JP2007062150A5 - - Google Patents

Download PDF

Info

Publication number
JP2007062150A5
JP2007062150A5 JP2005251033A JP2005251033A JP2007062150A5 JP 2007062150 A5 JP2007062150 A5 JP 2007062150A5 JP 2005251033 A JP2005251033 A JP 2005251033A JP 2005251033 A JP2005251033 A JP 2005251033A JP 2007062150 A5 JP2007062150 A5 JP 2007062150A5
Authority
JP
Japan
Prior art keywords
mold
regions
design layer
reinforcing fiber
main body
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.)
Granted
Application number
JP2005251033A
Other languages
Japanese (ja)
Other versions
JP4826176B2 (en
JP2007062150A (en
Filing date
Publication date
Application filed filed Critical
Priority to JP2005251033A priority Critical patent/JP4826176B2/en
Priority claimed from JP2005251033A external-priority patent/JP4826176B2/en
Publication of JP2007062150A publication Critical patent/JP2007062150A/en
Publication of JP2007062150A5 publication Critical patent/JP2007062150A5/ja
Application granted granted Critical
Publication of JP4826176B2 publication Critical patent/JP4826176B2/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Claims (6)

中空中子に配設された強化繊維の本体層と該本体層表面を覆う意匠層を含む強化繊維プリフォームであって、該意匠層は2以上の型からなる成形型の各型に対応する2以上の領域からなり、該領域間の境界部を対応する型のパーティング部に設けたことを特徴とする強化繊維プリフォーム。   A reinforcing fiber preform including a main body layer of reinforcing fibers disposed in a hollow core and a design layer covering the surface of the main body layer, wherein the design layer corresponds to each mold of a two or more molds A reinforcing fiber preform comprising two or more regions, wherein a boundary portion between the regions is provided in a corresponding parting portion. 前記領域間の意匠層の継ぎ目が型のパーティング部で挟むことができるように突出していることを特徴とする請求項1に記載の強化繊維プリフォーム。   The reinforcing fiber preform according to claim 1, wherein a seam of the design layer between the regions protrudes so as to be sandwiched between parting portions of the mold. 前記中空中子がブロー成形体であることを特徴とする請求項1または2のいずれかに記載の強化繊維プリフォーム。 Reinforcing fibers preform according to claim 1 or 2, wherein the in Kuchuko is blow molded article. 中空中子に配設された強化繊維の本体層と、該本体層表面を覆う2以上の型からなる成形型の各型に対応する2以上の領域からなる意匠層を含む強化繊維プリフォームを、意匠層の各領域間の境界部が成形型のパーティング部で挟圧させるように成形型に載置し、前記中空中子を圧空で膨張させながら圧空圧と同圧又は低圧で樹脂を加圧注入して含浸、硬化させて成形することを特徴とする中空構造FRPのRTM成形方法。   A reinforcing fiber preform including a reinforcing fiber main body layer disposed in a hollow core and a design layer including two or more regions corresponding to each mold of the two or more molds covering the surface of the main body layer. The design layer is placed on the mold so that the boundary between the regions of the design layer is clamped by the parting part of the mold, and the resin is applied at the same or low pressure as the pneumatic pressure while the hollow core is expanded with the compressed air. A method for RTM molding of a hollow structure FRP, wherein the molding is performed by pressure injection, impregnation and curing. 意匠層の領域間の境界部を型で挟圧した後に中空中子に圧空を封入することを特徴とする請求項に記載の中空構造FRPのRTM成形方法。 5. The method for RTM molding of a hollow structure FRP according to claim 4 , wherein the air pressure is sealed in the hollow core after the boundary between the regions of the design layer is clamped with a mold. 成形後、中空中子を一旦減圧し、上型を開放した状態で低圧の圧空を中子に封入して脱型することを特徴とする請求項またはのいずれかに記載の中空構造FRPのRTM成
形方法。
After molding, once reduced pressure a hollow core, hollow structure according to the low pressure of the compressed air in the open state of the upper mold to claim 4 or 5, characterized in that demolding enclosed in the core FRP RTM molding method.
JP2005251033A 2005-08-31 2005-08-31 Reinforcing fiber preform and RTM molding method Expired - Fee Related JP4826176B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2005251033A JP4826176B2 (en) 2005-08-31 2005-08-31 Reinforcing fiber preform and RTM molding method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2005251033A JP4826176B2 (en) 2005-08-31 2005-08-31 Reinforcing fiber preform and RTM molding method

