JPH08290479A - Molding method for composite material - Google Patents
Molding method for composite materialInfo
- Publication number
- JPH08290479A JPH08290479A JP7095330A JP9533095A JPH08290479A JP H08290479 A JPH08290479 A JP H08290479A JP 7095330 A JP7095330 A JP 7095330A JP 9533095 A JP9533095 A JP 9533095A JP H08290479 A JPH08290479 A JP H08290479A
- Authority
- JP
- Japan
- Prior art keywords
- molding
- preformed
- product
- mold
- pressure
- 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.)
- Pending
Links
Landscapes
- Laminated Bodies (AREA)
- Moulding By Coating Moulds (AREA)
Abstract
Description
【0001】[0001]
【産業上の利用分野】本発明は、複合材料、特に先進複
合材料(ACM)の成形方法の改良に関するものであ
る。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to an improved molding method for composite materials, especially advanced composite materials (ACM).
【0002】[0002]
【従来の技術】いわゆる先進複合材料(ACM)の成形
品については、炭素繊維、ガラス繊維等の補強繊維と熱
硬化性樹脂からなる成形中間材料を積層し、オートクレ
ーブ、真空バッグ、プレスなどの加圧成形法により、各
種成形物を得ている。オートクレーブ成形法では複雑曲
面成形物を高品質に得ることができるが、成形準備工程
が煩雑で、成形時間も長く、大量生産には向いていな
い。一方真空バッグ成形法は設備の制約が少なくなる
が、基本的には、オートクレーブ成形と同一工程をとる
必要があり、ピンホール、ボイド等の材料欠陥の面で
は、オートクレーブ法にやや劣る。またプレス成形法は
サイクルアップが可能でピンホール等の少ないものが得
られるが、形状、サイズに制約があり、型代が膨大にな
り、コスト的問題が生じることが多い。2. Description of the Related Art For molded articles of so-called advanced composite materials (ACM), reinforcing fibers such as carbon fibers and glass fibers and a molding intermediate material made of thermosetting resin are laminated and added to an autoclave, a vacuum bag, a press or the like. Various molded products are obtained by the pressure molding method. With the autoclave molding method, a complicated curved surface molded product can be obtained with high quality, but the molding preparation process is complicated, the molding time is long, and it is not suitable for mass production. On the other hand, the vacuum bag molding method is less restricted in equipment, but basically requires the same process as the autoclave molding, and is slightly inferior to the autoclave method in terms of material defects such as pinholes and voids. In addition, the press molding method can be cycled up with few pinholes and the like, but the shape and size are limited, the die cost becomes enormous, and cost problems often occur.
【0003】[0003]
【発明が解決しようとする課題】高性能先進複合材料
(ACM)の性能を落とすことなく、生産性を上げ、量
産に対応できる体制を創ることは、この業界の発展には
不可欠の要素であるが、従来の成形技術には、上述の通
り一長一短があり、未だ満足のいく成形法がないのが実
状である。本発明は一般工業用途のACM成形に適す
る、比較的低温で且つ短時間で成形可能な複合材料の成
形方法を提供するものである。[Problems to be Solved by the Invention] It is an essential element for the development of this industry to improve productivity and create a system capable of mass production without deteriorating the performance of high performance advanced composite materials (ACM). However, the conventional molding technique has advantages and disadvantages as described above, and in reality, there is no satisfactory molding method. The present invention provides a molding method of a composite material, which is suitable for ACM molding for general industrial use and can be molded at a relatively low temperature in a short time.
【0004】[0004]
【課題を解決するための手段】即ち、本発明の要旨は、
強化繊維と熱硬化性樹脂からなる成形中間材料を積層し
て60℃以下の温度で予備成形し、加熱温度調節可能な
成形型にセットして、伸縮性フィルムを介して成形物側
を減圧バッグにより脱気する工程と、伸縮性フィルムを
介して加熱気体で加圧する工程とを経て、型及び加熱気
体により加圧加熱硬化させることを特徴とする複合材料
の成形方法にある。That is, the gist of the present invention is as follows.
