[go: up one dir, main page]

RU2016129734A - Способ и устройство для производства профилированных элементов жесткости из композитного слоистого материала с уменьшенным образованием складок - Google Patents

Способ и устройство для производства профилированных элементов жесткости из композитного слоистого материала с уменьшенным образованием складок Download PDF

Info

Publication number
RU2016129734A
RU2016129734A RU2016129734A RU2016129734A RU2016129734A RU 2016129734 A RU2016129734 A RU 2016129734A RU 2016129734 A RU2016129734 A RU 2016129734A RU 2016129734 A RU2016129734 A RU 2016129734A RU 2016129734 A RU2016129734 A RU 2016129734A
Authority
RU
Russia
Prior art keywords
stiffener
pressing device
composite laminate
inner radius
parts
Prior art date
Application number
RU2016129734A
Other languages
English (en)
Other versions
RU2727627C2 (ru
Inventor
Кристофер Дэвид ОФФЕНСЕНД
Кирк Бен КАДЖИТА
Киеран П. ДЕВИС
Мэттью Р. СОЯ
Original Assignee
Зе Боинг Компани
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 Зе Боинг Компани filed Critical Зе Боинг Компани
Publication of RU2016129734A publication Critical patent/RU2016129734A/ru
Application granted granted Critical
Publication of RU2727627C2 publication Critical patent/RU2727627C2/ru

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B37/00Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B32B37/0007Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding involving treatment or provisions in order to avoid deformation or air inclusion, e.g. to improve surface quality
    • B32B37/0015Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding involving treatment or provisions in order to avoid deformation or air inclusion, e.g. to improve surface quality to avoid warp or curl
    • 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
    • B29C70/46Shaping 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
    • 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
    • B29C53/02Bending or folding
    • 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
    • B29C53/80Component parts, details or accessories; Auxiliary operations
    • 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
    • B29C70/06Fibrous reinforcements only
    • B29C70/10Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
    • B29C70/16Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
    • B29C70/22Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least two directions forming a two dimensional structure
    • B29C70/222Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least two directions forming a two dimensional structure the structure being shaped to form a three dimensional configuration
    • 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
    • B29C70/34Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation
    • 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
    • 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
    • B29C70/54Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
    • B29C70/549Details of caul plates, e.g. materials or shape
    • 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
    • B29C70/54Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
    • B29C70/56Tensioning reinforcements before or during shaping
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29DPRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D99/00Subject matter not provided for in other groups of this subclass
    • B29D99/0003Producing profiled members, e.g. beams
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B37/00Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B32B37/10Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the pressing technique, e.g. using action of vacuum or fluid pressure
    • B32B37/1018Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the pressing technique, e.g. using action of vacuum or fluid pressure using only vacuum
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B37/00Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B32B37/14Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers
    • B32B37/144Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers using layers with different mechanical or chemical conditions or properties, e.g. layers with different thermal shrinkage, layers under tension during bonding
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06Frames; Stringers; Longerons ; Fuselage sections
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/18Spars; Ribs; Stringers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64FGROUND 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
    • B64F5/00Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/10Manufacturing or assembling aircraft, e.g. jigs therefor
    • 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
    • B29L2031/001Profiled members, e.g. beams, sections
    • 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
    • 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
    • B29L2031/748Machines or parts thereof not otherwise provided for
    • B29L2031/7502Supports, machine frames or beds, worktables
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Composite Materials (AREA)
  • Chemical & Material Sciences (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Textile Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Transportation (AREA)
  • Fluid Mechanics (AREA)
  • Physics & Mathematics (AREA)
  • Quality & Reliability (AREA)
  • Moulding By Coating Moulds (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)

Claims (25)

