publication Critical patent/JP2016508900A5/ja
Application granted granted Critical
Publication of JP6357486B2 publication Critical patent/JP6357486B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

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
    • B29C70/38—Automated lay-up, e.g. using robots, laying filaments according to predetermined patterns
    • 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
    • B29C69/00—Combinations of shaping techniques not provided for in a single one of main groups B29C39/00 - B29C67/00, e.g. associations of moulding and joining techniques; Apparatus therefore
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/06—Fibrous reinforcements only
    • 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
    • B29C70/541—Positioning reinforcements in a mould, e.g. using clamping means for the reinforcement
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D99/00—Subject matter not provided for in other groups of this subclass
    • B29D99/0003—Producing profiled members, e.g. beams
    • 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
    • B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/06—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
    • B29K2105/12—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts of short lengths, e.g. chopped filaments, staple fibres or bristles
    • 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
    • B29K2307/04—Carbon
    • 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Robotics (AREA)
  • Moulding By Coating Moulds (AREA)
  • Mounting, Exchange, And Manufacturing Of Dies (AREA)
JP2015551676A 2013-01-07 2013-11-21 輪郭に合致した積層構造体を製作するための方法及び装置 Active JP6357486B2 (ja)

Applications Claiming Priority (5)

Application Number Priority Date Filing Date Title
US201361749881P 2013-01-07 2013-01-07
US61/749,881 2013-01-07
US13/901,813 2013-05-24
US13/901,813 US9314974B2 (en) 2013-01-07 2013-05-24 Method and apparatus for fabricating contoured laminate structures
PCT/US2013/071124 WO2014107243A1 (en) 2013-01-07 2013-11-21 Method and apparatus for fabricating contoured laminate structures

Publications (3)

Publication Number Publication Date
JP2016508900A JP2016508900A (ja) 2016-03-24
JP2016508900A5 JP2016508900A5 (enExample) 2017-01-05
JP6357486B2 true JP6357486B2 (ja) 2018-07-11

Family

ID=51060084

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2015551676A Active JP6357486B2 (ja) 2013-01-07 2013-11-21 輪郭に合致した積層構造体を製作するための方法及び装置

Country Status (8)

Country Link
US (3) US9314974B2 (enExample)
EP (2) EP2941342B1 (enExample)
JP (1) JP6357486B2 (enExample)
CN (1) CN104903080B (enExample)
BR (1) BR112015016158B1 (enExample)
CA (1) CA2897045C (enExample)
ES (1) ES2834957T3 (enExample)
WO (1) WO2014107243A1 (enExample)

