PT2668024T - Estruturas compósitas que têm contrafortes integrados com excentricidades suaves - Google Patents

Estruturas compósitas que têm contrafortes integrados com excentricidades suaves

Info

Publication number
PT2668024T
PT2668024T PT118022433T PT11802243T PT2668024T PT 2668024 T PT2668024 T PT 2668024T PT 118022433 T PT118022433 T PT 118022433T PT 11802243 T PT11802243 T PT 11802243T PT 2668024 T PT2668024 T PT 2668024T
Authority
PT
Portugal
Prior art keywords
runouts
smooth
making
same
composite structures
Prior art date
Application number
PT118022433T
Other languages
English (en)
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 PT2668024T publication Critical patent/PT2668024T/pt

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    • 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
    • B29C70/46Shaping 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
    • B29C70/48Shaping 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
    • 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
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    • B29B11/00Making preforms
    • B29B11/04Making preforms by assembling preformed material
    • 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
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    • B29C65/48Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
    • B29C65/4805Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding characterised by the type of adhesives
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    • B29C65/48Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
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    • B29C65/5057Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like positioned between the surfaces to be joined
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    • B29C65/56Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using mechanical means or mechanical connections, e.g. form-fits
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    • B29C66/05Particular design of joint configurations
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    • B29C66/131Single flanged joints, i.e. one of the parts to be joined being rigid and flanged in the joint area
    • 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
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/40General 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
    • B29C66/47Joining single elements to sheets, plates or other substantially flat surfaces
    • B29C66/472Joining single elements to sheets, plates or other substantially flat surfaces said single elements being substantially flat
    • 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
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
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    • B29C66/47Joining single elements to sheets, plates or other substantially flat surfaces
    • B29C66/472Joining single elements to sheets, plates or other substantially flat surfaces said single elements being substantially flat
    • B29C66/4722Fixing strips to surfaces other than edge faces
    • 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
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    • B29C66/40General 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
    • B29C66/47Joining single elements to sheets, plates or other substantially flat surfaces
    • B29C66/474Joining single elements to sheets, plates or other substantially flat surfaces said single elements being substantially non-flat
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
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    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/50General aspects of joining tubular articles; General aspects of joining long products, i.e. bars or profiled elements; General aspects of joining single elements to tubular articles, hollow articles or bars; General aspects of joining several hollow-preforms to form hollow or tubular articles
    • B29C66/51Joining tubular articles, profiled elements or bars; Joining single elements to tubular articles, hollow articles or bars; Joining several hollow-preforms to form hollow or tubular articles
    • B29C66/53Joining single elements to tubular articles, hollow articles or bars
    • B29C66/532Joining single elements to the wall of tubular articles, hollow articles or bars
    • 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
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
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    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
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    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
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    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
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    • B29C70/68Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks
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    • B29C66/73General 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 intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset
    • B29C66/739General 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 intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset
    • B29C66/7394General 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 intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of at least one of the parts being a thermoset
    • 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
    • B29K2101/00Use of unspecified macromolecular compounds as moulding material
    • B29K2101/10Thermosetting resins
