JPH0260938A - Laminated structure and its production - Google Patents
Laminated structure and its productionInfo
- Publication number
- JPH0260938A JPH0260938A JP63211763A JP21176388A JPH0260938A JP H0260938 A JPH0260938 A JP H0260938A JP 63211763 A JP63211763 A JP 63211763A JP 21176388 A JP21176388 A JP 21176388A JP H0260938 A JPH0260938 A JP H0260938A
- Authority
- JP
- Japan
- Prior art keywords
- resin
- laminated structure
- synthetic resin
- thermoplastic resin
- thermosetting
- 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
Links
Landscapes
- Reinforced Plastic Materials (AREA)
- Laminated Bodies (AREA)
Abstract
Description
【発明の詳細な説明】
(産業上の利用分野)
本発明は厚さムラのない、均一な各種成形品、特に圧縮
成形品を提供するための積層構造体を提供するものであ
り、ざらにかかる積層構)着体を安定して提供する積層
fSm体の製造方法に関する。Detailed Description of the Invention (Industrial Application Field) The present invention provides a laminated structure for providing various molded products with uniform thickness and uniformity, especially compression molded products. The present invention relates to a method for manufacturing a laminated fSm body which stably provides such a laminated structure.
(従来技術)
従来、合成繊維布帛などに熱硬化性樹脂を含浸又はコー
ティングしたシート状物(以下プリプレグと呼ぶ)を特
定の平面形状に裁断し、複数校定められた位相に組み付
けて立体成形されているが、かかる成形品の均一性は組
み付は時の成形作業者の熟練度に依存しているのが実情
でおる。(Prior art) Conventionally, a sheet material made of synthetic fiber cloth impregnated or coated with a thermosetting resin (hereinafter referred to as prepreg) is cut into a specific planar shape, and multiple pieces are assembled in a predetermined phase to be three-dimensionally formed. However, the reality is that the uniformity of such molded products depends on the skill level of the molding operator at the time of assembly.
(本発明が解決しようとする課題)
通常、布帛積層体を成形、特に圧縮成形する場合にはプ
リプレグを各層に一定の位相を持たせて予備的に組み付
け(以下プリフォームと呼ぶ)を行い、このプリフォー
ム品を、金型ヘチャージするかあるいは型締めして加熱
成形する。しかし、このチャージあるいは型締めの際に
、各層の布帛間相互位置(位相〉がズして均一な積層体
が得られないという欠点を有していた。この傾向は、特
に三次元曲面体のような複雑な形状に成形において填め
て大きく、改善が急がれていた。(Problems to be Solved by the Invention) Normally, when fabric laminates are molded, especially compression molded, prepregs are preliminarily assembled (hereinafter referred to as preform) with each layer having a certain phase. This preform product is charged into a mold or clamped and heat-molded. However, during this charging or mold clamping, the mutual position (phase) between the fabrics of each layer shifts, making it impossible to obtain a uniform laminate. It is difficult to fit such complex shapes into molding, and improvements are urgently needed.
本発明は、かかる三次元曲面体のような立体成形量のプ
リフォームにおいても、位相のズレがなく、均一な成形
品を提供し得る積層構造体を提供するものであり、ざら
にかかる積層構造体を安定して、かつ能率的に製造する
方法を提供するものである。The present invention provides a laminated structure that can provide a uniform molded product without phase shift even in a preform with a three-dimensional molding amount such as a three-dimensional curved body. The present invention provides a method for stably and efficiently producing a body.
(課題を解決するための手段)
本発明はかかる課題を解決するために次のような手段を
採用するものである。すなわち、(1)熱可塑性樹脂と
熱硬化性樹脂との合成樹脂混合物を含有する繊維イ「帛
からなる積層体において、部分的に融着された該合成樹
脂が該繊維布帛の相対的位置を固定していることを特徴
とする積層M4造体。(Means for Solving the Problems) The present invention adopts the following means to solve the problems. That is, (1) in a laminate consisting of fiber fabrics containing a synthetic resin mixture of a thermoplastic resin and a thermosetting resin, the partially fused synthetic resin controls the relative position of the fiber fabrics; A laminated M4 structure characterized by being fixed.
