IN2014DN08425A - - Google Patents

Info

Publication number
IN2014DN08425A
IN2014DN08425A IN8425DEN2014A IN2014DN08425A IN 2014DN08425 A IN2014DN08425 A IN 2014DN08425A IN 8425DEN2014 A IN8425DEN2014 A IN 8425DEN2014A IN 2014DN08425 A IN2014DN08425 A IN 2014DN08425A
Authority
IN
India
Prior art keywords
skin
forming surface
oml
barrel
tool
Prior art date
Application number
Other languages
English (en)
Inventor
Imparato Sabato Inserra
Pietrantonio Cerreta
Original Assignee
Alenia Aermacchi Spa
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 Alenia Aermacchi Spa filed Critical Alenia Aermacchi Spa
Publication of IN2014DN08425A publication Critical patent/IN2014DN08425A/en

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
    • B29C70/32—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 on a rotating mould, former or core
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B32B37/10—Methods 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
    • B32B37/1018—Methods 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
    • 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
    • B29C33/00—Moulds or cores; Details thereof or accessories therefor
    • B29C33/44—Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles
    • B29C33/48—Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles with means for collapsing or disassembling
    • B29C33/485—Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles with means for collapsing or disassembling cores or mandrels
    • 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
    • B29C70/40—Shaping or impregnating by compression not applied
    • B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/44—Shaping 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
    • B29C70/446—Moulding structures having an axis of symmetry or at least one channel, e.g. tubular structures, frames
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B32B37/0046—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by constructional aspects of the apparatus
    • 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
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/068—Fuselage sections
    • 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
    • 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
    • B64F5/50—Handling or transporting aircraft components
    • 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
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2309/00—Parameters for the laminating or treatment process; Apparatus details
    • B32B2309/60—In a particular environment
    • B32B2309/68—Vacuum
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2605/00—Vehicles
    • B32B2605/18—Aircraft
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Transportation (AREA)
  • Manufacturing & Machinery (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
  • Moulding By Coating Moulds (AREA)
IN8425DEN2014 2012-04-12 2013-04-12 IN2014DN08425A (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
ITTO20120317 ITTO20120317A1 (it) 2012-04-12 2012-04-12 Procedimento per la fabbricazione di barili integrali di fusoliera in materiale composito
PCT/IB2013/052928 WO2013153537A2 (fr) 2012-04-12 2013-04-12 Procédé de fabrication de corps de cylindre en une seule pièce dans un matériau composite

Publications (1)

Publication Number Publication Date
IN2014DN08425A true IN2014DN08425A (fr) 2015-05-08

Family

ID=46051811

Family Applications (1)

Application Number Title Priority Date Filing Date
IN8425DEN2014 IN2014DN08425A (fr) 2012-04-12 2013-04-12

Country Status (9)

Country Link
US (1) US9962917B2 (fr)
EP (1) EP2747987B1 (fr)
JP (1) JP6133968B2 (fr)
CN (1) CN104245288B (fr)
CA (1) CA2866552C (fr)
ES (1) ES2638164T3 (fr)
IN (1) IN2014DN08425A (fr)
IT (1) ITTO20120317A1 (fr)
WO (1) WO2013153537A2 (fr)