    • 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
    • B29K2105/06Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
    • B29K2105/08Condition, 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
    • B29K2105/0809Fabrics
    • B29K2105/0827Braided fabrics
    • 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
    • B29L2009/00Layered products
    • 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
    • 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C2001/0054Fuselage structures substantially made from particular materials
    • B64C2001/0072Fuselage structures substantially made from particular materials from composite materials
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/40Weight reduction
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T156/00Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/10Methods of surface bonding and/or assembly therefor
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/24Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24479Structurally defined web or sheet [e.g., overall dimension, etc.] including variation in thickness
    • Y10T428/24488Differential nonuniformity at margin
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/24Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24479Structurally defined web or sheet [e.g., overall dimension, etc.] including variation in thickness
    • Y10T428/24521Structurally defined web or sheet [e.g., overall dimension, etc.] including variation in thickness with component conforming to contour of nonplanar surface
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/24Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24479Structurally defined web or sheet [e.g., overall dimension, etc.] including variation in thickness
    • Y10T428/2457Parallel ribs and/or grooves
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/24Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24479Structurally defined web or sheet [e.g., overall dimension, etc.] including variation in thickness
    • Y10T428/24612Composite web or sheet

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Architecture (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • General Chemical & Material Sciences (AREA)
  • Moulding By Coating Moulds (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
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Families Citing this family (74)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9586699B1 (en) 1999-08-16 2017-03-07 Smart Drilling And Completion, Inc. Methods and apparatus for monitoring and fixing holes in composite aircraft
US9625361B1 (en) 2001-08-19 2017-04-18 Smart Drilling And Completion, Inc. Methods and apparatus to prevent failures of fiber-reinforced composite materials under compressive stresses caused by fluids and gases invading microfractures in the materials
DE102009060695A1 (de) * 2009-12-29 2011-07-07 Airbus Operations GmbH, 21129 Flugzeugrumpf und Hautfeld
US9682514B2 (en) 2010-06-25 2017-06-20 The Boeing Company Method of manufacturing resin infused composite parts using a perforated caul sheet
US8628717B2 (en) 2010-06-25 2014-01-14 The Boeing Company Composite structures having integrated stiffeners and method of making the same
US8940213B2 (en) 2010-06-25 2015-01-27 The Boeing Company Resin infusion of composite parts using a perforated caul sheet
US8636252B2 (en) 2010-06-25 2014-01-28 The Boeing Company Composite structures having integrated stiffeners with smooth runouts and method of making the same
GB201020152D0 (en) * 2010-11-29 2011-01-12 Airbus Uk Ltd Aircraft panel structure and aircraft panel structure manufacturing method for alleviation of stress
SE537320C2 (sv) * 2011-06-16 2015-04-07 Bassoe Technology Ab Borrtorn med förstyvat skal samt havsplattform
US8651419B2 (en) 2011-07-18 2014-02-18 The Boeing Company Flexible truss frame and method of making the same
GB201120707D0 (en) 2011-12-01 2012-01-11 Airbus Operations Ltd Leading edge structure
JP5991786B2 (ja) * 2012-07-20 2016-09-14 難波プレス工業株式会社 補強リブ付きプレス成形品及びその製造方法
EP2727820B1 (en) * 2012-10-31 2016-12-14 Airbus Operations S.L. Stringer
GB201301766D0 (en) * 2013-01-31 2013-03-20 Airbus Operations Ltd Structural assembly joint
GB201307066D0 (en) * 2013-04-18 2013-05-29 Airbus Operations Ltd Winglet and braided composite spar
EP2989003A4 (en) * 2013-04-25 2016-12-07 Saab Ab EXPIRATION OF A STAMPING ELEMENT
US10308343B2 (en) * 2013-05-30 2019-06-04 The Boeing Company Composite hat stiffener
US10086922B2 (en) * 2013-11-15 2018-10-02 The Boeing Company Low stress stiffener runout in Pi bonded structure
US10272619B2 (en) 2014-05-19 2019-04-30 The Boeing Company Manufacture of a resin infused one-piece composite truss structure
US9511540B2 (en) * 2014-08-07 2016-12-06 GM Global Technology Operations LLC Process for securing a micro-truss structure to a panel
US10086534B2 (en) 2014-10-17 2018-10-02 The Boeing Company Multifunctional mandrel end cap and method
US10040537B2 (en) * 2015-01-15 2018-08-07 The Boeing Company Laminate composite wing structures
FR3036684B1 (fr) * 2015-05-29 2019-05-10 Stelia Aerospace Raidisseur monobloc pour structure aeronautique
JP6292185B2 (ja) * 2015-07-07 2018-03-14 株式会社豊田自動織機 繊維積層体、繊維積層体の製造方法、及び繊維強化複合材
US9809297B2 (en) 2015-08-26 2017-11-07 The Boeing Company Structures containing stiffeners having transition portions
CN204915569U (zh) * 2015-09-17 2015-12-30 延锋彼欧宁波汽车外饰系统有限公司 一种保险杠总成
EP3173223A1 (en) * 2015-11-27 2017-05-31 Airbus Operations GmbH A method for manufacturing an aircraft structure component
NL2015927B1 (en) * 2015-12-08 2017-06-28 Atg Europe B V Composite grid structure.
