ITTO20060463A1 - EQUIPMENT AND PROCEDURE FOR THE MANUFACTURE OF A FUSELAGE TRUNK - Google Patents

EQUIPMENT AND PROCEDURE FOR THE MANUFACTURE OF A FUSELAGE TRUNK

Info

Publication number
ITTO20060463A1
ITTO20060463A1 ITTO20060463A ITTO20060463A1 IT TO20060463 A1 ITTO20060463 A1 IT TO20060463A1 IT TO20060463 A ITTO20060463 A IT TO20060463A IT TO20060463 A1 ITTO20060463 A1 IT TO20060463A1
Authority
IT
Italy
Prior art keywords
procedure
manufacture
equipment
fuselage
trunk
Prior art date
Application number
Other languages
Italian (it)
Inventor
Claudio Berionni
Adriano Moreggia
Original Assignee
Alenia Aeronautica Spa
Moreggia S P A
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 Aeronautica Spa, Moreggia S P A filed Critical Alenia Aeronautica Spa
Priority to ITTO20060463 priority Critical patent/ITTO20060463A1/en
Priority to PCT/IB2007/052396 priority patent/WO2007148301A2/en
Publication of ITTO20060463A1 publication Critical patent/ITTO20060463A1/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
    • 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
    • B29C53/00—Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
    • B29C53/80—Component parts, details or accessories; Auxiliary operations
    • B29C53/82—Cores or mandrels
    • B29C53/821—Mandrels especially adapted for winding and joining
    • B29C53/824—Mandrels especially adapted for winding and joining collapsible, e.g. elastic or inflatable; with removable parts, e.g. for regular shaped, straight tubular articles
    • 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
    • B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
    • B29C70/38—Automated lay-up, e.g. using robots, laying filaments according to predetermined patterns
    • B29C70/386—Automated tape laying [ATL]
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Robotics (AREA)
  • Moulding By Coating Moulds (AREA)
ITTO20060463 2006-06-23 2006-06-23 EQUIPMENT AND PROCEDURE FOR THE MANUFACTURE OF A FUSELAGE TRUNK ITTO20060463A1 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
ITTO20060463 ITTO20060463A1 (en) 2006-06-23 2006-06-23 EQUIPMENT AND PROCEDURE FOR THE MANUFACTURE OF A FUSELAGE TRUNK
PCT/IB2007/052396 WO2007148301A2 (en) 2006-06-23 2007-06-21 Apparatus and a method for fabricating a fuselage section

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ITTO20060463 ITTO20060463A1 (en) 2006-06-23 2006-06-23 EQUIPMENT AND PROCEDURE FOR THE MANUFACTURE OF A FUSELAGE TRUNK

Publications (1)

Publication Number Publication Date
ITTO20060463A1 true ITTO20060463A1 (en) 2007-12-24

Family

ID=38669090

Family Applications (1)

Application Number Title Priority Date Filing Date
ITTO20060463 ITTO20060463A1 (en) 2006-06-23 2006-06-23 EQUIPMENT AND PROCEDURE FOR THE MANUFACTURE OF A FUSELAGE TRUNK

Country Status (2)

Country Link
IT (1) ITTO20060463A1 (en)
WO (1) WO2007148301A2 (en)

