ATE544582T1 - Herstellungsverfahren von modularverbundstoff - Google Patents
Herstellungsverfahren von modularverbundstoffInfo
- Publication number
- ATE544582T1 ATE544582T1 AT08171011T AT08171011T ATE544582T1 AT E544582 T1 ATE544582 T1 AT E544582T1 AT 08171011 T AT08171011 T AT 08171011T AT 08171011 T AT08171011 T AT 08171011T AT E544582 T1 ATE544582 T1 AT E544582T1
- Authority
- AT
- Austria
- Prior art keywords
- production process
- modular composite
- composite
- modular
- composite modules
- Prior art date
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
- B29C70/38—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
- B29C31/00—Handling, e.g. feeding of the material to be shaped, storage of plastics material before moulding; Automation, i.e. automated handling lines in plastics processing plants, e.g. using manipulators or robots
- B29C31/04—Feeding of the material to be moulded, e.g. into a mould cavity
- B29C31/08—Feeding of the material to be moulded, e.g. into a mould cavity of preforms to be moulded, e.g. tablets, fibre reinforced preforms, extruded ribbons, tubes or profiles; Manipulating means specially adapted for feeding preforms, e.g. supports conveyors
-
- 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
-
- 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
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/10—Manufacturing or assembling aircraft, e.g. jigs therefor
-
- 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
- B29C35/00—Heating, cooling or curing, e.g. crosslinking or vulcanising; Apparatus therefor
- B29C35/02—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould
-
- 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
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/11—Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
- B29C66/116—Single bevelled joints, i.e. one of the parts to be joined being bevelled in the joint area
- B29C66/1162—Single bevel to bevel joints, e.g. mitre joints
-
- 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
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/12—Joint cross-sections combining only two joint-segments; Tongue and groove joints; Tenon and mortise joints; Stepped joint cross-sections
- B29C66/128—Stepped joint cross-sections
- B29C66/1282—Stepped joint cross-sections comprising at least one overlap joint-segment
-
- 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
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/12—Joint cross-sections combining only two joint-segments; Tongue and groove joints; Tenon and mortise joints; Stepped joint cross-sections
- B29C66/128—Stepped joint cross-sections
- B29C66/1286—Stepped joint cross-sections comprising at least one bevelled joint-segment
-
- 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
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/40—General aspects of joining substantially flat articles, e.g. plates, sheets or web-like materials; Making flat seams in tubular or hollow articles; Joining single elements to substantially flat surfaces
- B29C66/41—Joining substantially flat articles ; Making flat seams in tubular or hollow articles
- B29C66/43—Joining a relatively small portion of the surface of said articles
- B29C66/432—Joining a relatively small portion of the surface of said articles for making tubular articles or closed loops, e.g. by joining several sheets ; for making hollow articles or hollow preforms
- B29C66/4326—Joining a relatively small portion of the surface of said articles for making tubular articles or closed loops, e.g. by joining several sheets ; for making hollow articles or hollow preforms for making hollow articles or hollow-preforms, e.g. half-shells
-
- 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
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/40—General aspects of joining substantially flat articles, e.g. plates, sheets or web-like materials; Making flat seams in tubular or hollow articles; Joining single elements to substantially flat surfaces
- B29C66/41—Joining substantially flat articles ; Making flat seams in tubular or hollow articles
- B29C66/43—Joining a relatively small portion of the surface of said articles
- B29C66/435—Making large sheets by joining smaller ones or strips together
-
