JPH06184901A - Composite fiber assembly - Google Patents

Composite fiber assembly

Info

Publication number
JPH06184901A
JPH06184901A JP4342016A JP34201692A JPH06184901A JP H06184901 A JPH06184901 A JP H06184901A JP 4342016 A JP4342016 A JP 4342016A JP 34201692 A JP34201692 A JP 34201692A JP H06184901 A JPH06184901 A JP H06184901A
Authority
JP
Japan
Prior art keywords
thickness
fiber composite
weight
except
laminate
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
JP4342016A
Other languages
Japanese (ja)
Other versions
JP2960269B2 (en
Inventor
Katsuhiko Yamaji
克彦 山路
Michiaki Sasayama
道章 笹山
Akira Shibata
亮 柴田
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.)
Sekisui Chemical Co Ltd
Original Assignee
Sekisui Chemical Co Ltd
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 Sekisui Chemical Co Ltd filed Critical Sekisui Chemical Co Ltd
Priority to JP4342016A priority Critical patent/JP2960269B2/en
Publication of JPH06184901A publication Critical patent/JPH06184901A/en
Application granted granted Critical
Publication of JP2960269B2 publication Critical patent/JP2960269B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Abstract

PURPOSE:To provide a composite fiber assembly having such thickness as to be consistently high in mechanical strength despite varying in its weight and good in press formability. CONSTITUTION:The composite fiber assembly is such that numerous glass fibers including those oriented in the thickness direction are mutually, partly bound through high-density polyethylene and there are numerous fine voids throughout. The thickness T (mm) of the assembly, depending on its weight W (kg/m<2>), satisfies the following relationships: when 0.4<=W<=0.9, 4W-0.5<=T<=5W+1, and when 0.9W<=1.7, 6W-2.3<=T<=8W-1.7.

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【産業上の利用分野】本発明は、自動車用内装材や建築
用内装材等に用いられる繊維複合体に関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a fiber composite used for interior materials for automobiles and interior materials for construction.

【0002】[0002]

【従来の技術】一般に、上記内装材には、軽量で、剛
性、耐熱性、成形性等の性能に優れた材料が要求され
る。従来より、この種の材料として、厚さ方向に配向さ
れているものを含む多数の無機繊維が相互に部分的に熱
可塑性樹脂で接合されかつ全体にわたって多数の空隙を
有する繊維複合体が知られている(特開平1−1565
62号公報参照)。
2. Description of the Related Art Generally, the above interior materials are required to be lightweight and have excellent properties such as rigidity, heat resistance and moldability. Conventionally, as this type of material, a fiber composite is known in which a large number of inorganic fibers including those oriented in the thickness direction are partially bonded to each other with a thermoplastic resin and have a large number of voids throughout. (Japanese Patent Laid-Open No. 1-1565)
No. 62).

【0003】[0003]

【発明が解決しようとする課題】従来の上記繊維複合体
をプレス成形する場合、通常、加熱してからプレスす
る。加熱前の種々の厚さの繊維複合体について、プレス
成形して得た成形品の強度を比較したところ、繊維複合
体の厚さを大きくしていくとある厚さを境にして強度が
低下していくことが判明した。この現象を重量が700
g/m2 の繊維複合体について調べた結果を図1に示
す。
When the above-mentioned conventional fiber composite is press-molded, it is usually heated and then pressed. When the strength of the molded products obtained by press molding was compared for the fiber composites of various thicknesses before heating, the strength decreased when the thickness of the fiber composites was increased. It turned out to do. Weight of 700
FIG. 1 shows the result of examination on the g / m 2 fiber composite.

