GB2571173B - Layup tools that facilitate transfer of laminates to cure tools - Google Patents

Layup tools that facilitate transfer of laminates to cure tools Download PDF

Info

Publication number
GB2571173B
GB2571173B GB1820204.4A GB201820204A GB2571173B GB 2571173 B GB2571173 B GB 2571173B GB 201820204 A GB201820204 A GB 201820204A GB 2571173 B GB2571173 B GB 2571173B
Authority
GB
United Kingdom
Prior art keywords
tools
laminates
layup
cure
facilitate transfer
Prior art date
Legal status (The legal status 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 status listed.)
Active
Application number
GB1820204.4A
Other versions
GB2571173A (en
GB201820204D0 (en
Inventor
Scott Ingram Timothy
Emile Brochon Timothy
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Boeing Co
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 GB201820204D0 publication Critical patent/GB201820204D0/en
Publication of GB2571173A publication Critical patent/GB2571173A/en
Application granted granted Critical
Publication of GB2571173B publication Critical patent/GB2571173B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • 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
    • B29C70/342Shaping 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 using isostatic pressure
    • 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
    • B29C70/38Automated lay-up, e.g. using robots, laying filaments according to predetermined patterns
    • 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
    • B29C33/00Moulds or cores; Details thereof or accessories therefor
    • B29C33/44Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles
    • B29C33/48Moulds 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Robotics (AREA)
  • Moulding By Coating Moulds (AREA)
GB1820204.4A 2017-12-18 2018-12-12 Layup tools that facilitate transfer of laminates to cure tools Active GB2571173B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US201715545640A 2017-12-18 2017-12-18

Publications (3)

Publication Number Publication Date
GB201820204D0 GB201820204D0 (en) 2019-01-23
GB2571173A GB2571173A (en) 2019-08-21
GB2571173B true GB2571173B (en) 2022-09-07

Family

ID=82839481

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1820204.4A Active GB2571173B (en) 2017-12-18 2018-12-12 Layup tools that facilitate transfer of laminates to cure tools

Country Status (1)

Country Link
GB (1) GB2571173B (en)

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0833733A1 (en) * 1995-05-10 1998-04-08 McDONNELL DOUGLAS CORPORATION Fabrication of large hollow composite structure
US20060145049A1 (en) * 2004-12-01 2006-07-06 The Boeing Company Segmented flexible barrel lay-up mandrel
EP2103404A2 (en) * 2008-03-21 2009-09-23 Rohr, Inc. Apparatus and method for making a tubular composite barrel
US20100154990A1 (en) * 2008-12-19 2010-06-24 Brennan Joseph D Composite stiffener positioning and vacuum bag installation device
EP2747987A2 (en) * 2012-04-12 2014-07-02 Alenia Aermacchi S.p.A. A method of manufacturing single piece fuselage barrels in a composite material

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0833733A1 (en) * 1995-05-10 1998-04-08 McDONNELL DOUGLAS CORPORATION Fabrication of large hollow composite structure
US20060145049A1 (en) * 2004-12-01 2006-07-06 The Boeing Company Segmented flexible barrel lay-up mandrel
EP2103404A2 (en) * 2008-03-21 2009-09-23 Rohr, Inc. Apparatus and method for making a tubular composite barrel
US20100154990A1 (en) * 2008-12-19 2010-06-24 Brennan Joseph D Composite stiffener positioning and vacuum bag installation device
EP2747987A2 (en) * 2012-04-12 2014-07-02 Alenia Aermacchi S.p.A. A method of manufacturing single piece fuselage barrels in a composite material

Also Published As

Publication number Publication date
GB2571173A (en) 2019-08-21
GB201820204D0 (en) 2019-01-23

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