Families Citing this family (32)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
US9505354B2 (en) 2013-09-16 2016-11-29 The Boeing Company Carbon fiber reinforced polymer cargo beam with integrated cargo stanchions and c-splices
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
US9889610B2 (en) * 2014-07-29 2018-02-13 The Boeing Company Automated ply forming and compaction using flexible roller contact
US9636876B2 (en) 2014-10-29 2017-05-02 The Boeing Company Method, device and apparatus for vacuum forming composite laminates
GB2533567A (en) * 2014-12-19 2016-06-29 Airbus Operations Ltd Method of forming laminar composite charge
US10086596B2 (en) * 2015-03-12 2018-10-02 The Boeing Company Apparatus and method for automated layup of composite structures
US10800111B2 (en) 2015-06-16 2020-10-13 The Boeing Company Composite structure fabrication systems and methods
US20180327071A1 (en) 2017-05-10 2018-11-15 The Boeing Company Systems and methods for aircraft integrated composite frames
GB2566433A (en) * 2017-07-13 2019-03-20 Spirit Aerosystems Europe Ltd Composite lay-up apparatus and method
US10688711B2 (en) 2017-07-14 2020-06-23 The Boeing Company Heat blanket assembly for forming a composite charge
US10703055B2 (en) 2017-07-14 2020-07-07 The Boeing Company Clamping system for holding a composite charge during forming over a forming mandrel
US10843449B2 (en) 2017-12-14 2020-11-24 The Boeing Company Method and apparatus for forming composite plies on contoured tool surfaces
US11014314B2 (en) 2018-06-28 2021-05-25 The Boeing Company End effector for forming prepreg plies on highly contoured surfaces
US10994502B2 (en) 2018-11-01 2021-05-04 The Boeing Company Lamination system and method using a plurality of static lamination heads
US10960615B2 (en) 2018-11-13 2021-03-30 The Boeing Company System and method for laminating a composite laminate along a continuous loop lamination path
JP7199940B2 (ja) 2018-12-03 2023-01-06 川崎重工業株式会社 複合材料製航空機用部品およびその製造方法
US11401023B2 (en) 2019-01-11 2022-08-02 The Boeing Company Aircraft cargo floor architecture and method of modifying the aircraft cargo floor architecture
JP7478758B2 (ja) 2019-06-14 2024-05-07 フィブ・マシニング・システムズ，インコーポレーテッド モジュール式繊維配置ヘッド
US11148373B2 (en) 2019-07-01 2021-10-19 The Boeing Company System and method for laying up a composite laminate having integrally laminated filler elements
US11507535B2 (en) 2019-10-16 2022-11-22 International Business Machines Corporation Probabilistic verification of linked data
EP3822068B1 (en) * 2019-11-13 2023-07-19 Airbus Operations, S.L.U. Device and method for forming a composite laminate for obtaining a z-shaped profile
US11260640B2 (en) 2020-02-06 2022-03-01 Fives Machining Systems, Inc. Tape lamination machine scrap collection assembly
US11498324B2 (en) 2020-02-06 2022-11-15 Fives Machining Systems, Inc. Tape lamination machine cutting assembly
US11141937B2 (en) 2020-02-06 2021-10-12 Fives Machining Systems, Inc. Tape lamination head with tape tension control system
WO2021200047A1 (ja) * 2020-03-31 2021-10-07 川崎重工業株式会社 航空機部品の中間生成品の製造方法および航空機部品
WO2021255880A1 (ja) * 2020-06-17 2021-12-23 三菱重工業株式会社 治具及び複合材の加工方法
EP4000880B1 (en) 2020-11-18 2025-06-11 The Boeing Company Fabrication of curved composite preforms for aircraft via assembly lines
NL2027437B1 (en) 2021-01-26 2022-08-19 Boeing Co Fabrication of curved composite preforms for aircraft via assembly lines
JP2022080872A (ja) * 2020-11-18 2022-05-30 ザ・ボーイング・カンパニー アセンブリラインを介した航空機用の湾曲した複合材プリフォームの製造

Family Cites Families (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3003552C2 (de) 1980-01-31 1982-06-24 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Flächenbauteil, insbesondere für ein Luftfahrzeug
US4601775A (en) * 1985-06-03 1986-07-22 Cincinnati Milacron Inc. Compliant presser member for composite tape laying machine
US5352306A (en) 1993-05-27 1994-10-04 Cincinnati Milacron Inc. Tape laying apparatus and method
US6298896B1 (en) 2000-03-28 2001-10-09 Northrop Grumman Corporation Apparatus for constructing a composite structure
AU2003270696A1 (en) 2002-09-12 2004-05-04 David Groppe Precision feed end-effector composite fabric tape-laying apparatus and method
US7341086B2 (en) 2004-10-29 2008-03-11 The Boeing Company Automated fabric layup system and method
ES2338551T3 (es) 2004-12-06 2010-05-10 Saab Ab Procedimiento de fabricacion de un brazo curvado de material compuesto.
US8557165B2 (en) 2008-10-25 2013-10-15 The Boeing Company Forming highly contoured composite parts
US7993480B2 (en) * 2007-11-17 2011-08-09 The Boeing Company Method and apparatus for placing plies on curved substrates
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
US7362437B2 (en) * 2006-03-28 2008-04-22 The Boeing Company Vision inspection system device and method
ES2640246T3 (es) 2008-01-31 2017-11-02 Orbital Atk, Inc. Un aparato de colocación de herramienta de aporte de rigidez y el método correspondiente
US9090028B2 (en) 2008-04-17 2015-07-28 The Boeing Company Method for producing contoured composite structures and structures produced thereby
US8349105B2 (en) 2008-04-17 2013-01-08 The Boeing Company Curved composite frames and method of making the same
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
FR2942741B1 (fr) 2009-03-05 2014-05-16 Mediterranee Const Ind Procede et dispositif de fabrication automatisee d'au moins une piece allongee a une ou plusieurs couches en materiaux composites
US8282760B2 (en) * 2010-06-10 2012-10-09 Haworth, Inc. Apparatus and process for wrapping and securing edge flaps of flexible cover sheet to panel structure
DE102010039955A1 (de) * 2010-08-30 2012-03-01 Deutsches Zentrum für Luft- und Raumfahrt e.V. Fertigungsanlage zur Herstellung von Faserverbundmaterial-Bauteilen
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
JP2012146067A (ja) * 2011-01-11 2012-08-02 Nippon Software Management Kk 核酸情報処理装置およびその処理方法
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
US20140338829A1 (en) 2013-05-20 2014-11-20 Invisible Gadget Guard, Inc. Protective Film Installation Apparatus and Method
US11014314B2 (en) 2018-06-28 2021-05-25 The Boeing Company End effector for forming prepreg plies on highly contoured surfaces