(2)熱可塑性樹脂と熱硬化性樹脂との合成樹脂混合物
を含浸した繊維布帛を複数枚積層した後、部分的に加熱
処理して、該合成樹脂を融着することを特徴とする積層
構造体の製造方法。(2) A laminated structure characterized by laminating a plurality of fiber fabrics impregnated with a synthetic resin mixture of a thermoplastic resin and a thermosetting resin, and then partially heat-treated to fuse the synthetic resin. How the body is manufactured.
(3)前記加熱処理が、超音波によるものである請求項
(1)記載の積層構造体の製造方法である。(3) The method for manufacturing a laminated structure according to claim (1), wherein the heat treatment is performed using ultrasonic waves.
本発明に適用されるwjMとしては、たとえばナイロン
、ポリエステル、ポリウレタン、ポリアクリロニトリル
、ポリプロピレン、ビニロン、芳香族ポリアミド、高強
力ポリエチレン、高強力ポリビニルアルコール、高強力
アクリロニトリルなどのポリマーからなる繊維およびフ
ッ素繊維、炭素I!、ガラスw4維、金属繊維などが挙
げられる。Examples of wjM applicable to the present invention include fibers made of polymers such as nylon, polyester, polyurethane, polyacrylonitrile, polypropylene, vinylon, aromatic polyamide, high-strength polyethylene, high-strength polyvinyl alcohol, and high-strength acrylonitrile, and fluorine fibers; Carbon I! , glass W4 fiber, metal fiber, etc.
かかる繊維からなる布帛としては、たとえば織物、編物
、不織布などのシート状物が適用できる。As the fabric made of such fibers, for example, sheet-like materials such as woven fabrics, knitted fabrics, and nonwoven fabrics can be used.
本発明は、融着性、形態安定性の上から、熱可塑性樹脂
と熱硬化性樹脂の2種の合成樹脂混合物を適用する。In the present invention, a mixture of two types of synthetic resins, a thermoplastic resin and a thermosetting resin, is used in terms of fusion properties and shape stability.
本発明の熱可塑性樹脂は隣接する層を融着して布帛相互
の位置決め(位相)をする機能を有するものであり、単
に可塑性や接着性を有するもののみならず、さらに加熱
によって熱硬化成分と反応し共重合体となるものであっ
てもよい。かかる熱可塑性樹脂としては、たとえばポリ
アミド樹脂、ポリエステル樹脂、ポリウレタン樹脂、メ
タアクリル樹脂、ポリビニルブチラール樹脂などがあげ
られる。The thermoplastic resin of the present invention has the function of fusing adjacent layers and positioning (phase) the fabrics, and not only has plasticity and adhesive properties, but also has a thermosetting component when heated. It may also react to form a copolymer. Examples of such thermoplastic resins include polyamide resins, polyester resins, polyurethane resins, methacrylic resins, and polyvinyl butyral resins.
また熱硬化性樹脂としては、たとえば不飽和ポリエステ
ル樹脂、架橋性ポリウレタン樹脂、エポキシ樹脂、フェ
ノール樹脂、ビニルエステル樹脂、ユリア樹脂、メラミ
ン樹脂、ポリイミド樹脂などがめげられる。Examples of thermosetting resins include unsaturated polyester resins, crosslinkable polyurethane resins, epoxy resins, phenol resins, vinyl ester resins, urea resins, melamine resins, and polyimide resins.
かかる熱可塑性樹脂と熱硬化性樹脂とは、それぞれの樹
脂群から少なくとも1種選択して混合する。混合樹脂組
成として、特に好ましい組み合せはポリビニルブチラー
ル樹脂とフェノール樹脂であり、この混合樹脂組成のも
のはプリプレグの加工性や融着特性に優れている。At least one type of such thermoplastic resin and thermosetting resin is selected from each resin group and mixed. A particularly preferred combination of mixed resin compositions is polyvinyl butyral resin and phenol resin, and this mixed resin composition has excellent prepreg processability and fusion properties.
熱可塑性樹脂/熱硬化性樹脂の混合比は適用される樹脂
の特性や成形品の使用目的によって選ばれるが、好まし
くは20/80〜70/ 30、さらに好ましくは40
/ 60〜60/ 40の範囲を採用する。熱可塑性樹
脂が20%以下では融着性が低下する傾向を示し、70
%以上になると成形性が悪くなる傾向が出てくる。The mixing ratio of thermoplastic resin/thermosetting resin is selected depending on the characteristics of the applied resin and the intended use of the molded product, but is preferably 20/80 to 70/30, more preferably 40/80.