A molding intermediate material consisting of reinforced fiber and thermosetting resin is laminated, preformed at a temperature of 60 ° C or less, set in a mold capable of adjusting heating temperature, and a decompression bag is formed on the side of the molded product through an elastic film. And a step of pressurizing with heated gas through the stretchable film, followed by press-heating and curing with a mold and heated gas.
【0005】本発明で用いる成形中間材料としては、炭
素繊維、アラミド繊維、ガラス繊維、アルミナ繊維など
いわゆる高強度高弾性率繊維に対して、70〜130℃
の比較的低温で硬化可能なエポキシ樹脂、不飽和ポリエ
ステル樹脂、ビニルエステル樹脂、フェノール樹脂から
選ばれる熱硬化性樹脂を含浸した成形中間材料が挙げら
れるが、その形態は、織物、一方向引き揃えシート、短
繊維の各種配向シートなど、通常の加圧成形加工に用い
られる材料や、ロービングプリプレグ、シートモールデ
ィングコンパウンドなどが挙げられる。プリプレグと
は、これらの織物、一方向引き揃えシート、ロービング
などに、エポキシ、ビニルエステル、フェノール系など
の熱硬化型樹脂を、溶液含浸法、フィルム含浸法などで
含浸した、未硬化でタックを有する樹脂含浸中間材料を
さす。このようなプリプレグは型に沿わせて積層し、加
圧下加熱すると、型形状に合った成形物となる成形中間
材料である。The molding intermediate material used in the present invention is 70 to 130 ° C. for so-called high strength and high elastic modulus fibers such as carbon fiber, aramid fiber, glass fiber and alumina fiber.
Molding intermediate materials impregnated with a thermosetting resin selected from epoxy resins, unsaturated polyester resins, vinyl ester resins, and phenolic resins, which can be cured at relatively low temperatures, include woven fabrics and unidirectionally aligned materials. Examples of the material include materials used for ordinary pressure molding such as sheets and various oriented sheets of short fibers, roving prepreg, and sheet molding compounds. A prepreg is an uncured tack obtained by impregnating these woven fabrics, unidirectionally aligned sheets, rovings, etc., with a thermosetting resin such as epoxy, vinyl ester, or phenol by a solution impregnation method or a film impregnation method. It refers to the resin-impregnated intermediate material that it has. Such a prepreg is a molding intermediate material that is laminated along a mold and is heated under pressure to form a molded product that matches the shape of the mold.
【0006】本発明では、これらの成形中間材料に対
し、成形サイクルを上げるための、種々の工夫が組み合
わされて採用される。まず、成形中間材料を成形品の賦
形に必要なパターンにカットして積層し、60℃以下の
加熱下で予備成形(プリフォーム)する。得られた予備
成形品を加熱温度調節可能な成形型にセットする。In the present invention, these molding intermediate materials are employed in combination with various measures for increasing the molding cycle. First, a molding intermediate material is cut into a pattern necessary for shaping a molded product, laminated, and preformed (preform) under heating at 60 ° C. or less. The preform thus obtained is set in a mold whose heating temperature can be adjusted.
【0007】次いで、加圧加熱成形する方法として、本
発明では、伸縮可変性を有する真空圧空成形機を用いた
成形法を採用する。つまり、加熱可能な型を下面に配
し、伸縮性ゴム系フィルムで下部を形成する加熱加圧気
体箱体上面板を有する真空圧空成形機(図1)によっ
て、予備成形された成形中間材料の上部に伸縮性フィル
ムをフィットさせ、減圧にして、予備成形品の脱気を行
い、次いで伸縮性フィルム箱に加圧加熱空気を流入し
て、加圧加熱することで成形物を得るのである。Next, as the method of pressure heating and molding, in the present invention, a molding method using a vacuum pressure air molding machine having expansion and contraction variability is adopted. That is, a heatable mold is arranged on the lower surface, and a vacuum pressure air molding machine (FIG. 1) having a heating and pressurizing gas box upper surface plate that forms a lower portion with a stretchable rubber-based film is used to form a preformed intermediate material. A stretched film is fitted on the upper part, the pressure is reduced, the preform is degassed, and then pressurized heated air is flown into the stretchable film box to be heated under pressure to obtain a molded product.
