JP2650349B2 - Laminated structure and manufacturing method thereof - Google Patents

Laminated structure and manufacturing method thereof

Info

Publication number
JP2650349B2
JP2650349B2 JP63211763A JP21176388A JP2650349B2 JP 2650349 B2 JP2650349 B2 JP 2650349B2 JP 63211763 A JP63211763 A JP 63211763A JP 21176388 A JP21176388 A JP 21176388A JP 2650349 B2 JP2650349 B2 JP 2650349B2
Authority
JP
Japan
Prior art keywords
resin
laminated structure
fiber
thermoplastic resin
prepreg
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.)
Expired - Lifetime
Application number
JP63211763A
Other languages
Japanese (ja)
Other versions
JPH0260938A (en
Inventor
直樹 今枝
昇 岸上
真 工藤
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.)
TORE KK
Original Assignee
TORE KK
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 TORE KK filed Critical TORE KK
Priority to JP63211763A priority Critical patent/JP2650349B2/en
Publication of JPH0260938A publication Critical patent/JPH0260938A/en
Application granted granted Critical
Publication of JP2650349B2 publication Critical patent/JP2650349B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Landscapes

  • Reinforced Plastic Materials (AREA)
  • Laminated Bodies (AREA)

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、さらにかかる積層構造体を安定して提供する積層
構造体の製造方法に関する。
DETAILED DESCRIPTION OF THE INVENTION (Industrial application field) The present invention is to provide a laminated structure for providing various molded articles having a uniform thickness, and in particular, compression molded articles. The present invention relates to a method for manufacturing a laminated structure that stably provides 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
特定の平面形状に栽断し、複数枚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
組み付け時の成形作業者の熟練度に依存しているのが実
情である。
(Prior art) Conventionally, a sheet-like material (hereinafter, referred to as a prepreg) in which a thermosetting resin is impregnated or coated with a synthetic fiber cloth or the like is cut into a specific plane shape, and a plurality of sheets are assembled into a predetermined phase and three-dimensionally molded. However, the uniformity of such a molded article depends on the skill of a 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、金型へ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、このチャージありは型締めの際
に、各層の布帛間相互位置(位相)がズレて均一な積層
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極
めて大きく、改善が急がれていた。
(Problems to be Solved by the Present Invention) Usually, when forming a fabric laminate, particularly in the case of compression molding, a prepreg is preliminarily assembled with a certain phase in each layer (hereinafter referred to as a preform), This preform product is charged into a mold or clamped and molded by heating. However, with this charge, there is a disadvantage that the mutual positions (phases) between the fabrics of the respective layers are displaced during mold clamping, so that a uniform laminate cannot be obtained. This trend is
In particular, molding into a complicated shape such as a three-dimensional curved body is extremely large, and improvement has been urgently needed.

本発明は、かかる三次元曲面体のような立体成形品の
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、さ
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 capable of providing a uniform molded product without a phase shift even in a preform of a three-dimensional molded product such as a three-dimensional curved body, and further provides such a laminated structure. Is provided stably and efficiently.

(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、本発明の積層構造体
は、熱可塑性樹脂と熱硬化性樹脂との合成樹脂混合物を
含有する繊維布帛からなる積層体において、該繊維布帛
同士が熱融着によって部分的に位置決めされていること
を特徴とするものであり、また、かかる積層構造体の製
造方法は、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、該熱可塑性樹脂を溶融させて該繊維布帛
同士の位置決めをすることを特徴とするものである。
(Means for Solving the Problems) The present invention employs the following means to solve the problems. That is, in the laminate structure of the present invention, in a laminate made of a fiber cloth containing a synthetic resin mixture of a thermoplastic resin and a thermosetting resin, the fiber cloths are partially positioned by heat fusion. In addition, the method for manufacturing such a laminated structure is characterized in that a plurality of fiber fabrics impregnated with a synthetic resin mixture of a thermoplastic resin and a thermosetting resin are laminated, and then partially heat-treated. Then, the thermoplastic resin is melted to position the fiber cloths.

本発明に適用される繊維としては、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、炭素繊維、ガラス繊維、金属繊維なとが挙
げられる。
Examples of the fibers applied 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 fiber, glass fiber, and metal fiber.

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 a fabric made of such fibers, for example, a sheet material such as a woven fabric, a knitted fabric, or a nonwoven fabric can be applied.

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 kinds of synthetic resins, a thermoplastic resin and a thermosetting resin, is applied from the viewpoint of fusing property and form 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 a function of positioning (phase) between fabrics by fusing adjacent layers,
Not only those having plasticity and adhesiveness but also those which react with a thermosetting component by heating to form a copolymer may be used. Such thermoplastic resins include, for example, polyamide resins, polyester resins, polyurethane resins,
Examples include methacrylic resin and polyvinyl butyral resin.

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あげられる。
Examples of the thermosetting resin include an unsaturated polyester resin, a crosslinkable polyurethane resin, an epoxy resin, a phenol resin, a vinyl ester resin, a urea resin, a melamine resin, and a polyimide resin.