A range of /60 to 60/40 is adopted. When the thermoplastic resin content is less than 20%, the fusion properties tend to decrease, and the
% or more, moldability tends to deteriorate.
合成繊維/合成樹脂の重量比は成形品の使用目的によっ
て決められるが、好ましくは5/95〜501501さ
らには10/90〜40/60の範囲から選択される。The weight ratio of synthetic fiber/synthetic resin is determined depending on the intended use of the molded article, and is preferably selected from the range of 5/95 to 501501, and more preferably 10/90 to 40/60.
本発明のプリプレグシートは、−殻内な溶液含浸法ある
いはコーティング法などの方法により形成される。The prepreg sheet of the present invention is formed by a method such as an in-shell solution impregnation method or a coating method.
本発明のフリプレグは層間の合成樹脂が部分的に融着し
ている点に特徴を有するが、その融着面積および融着範
囲はプリプレグ裁断品の形状やプリフォーム品の形状な
どによって決められる。通常は表面積の5パーセント以
下で十分である。The flip-preg of the present invention is characterized in that the synthetic resin between the layers is partially fused, and the fused area and range are determined by the shape of the cut prepreg product, the shape of the preform product, etc. Usually less than 5 percent of the surface area is sufficient.
かかる融着方法としては小面積の加熱が可能な手法を好
ましく採用し得るが、特に超音波ウエルダーの使用が作
業効率の面から選択される。As such a welding method, a method capable of heating a small area can be preferably employed, and in particular, the use of an ultrasonic welder is selected from the viewpoint of work efficiency.
融着条件としては、熱可塑性樹脂の軟化温度以上かつ熱
硬化性樹脂の硬化温度以下あるいは硬化が進行しない範
囲の時間などの条件が選択されるが、要は布帛層が成形
時に剥離しない程度に融着しておれば充分である。The fusion conditions are selected to be above the softening temperature of the thermoplastic resin and below the curing temperature of the thermosetting resin, or for a time within a range where curing does not proceed, but the key is to ensure that the fabric layer does not peel off during molding. It is sufficient if they are fused.
このようにして組み付けられた積層品は各層の位相が正
確に固定されたプリフォーム品である。The laminate product assembled in this manner is a preform product in which the phase of each layer is accurately fixed.
次に実施例により本発明をさらに具体的に説明する。Next, the present invention will be explained in more detail with reference to Examples.
(実施例)
実施例1
ナイロン6Bili維1200デニール使い、織密度;
19×19本/inS貿徂: 226 g/mの平織に
ポリビニルブチラール/フェノール樹脂(混合比501
50 ” IJ −530”ロードファーイースト社製
)を56g/洸の付着量になるように○浸したプリプレ
グ(第1図)を直径50cmの6枚の多弁形に裁断し、
各々の弁の中心に標線を印し、弁の端から20mm内側
の標線上と該中心から半径120mmの円周上で、かつ
多弁形の弁の中心部分に融着点を印した(第2図)。こ
のプリプレグを24枚用意した。(Example) Example 1 Nylon 6Bili fiber 1200 denier was used, weaving density;
19 x 19 pieces/inS trade: 226 g/m plain weave with polyvinyl butyral/phenol resin (mixing ratio 501
The prepreg (Fig. 1) soaked with 50"IJ-530" (manufactured by Road Far East Co., Ltd.) to a coating weight of 56 g/Ko was cut into 6 multi-petal shapes with a diameter of 50 cm.
A marked line was marked at the center of each valve, and a fusion point was marked on the marked line 20 mm inside from the end of the valve, on the circumference with a radius of 120 mm from the center, and at the center of the multi-valved valve (No. Figure 2). 24 sheets of this prepreg were prepared.
直径30Cmの半球状の組み付は容器の中に1枚目のプ
リプレグ(点線)を半球形に置き、2枚目のプ1ノブレ
グ(実線〉を1枚目に対して位相を15゜ずらして置い
た。ハンドタイプの超音波ウエルダーを用いて、プリプ
レグの融着点を、2枚の層が軽く融着する程度に照射し
て、直径1Qmmの円形面を融着した(第3図)。この
准看積層体の上に次のシートを積層し、同様に融着した
。この操作を繰り返し24枚のプリプレグを組み付けて
半球状のプリフォーム品を得た。このプリフォ−ム品は
各層の位相が正確に固定され、かつ少々の外力では位相
の乱れは生じなかった。To assemble a hemispherical shape with a diameter of 30 cm, place the first prepreg (dotted line) in a hemispherical shape in the container, and shift the phase of the second prepreg (solid line) by 15 degrees with respect to the first prepreg. Using a hand-type ultrasonic welder, the fusion point of the prepreg was irradiated to such an extent that the two layers were lightly fused, and a circular surface with a diameter of 1 Q mm was fused (Fig. 3). The next sheet was laminated on top of this laminate and fused in the same way.This operation was repeated to assemble 24 sheets of prepreg to obtain a hemispherical preform product. The phase was accurately fixed, and no phase disturbance occurred even with a small amount of external force.