【0008】この方法によれば、オートクレーブ成形や
真空バック成形のように、真空バッグ形成のための手間
が不要であり、加圧工程を組み合わせるため、真空バッ
グ成形より、ピンホールやボイドの少ない製品が得られ
る。また加熱温度の設定を適宜選ぶことにより、比較的
低温低圧で、短時間に成形が行えるので量産成形、低コ
スト成形法として極めて有用である。尚、本発明の予備
成形の段階で必要に応じて、密着性のよいゲルコートを
施しておき、表面層に問題になるようなピンホールのな
い成形物を形成することも可能である。According to this method, unlike the autoclave molding and the vacuum bag molding, the labor for forming the vacuum bag is unnecessary, and since the pressurizing process is combined, the product having less pinholes and voids than the vacuum bag molding. Is obtained. Further, by appropriately selecting the setting of the heating temperature, it is possible to perform molding at a relatively low temperature and low pressure in a short time, which is extremely useful as a mass production molding and a low cost molding method. If necessary, a gel coat having good adhesiveness may be applied at the stage of preforming of the present invention to form a pinhole-free molded product having a problem in the surface layer.
【0009】[0009]
【実施例】本発明を実施例により更に具体的に説明す
る。 (実施例1)三菱レイヨン(株)製弾性率24トン/m
m2 、3000フィラメントの炭素繊維クロスを作製
し、80℃硬化型エポキシ樹脂を含浸して、成形中間材
料(A)を作製した。次いで自転車ホイルの予備成形型
を用いて、パターンカットされた前記成形中間材料
(A)を積層し、真空ドレープ成形法によって、50℃
で1気圧の加圧により予備成形してホイル2つのシェル
を得た。この予備成形された表裏のシェルを図1に示す
真空圧空成形機を用いて、加熱可能な成形型15にセッ
トし、伸縮性シリコンゴムフィルム8で被覆された空間
を減圧として予備成形品の脱気を行い、ヒーターの加熱
を開始し、上面圧空箱に空気加熱機19を介して加熱加
圧気体を導入することにより3kg/mm2 、120℃
で15分間、加圧加熱成形を行った。これにより得られ
たホイルシェルは、表面にはピンホールは殆ど発生して
おらず、続く接合工程、クリアー塗装によって、綺麗な
表面の炭素繊維強化樹脂製自転車ホイルとすることがで
きた。このときの成形サイクル時間は30分であった。EXAMPLES The present invention will be described more specifically by way of examples. (Example 1) Elastic modulus of 24 tons / m manufactured by Mitsubishi Rayon Co., Ltd.
A carbon fiber cloth having m 2 and 3000 filaments was prepared and impregnated with a 80 ° C. curable epoxy resin to prepare a molding intermediate material (A). Then, the pattern-cut molding intermediate material (A) is laminated using a bicycle wheel preforming mold, and the temperature is 50 ° C. by a vacuum drape molding method.
It was preformed by pressurizing at 1 atm to obtain two shells of foil. The preformed front and back shells are set in a mold 15 which can be heated by using the vacuum pressure air forming machine shown in FIG. 1, and the space covered with the elastic silicone rubber film 8 is depressurized to remove the preformed product. 3 kg / mm 2 , 120 ° C. by heating and starting heating of the heater, and introducing heated pressurized gas into the upper surface compressed air box through the air heater 19.
And heat-molded under pressure for 15 minutes. The foil shell thus obtained had almost no pinholes on its surface, and a carbon fiber reinforced resin bicycle wheel having a clean surface could be obtained by the subsequent joining step and clear coating. The molding cycle time at this time was 30 minutes.
【0010】尚、比較のために従来のオートクレーブ成
形法で同様の成形品を製造したところ6時間の成形サイ
クルが必要であった。また成形副資材のロスが大きかっ
た。For comparison, when a similar molded product was manufactured by the conventional autoclave molding method, a molding cycle of 6 hours was required. Also, the loss of molding auxiliary materials was large.