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。
Such a thermoplastic resin and a thermosetting resin are mixed by selecting at least one from each resin group. As a mixed resin composition, a particularly preferred combination is a polyvinyl butyral resin and a phenol resin, and the mixed resin composition has excellent prepreg workability and fusion characteristics.

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 the thermoplastic resin / thermosetting resin is selected depending on the characteristics of the applied resin and the purpose of use of the molded article, but is preferably 20/80 to 70/30, more preferably 40/60 to 60/40. Adopt a range. When the thermoplastic resin content is 20% or less, the fusibility tends to decrease, and when the thermoplastic resin content exceeds 70%, the 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5/95〜50/50、さらには1
0/90〜40/60の範囲から選択される。
The weight ratio of synthetic fiber / synthetic resin is determined depending on the purpose of use of the molded article, but is preferably 5/95 to 50/50, and more preferably 1/95 to 50/50.
It is selected from the range of 0/90 to 40/60.

本発明のプリプレグシートは、一般的な溶液含浸法あ
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 general method such as a solution impregnation method or a coating method.

本発明のプ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 prepreg of the present invention is characterized in that the synthetic resin between the layers is partially fused, and the fusion area and the fusion range are determined by the shape of the prepreg cut product and the shape of the preform product. 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 fusion method, a method capable of heating a small area can be preferably adopted, but use of an ultrasonic welder is particularly selected from the viewpoint of working 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。
As the fusing conditions, conditions such as a time above the softening temperature of the thermoplastic resin and below the curing temperature of the thermosetting resin or a range in which the curing does not proceed are selected. It is enough 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 laminated 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 described more specifically with reference to examples.

(実施例) 実施例1 ナイロン6繊維1200デニール使い、織密度;19×19本/
in、質量;226g/m2の平織にポリビニルブチラール/フェ
ノール樹脂(混合比50/50“LJ−530"ロードファーイー
スト社製)を56g/m2の付着量になるように含浸したプリ
プレグ(第1図)を直径50cmの6枚の多弁形に栽断し、
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 Use of 1200 denier nylon 6 fiber, woven density: 19 × 19 /
in, mass: 226 g / m 2 plain weave, impregnated with polyvinyl butyral / phenol resin (mixing ratio 50/50 “LJ-530” manufactured by Road Far East Co., Ltd.) so as to have an adhesion amount of 56 g / m 2 (No. Fig. 1) is cut into six multi-valve shapes with a diameter of 50cm.
A marking line was marked at the center of each valve, and a fusion point was marked on the marking line inside 20 mm from the end of the valve, on a circumference having a radius of 120 mm from the center, and at the center of the multi-valve valve (No. 2). 24 prepregs were prepared.

直径30cmの半球状の組み付け容器の中に1枚目のプリ
プレグ(点線)を半球形に置き、2枚目のプリプレグ
(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10mmの円形面を融着した(第3図)。この融着積層
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。このプリフォーム品は各層の位相
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。
The first prepreg (dotted line) was placed in a hemispherical shape in a hemispherical assembly container having a diameter of 30 cm, and the second prepreg (solid line) was placed with a phase shift of 15 ° with respect to the first.
Using a hand-type ultrasonic welder, irradiate the fusion point of the prepreg to the extent that the two layers fuse lightly,
A circular surface having a diameter of 10 mm was fused (FIG. 3). The next sheet was laminated on the fused laminate and fused in the same manner. This operation was repeated to assemble 24 prepregs to obtain a hemispherical preform. In this preform product, the phase of each layer was accurately fixed, and the phase was not disturbed by a small 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得
た。
This preform product was transferred to a hemispherical mold having a diameter of 25 cm, and was molded at 160 ° C./100 ton for 30 minutes 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、貫通孔の位置における実質積層
枚数を数えた。
Through holes were drilled at 12 locations on the circumference of the molded product 80 mm above the lower edge of the periphery. Next, 20 layers were mechanically peeled one by one from the inside, and the actual number of layers at the position of the through hole 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 assembled without bonding between layers. Example 1
Under the same conditions as above, a hemispherical molded product was obtained.

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、貫通孔の位置における実質積層
枚数を数えた。
Through holes were drilled at 12 locations on the circumference of the molded product 80 mm above the lower edge of the periphery. Next, 20 layers were mechanically peeled one by one from the inside, and the actual number of layers at the position of the through hole was counted.

この結果を表1および表2に示した。 The results are shown in Tables 1 and 2.

上記表から明らかなように、実施例1は全箇所で均一
な積層状態が得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あった。
As is clear from the above table, in Example 1, a uniform lamination state was obtained at all locations, whereas in Comparative Example 1, the layers were misaligned and the lamination was non-uniform.

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、ポリビニルブチ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, a phenolic resin was not mixed as a resin to be used, but only a polyvinyl butyral resin was used. Molded.