このプリフォーム品を直径25Cmの半球状の金型に移
し、160℃/100tOnで30分成形して半球形の
成形品を1qた。This preform product was transferred to a hemispherical mold with a diameter of 25 cm, and molded at 160° C./100 tOn for 30 minutes to obtain 1 q of hemispherical molded products.
この成形品の周縁下端−から80mm上方の円周上に1
2か所ドリルで貫通孔をあけた。つぎに内側から1枚ず
つ20枚の層を機械的にはがし、目通孔の位置にお【ブ
る実質積層枚数を数えた。1 on the circumference 80mm above the lower edge of this molded product
I drilled two through holes with a drill. Next, the 20 layers were mechanically peeled off one by one from the inside, and the actual number of laminated layers at the positions of the through holes was counted.
この結果を表1に示した。The results are shown in Table 1.
比較例1
実施例1と同じプリプレグを用い、層間を接着しないで
組み付けたプリフォーム品を作った。これを実施例1と
同条件で成形して半球形の成形品を得た。Comparative Example 1 Using the same prepreg as in Example 1, a preform product was produced by assembling the layers without adhesion. This was molded under the same conditions as in Example 1 to obtain a hemispherical molded product.
この成形品の周縁下端から80mm上方の円周上に12
か所ドリルで貫通孔を必りた。つぎに内側から1枚ずつ
20枚の府を機械的にはがし、貫通孔の位置にあける実
質積層枚数を数えた。12 on the circumference 80mm above the lower edge of this molded product.
I drilled through holes in places. Next, 20 sheets were mechanically peeled off one by one from the inside, and the actual number of laminated sheets to be punched at the position of the through hole was counted.
この結果を表1J3よび表2に示した。The results are shown in Tables 1J3 and 2.
表 1
表 2
上記衣から明らかなように、実施例1は全箇所で均一な
積層状態が1qられているのに対して、比較例1では層
間にズレを生じ積層が不均一なものでめった。Table 1 Table 2 As is clear from the above coating, Example 1 had a uniform lamination state at all locations, whereas Comparative Example 1 had misalignment between layers and was rarely laminated unevenly. .
比較例2
実施例1において、使用する樹脂としてフェノール樹脂
は混合しないで、ポリビニルブヂラール樹脂のみを用い
て、後は実施例1と同様にして、プリフォーム品を作り
、これを金型に装填して成形した。Comparative Example 2 In Example 1, only polyvinylbutyral resin was used as the resin without mixing the phenol resin, and the rest was carried out in the same manner as in Example 1 to produce a preform product, which was then molded into a mold. Loaded and molded.
この成形品は部分的にフクレを有するものであり、ざら
に金型からの離型時の離型性が極めて悪く、正常な成形
品が得られにくいことが判明した。It was found that this molded product had some blisters and had extremely poor releasability when released from the mold, making it difficult to obtain a normal molded product.
(発明の効果〉
本発明は、プリプレグを複数枚子ねて作られる成形品、
特に三次元曲面体のように複雑な形状の成形品において
、積層イ[帛の位置決めが簡単容易で、かつ安定して達
成でき、しかも成形中にも位相のズレか発生しないとい
う特徴を発揮するので、各種の積層体の成形に有効に適
用される。(Effect of the invention) The present invention provides a molded product made by plying a plurality of sheets of prepreg,
In particular, for molded products with complex shapes such as three-dimensional curved objects, the laminated fabric can be positioned easily and stably, and it also exhibits the characteristics that no phase shift occurs during molding. Therefore, it can be effectively applied to molding various laminates.