1. Способ изготовления профилированного элемента жесткости из композитного слоистого материала, включающий
сборку по существу плоской заготовки композитного слоистого материала;
формование заготовки композитного слоистого материала по существу с получением прямолинейного элемента жесткости, имеющего необходимую форму поперечного сечения;
формование профиля в элементе жесткости, имеющем внутренний радиус и внешний радиус; и
уменьшение деформации сжатия на внутреннем радиусе во время формования профиля.
2. Способ по п. 1, согласно которому сборка заготовки композитного слоистого материала включает укладку частей слоя препрега, каждая из которых обладает ориентацией волокон под углом 0°.
3. Способ по п. 2, согласно которому укладка частей слоя препрега включает их перекрытие.
4. Способ по п. 1, согласно которому формование профиля в элементе жесткости включает:
размещение прямолинейного элемента жесткости на криволинейной поверхности приспособления,
размещение устройства прессования на прямолинейном элементе жесткости и
использование устройства прессования для прессования элемента жесткости с упором в криволинейную поверхность приспособления.
5. Способ по п. 4, согласно которому уменьшение деформации сжатия на внутреннем радиусе включает увеличение деформации растяжения на внешнем радиусе устройства прессования.
6. Способ по п. 5, согласно которому увеличение деформации растяжения на внешнем радиусе устройства прессования выполнено посредством образования набора щелей во внешнем радиусе устройства прессования.
7. Способ по п. 4, согласно которому
уменьшение деформации сжатия на внутреннем радиусе элемента жесткости из композитного слоистого материала выполнено посредством использования устройства прессования для приложения силы натяжения к внешним концевым частям элемента жесткости из композитного слоистого материала.
8. Устройство для формования профилированного элемента жесткости из композитного слоистого материала, содержащее
профилированное устройство прессования, выполненное с возможностью формования и прессования элемента жесткости из композитного слоистого материала с упором в криволинейную поверхность приспособления, причем
устройство прессования имеет кривизну, превышающую кривизну поверхности приспособления.
9. Устройство по п. 8, в которому устройство прессования выполнено расширяемым и обеспечивающим приложение силы натяжения к элементу жесткости при формовании элемента жесткости с упором в поверхность приспособления.
10. Устройство по п. 9, в котором
устройство прессования имеет шляповидное поперечное сечение, имеющее часть в виде днища, пару частей в виде полок, пару частей в виде стенок, соединяющих часть в виде днища и части в виде полок, причем
часть в виде днища содержит набор отделенных друг от друга щелей.
11. Устройство по п. 8, в котором
устройство прессования содержит участок внутреннего радиуса и участок внешнего радиуса, причем
участок внутреннего радиуса содержит набор щелей, обеспечивающих возможность изгиба устройства прессования.
RU2016129734A 2015-10-06 2016-07-20 Способ и устройство для производства профилированных элементов жесткости из композитного слоистого материала с уменьшенным образованием складок RU2727627C2 (ru)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US14/876,475 2015-10-06
US14/876,475 US10399283B2 (en) 2015-10-06 2015-10-06 Method and device for producing contoured composite laminate stiffeners with reduced wrinkling

Publications (2)

Publication Number Publication Date
RU2016129734A true RU2016129734A (ru) 2018-01-25
RU2727627C2 RU2727627C2 (ru) 2020-07-22

Family

ID=56507450

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2016129734A RU2727627C2 (ru) 2015-10-06 2016-07-20 Способ и устройство для производства профилированных элементов жесткости из композитного слоистого материала с уменьшенным образованием складок

Country Status (6)