この成形品は部分的にフクレを有するものであり、さ
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 blisters partially, had extremely poor releasability upon release from the mold, and it was 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重ねて作られる成形
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、積層布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が発生しないと
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。
(Effects of the Invention) The present invention achieves easy and stable positioning of a laminated fabric in a molded product made by laminating a plurality of prepregs, particularly in a molded product having a complicated shape such as a three-dimensional curved body. It can be applied to the molding of various laminates because it exhibits the feature that it can be formed and does not cause a phase shift during molding.

【図面の簡単な説明】[Brief description of the drawings]

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:プリプレグシート、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:プリフォーム品
FIG. 1 is a cross-sectional view showing an example of a resin-impregnated multi-valve fabric for a laminated structure according to the present invention, FIG. 2 is an example of a cut prepreg sheet on which a fusion point is marked, and FIG. This is an example. In the figure, 1: synthetic fiber fabric, 2: synthetic resin 3: prepreg sheet, 4: fusion point 5: cut prepreg sheet, 6: first sheet 7: second sheet, 8: fused part 9: preform Goods

Claims (3)

(57)【特許請求の範囲】(57) [Claims] 【請求項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布帛からなる積層体において、該
繊維布帛同士が熱融着によって部分的に位置決めされて
いることを特徴とする積層構造体。
1. A laminate comprising a fiber cloth containing a synthetic resin mixture of a thermoplastic resin and a thermosetting resin, wherein the fiber cloths are partially positioned by heat fusion. Laminated structure.
【請求項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、該熱可塑性樹脂を溶融させて該繊維布
帛同士の位置決めをすることを特徴とする積層構造体の
製造方法。
2. After laminating a plurality of fiber cloths impregnated with a synthetic resin mixture of a thermoplastic resin and a thermosetting resin, the fiber cloths are partially heated and melted to melt the thermoplastic resin. A method for manufacturing a laminated structure, comprising:
【請求項3】前記加熱処理が、超音波によるものである
請求項(2)記載の積層構造体の製造方法。
3. The method according to claim 2, wherein the heat treatment is performed by ultrasonic waves.
JP63211763A 1988-08-25 1988-08-25 Laminated structure and manufacturing method thereof Expired - Lifetime JP2650349B2 (en)

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 JPH0260938A (en) 1990-03-01
JP2650349B2 true 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)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1945430A4 (en) * 2005-10-11 2011-06-29 Cooperative Res Ct For Advanced Composite Structures Ltd A method of binding dry reinforcement fibres

Family Cites Families (3)

* Cited by examiner, † Cited by third party
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
ZA84548B (en) * 1983-05-20 1984-12-24 Union Carbide Corp Impact resistant matrix resins for advanced composites

Also Published As

Publication number Publication date
JPH0260938A (en) 1990-03-01

Similar Documents

Publication Publication Date Title
US4407885A (en) Composite article
US4410385A (en) Method of making a composite article
JP5658176B2 (en) Fiber-reinforced resin sheet and fiber-reinforced resin molded body using the same
EP0361796B1 (en) Method of producing a formable composite material
US5364686A (en) Manufacture of a three-dimensionally shaped textile material and use thereof
US3664909A (en) Needled resin fibrous article
WO2013089235A1 (en) Fibre-reinforced resin moulding, and vehicle interior material using same
JPH0742049A (en) Preparation of knitted fabric and fiber-reinforced laminate for using preparation of fiber-reinforced composite material and laminate
KR102555544B1 (en) Textile substrate made of reinforcing fibers
US4471018A (en) Thermoplastic laminate having masked surface fabric veil layer
AU2017244829B2 (en) Reinforced fiber laminate sheet, fiber-reinforced resin molded body, and method for manufacturing reinforced fiber laminate sheet
JP2650349B2 (en) Laminated structure and manufacturing method thereof
JP2002321215A (en) Preform and molding thereof
JP2000198158A (en) Fiber-reinforced material
AU2011264449B2 (en) Method of making automotive body parts
JP7467840B2 (en) Reinforced fiber substrate, reinforced fiber laminate, and fiber reinforced resin
JP5777972B2 (en) Fiber-reinforced resin molded body and vehicle interior material using the same
JPH05269909A (en) Fiber reinforced resin molded product
JP2831673B2 (en) Method for producing fiber molded body
US2875474A (en) Process of shaping resin-impregnated filamentary material
JP4376118B2 (en) Multi-axis fabric, preform material, and fiber reinforced plastic molding
JPH01209131A (en) Fibrous laminate and preparation thereof
JPH10317265A (en) Fiber material for reinforcing in one direction, molding using the material, and its molded product
JP5788734B2 (en) Fiber-reinforced resin molded body and vehicle interior material using the same
JPS6342036B2 (en)

Legal Events

Date Code Title Description
FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20080516

Year of fee payment: 11

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20090516

Year of fee payment: 12

EXPY Cancellation because of completion of term
FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20090516

Year of fee payment: 12