第1図は本発明の積層構造体用の樹脂含浸多弁布帛の一
例を示す断面図であり、第2図は融着点を印した裁断プ
リプレグシートの一例であり、第3図はプリフォーム品
の一例である。
図中
1:合成繊維布帛 2:合成樹脂
3ニブリプレグシート 4:融着点
5:裁断プリプレグシート6:1枚目シート7:2枚目
シート 8:融着部分
9ニブリフオ一ム品Fig. 1 is a cross-sectional view showing an example of a resin-impregnated multi-valve fabric for a laminated structure of the present invention, Fig. 2 is an example of a cut prepreg sheet with fusing points marked, and Fig. 3 is a preform product. This is an example. In the figure: 1: Synthetic fiber fabric 2: Synthetic resin 3 Nibbly preg sheet 4: Fusion point 5: Cutting prepreg sheet 6: First sheet 7: Second sheet 8: Fusion part 9 Nibbly formed product
Claims (3)
を含有する繊維布帛からなる積層体において、部分的に
融着された該合成樹脂が該繊維布帛の相対的位置を固定
していることを特徴とする積層構造体。(1) In a laminate made of fiber fabric containing a synthetic resin mixture of a thermoplastic resin and a thermosetting resin, the partially fused synthetic resin fixes the relative position of the fiber fabric. A laminated structure characterized by:
を含浸した繊維布帛を複数枚積層した後、部分的に加熱
処理して、該合成樹脂を融着することを特徴とする積層
構造体の製造方法。(2) A laminated structure characterized by laminating a plurality of fiber fabrics impregnated with a synthetic resin mixture of a thermoplastic resin and a thermosetting resin, and then partially heat-treated to fuse the synthetic resin. How the body is manufactured.
(1)記載の積層構造体の製造方法。(3) The method for manufacturing a laminated structure according to claim (1), wherein the heat treatment is performed using ultrasonic waves.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP63211763A JP2650349B2 (en) | 1988-08-25 | 1988-08-25 | Laminated structure and manufacturing method thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP63211763A JP2650349B2 (en) | 1988-08-25 | 1988-08-25 | Laminated structure and manufacturing method thereof |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPH0260938A true JPH0260938A (en) | 1990-03-01 |
| JP2650349B2 JP2650349B2 (en) | 1997-09-03 |
Family
ID=16611178
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP63211763A Expired - Lifetime JP2650349B2 (en) | 1988-08-25 | 1988-08-25 | Laminated structure and manufacturing method thereof |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JP2650349B2 (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2007041782A1 (en) * | 2005-10-11 | 2007-04-19 | Crc For Advanced Composite Structures Limited | A method of binding dry reinforcement fibres |
| CN118683135A (en) * | 2024-06-14 | 2024-09-24 | 深圳大学 | A carbon fiber reinforced resin-based composite material plate capable of being recycled as a whole, a preparation method and a recycling method |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5145195A (en) * | 1974-10-16 | 1976-04-17 | Hitachi Chemical Co Ltd | TEISHUSHUKUUSEIFUHOWAHORIESUTERUJUSHISOSEIBUTSU |
| JPS5887042A (en) * | 1981-11-19 | 1983-05-24 | 東レ株式会社 | Reinforcing material for fiber reinforced resin |
| JPS59215315A (en) * | 1983-05-20 | 1984-12-05 | アモコ・コーポレイション | Impact resistant mother material resin for high composite material |
-
1988
- 1988-08-25 JP JP63211763A patent/JP2650349B2/en not_active Expired - Lifetime
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5145195A (en) * | 1974-10-16 | 1976-04-17 | Hitachi Chemical Co Ltd | TEISHUSHUKUUSEIFUHOWAHORIESUTERUJUSHISOSEIBUTSU |
| JPS5887042A (en) * | 1981-11-19 | 1983-05-24 | 東レ株式会社 | Reinforcing material for fiber reinforced resin |
| JPS59215315A (en) * | 1983-05-20 | 1984-12-05 | アモコ・コーポレイション | Impact resistant mother material resin for high composite material |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2007041782A1 (en) * | 2005-10-11 | 2007-04-19 | Crc For Advanced Composite Structures Limited | A method of binding dry reinforcement fibres |
| CN118683135A (en) * | 2024-06-14 | 2024-09-24 | 深圳大学 | A carbon fiber reinforced resin-based composite material plate capable of being recycled as a whole, a preparation method and a recycling method |
Also Published As
| Publication number | Publication date |
|---|---|
| JP2650349B2 (en) | 1997-09-03 |
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