US10273935B2 (en) 2016-01-15 2019-04-30 General Electric Company Rotor blades having structural skin insert and methods of making same
US20170274577A1 (en) * 2016-03-24 2017-09-28 The Boeing Company Composite structures with stiffeners and method of making the same
DE102016208783A1 (de) * 2016-05-20 2017-11-23 Continental Teves Ag & Co. Ohg Verfahren zum Ummanteln einer elektrischen Einheit und elektrisches Bauelement
DE102016208782A1 (de) * 2016-05-20 2017-11-23 Continental Teves Ag & Co. Ohg Verfahren zum Ummanteln einer elektrischen Einheit und elektrisches Bauelement
US9707898B1 (en) 2016-07-11 2017-07-18 Ford Global Technologies, Llc Extruded multi-layer molded running board
US10814602B2 (en) * 2016-09-14 2020-10-27 The Boeing Company Method of producing cored composite parts
CN109562578B (zh) * 2016-09-29 2020-12-08 株式会社斯巴鲁 复合材料结构体和复合材料结构体的制造方法
US10248158B2 (en) * 2016-10-21 2019-04-02 Microsoft Technology Licensing, Llc Enclosure assembly and monitor device including same
US10365180B2 (en) * 2016-12-15 2019-07-30 The Boeing Company Non-destructive leak source detection and identification for complex bagging in conjunction with flow measurement systems
CN107052715B (zh) * 2017-03-30 2019-03-01 陕西飞机工业(集团)有限公司 一种大型机翼整体壁板数控加工方法
CN108688192B (zh) * 2017-04-12 2020-11-03 深圳市泰格尔航天航空科技有限公司 一种c型梁复合材料成型工装及复合材料c型梁成型方法
EP3428062A1 (en) * 2017-07-11 2019-01-16 Airbus Operations GmbH A leading edge structure for a flow control system of an aircraft
JP6774571B2 (ja) * 2017-07-25 2020-10-28 株式会社Subaru 複合材成形治具及び複合材成形方法
US10974806B2 (en) * 2017-10-05 2021-04-13 Gulfstream Aerospace Corporation Unified canopies for aircraft
US11519291B2 (en) * 2018-01-11 2022-12-06 Raytheon Technologies Corporation Integral stiffening rail for braided composite gas turbine engine component
US10669005B2 (en) * 2018-02-27 2020-06-02 The Boeing Company Solid laminate stringer
EP3763516A4 (en) * 2018-03-05 2021-11-24 Nippi Corporation METHOD FOR MANUFACTURING A HONEYCOMB-SHAPED SANDWICH COMPOSITE MATERIAL
CN108438199A (zh) * 2018-03-23 2018-08-24 太原科技大学 一种提高飞机蒙皮承载力的复合材料加强件
JP6692388B2 (ja) * 2018-06-11 2020-05-13 本田技研工業株式会社 車体後部構造
US11433990B2 (en) * 2018-07-09 2022-09-06 Rohr, Inc. Active laminar flow control system with composite panel
US11485468B2 (en) * 2018-09-27 2022-11-01 The Boeing Company Thermoplastic multi-grid overmolded/co-consolidated aircraft fuselage structure
US10994823B2 (en) 2018-10-11 2021-05-04 The Boeing Company Beaded panels and method of forming beaded panels
US11052617B2 (en) 2018-11-01 2021-07-06 The Boeing Company Fabrication of plank stringers
US11491750B2 (en) * 2019-01-07 2022-11-08 Varial Surf Technology, Inc. Moldless vacuum infusion process
GB2581835A (en) * 2019-03-01 2020-09-02 Airbus Operations Ltd Composite stiffener
WO2020212087A1 (en) * 2019-04-18 2020-10-22 Teijin Carbon Europe Gmbh Wedge filler preform
US10919256B2 (en) * 2019-05-09 2021-02-16 The Boeing Company Composite structure having a variable gage and methods for forming a composite structure having a variable gage
US10913215B2 (en) * 2019-05-09 2021-02-09 The Boeing Company Composite structure having a variable gage and methods for forming a composite structure having a variable gage
US10919260B2 (en) * 2019-05-09 2021-02-16 The Boeing Company Composite structure having a variable gage and methods for forming a composite structure having a variable gage
WO2020229501A1 (en) * 2019-05-14 2020-11-19 Airbus Operations Limited Aircraft panel assembly
CN110370676B (zh) * 2019-07-11 2021-05-25 航天海鹰(镇江)特种材料有限公司 一种高强度软性工装实现l型加强筋与c型框结构复材制件共固化的方法
US10994500B1 (en) 2019-11-19 2021-05-04 The Boeing Company System and method for a composite panel