Country Link
US (1) US10399283B2 (ru)
EP (1) EP3162544B1 (ru)
CN (2) CN106985488B (ru)
ES (1) ES2760944T3 (ru)
PT (1) PT3162544T (ru)
RU (1) RU2727627C2 (ru)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10392132B2 (en) * 2016-07-29 2019-08-27 The Boeing Company Curved aircraft substructure repair systems and methods
US11104113B2 (en) * 2017-04-19 2021-08-31 The Boeing Company Systems and methods for assembling elongate composite structures
US11833570B2 (en) * 2018-03-30 2023-12-05 Nippon Steel Corporation Method for manufacturing shaped part
EP3623143B1 (en) * 2018-09-11 2021-05-05 Airbus Operations, S.L. Methods for manufacturing curved omega stringers and z shaped stringers of composite material and for manufacturing a composite material stiffened panel with curvature
US11358345B2 (en) * 2019-01-02 2022-06-14 The Boeing Company Internal tooling for composite parts
US20200254702A1 (en) * 2019-02-07 2020-08-13 The Boeing Company Apparatus and method to tailor fiber distortion in composite parts
US11426957B2 (en) * 2019-10-14 2022-08-30 The Boeing Company Flexible caul and method of making the same
US11518121B2 (en) 2019-10-14 2022-12-06 The Boeing Company Constrained creep forming of contoured composite stiffeners
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
CN114193688A (zh) * 2020-09-17 2022-03-18 波音公司 包含平面外特征的复合桁条的净形状形成
EP3970938B1 (en) 2020-09-17 2024-08-07 The Boeing Company Tool and method for forming contoured composite stringers having reduced wrinkling
EP3970939B1 (en) 2020-09-17 2025-03-05 The Boeing Company Constrained forming of contoured composite hat stringers
EP4035877B1 (en) 2021-01-29 2024-05-01 The Boeing Company Forming system and method for forming a contoured composite structure
US11806954B2 (en) 2021-12-14 2023-11-07 The Boeing Company Wrinkle mitigation in contoured composite stiffeners
EP4360858A1 (en) * 2022-10-28 2024-05-01 Airbus Operations, S.L.U. Structural element for aircrafts and method for manufacturing said structural element

Family Cites Families (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3277865D1 (en) 1982-07-19 1988-02-04 Boeing Co Method and apparatus for fiber lamination
US4861406A (en) 1987-08-17 1989-08-29 The Boeing Company Method and apparatus for handling plies of composite material
JPH0245110A (ja) * 1988-08-08 1990-02-15 Piramitsudo:Kk 巻癖を付けた末加硫ゴム部材の巻取用ライナーおよびその製造方法
DE3905520A1 (de) 1989-02-23 1990-08-30 Ullrich Lippert Sicherheitsvorrichtung und verfahren zur bereitstellung von betaetigungseinheiten
JP2765981B2 (ja) * 1989-08-28 1998-06-18 富士重工業株式会社 複合材の折曲成形方法および折曲成形装置
US5348602A (en) * 1993-06-08 1994-09-20 General Electric Company Method for making a bonded laminated article bend portion
US6045651A (en) 1993-09-07 2000-04-04 The Boeing Company Hand assisted lamination system
US5700347A (en) 1996-01-11 1997-12-23 The Boeing Company Thermoplastic multi-tape application head
US7137182B2 (en) 2002-11-22 2006-11-21 The Boeing Company Parallel configuration composite material fabricator
US7534387B2 (en) * 2004-02-25 2009-05-19 The Boeing Company Apparatus and methods for processing composite components using an elastomeric caul
US7357166B2 (en) 2004-11-24 2008-04-15 The Boeing Company Flexible mandrel for highly contoured composite stringer
ES2267367B1 (es) * 2004-12-30 2009-05-01 Airbus España S.L. Procedimiento y util para el encintado de moldes de piezas curvas.
DE102005044823B3 (de) 2005-09-20 2007-05-16 Airbus Gmbh Verfahren und Vorrichtung zum Aufbringen dünner Materiallagen auf eine Reliefform
DE102006031326B4 (de) 2006-07-06 2010-09-23 Airbus Deutschland Gmbh Formkern und Verfahren zur Herstellung eines Faserverbundbauteils für die Luft- und Raumfahrt
US7644491B2 (en) 2006-10-17 2010-01-12 The Boeing Company Device for assembling composite structure incorporating flipper assemblies
US7814644B2 (en) 2006-10-17 2010-10-19 The Boeing Company Positioning assembly for composite structure
US7788784B2 (en) 2006-10-17 2010-09-07 The Boeing Company Method of assembling composite structure
FR2928295B1 (fr) 2008-03-07 2017-12-08 Duqueine Rhone Alpes Procede et dispositif de moulage d'une piece courbe en materiau composite,et piece correspondante.
DE102009029575B4 (de) 2009-09-18 2011-06-22 Airbus Operations GmbH, 21129 Verfahren zur Versteifung eines Faserverbundbauteils und Anordnung zur Herstellung eines versteiften Faserverbundteils
US8997642B2 (en) 2011-08-08 2015-04-07 The Boeing Company Method for transporting, placing and compacting composite stiffeners
US9931807B2 (en) 2011-08-08 2018-04-03 The Boeing Company Flexible compactor with reinforcing spine
FR2991624B1 (fr) 2012-06-12 2015-03-06 Airbus Operations Sas Procede de realisation d'un profile courbe en materiau composite a partir d'une preforme rectiligne de nappes de fibres
US9649809B2 (en) * 2012-11-02 2017-05-16 The Boeing Company Wrinkle diffuser system for composites
DE102014216160A1 (de) * 2014-08-14 2016-02-18 Airbus Operations Gmbh Formkern, Verfahren und System zur Herstellung gekrümmter Verbundkomponenten