【0011】[0011]
【発明の効果】本発明によれば、成形中間材料を比較的
低温で予備成形した後、真空圧空成形法を組み合わせ
て、加圧加熱成形することにより、比較的低温で且つ短
時間で高性能の複合材料を得ることができる。According to the present invention, by performing preforming of a molding intermediate material at a relatively low temperature and then combining with a vacuum pressure air molding method, press-heating molding can be performed, thereby achieving high performance at a relatively low temperature in a short time. Can be obtained.
【図1】本発明の実施に使用する装置の一例を示す断面
図である。FIG. 1 is a sectional view showing an example of an apparatus used for carrying out the present invention.
1 ベースワーク 2 ヒータ 3 真空ライン 4 プレスワーク 5 コンプレッサ 6 圧空貯蔵タンク 7 圧空バルブ 8 伸縮性フィルム 9 シール 10 ヒータ 11 送風ファン 12 減圧バルブ 13 フレーム 14 油圧シリンダー 15 成形型 16 プリプレグ 17 ブリードクロス 18 真空ポンプ 19 空気加熱機 1 Basework 2 Heater 3 Vacuum Line 4 Presswork 5 Compressor 6 Compressed Air Storage Tank 7 Compressed Air Valve 8 Stretchable Film 9 Seal 10 Heater 11 Blower Fan 12 Pressure Reduction Valve 13 Frame 14 Hydraulic Cylinder 15 Mold 16 Prepreg 17 Bleed Cross 18 Vacuum Pump 19 Air heater
───────────────────────────────────────────────────── フロントページの続き (51)Int.Cl.6 識別記号 庁内整理番号 FI 技術表示箇所 B29L 9:00 ─────────────────────────────────────────────────── ─── Continuation of the front page (51) Int.Cl. 6 Identification code Internal reference number FI technical display location B29L 9:00
Claims (1)
間材料を積層して60℃以下の温度で予備成形し、加熱
温度調節可能な成形型にセットして、伸縮性フィルムを
介して成形物側を減圧バッグにより脱気する工程と、伸
縮性フィルムを介して加熱気体で加圧する工程とを経
て、型及び加熱気体により加圧加熱硬化させることを特
徴とする複合材料の成形方法。1. A molding intermediate material comprising a reinforcing fiber and a thermosetting resin is laminated, preformed at a temperature of 60 ° C. or lower, set in a mold capable of controlling heating temperature, and molded via a stretchable film. A method for molding a composite material, comprising: degassing the object side with a decompression bag; and pressurizing with heated gas through a stretchable film, followed by pressurizing and heating and curing with a mold and heated gas.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP7095330A JPH08290479A (en) | 1995-04-20 | 1995-04-20 | Molding method for composite material |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP7095330A JPH08290479A (en) | 1995-04-20 | 1995-04-20 | Molding method for composite material |
Publications (1)
Publication Number | Publication Date |
---|---|
JPH08290479A true JPH08290479A (en) | 1996-11-05 |
Family
ID=14134719
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP7095330A Pending JPH08290479A (en) | 1995-04-20 | 1995-04-20 | Molding method for composite material |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH08290479A (en) |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR20000067592A (en) * | 1999-04-26 | 2000-11-25 | 국중석 | A Development about Vacuum Bag Method of Wet Resin FRP |
EP1923921A2 (en) | 2006-11-16 | 2008-05-21 | NPC Incorporated | Laminating apparatus |
CN109228276A (en) * | 2018-11-20 | 2019-01-18 | 西部(银川)通用航空飞机制造有限公司 | A kind of aircraft cabin cover thermal forming device and preparation method thereof |
CN109375391A (en) * | 2018-09-30 | 2019-02-22 | 云谷(固安)科技有限公司 | The process equipment and processing method of display module |
WO2019171683A1 (en) * | 2018-03-05 | 2019-09-12 | 日本飛行機株式会社 | Method for forming honeycomb sandwich composite material and jig used therefor |
CN110654040A (en) * | 2019-09-27 | 2020-01-07 | 珂尔默(东莞)制造技术有限公司 | Thermal diaphragm preforming device for composite material shell and working method of thermal diaphragm preforming device |
CN111590924A (en) * | 2020-05-29 | 2020-08-28 | 常州市新创智能科技有限公司 | Thermal diaphragm forming system |