US11667371B2 (en) 2020-04-03 2023-06-06 The Boeing Company Composite materials having reinforced access openings
US11643184B2 (en) * 2020-07-29 2023-05-09 The Boeing Company Wing assembly having discretely stiffened composite wing panels
US11760463B2 (en) 2020-07-29 2023-09-19 The Boeing Company Structure having net-area-tension joint
CA3120840A1 (en) 2020-07-29 2022-01-29 The Boeing Company Wing assembly having wing joints joining outer wing structures to centerwing structure
CA3122789C (en) * 2020-07-29 2024-06-11 The Boeing Company Bead-stiffened movable surfaces
WO2022039226A1 (ja) * 2020-08-19 2022-02-24 川崎重工業株式会社 複合材料製パネル構造体およびその製造方法
GB202015876D0 (en) * 2020-10-07 2020-11-18 Lm Wind Power As A precured fibrous strip for a load-carrying structure for a wind turbine blade
CA3105549A1 (en) 2020-10-22 2022-04-22 Transtex Inc. Ribbed aerodynamic skirt panel and assembly thereof
CN113199786B (zh) * 2021-04-29 2023-09-26 上海电气风电集团股份有限公司 风机叶片用腹板的制造方法
GB2612957A (en) * 2021-11-08 2023-05-24 Airbus Operations Ltd Stiffener with core and shell
GB2615755A (en) * 2022-02-15 2023-08-23 Airbus Operations Ltd Fuel tank stringer with flow passage
DE102022110887A1 (de) * 2022-05-03 2023-11-09 Premium Aerotec Gmbh Verfahren zum Herstellen eines Bauteils aus einem Verbundmaterial mit lokal erhöhter DickeVerfahren zum Herstellen eines Bauteils aus einem Verbundmaterial mit lokal erhöhter Dicke
US11933046B1 (en) * 2022-07-14 2024-03-19 Anthony Attalla Stiff wall panel assembly for a building structure and associated method(s)
US20240208633A1 (en) * 2022-12-21 2024-06-27 Rapidflight Holdings, Llc Additive manufactured aircraft structure with reinforcements and method of making the same

Family Cites Families (51)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2709973A (en) * 1952-11-13 1955-06-07 Pullman Standard Car Mfg Co Railway car side wall
US3339333A (en) * 1965-04-05 1967-09-05 Metcom Products Co Back-up tab for siding
US3775238A (en) * 1971-06-24 1973-11-27 J Lyman Structural composite material
DE2336541C3 (de) * 1973-07-18 1980-04-24 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Anordnung zum Einleiten von Kräften in ein flächiges Bauteil mit Sandwichstruktur
US4357292A (en) 1981-08-27 1982-11-02 International Grating, Inc. Method of molding in solid floor plate to a fiberglass reinforced molded resin grating
US4606961A (en) 1984-10-09 1986-08-19 The Boeing Company Discretely stiffened composite panel
US4942013A (en) 1989-03-27 1990-07-17 Mcdonnell Douglas Corporation Vacuum resin impregnation process
AU7889491A (en) * 1990-06-01 1991-12-31 Domecrete Ltd. Reinforcing element
US5439635A (en) 1993-02-18 1995-08-08 Scrimp Systems, Llc Unitary vacuum bag for forming fiber reinforced composite articles and process for making same
US5567499A (en) 1995-01-03 1996-10-22 The Boeing Company Resin transfer molding in combination with honeycomb core
US5569508A (en) 1995-01-03 1996-10-29 The Boeing Company Resin transfer molding with honeycomb core and core filler
NL1001725C2 (nl) 1995-11-23 1997-05-27 Plastisol Nv Werkwijze voor het vervaardigen van een plaat uit kunststof met hoge draagkracht, alsmede een kunststof plaat vervaardigd volgens die werkwijze.
US5771680A (en) 1995-12-21 1998-06-30 General Electric Company Stiffened composite structures and method of making thereof
US6231941B1 (en) 1998-07-14 2001-05-15 The Boeing Company Radius fillers for a resin transfer molding process
ES2168027B1 (es) * 1998-12-18 2003-10-01 Airbus Espana Sl Un procedimiento de union a traccion-compresion de caracter desmontable y/o fijo para aplicar a materiales compuestos.