- 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
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/72—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
- B29C66/721—Fibre-reinforced materials
-
- 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
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/72—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
- B29C66/721—Fibre-reinforced materials
- B29C66/7212—Fibre-reinforced materials characterised by the composition of the fibres
-
- 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
- B29K2105/08—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts of continuous length, e.g. cords, rovings, mats, fabrics, strands or yarns
- B29K2105/0872—Prepregs
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C2001/0054—Fuselage structures substantially made from particular materials
- B64C2001/0072—Fuselage structures substantially made from particular materials from composite materials
-
- 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
-
- 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
- Y10T156/1036—Bending of one piece blank and joining edges to form article
-
- 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
- Y10T156/1074—Separate cutting of separate sheets or webs
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US11/952,222 US8916010B2 (en) | 2007-12-07 | 2007-12-07 | Composite manufacturing method |
Publications (1)
Publication Number | Publication Date |
---|---|
ATE544582T1 true ATE544582T1 (de) | 2012-02-15 |
Family
ID=40343503
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AT08171011T ATE544582T1 (de) | 2007-12-07 | 2008-12-08 | Herstellungsverfahren von modularverbundstoff |
Country Status (8)
Country | Link |
---|---|
US (1) | US8916010B2 (de) |
EP (2) | EP2444240B1 (de) |
JP (1) | JP5646141B2 (de) |
KR (1) | KR101511384B1 (de) |
CN (1) | CN101492098B (de) |
AT (1) | ATE544582T1 (de) |
ES (2) | ES2382078T3 (de) |
PT (1) | PT2444240T (de) |
Families Citing this family (45)
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US7849729B2 (en) | 2006-12-22 | 2010-12-14 | The Boeing Company | Leak detection in vacuum bags |
US8568551B2 (en) | 2007-05-22 | 2013-10-29 | The Boeing Company | Pre-patterned layup kit and method of manufacture |
US9770871B2 (en) | 2007-05-22 | 2017-09-26 | The Boeing Company | Method and apparatus for layup placement |
US8333864B2 (en) | 2008-09-30 | 2012-12-18 | The Boeing Company | Compaction of prepreg plies on composite laminate structures |
US8936695B2 (en) | 2007-07-28 | 2015-01-20 | The Boeing Company | Method for forming and applying composite layups having complex geometries |
US8707766B2 (en) | 2010-04-21 | 2014-04-29 | The Boeing Company | Leak detection in vacuum bags |
US8752293B2 (en) | 2007-12-07 | 2014-06-17 | The Boeing Company | Method of fabricating structures using composite modules and structures made thereby |
US8916010B2 (en) | 2007-12-07 | 2014-12-23 | The Boeing Company | Composite manufacturing method |
US8349105B2 (en) * | 2008-04-17 | 2013-01-08 | The Boeing Company | Curved composite frames and method of making the same |
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 |
EP2226186A1 (de) * | 2009-03-06 | 2010-09-08 | Lm Glasfiber A/S | Verfahren und Produktionslinie zur Herstellung von Windturbinenblättern |
DE102010013131A1 (de) * | 2009-12-21 | 2011-06-22 | REHAU AG + Co., 95111 | Verfahren zur Herstellung von endlosfaserverstärkten Formteilen aus thermoplastischem Kunststoff sowie Kraftfahrzeugformteil |
US20120152432A1 (en) * | 2010-12-15 | 2012-06-21 | Samuel Francis Pedigo | Methods and systems for fiber placement using a stationary dispenser |
US20140086734A1 (en) * | 2012-09-21 | 2014-03-27 | General Electric Company | Method and system for fabricating composite containment casings |
US9003644B2 (en) | 2012-10-15 | 2015-04-14 | Stmicroelectronics Pte Ltd | PNP apparatus and PNP tool head with direct bonding pressure pick-up tip |
DE102012112416A1 (de) * | 2012-12-17 | 2014-06-18 | Rehau Ag + Co | Verfahren zur Herstellung eines mehrlagigen Vorgeleges aus faserverstärkten Matten mit einer die Fasern zumindest teilweise umgebenden thermoplastischen Matrix, sowie Fertigungsanlage zur Durchführung des Verfahrens |
CN104955632B (zh) * | 2012-12-21 | 2017-06-16 | 维斯塔斯风力系统有限公司 | 用于风轮机叶片构建的导轨装置 |