【0004】また、上記繊維複合体を成形する際、ま
ず、その熱可塑性樹脂の融点以上に加熱するが、熱可塑
性樹脂が溶融すると、多数の無機繊維が厚さ方向に配向
されているものを含んでいるため、これらの復元しよう
とする力が働き、繊維複合体が膨張してその厚さが増大
する。ところが、繊維複合体の厚さを小さくしていくと
ある厚さを境にして加熱しても繊維複合体が十分に膨張
せず、厚さが余り増大しないことが判明した。プレス成
形する際、厚さが不充分であると、金型の形状通り正確
に成形せられないうらみがある。
When molding the above-mentioned fiber composite, first, the thermoplastic resin is heated to a temperature above its melting point, but when the thermoplastic resin is melted, a large number of inorganic fibers are oriented in the thickness direction. Because of the inclusion, these restoring forces act to expand the fiber composite and increase its thickness. However, it has been found that when the thickness of the fiber composite is reduced, the fiber composite does not expand sufficiently even when heated at a certain thickness as a boundary, and the thickness does not increase so much. In the case of press molding, if the thickness is insufficient, there is a cavitation that the molding cannot be performed accurately according to the shape of the mold.

【0005】本発明の目的は、重量が変っても常に強度
が大でしかもプレス成形性のよい厚さの繊維複合体を提
供することにある。
An object of the present invention is to provide a fiber composite having a thickness which is always high in strength even when the weight is changed and has good press moldability.

【0006】[0006]

【課題を解決するための手段】本発明による繊維複合体
は、厚さ方向に配向されているものを含む多数の無機繊
維が相互に部分的に熱可塑性樹脂で接合されかつ全体に
わたって多数の微細な空隙を有する繊維複合体におい
て、その厚さT(mm)が重量W(kg/m2 )の関数
で 0.4≦W≦0.9のとき、4W−0.5≦T≦5W+
1 0.9<W≦1.7のとき、6W−2.3≦T≦8W−
1.7 の範囲にあることを特徴とするものである。
The fiber composite according to the present invention comprises a large number of inorganic fibers, which are partially bonded to each other with a thermoplastic resin, including a plurality of inorganic fibers including those oriented in the thickness direction. In a fiber composite having various voids, when the thickness T (mm) is 0.4 ≦ W ≦ 0.9 as a function of weight W (kg / m 2 ), 4W−0.5 ≦ T ≦ 5W +
When 1 0.9 <W ≦ 1.7, 6W−2.3 ≦ T ≦ 8W−
It is characterized by being in the range of 1.7.

【0007】繊維複合体の厚さを上記範囲に限定したの
は、つぎの理由による。すなわち、強度が低下する繊維
複合体の限界厚さは、繊維複合体の重量によって変化
し、重量が大きくなる程限界厚さも大きくなる。したが
って、この場合の適性厚さT(mm)は重量W(kg/
2 )の関数であるから、次式のようになる。
The reason why the thickness of the fiber composite is limited to the above range is as follows. That is, the limit thickness of the fiber composite in which the strength decreases decreases depending on the weight of the fiber composite, and the larger the weight, the greater the limit thickness. Therefore, the appropriate thickness T (mm) in this case is the weight W (kg /
Since it is a function of m 2 ), the following equation is obtained.

【0008】0.4≦W≦0.9のとき、T≦5W+1 0.9<W≦1.7のとき、T≦8W−1.7 また、成形の際の加熱時に厚さが満足しうるように増大
しない繊維繊維複合体の限界厚さは、繊維複合体の重量
によって変化し、重量が大きくなる程限界厚さも大きく
なる。したがって、この場合の適性厚さT(mm)も重
量W(kg/m 2 )の関数であるから、次式のようにな
る。
When 0.4 ≦ W ≦ 0.9, T ≦ 5W + 1 0.9 <W ≦ 1.7, T ≦ 8W-1.7 Further, the thickness is satisfied at the time of heating during molding. Increase as possible
Not fiber Fiber composite limit thickness is the weight of fiber composite
The limit thickness increases as the weight increases.
Become. Therefore, the appropriate thickness T (mm) in this case is also heavy.
Quantity W (kg / m 2) Function,
It