Also Published As

Publication number Publication date
CN106985488B (zh) 2020-06-30
RU2727627C2 (ru) 2020-07-22
ES2760944T3 (es) 2020-05-18
EP3162544A1 (en) 2017-05-03
PT3162544T (pt) 2019-11-25
CN106985488A (zh) 2017-07-28
US10399283B2 (en) 2019-09-03
US20170095983A1 (en) 2017-04-06
CN111619188A (zh) 2020-09-04
CN111619188B (zh) 2022-02-08
EP3162544B1 (en) 2019-09-04

Similar Documents

Publication Publication Date Title
RU2016129734A (ru) Способ и устройство для производства профилированных элементов жесткости из композитного слоистого материала с уменьшенным образованием складок
JP2015518772A5 (ru)
CN104619480B (zh) 用于制造带凸缘的构件的设备和制造带凸缘的构件的方法
RU2498903C2 (ru) Элемент жесткости с наклонным участком, устройство и способ для изготовления такого элемента жесткости
WO2015136452A1 (en) Composite structure and manufacturing method thereof
WO2009115736A3 (fr) Procédé et dispositif de moulage d'une pièce courbe en matériau composite, et pièce correspondante
WO2014182825A3 (en) Method of manufacturing a composite material
WO2013006371A3 (en) Glass bending method and apparatus
US10766224B2 (en) Panel made of laminates and method of manufacturing the same
CN106457697A (zh) 用于制造设有单向纤维稀松布的smc构件的方法
WO2016142441A3 (en) Wrapped object, mandrel therefor and method
RU2016150578A (ru) Способ изготовления штампованного изделия и пресс-форма
EP3235629B1 (en) Composite structure and method for molding composite structure
WO2017071852A3 (de) Kernsystem, verwendung des kernsystems bei der herstellung eines faserverbundbauteils sowie verfahren zur herstellung eines faserverbundbauteils
JP5682843B2 (ja) 長繊維強化樹脂成形体とその製造方法
JP6136381B2 (ja) 繊維強化熱可塑性樹脂成形体の製造方法
EP2087951A3 (en) Segmented mandrel for high temperature bonding of metallic axisymmetric shells having complex curvatures
JP2014172241A5 (ja) 繊維強化熱可塑性樹脂成形体の製造方法
JPWO2019188195A5 (ru)
CN110370682A (zh) 一种带角材的大曲率c型框复合材料制件成型方法
FR2963273B1 (fr) Procede de fabrication d'un panneau raidi en materiau composite
WO2016151394A3 (fr) Procede de fabrication d'un composant micromecanique anisotropique
CN103912545B (zh) 组合紧固装置连接件
CN203805454U (zh) Oca光学胶生产装置
CN205498176U (zh) 复合空心板结构