CN114603881A (en) * | 2022-03-16 | 2022-06-10 | 广州科莱瑞迪医疗器材股份有限公司 | Die pressing equipment and processing method for composite material |
-
1995
- 1995-04-20 JP JP7095330A patent/JPH08290479A/en active Pending
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR20000067592A (en) * | 1999-04-26 | 2000-11-25 | 국중석 | A Development about Vacuum Bag Method of Wet Resin FRP |
EP1923921A2 (en) | 2006-11-16 | 2008-05-21 | NPC Incorporated | Laminating apparatus |
EP1923921A3 (en) * | 2006-11-16 | 2008-07-02 | NPC Incorporated | Laminating apparatus |
US8028735B2 (en) | 2006-11-16 | 2011-10-04 | Npc Incorporated | Laminating apparatus |
WO2019171683A1 (en) * | 2018-03-05 | 2019-09-12 | 日本飛行機株式会社 | Method for forming honeycomb sandwich composite material and jig used therefor |
JPWO2019171683A1 (en) * | 2018-03-05 | 2020-05-28 | 日本飛行機株式会社 | Method for forming honeycomb sandwich composite material and jig used therefor |
CN109375391A (en) * | 2018-09-30 | 2019-02-22 | 云谷(固安)科技有限公司 | The process equipment and processing method of display module |
CN109228276A (en) * | 2018-11-20 | 2019-01-18 | 西部(银川)通用航空飞机制造有限公司 | A kind of aircraft cabin cover thermal forming device and preparation method thereof |
CN110654040A (en) * | 2019-09-27 | 2020-01-07 | 珂尔默(东莞)制造技术有限公司 | Thermal diaphragm preforming device for composite material shell and working method of thermal diaphragm preforming device |
CN111590924A (en) * | 2020-05-29 | 2020-08-28 | 常州市新创智能科技有限公司 | Thermal diaphragm forming system |
CN114603881A (en) * | 2022-03-16 | 2022-06-10 | 广州科莱瑞迪医疗器材股份有限公司 | Die pressing equipment and processing method for composite material |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US5106568A (en) | Method and apparatus for vacuum bag molding of composite materials | |
US9108395B2 (en) | Single vacuum debulk composite panel repair | |
EP1507647B1 (en) | Controlled atmospheric pressure resin infusion process | |
US5527414A (en) | Method for high pressure co-cure molding of lightweight honeycomb core composite articles having ramped surfaces utilizing low density, stabilized ramped honeycomb cores | |
EP0195562B1 (en) | Method of producing shaped articles from reinforced composites | |
US6620369B1 (en) | Net molding of resin composite parts | |
EP0904929B1 (en) | Method for forming a caul plate during moulding of a part | |
US20080210372A1 (en) | Composite article debulking process | |
US6739861B2 (en) | High pressure co-cure of lightweight core composite article utilizing a core having a plurality of protruding pins | |
EP1162055A1 (en) | Vacuum membrane moulding of a layered composite material | |
NO174335B (en) | Method for producing molded articles of plastic composite material | |
WO1980002528A1 (en) | Method of fabricating a composite structure | |
JP2009542483A (en) | Manufacturing method of composite parts | |
WO2013178755A1 (en) | Press moulding method | |
US20090218713A1 (en) | Vacuum heat-set of net shape latex vacuum bags | |
JPH08290479A (en) | Molding method for composite material | |
JPH08118381A (en) | Manufacture of cfrp molded product | |
JP3121070B2 (en) | Molding method of fiber reinforced composite | |
JPS62259819A (en) | Manufacture of fiber reinforced plastic material | |
Legrand et al. | A study of the feasibility of a monoblock racing motorcycle rim | |
KR102407607B1 (en) | Complex materials forming device | |
JPH05237954A (en) | Manufacture of curved honeycomb panel | |
US8097198B2 (en) | Manufacturing method with vacuum bag | |
JPH08258162A (en) | Integrally molding method for complicated structure | |
JPH06190956A (en) | Production of honeycomb sandwich panel |