【0009】 0.4≦W≦0.9のとき、4W−0.5≦T 0.9<W≦1.7のとき、6W−2.3≦T 無機繊維としては、ガラス繊維、ロックウール、セラミ
ック繊維、炭素繊維等があげられ、その長さは後述のマ
ット状物の成形性の点から5〜200mmが好ましく、
50〜100mmのものが70重量%以上含まれている
のがより好ましい。また、その太さは細くなると機械的
強度が低下し、太くなると重くなって嵩密度が小さくな
るので、3〜30μmが好ましく、より好ましくは5〜
20μmである。
When 0.4 ≦ W ≦ 0.9, 4W−0.5 ≦ T 0.9 <W ≦ 1.7, 6W−2.3 ≦ T As the inorganic fiber, glass fiber, lock Wool, ceramic fibers, carbon fibers and the like can be mentioned, and the length thereof is preferably 5 to 200 mm from the viewpoint of moldability of the mat-like material described later,
It is more preferable that 70% by weight or more of 50 to 100 mm is contained. Further, when the thickness is thin, the mechanical strength is lowered, and when the thickness is thick, the weight is heavy and the bulk density is small. Therefore, the thickness is preferably 3 to 30 μm, more preferably 5 to 5 μm.
It is 20 μm.

【0010】熱可塑性樹脂としては、ポリエチレン、ポ
リプロピレン、飽和ポリエステル、ポリアミド、ポリス
チレン、ポリビニルブチラール、ポリウレタン等があげ
られる。そして、繊維複合体を後述のマット状物から得
る場合、その両面に熱可塑性樹脂をフィルムとして積層
する必要がある。このフィルムの厚さはマット状物を構
成する無機繊維との割合で適宜決定せられる。
Examples of the thermoplastic resin include polyethylene, polypropylene, saturated polyester, polyamide, polystyrene, polyvinyl butyral and polyurethane. When the fiber composite is obtained from the mat-like material described later, it is necessary to laminate the thermoplastic resin as a film on both surfaces thereof. The thickness of this film can be appropriately determined by the ratio with the inorganic fibers constituting the mat-like material.

【0011】繊維複合体はマット状物から得られるが、
このマット状物の製造方法としては、無機繊維をカード
マシンに供給し、解繊、混繊し、ニードルパンチ処理す
る方法があげられる。ニードルパンチ密度は、1cm2
当り30〜200箇所が好ましい。ニードルパンチの施
された部分の無機繊維がマット状物の厚さ方向に配向せ
られる。なお、無機繊維を接着するためやマット状物の
かさを増すために、ポリエチレン、ポリプロピレン、飽
和ポリエステル、ポリアミド、ポリアクリロニトリル等
の熱可塑性有機繊維をマット状物中に10〜30重量%
添加するのが好ましい。また、無機繊維を均一に接合す
るために、解繊する際粉体状熱可塑性樹脂を混合しても
よいし、マット状物にした後これに粉体状熱可塑性樹脂
や熱可塑性樹脂のエマルジョンを散布してもよい。
Fiber composites are obtained from mats,
Examples of the method for producing the mat-like material include a method in which inorganic fibers are supplied to a card machine, defibrated, mixed, and needle punched. Needle punch density is 1 cm 2
30 to 200 locations are preferable. The inorganic fibers in the needle-punched portion are oriented in the thickness direction of the mat-like material. In order to bond the inorganic fibers and increase the bulk of the mat-like material, thermoplastic organic fibers such as polyethylene, polypropylene, saturated polyester, polyamide and polyacrylonitrile are contained in the mat-like material in an amount of 10 to 30% by weight.
It is preferable to add it. Further, in order to bond the inorganic fibers uniformly, a powdery thermoplastic resin may be mixed at the time of defibration, or a powdery thermoplastic resin or an emulsion of the thermoplastic resin may be added to the mat-like material after the mat-like material is formed. May be sprayed.