US9817452B2 (en) * | 2013-01-11 | 2017-11-14 | The Boeing Company | System and method for thermal management guidance |
DE102013223307A1 (de) * | 2013-11-15 | 2015-05-21 | Bayerische Motoren Werke Aktiengesellschaft | Verfahren zur Herstellung einer Bauteilstruktur aus mehreren Bauteilen, Bauteilstruktur und Fahrzeug |
US9370922B1 (en) | 2014-03-18 | 2016-06-21 | The Boeing Company | Systems and methods for stretch-forming multi-thickness composite skins |
AU2015250687B2 (en) | 2014-04-24 | 2018-10-04 | Bae Systems Plc | Assembly tool production |
WO2015162406A2 (en) | 2014-04-24 | 2015-10-29 | Bae Systems Plc | Production of airframe components |
GB2527889B (en) | 2014-04-24 | 2017-06-21 | Bae Systems Plc | Airframe production |
GB2544252B (en) | 2014-04-24 | 2018-09-12 | Bae Systems Plc | Machining fixture production |
EP3134785B1 (de) | 2014-04-24 | 2021-06-02 | BAE Systems PLC | Flugzeugflugwerkanordnung |
GB2529276B (en) | 2014-04-24 | 2018-07-11 | Bae Systems Plc | Production of Systems |
US9937549B2 (en) * | 2014-07-09 | 2018-04-10 | The Boeing Company | Two-stage riveting |
US9724845B2 (en) * | 2014-11-13 | 2017-08-08 | The Boeing Company | Systems and methods for making indexed prepreg composite sheets and laminated composite articles |
GB2532451B (en) | 2014-11-19 | 2018-12-26 | Bae Systems Plc | Object production |
CN105644803B (zh) * | 2014-12-02 | 2019-11-08 | 波音公司 | 制造强化复合机翼面板/蒙皮的设备及方法 |
US10800111B2 (en) | 2015-06-16 | 2020-10-13 | The Boeing Company | Composite structure fabrication systems and methods |
US10519965B2 (en) | 2016-01-15 | 2019-12-31 | General Electric Company | Method and system for fiber reinforced composite panels |
US10041889B2 (en) * | 2016-08-01 | 2018-08-07 | The Boeing Company | System and method for high speed surface and subsurface FOD and defect detection |
US10692204B2 (en) | 2016-08-01 | 2020-06-23 | The Boeing Company | System and method for high speed surface and subsurface FOD and defect detection |
US10391723B2 (en) * | 2017-08-31 | 2019-08-27 | The Boeing Company | Rotary compaction tool |
GB2567684B (en) * | 2017-10-20 | 2022-03-30 | Mclaren Automotive Ltd | Composite manufacturing |
US10926490B2 (en) * | 2018-04-09 | 2021-02-23 | The Boeing Company | Composite laminate forming apparatus and method therefor |
US10682821B2 (en) | 2018-05-01 | 2020-06-16 | Divergent Technologies, Inc. | Flexible tooling system and method for manufacturing of composite structures |
US11247413B2 (en) | 2018-12-17 | 2022-02-15 | The Boeing Company | Composite parts including hybrid plies, methods of forming the composite parts, and systems for forming the composite parts |
US20220152769A1 (en) * | 2020-11-18 | 2022-05-19 | The Boeing Company | Indexing apparatus and method of indexing |
US20220153452A1 (en) * | 2020-11-18 | 2022-05-19 | The Boeing Company | Fabrication line, systems, and methods for fuselage sections |
US11541576B1 (en) * | 2021-09-17 | 2023-01-03 | Blended Wing Aircraft, Inc. | Systems and methods for manufacture of a modular aircraft |
CN114735160B (zh) * | 2022-04-14 | 2023-06-20 | 青岛杰瑞工控技术有限公司 | 一种玻璃钢船艇糊制装置及船艇糊制工艺 |
US11866201B2 (en) * | 2022-05-03 | 2024-01-09 | The Boeing Company | Method and apparatus for the application of frame to fuselage pull-up force via fuselage skin waterline tensioning |
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-
2007
- 2007-12-07 US US11/952,222 patent/US8916010B2/en active Active
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2008
- 2008-11-18 KR KR20080114356A patent/KR101511384B1/ko active IP Right Grant
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- 2008-12-08 EP EP12151305.5A patent/EP2444240B1/de active Active
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EP2444240A1 (de) | 2012-04-25 |
EP2067611A1 (de) | 2009-06-10 |
JP2009137578A (ja) | 2009-06-25 |
KR101511384B1 (ko) | 2015-04-10 |
US8916010B2 (en) | 2014-12-23 |
ES2628443T3 (es) | 2017-08-02 |
ES2382078T3 (es) | 2012-06-05 |
PT2444240T (pt) | 2017-04-06 |
KR20090060144A (ko) | 2009-06-11 |
EP2444240B1 (de) | 2017-03-15 |
EP2067611B1 (de) | 2012-02-08 |
US20090145545A1 (en) | 2009-06-11 |
CN101492098A (zh) | 2009-07-29 |
CN101492098B (zh) | 2016-05-18 |
JP5646141B2 (ja) | 2014-12-24 |
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