US6319447B1 (en) 1999-04-09 2001-11-20 The Boeing Company Resin transfer molding process
JP4526698B2 (ja) 2000-12-22 2010-08-18 富士重工業株式会社 複合材成形品及びその製造方法
US6586054B2 (en) 2001-04-24 2003-07-01 The United States Of America As Represented By The Secretary Of The Army Apparatus and method for selectively distributing and controlling a means for impregnation of fibrous articles
US6840750B2 (en) 2001-06-11 2005-01-11 The Boeing Company Resin infusion mold tool system and vacuum assisted resin transfer molding with subsequent pressure bleed
US7138028B2 (en) 2001-07-26 2006-11-21 The Boeing Company Vacuum assisted resin transfer method for co-bonding composite laminate structures
US6630095B2 (en) 2001-08-01 2003-10-07 Lockheed Martin Corporation Method for making composite structures
US6627142B2 (en) 2001-08-01 2003-09-30 Lockheed Martin Corporation Apparatus for making composite structures and method for making same
DE10140166B4 (de) 2001-08-22 2009-09-03 Eads Deutschland Gmbh Verfahren und Vorrichtung zur Herstellung von faserverstärkten Bauteilen mittels eines Injektionsverfahrens
US6811733B2 (en) 2001-11-13 2004-11-02 The Boeing Company Resin transfer molding multi-part/shim tooling (RTM-MPST)
DE10203975C1 (de) 2002-01-31 2003-01-23 Eads Deutschland Gmbh Verfahren und Vorrichtung zur Herstellung von faserverstärkten Bauteilen
EP1507647B1 (en) 2002-05-29 2012-09-12 The Boeing Company Controlled atmospheric pressure resin infusion process
US7204951B2 (en) 2002-07-30 2007-04-17 Rocky Mountain Composites, Inc. Method of assembling a single piece co-cured structure
US7419627B2 (en) 2002-09-13 2008-09-02 Northrop Grumman Corporation Co-cured vacuum-assisted resin transfer molding manufacturing method
US6896841B2 (en) 2003-03-20 2005-05-24 The Boeing Company Molding process and apparatus for producing unified composite structures
FR2866626B1 (fr) * 2004-02-20 2006-05-19 Airbus France Arret de raidisseur a pentes decalees et panneau muni d'un tel arret
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
US7080805B2 (en) 2004-05-05 2006-07-25 The Boeing Company Stiffened structures and associated methods
US7510757B2 (en) 2005-02-01 2009-03-31 The Boeing Company Cellular composite grid-stiffened structure
WO2006096647A2 (en) 2005-03-07 2006-09-14 Scientific Composites Method for making a dial table
US7633040B2 (en) 2005-11-14 2009-12-15 The Boeing Company Bulk resin infusion system apparatus and method
US8043453B2 (en) 2005-12-23 2011-10-25 The Boeing Company System and method for reworking composites
US7459048B2 (en) 2006-01-31 2008-12-02 The Boeing Company One-piece inner shell for full barrel composite fuselage
GB0619512D0 (en) * 2006-10-03 2006-11-15 Airbus Uk Ltd Fitting
AU2008227492B2 (en) 2007-03-20 2013-02-14 Mitsubishi Heavy Industries, Ltd. Method of vacuum-assisted RTM
GB0712552D0 (en) * 2007-06-29 2007-08-08 Airbus Uk Ltd Elongate composite structural members and improvements therein
US8042767B2 (en) 2007-09-04 2011-10-25 The Boeing Company Composite fabric with rigid member structure
US8042315B2 (en) * 2007-09-14 2011-10-25 Spectrum Aeronautical, Llc Reinforced composite panel
FR2922516B1 (fr) * 2007-10-18 2010-04-16 Airbus France Eclissage de raidisseurs en omega au niveau d'une jonction circonferentielle d'un fuselage d'avion
DE102008059653B4 (de) 2008-11-28 2015-07-09 Gkn Aerospace Services Ltd. Flächiges Bauteil eines Fluggerätes und Verfahren zu dessen Herstellung
GB0912015D0 (en) 2009-07-10 2009-08-19 Airbus Operations Ltd Stringer
ES2392236B1 (es) * 2010-01-15 2013-10-09 Airbus Operations, S.L. Componente de aeronave con paneles rigidizados con larguerillos.
US8940213B2 (en) 2010-06-25 2015-01-27 The Boeing Company Resin infusion of composite parts using a perforated caul sheet
US8636252B2 (en) * 2010-06-25 2014-01-28 The Boeing Company Composite structures having integrated stiffeners with smooth runouts and method of making the same
US9682514B2 (en) 2010-06-25 2017-06-20 The Boeing Company Method of manufacturing resin infused composite parts using a perforated caul sheet
US8628717B2 (en) 2010-06-25 2014-01-14 The Boeing Company Composite structures having integrated stiffeners and method of making the same
ES2398985B1 (es) * 2011-03-14 2014-02-14 Airbus Operations S.L. Dispositivos de transferencia de carga en la terminación de un larguerillo.

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KR20130141562A (ko) 2013-12-26
EP2668024A1 (en) 2013-12-04
ES2784175T3 (es) 2020-09-22
JP6005661B2 (ja) 2016-10-12
US9440402B2 (en) 2016-09-13
US20150328846A1 (en) 2015-11-19
EP2668024B1 (en) 2020-02-19
CA2822577C (en) 2018-05-15
US20120052247A1 (en) 2012-03-01
JP2014510879A (ja) 2014-05-01
WO2012102789A1 (en) 2012-08-02
CA2822577A1 (en) 2012-08-02
US8636252B2 (en) 2014-01-28
KR101900967B1 (ko) 2018-09-20
CN103370185A (zh) 2013-10-23
EP3533594A1 (en) 2019-09-04

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