【0012】つぎに、得られたマット状物の両面に熱可
塑性樹脂フィルムを積層し、この積層物を熱可塑性樹脂
の溶融温度に加熱し、この温度を保ったまま加圧圧縮す
る。この際の圧力は0.1〜5kg/cm2 、加圧時間
は1〜30秒が好ましい。
Next, a thermoplastic resin film is laminated on both surfaces of the obtained mat-like material, the laminate is heated to the melting temperature of the thermoplastic resin, and pressurized and compressed while maintaining this temperature. The pressure at this time is preferably 0.1 to 5 kg / cm 2 , and the pressing time is preferably 1 to 30 seconds.

【0013】最後に、上記温度に保ったまま圧縮を解除
しマット状物の両表面を真空吸着して膨らませ、重量と
厚さの関係が上記の範囲を満足するように、強制的に厚
みを増大させる。
Finally, while keeping the above temperature, the compression is released and both surfaces of the mat-like material are vacuum-sucked to be inflated, and the thickness is forcibly changed so that the relationship between the weight and the thickness satisfies the above range. Increase.

【0014】上記の工程において、熱可塑性樹脂フィル
ムは溶融され圧縮されて溶融樹脂がマット状物に含浸さ
れる。また、無機繊維に繊維状、粉末状等の熱可塑性樹
脂が混合されている場合は、これらも溶融されて無機繊
維を接合する。この際、圧力及び加圧時間を制御して溶
融樹脂がマット状物の内部まで均一に含浸される前に圧
縮を解除すると、溶融樹脂は内部よりも表面部に密に含
浸され、多数の無機繊維が相互に部分的に熱可塑性樹脂
で接合され、表面に多数の細孔が生じるとともに、全体
にわたって多数の微細な空隙を有する繊維複合体が得ら
れるので好ましい。
In the above process, the thermoplastic resin film is melted and compressed to impregnate the matte material with the molten resin. When the inorganic fibers are mixed with a fibrous or powdery thermoplastic resin, these are also melted to bond the inorganic fibers. At this time, if the compression is released before the molten resin is uniformly impregnated into the mat-like material by controlling the pressure and the pressurization time, the molten resin is more densely impregnated in the surface portion than in the inside, and a large number of inorganic It is preferable that the fibers are partially bonded to each other with a thermoplastic resin, a large number of pores are formed on the surface, and a fiber composite having a large number of fine voids throughout is obtained.

【0015】なお、加熱加圧する際に賦形成形してもよ
いが、加熱加圧の際には板状体にしておき、使用する際
に再度加熱加圧して賦形成形してもよい。特に自動車用
天井材として使用する際には板状体としておき、発泡体
や化粧用表皮材を積層して異形成形用の金型に供給し、
熱接着するとともに賦形成形するのが好ましい。
Although it may be shaped during heating and pressing, it may be formed into a plate-like shape during heating and pressing and then heated and pressed again before use to shape it. Especially when it is used as a ceiling material for automobiles, it is made into a plate-like body, and a foam or a cosmetic skin material is laminated and supplied to a mold for a different shape,
It is preferable to heat-bond and shape-form.

【0016】無機繊維と熱可塑性樹脂の比率は、熱可塑
性樹脂の量が少なくなると接合部分が少なくなり、繊維
複合体の機械的強度が低下し、逆に多くなると空隙率が
低下するので、重量比で1:4〜4:1が好ましい。繊
維複合体の密度は大きくなると重くなり、小さくなると
機械的強度が低下するので、0.01〜0.2g/cm
2 が好ましく、また、全体としての空隙率は70〜98
%が好ましい。さらに、無機繊維を接合している熱可塑
性樹脂は、繊維複合体の内部よりも表面部に密に分布し
ており、表面部の空隙率は内部より低くなされている
が、表面部の空隙率が50〜95%であって内部の空隙
率が85〜99%であるのが好ましい。
The ratio of the inorganic fiber to the thermoplastic resin is such that when the amount of the thermoplastic resin is small, the number of joints is small, the mechanical strength of the fiber composite is low, and when the ratio is large, the porosity is low. A ratio of 1: 4 to 4: 1 is preferred. When the density of the fiber composite increases, it becomes heavier, and when it decreases, the mechanical strength decreases, so 0.01 to 0.2 g / cm.
2 is preferable, and the total porosity is 70 to 98.
% Is preferred. Furthermore, the thermoplastic resin bonding the inorganic fibers is more densely distributed on the surface than in the interior of the fiber composite, and the porosity of the surface is lower than that of the interior, but the porosity of the surface is Is 50 to 95% and the internal porosity is preferably 85 to 99%.