Families Citing this family (36)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103644083A (zh) * 2013-12-06 2014-03-19 内蒙古金岗重工有限公司 一种风力发电机的复合材料塔筒及其制备方法和制备模具
CN106132673B (zh) 2014-03-04 2018-03-16 庞巴迪公司 使用透气聚乙烯真空膜形成复合叠层堆叠的方法和装置
KR101573750B1 (ko) 2014-03-24 2015-12-03 동화에이.시.엠. 주식회사 스트링거가 일체화된 항공기 동체 제작방법
US9873500B2 (en) * 2014-09-16 2018-01-23 The Boeing Company Process and apparatus for handling, installing, compacting, splicing, and/or assembling composite stringers
CN104924628B (zh) * 2015-04-29 2017-06-06 中航复合材料有限责任公司 整体复合材料加筋筒体的成型方法、铺叠工装、固化模和长桁定位装置
DE102015120785A1 (de) * 2015-11-30 2017-06-01 Airbus Operations Gmbh Verfahren zur Herstellung eines Fahrzeugkabinenteils
US10723085B2 (en) * 2015-12-17 2020-07-28 Rohr, Inc. Method of extracting mandrel for hollow-hat panel production
US11479333B2 (en) 2016-12-16 2022-10-25 Manuel Torres Martinez Method for manufacturing a one-piece reinforced structure and obtained structure
CN106799851B (zh) * 2016-12-27 2019-07-30 中国商用飞机有限责任公司 基于铺丝技术的复合材料帽形加筋壁板的成型制造方法
GB201704890D0 (en) * 2017-03-28 2017-05-10 Composite Tech And Applications Ltd A tool for manufacturing a composite component
CN107139504B (zh) * 2017-04-01 2019-12-06 中国商用飞机有限责任公司北京民用飞机技术研究中心 复合材料帽形长桁预成型及其加筋壁板固化的芯模及方法
US10926435B2 (en) * 2017-05-03 2021-02-23 The Boeing Company Foam mandrel assembly
US10532828B2 (en) 2017-06-30 2020-01-14 The Boeing Company Apparatus, systems, and methods for automated part installation
US10828851B2 (en) * 2017-07-28 2020-11-10 The Boeing Company Slip sheet with compensation surface
GB2571173B (en) * 2017-12-18 2022-09-07 Boeing Co Layup tools that facilitate transfer of laminates to cure tools
US11407185B2 (en) 2017-12-18 2022-08-09 The Boeing Company Layup tools that facilitate transfer of laminates to cure tools
US10520933B2 (en) 2018-04-13 2019-12-31 The Boeing Company System and method for removing a workpiece from a manufacturing fixture
EP3584150B1 (fr) * 2018-06-19 2024-05-01 Airbus Operations, S.L.U. Procédé de fabrication d'une section arrière d'aéronef et section arrière d'aéronef fabriquée par ledit procédé
US11325688B2 (en) * 2019-05-09 2022-05-10 The Boeing Company Composite stringer and methods for forming a composite stringer
US10857751B2 (en) * 2019-05-09 2020-12-08 The Boeing Company Composite stringer and methods for forming a composite stringer
IT202000018139A1 (it) * 2020-07-27 2022-01-27 Leonardo Spa Procedimento per la fabbricazione di un componente strutturale in materiale composito irrigidito con almeno un corrente
US11866200B2 (en) * 2020-11-18 2024-01-09 The Boeing Company Pulsed line fabrication for a fuselage using work stations
US12077319B2 (en) 2020-11-18 2024-09-03 The Boeing Company Fabrication line, systems, and methods for fuselage sections
NL2027417B1 (en) * 2021-01-26 2022-08-26 Boeing Co Fabrication line, systems, and methods for fuselage sections
JP2022080864A (ja) * 2020-11-18 2022-05-30 ザ・ボーイング・カンパニー 未固化の胴体構成要素のための複合組立
EP4000910B1 (fr) 2020-11-18 2024-02-28 The Boeing Company Ligne, systèmes et procédés de fabrication de sections de fuselage
EP4000841B1 (fr) * 2020-11-18 2025-01-01 The Boeing Company Ensemble composite pour composants de fuselage non durcis
NL2027399B1 (en) * 2021-01-26 2022-08-17 Boeing Co Composite assembly for unhardened fuselage components
US11938689B2 (en) * 2020-11-18 2024-03-26 The Boeing Company Apparatus and method for processing a composite structure
EP4015182A1 (fr) * 2020-12-18 2022-06-22 The Boeing Company Mandrin segmenté pour fabrication composite
AU2021414394A1 (en) 2020-12-28 2023-07-20 Leonardo S.P.A. Method for the manufacture of a structural component in composite material reinforced with stiffening stringers and structural component
US11660829B2 (en) 2021-02-09 2023-05-30 Spirit Aerosystems, Inc. Method of seamlessly bagging composite parts
TR2021012137A2 (tr) * 2021-07-30 2023-02-21 Tusas Tuerk Havacilik Ve Uzay Sanayii Anonim Sirketi Bir kompozit üretim sistemi.
CN114654633B (zh) * 2022-04-24 2023-08-22 盐城鸿源环保科技有限公司 一种钢衬塑储罐辅助生产加工设备
CN115871251A (zh) * 2022-12-06 2023-03-31 溧阳二十八所系统装备有限公司 真空辅助成型系统及其使用方法
CN116461118A (zh) * 2023-04-06 2023-07-21 中航复合材料有限责任公司 一种复合材料机身筒段整体成型方法

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2935722B2 (ja) * 1990-02-28 1999-08-16 富士重工業株式会社 航空機の胴体構造およびその成形方法
US6510961B1 (en) * 1999-04-14 2003-01-28 A&P Technology Integrally-reinforced braided tubular structure and method of producing the same
US7083698B2 (en) 2003-08-22 2006-08-01 The Boeing Company Automated composite lay-up to an internal fuselage mandrel
US7048024B2 (en) 2003-08-22 2006-05-23 The Boeing Company Unidirectional, multi-head fiber placement
US7282107B2 (en) 2003-08-22 2007-10-16 The Boeing Company Multiple head automated composite laminating machine for the fabrication of large barrel section components
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
US7503368B2 (en) * 2004-11-24 2009-03-17 The Boeing Company Composite sections for aircraft fuselages and other structures, and methods and systems for manufacturing such sections
ITTO20060463A1 (it) 2006-06-23 2007-12-24 Alenia Aeronautica Spa Apparecchiatura e procedimento per la fabbricazione di un tronco di fusoliera
DE102007027113B4 (de) * 2007-06-13 2013-09-12 Airbus Operations Gmbh Verfahren zur Fertigung von Rumpfzellenabschnitten für Flugzeuge aus Faserverbundwerkstoffen sowie Vorrichtung
DE102007060029A1 (de) * 2007-12-13 2009-06-18 Airbus Deutschland Gmbh Verfahren und Vorrichtung zur Herstellung röhrenförmiger Strukturbauteile
DE102009056978A1 (de) 2009-12-07 2011-06-09 Airbus Operations Gmbh Vorrichtung und Verfahren zur Herstellung einer aus einem Faserverbundwerkstoff bestehenden Rumpfschale für ein Luftfahrzeug
JP5576651B2 (ja) * 2009-12-25 2014-08-20 川崎重工業株式会社 複合材料構造物製造用マンドレルの組立方法およびマンドレルの組立装置

Also Published As

Publication number Publication date
ITTO20120317A1 (it) 2013-10-13
CA2866552A1 (fr) 2013-10-17
WO2013153537A2 (fr) 2013-10-17
EP2747987B1 (fr) 2017-05-24
CN104245288B (zh) 2016-11-23
JP6133968B2 (ja) 2017-05-24
US20150122413A1 (en) 2015-05-07
CN104245288A (zh) 2014-12-24
CA2866552C (fr) 2019-09-03
JP2015519225A (ja) 2015-07-09
WO2013153537A3 (fr) 2013-12-05
US9962917B2 (en) 2018-05-08
EP2747987A2 (fr) 2014-07-02
ES2638164T3 (es) 2017-10-19

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