ITTO20120317A1 - Procedimento per la fabbricazione di barili integrali di fusoliera in materiale composito - Google Patents

Procedimento per la fabbricazione di barili integrali di fusoliera in materiale composito

Info

Publication number
ITTO20120317A1
ITTO20120317A1 ITTO20120317A ITTO20120317A1 IT TO20120317 A1 ITTO20120317 A1 IT TO20120317A1 IT TO20120317 A ITTO20120317 A IT TO20120317A IT TO20120317 A1 ITTO20120317 A1 IT TO20120317A1
Authority
IT
Italy
Prior art keywords
full
skin
forming surface
oml
barrel
Prior art date
Application number
Other languages
English (en)
Inventor
Pietro Cerreta
Imparato Sabato Inserra
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
Priority to ITTO20120317 priority Critical patent/ITTO20120317A1/it
Priority to CA2866552A priority patent/CA2866552C/en
Priority to US14/394,005 priority patent/US9962917B2/en
Priority to CN201380019422.7A priority patent/CN104245288B/zh
Priority to IN8425DEN2014 priority patent/IN2014DN08425A/en
Priority to EP13725785.3A priority patent/EP2747987B1/en
Priority to ES13725785.3T priority patent/ES2638164T3/es
Priority to PCT/IB2013/052928 priority patent/WO2013153537A2/en
Priority to JP2015505063A priority patent/JP6133968B2/ja
Publication of ITTO20120317A1 publication Critical patent/ITTO20120317A1/it

Links

Classifications

    • 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
    • B29C70/30—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
    • 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)
ITTO20120317 2012-04-12 2012-04-12 Procedimento per la fabbricazione di barili integrali di fusoliera in materiale composito ITTO20120317A1 (it)

Priority Applications (9)

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
CA2866552A CA2866552C (en) 2012-04-12 2013-04-12 A method of manufacturing single piece fuselage barrels in composite material
US14/394,005 US9962917B2 (en) 2012-04-12 2013-04-12 Method of manufacturing single piece fuselage barrels in composite material
CN201380019422.7A CN104245288B (zh) 2012-04-12 2013-04-12 制造以单片式复合材料制成的机身筒的方法
IN8425DEN2014 IN2014DN08425A (it) 2012-04-12 2013-04-12
EP13725785.3A EP2747987B1 (en) 2012-04-12 2013-04-12 A method of manufacturing single piece fuselage barrels in a composite material
ES13725785.3T ES2638164T3 (es) 2012-04-12 2013-04-12 Un procedimiento de fabricación de cuerpos cilíndricos de fuselaje de una sola pieza en un material compuesto
PCT/IB2013/052928 WO2013153537A2 (en) 2012-04-12 2013-04-12 A method of manufacturing single piece fuselage barrels in a composite material
JP2015505063A JP6133968B2 (ja) 2012-04-12 2013-04-12 複合材料の単体の機体胴部を製作する方法

Applications Claiming Priority (1)

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

Publications (1)

Publication Number Publication Date
ITTO20120317A1 true ITTO20120317A1 (it) 2013-10-13

Family

ID=46051811

Family Applications (1)

Application Number Title Priority Date Filing Date
ITTO20120317 ITTO20120317A1 (it) 2012-04-12 2012-04-12 Procedimento per la fabbricazione di barili integrali di fusoliera in materiale composito

Country Status (9)

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

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US10293559B2 (en) 2014-03-04 2019-05-21 Bombardier Inc. Method and apparatus for forming a composite laminate stack using a breathable polyethylene vacuum film
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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
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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
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ES2981087T3 (es) * 2018-06-19 2024-10-07 Airbus Operations Slu Procedimiento de fabricación de una sección trasera de una aeronave y sección trasera de aeronave fabricada según dicho procedimiento
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
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
JP2022080870A (ja) * 2020-11-18 2022-05-30 ザ・ボーイング・カンパニー 複合構造を処理するための装置及び方法
NL2027399B1 (en) * 2021-01-26 2022-08-17 Boeing Co Composite assembly for unhardened fuselage components
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US12077319B2 (en) 2020-11-18 2024-09-03 The Boeing Company Fabrication line, systems, and methods for fuselage sections
US11866200B2 (en) * 2020-11-18 2024-01-09 The Boeing Company Pulsed line fabrication for a fuselage using work stations
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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

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US20090139641A1 (en) * 2004-11-24 2009-06-04 The Boeing Company Composite sections for aircraft fuselages and other structures, and methods and systems for manufacturing such sections
DE102007027113A1 (de) * 2007-06-13 2008-12-18 Airbus Deutschland Gmbh Verfahren zur Fertigung von Rumpfzellenabschnitten für Flugzeuge mit Faserverbundwerkstoffen sowie Vorrichtung
DE102007060029A1 (de) * 2007-12-13 2009-06-18 Airbus Deutschland Gmbh Verfahren und Vorrichtung zur Herstellung röhrenförmiger Strukturbauteile
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Also Published As

Publication number Publication date
EP2747987A2 (en) 2014-07-02
WO2013153537A3 (en) 2013-12-05
ES2638164T3 (es) 2017-10-19
EP2747987B1 (en) 2017-05-24
WO2013153537A2 (en) 2013-10-17
CA2866552C (en) 2019-09-03
JP2015519225A (ja) 2015-07-09
CN104245288A (zh) 2014-12-24
CA2866552A1 (en) 2013-10-17
US9962917B2 (en) 2018-05-08
CN104245288B (zh) 2016-11-23
IN2014DN08425A (it) 2015-05-08
US20150122413A1 (en) 2015-05-07
JP6133968B2 (ja) 2017-05-24

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