【0017】本発明の繊維複合体にフィルム、発泡シー
ト、金属板等を積層したり、繊維複合体を他の物品に接
着しやすいように繊維複合体の表面に粘着剤や接着剤を
積層してもよいし、ポリエチレン発泡体、ポリプロピレ
ン発泡体、ポリウレタン発泡体、ゴム発泡体等の独立気
泡もしくは連続気泡を有する発泡体や不織布、織布、塩
化ビニルレザー等の化粧用表皮材を積層してもよい。
A film, a foamed sheet, a metal plate or the like is laminated on the fiber composite of the present invention, or an adhesive or an adhesive is laminated on the surface of the fiber composite so that the fiber composite can be easily adhered to other articles. You may also laminate polyethylene foam, polypropylene foam, polyurethane foam, foam with open or closed cells such as rubber foam or non-woven fabric, woven cloth, vinyl chloride leather or other cosmetic skin material. Good.

【0018】なお、本発明の繊維複合体を加熱すると厚
さが増大する理由については不明な点もあるが、上述の
ニードルパンチ処理により無機繊維が圧縮により屈曲さ
れていて、これが加熱による樹脂の溶融に伴って原状に
復そうとすることに起因するものと推察される。
Although there is an unclear reason why the thickness increases when the fiber composite of the present invention is heated, the inorganic fibers are bent by compression by the above-mentioned needle punching treatment. It is presumed that this is due to the attempt to restore the original state due to melting.

【0019】[0019]

【作用】本発明は、上述のような構成を有するので、繊
維複合体をそれぞれの重量との関係において、十分な強
度と、加熱成形する際の加熱時に、成形性を満足させう
るに十分な厚さの増大を保証する厚さとすることができ
る。
Since the present invention has the above-mentioned constitution, it has sufficient strength in relation to each weight of the fiber composite and sufficient moldability at the time of heating during heat molding. It can be of a thickness that guarantees an increase in thickness.

【0020】[0020]

【実施例】つぎに、本発明の実施例を比較例とともに説
明する。
EXAMPLES Next, examples of the present invention will be described together with comparative examples.

【0021】実施例1 この実施例では、厚さ方向に配向されているものを含む
多数のガラス繊維が相互に部分的に高密度ポリエチレン
で接合されかつ全体にわたって多数の微細な空隙を有す
る繊維複合体であって、その重量が0.6kg/m2
あるので、厚さを3.5mmとしたものである。
Example 1 In this example, a fiber composite in which a number of glass fibers, including those oriented in the thickness direction, are partially bonded to each other with high density polyethylene and have a number of fine voids throughout Since it is a body and its weight is 0.6 kg / m 2 , it has a thickness of 3.5 mm.