Publications (3)

Publication Number Publication Date
JP2007062150A JP2007062150A (en) 2007-03-15
JP2007062150A5 true JP2007062150A5 (en) 2008-10-16
JP4826176B2 JP4826176B2 (en) 2011-11-30

Family

ID=37924924

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2005251033A Expired - Fee Related JP4826176B2 (en) 2005-08-31 2005-08-31 Reinforcing fiber preform and RTM molding method

Country Status (1)

Country Link
JP (1) JP4826176B2 (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102007060029A1 (en) * 2007-12-13 2009-06-18 Airbus Deutschland Gmbh Method and device for producing tubular structural components
JP2013022835A (en) * 2011-07-21 2013-02-04 Mitsubishi Heavy Ind Ltd Method and apparatus for producing at least two products including fiber-reinforced resin
WO2014163297A1 (en) * 2013-04-03 2014-10-09 주식회사 지우테크 Panel member for commercial vehicle container
FR3059934B1 (en) * 2016-12-14 2018-11-30 Safran Aircraft Engines A NEEDLE IMPREGNATION MOLD FOR PRODUCING A WORKPIECE FROM A WOVEN PREFORM

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0272935A (en) * 1988-09-08 1990-03-13 Toyota Motor Corp Molding method of hollow body made of fibre reinforced plastic
JPH03208625A (en) * 1990-01-12 1991-09-11 Mitsubishi Electric Corp Production of hollow structure made of fiber reinforced composite material
JPH04103319A (en) * 1990-08-24 1992-04-06 Mitsubishi Motors Corp Hollow resin injection molding method

Similar Documents

Publication Publication Date Title
US11000977B2 (en) Molding method for fiber-reinforced plastic structure and vehicle wheel
AU2003200918B2 (en) A method for the manufacture of a component by composite fibre construction
CN101143492A (en) Compression type RTM forming method
RU2009103204A (en) METHOD FOR PRODUCING A CONSTRUCTIVE COMPONENT FROM FIBER REINFORCED COMPOSITE MATERIAL FOR THE AEROSPACE INDUSTRY, SHAPED ROD FOR MANUFACTURING THIS COMPONENT AND A CONSTRUCTIVE COMPONENT
CN103496179A (en) Molding method for composite material structural member with I-shaped section
CN104589670B (en) A kind of gas path design method of composite cavity structure air bag shaping
DK2030763T3 (en) Evacuation process for use in a process for making a composite structure
WO2018133177A1 (en) Application of hsm process in wing moulding and method for moulding wing
JP2007062150A5 (en)
JP2009202440A5 (en)
CN106891546A (en) A kind of forming method for becoming wall thickness composite skirt
KR20130105013A (en) Light-resin transfer molding for fiber-reinforced plastic
JP2009073070A5 (en)
CN108032529A (en) A kind of thermoplasticity answers material molding component core preparation method
CN103692580A (en) Die for making composite material curved pipe and making method thereof
ATE265312T1 (en) METHOD FOR PRODUCING A PROFILED, BOWL-LIKE OBJECT AND A MOLD USABLE FOR THIS
CN202137957U (en) RTM (resin transfer molding) soft mould
JP2003094448A (en) Manufacturing method for frp hollow structure
ATE323590T1 (en) METHOD FOR SHAPING A FIBER REINFORCED PLASTIC RESIN ARTICLE AND FIBER REINFORCED PLASTIC RESIN ARTICLE
JP2007196685A5 (en)
CN110142985B (en) Paving and curing integrated core mold and application method thereof
CN100500406C (en) Air pressure forming method for producing glass fibre reinforced plastic
Michaeli et al. Production of structural hollow fibre reinforced components using a combined RTM and blow-up technology
JP2007038689A5 (en)
CN201325131Y (en) Auxiliary perform mandrel model for carbon fiber product production