Also Published As

Publication number Publication date
BR112015016158A2 (pt) 2017-07-11
US20160214330A1 (en) 2016-07-28
CN104903080A (zh) 2015-09-09
US9314974B2 (en) 2016-04-19
US10464265B2 (en) 2019-11-05
CA2897045C (en) 2017-08-29
JP2016508900A (ja) 2016-03-24
WO2014107243A1 (en) 2014-07-10
US20200039154A1 (en) 2020-02-06
CN104903080B (zh) 2018-09-07
EP2941342A1 (en) 2015-11-11
EP3750694A1 (en) 2020-12-16
CA2897045A1 (en) 2014-07-10
US11534989B2 (en) 2022-12-27
EP3750694B1 (en) 2023-06-21
EP2941342B1 (en) 2020-09-09
ES2834957T3 (es) 2021-06-21
BR112015016158A8 (pt) 2019-10-22
BR112015016158B1 (pt) 2021-04-20
US20140190625A1 (en) 2014-07-10

Similar Documents

Publication Publication Date Title
JP6357486B2 (ja) 輪郭に合致した積層構造体を製作するための方法及び装置
US10828846B2 (en) Method and apparatus for fabricating contoured laminate structures
EP2444240B1 (en) Composite manufacturing method using an assembly of composite modules
US11807395B2 (en) Assembly line fabrication and assembly of aircraft wings
CN114516413A (zh) 用于机身段的制造线、系统和方法
CN114536816A (zh) 用于未硬化机身部件的复合组件
US11753184B2 (en) Assembly line fabrication and assembly of aircraft wings
US11643224B2 (en) Assembly line fabrication and assembly of aircraft wings
US12187457B2 (en) Assembly line fabrication and assembly of aircraft wings
EP4000899A1 (en) Method and system for carrying a wing panel of an aircraft
US12296984B2 (en) Assembly line fabrication and assembly of aircraft wings
HK1164221B (en) Composite manufacturing method using an assembly of composite modules
HK1164221A (en) Composite manufacturing method using an assembly of composite modules

Legal Events

Date Code Title Description
A521 Request for written amendment filed

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20161117

A621 Written request for application examination

Free format text: JAPANESE INTERMEDIATE CODE: A621

Effective date: 20161117

A131 Notification of reasons for refusal

Free format text: JAPANESE INTERMEDIATE CODE: A131

Effective date: 20171010

A521 Request for written amendment filed

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20180109

A131 Notification of reasons for refusal

Free format text: JAPANESE INTERMEDIATE CODE: A131

Effective date: 20180130

A521 Request for written amendment filed

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20180426

TRDD Decision of grant or rejection written
A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

Effective date: 20180522

A61 First payment of annual fees (during grant procedure)

Free format text: JAPANESE INTERMEDIATE CODE: A61

Effective date: 20180618

R150 Certificate of patent or registration of utility model

Ref document number: 6357486

Country of ref document: JP

Free format text: JAPANESE INTERMEDIATE CODE: R150

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250