ATE513666T1 - Maschine und verfahren zum bilden eines holms aus verbundwerkstoff durch drapieren - Google Patents

Maschine und verfahren zum bilden eines holms aus verbundwerkstoff durch drapieren

Info

Publication number
ATE513666T1
ATE513666T1 AT03077556T AT03077556T ATE513666T1 AT E513666 T1 ATE513666 T1 AT E513666T1 AT 03077556 T AT03077556 T AT 03077556T AT 03077556 T AT03077556 T AT 03077556T AT E513666 T1 ATE513666 T1 AT E513666T1
Authority
AT
Austria
Prior art keywords
mandrel
forming
machine
frame
draping
Prior art date
Application number
AT03077556T
Other languages
English (en)
Inventor
Kurtis S Willden
Raymond N Henderson
Gary E Pfitzner
Surenda R Parekh
Christopher G Harris
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
Application granted granted Critical
Publication of ATE513666T1 publication Critical patent/ATE513666T1/de

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
    • B29C70/34—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 and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation
    • B29C70/342—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 and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation using isostatic pressure
    • 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
    • B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
    • B29C70/541—Positioning reinforcements in a mould, e.g. using clamping means for the reinforcement
    • 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
    • B29C33/30—Mounting, exchanging or centering
    • B29C33/307—Mould plates mounted on frames; Mounting the mould plates; Frame constructions therefor
    • 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
    • B29C51/00—Shaping by thermoforming, i.e. shaping sheets or sheet like preforms after heating, e.g. shaping sheets in matched moulds or by deep-drawing; Apparatus therefor
    • B29C51/08—Deep drawing or matched-mould forming, i.e. using mechanical means only
    • B29C51/082—Deep drawing or matched-mould forming, i.e. using mechanical means only by shaping between complementary mould parts
    • B29C51/087—Deep drawing or matched-mould forming, i.e. using mechanical means only by shaping between complementary mould parts with at least one of the mould parts comprising independently movable sections

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Composite Materials (AREA)
  • Mechanical Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
AT03077556T 2002-08-30 2003-08-14 Maschine und verfahren zum bilden eines holms aus verbundwerkstoff durch drapieren ATE513666T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US10/233,269 US7118370B2 (en) 2002-08-30 2002-08-30 Composite spar drape forming machine

Publications (1)

Publication Number Publication Date
ATE513666T1 true ATE513666T1 (de) 2011-07-15

Family

ID=31495413

Family Applications (1)

Application Number Title Priority Date Filing Date
AT03077556T ATE513666T1 (de) 2002-08-30 2003-08-14 Maschine und verfahren zum bilden eines holms aus verbundwerkstoff durch drapieren

Country Status (5)

Country Link
US (3) US7118370B2 (de)
EP (1) EP1393873B1 (de)
AT (1) ATE513666T1 (de)
CA (2) CA2436031C (de)
ES (1) ES2365702T3 (de)

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US7968169B2 (en) * 2007-08-07 2011-06-28 The Boeing Company Compound contoured composite beams and fabrication methods
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US11865825B2 (en) * 2019-10-14 2024-01-09 The Boeing Company System, method, and apparatus for use in ply compaction in forming a composite structure
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US11498288B2 (en) 2020-02-11 2022-11-15 The Boeing Company Forming systems and methods for drape forming a composite charge
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Also Published As

Publication number Publication date
US7651650B2 (en) 2010-01-26
US8236222B2 (en) 2012-08-07
CA2663905A1 (en) 2004-02-29
US20040041304A1 (en) 2004-03-04
CA2436031A1 (en) 2004-02-29
CA2436031C (en) 2009-11-03
ES2365702T3 (es) 2011-10-10
US7118370B2 (en) 2006-10-10
US20100043941A1 (en) 2010-02-25
US20060291991A1 (en) 2006-12-28
EP1393873A3 (de) 2007-07-25
CA2663905C (en) 2011-07-12
EP1393873A2 (de) 2004-03-03
EP1393873B1 (de) 2011-06-22

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