Families Citing this family (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2008025860A1 (en) * 2006-08-31 2008-03-06 Airbus España, S.L. Tubular components for fuselages and methods and tools for producing same
US20090033040A1 (en) * 2007-07-31 2009-02-05 Vought Aircraft Industries, Inc. Automated fiber placement mandrel joint configuration
GB0810870D0 (en) 2008-06-13 2008-07-23 Advanced Composite Components Tooling
DE102009056978A1 (en) * 2009-12-07 2011-06-09 Airbus Operations Gmbh Apparatus and method for producing a fiber composite fuselage shell for an aircraft
FR2953754B1 (en) 2009-12-16 2018-03-02 Airbus Operations TOOLING FOR MANUFACTURING A PANEL OF COMPOSITE MATERIAL, PARTICULARLY AN AIRCRAFT FUSELAGE
JP5576650B2 (en) * 2009-12-25 2014-08-20 川崎重工業株式会社 Molds for manufacturing composite material structures
DE102010051739B3 (en) * 2010-11-19 2011-12-29 Siempelkamp Maschinen- Und Anlagenbau Gmbh & Co. Kg Method and device for producing cylindrical large structures
DE102011010539A1 (en) * 2011-02-07 2012-08-09 Airbus Operations Gmbh An upgrading device and method for producing a fuselage for an aircraft consisting of a fiber composite material
US8955206B2 (en) * 2011-07-12 2015-02-17 The Boeing Company Method and apparatus for creating a layup of reinforcing fibers
GB201116476D0 (en) * 2011-09-26 2011-11-09 Rolls Royce Plc Mandrel for forming a component
WO2013102462A1 (en) * 2012-01-04 2013-07-11 Dencam Composite A/S Master model structure
US8714226B2 (en) * 2012-02-27 2014-05-06 The Boeing Company Automated fiber placement including layup mandrel tool
ITTO20120286A1 (en) * 2012-03-30 2013-10-01 Alenia Aermacchi Spa BINDING SYSTEM SECTORS BELONGING TO A DEVICE FOR THE REALIZATION OF A AIRCRAFT FUSELAGE SECTION
ITTO20120284A1 (en) 2012-03-30 2013-10-01 Alenia Aermacchi Spa DRIVE SYSTEM SECTORS BELONGING TO A DEVICE FOR THE CONSTRUCTION OF A AIRCRAFT FUSELAGE SECTION
ITTO20120285A1 (en) * 2012-03-30 2013-10-01 Alenia Aermacchi Spa SYSTEM FOR LOCKING SECTORS BELONGING TO A DEVICE FOR REALIZING A FUSELAGE SECTION OF A PLANE
ITTO20120287A1 (en) * 2012-03-30 2013-10-01 Alenia Aermacchi Spa POSITIONING SYSTEM SECTORS BELONGING TO A DEVICE FOR THE CONSTRUCTION OF A AIRCRAFT FUSELAGE SECTION
ITTO20120317A1 (en) 2012-04-12 2013-10-13 Alenia Aermacchi Spa PROCEDURE FOR THE MANUFACTURE OF FULL-FULL-TYPE COMPOSITE FUSER-BEARING BARRELS
FR3009992B1 (en) * 2013-08-28 2015-09-11 Aircelle Sa KEY TOOLING AND COMPOSITE PANEL IN PARTICULAR FOR AN AIRCRAFT ENGINE NACELLE MANUFACTURED USING SUCH TOOLS
US9597843B2 (en) * 2014-05-15 2017-03-21 The Boeing Company Method and apparatus for layup tooling
US10173348B2 (en) 2015-09-14 2019-01-08 Bell Helicopter Textron Inc. Modular mandrel for monolithic composite fuselage
US10906210B2 (en) 2017-01-25 2021-02-02 The Boeing Company Mandrel for composite part fabrication and repair
FR3100232B1 (en) 2019-08-30 2022-01-14 Airbus ASSEMBLY COMPRISING A SUPPORT TOWER AND AT LEAST TWO SUPPORT SYSTEMS FOR PANELS OF A FUSELAGE SECTION OF AN AIRCRAFT
US20210299958A1 (en) * 2020-03-28 2021-09-30 Karl Joseph Dodds Gifford Shrinkable platform for 3D printer
EP4015182A1 (en) * 2020-12-18 2022-06-22 The Boeing Company Segmented mandrel for composite fabrication
FR3121383A1 (en) 2021-04-01 2022-10-07 Airbus Operations TOOL FOR MANUFACTURING A SELF-STRAINED PANEL AND METHOD FOR MANUFACTURING A SELF-STRAINED PANEL USING SUCH TOOL
IT202200007511A1 (en) * 2022-04-14 2023-10-14 Leonardo Spa EQUIPMENT AND PROCEDURE FOR THE CREATION OF A STRUCTURAL ELEMENT IN COMPOSITE MATERIAL

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1467476A (en) * 1966-02-03 1967-01-27 Reducible section molding mandrel
DE2011566A1 (en) * 1970-03-11 1971-09-23 Robert Adam & Sohn Ohg Und App Adjustable core for moulding reinforced synt
US4436574A (en) * 1982-12-13 1984-03-13 Eagle-Picher Industries, Inc. Radial mandrel
DE3522233A1 (en) * 1985-06-21 1987-01-02 Basf Ag WINDING THORN FOR THE PRODUCTION OF TUBE BODIES FROM RESIN-DRINKED FIBER STRIPS
CA2299487C (en) * 2000-02-24 2002-08-27 Lembit Siilats Collapsible mandrel
FR2841494B1 (en) * 2002-06-27 2005-11-25 Airbus France KEY MOLDING TOOLS, IN PARTICULAR FOR THE PRODUCTION OF AIR INTAKE WITHOUT ECLISSE
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

Also Published As

Publication number Publication date
WO2007148301A3 (en) 2008-03-06
WO2007148301A2 (en) 2007-12-27

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