【0022】この繊維複合体は、つぎのようにして製造
せられたものである。すなわち、長さ50mm、直径1
3μmのガラス繊維と、長さ50mm、直径10μmの
ポリプロピレン繊維を重量比3:1でカードマシンに供
給し、解繊した後1cm2 当り100箇所のニードルパ
ンチを行なって厚さ6mm、平均重量400g/m2
マット状物を得た。マット状物の両面に厚さ105μ
m、平均重量100g/m2 の高密度ポリエチレンフィ
ルムを積層し、得られた積層物を2枚のポリテトラフル
オロエチレンフィルムの間に挾んで、200℃で3分間
加熱した後、200℃に加熱したプレスにより5kg/
cm2 で加圧して0.8mmに圧縮し、200℃に保っ
たまま両面のポリテトラフルオロエチレンフィルムを厚
さ方向に真空吸引して引っぱり、厚さ3.5mmまで積
層物を膨らませた後冷却し、ポリテトラフルオロエチレ
ンフィルムを剥離して厚さ3.5mmの本発明の繊維複
合体を得た。得られた繊維複合体を再度200℃まで加
熱して厚さ方向に膨張させ、厚さを測定して4.0mm
になるようにプレス成形し、成形品の曲げ強度をJIS
K7221に準拠して測定した。
This fiber composite is manufactured as follows. That is, length 50 mm, diameter 1
3 μm glass fiber and 50 mm long, 10 μm diameter polypropylene fiber were supplied to a card machine at a weight ratio of 3: 1, and after defibration, 100 points were punched per 1 cm 2 to obtain a thickness of 6 mm and an average weight of 400 g. A mat-like product having a thickness of / m 2 was obtained. 105μ thickness on both sides of mat
m, a high-density polyethylene film having an average weight of 100 g / m 2 was laminated, and the obtained laminate was sandwiched between two polytetrafluoroethylene films, heated at 200 ° C. for 3 minutes, and then heated at 200 ° C. 5 kg /
Pressurized with cm 2 and compressed to 0.8 mm, while keeping the temperature at 200 ° C., vacuum suction the polytetrafluoroethylene film on both sides in the thickness direction to pull it, expand the laminate to a thickness of 3.5 mm, and then cool. Then, the polytetrafluoroethylene film was peeled off to obtain a fiber composite of the present invention having a thickness of 3.5 mm. The obtained fiber composite is heated again to 200 ° C. to expand in the thickness direction, and the thickness is measured to be 4.0 mm.
And press-mold it so that the bending strength of the molded product is JIS
It measured based on K7221.

【0023】実施例2 この実施例の繊維複合体は、その重量が0.6kg/m
2 であるので、厚さを2.3mmとした以外は実施例1
と同様である。
Example 2 The fiber composite of this example has a weight of 0.6 kg / m.
Since the thickness is 2 , Example 1 is used except that the thickness is 2.3 mm.
Is the same as.

【0024】すなわち、この繊維複合体は、加熱した積
層物を真空吸引により2.3mmまで膨らませたこと以
外は実施例1と同様の製造方法で得られたものである。
加熱後厚さ4mmにプレス成形した成形品の曲げ強度を
実施例1と同様に測定した。 実施例3 この実施例の繊維複合体は、その重量が0.8kg/m
2 であるので、厚さを4.5mmとした以外は実施例1
と同様のものである。
That is, this fiber composite was obtained by the same manufacturing method as in Example 1 except that the heated laminate was expanded to 2.3 mm by vacuum suction.
The bending strength of a molded product press-molded to a thickness of 4 mm after heating was measured in the same manner as in Example 1. Example 3 The fiber composite of this example has a weight of 0.8 kg / m.
2 is the same as Example 1 except that the thickness is 4.5 mm.
Is similar to.

【0025】この繊維複合体は、つぎのようにして製造
せられたものである。すなわち、長さ50mm、直径1
3μmのガラス繊維と、長さ50mm、直径10μmの
ポリプロピレン繊維を重量比3:1でカードマシンに供
給し、解繊した後1cm2 当り100箇所のニードルパ
ンチを行なって厚さ7mm、平均重量550g/m2
マット状物を得た。マット状物の両面に厚さ130μ
m、平均重量125g/m2 の高密度ポリエチレンフィ
ルムを積層し、得られた積層物を2枚のポリテトラフル
オロエチレンフィルムの間に挾んで、200℃で3分間
加熱した後、200℃に加熱したプレスにより5kg/
cm2 で加圧して0.8mmに圧縮し、200℃に保っ
たまま両面のポリテトラフルオロエチレンフィルムを厚
さ方向に真空吸引して引っぱり、厚さ4.5mmまで積
層物を膨らませた後冷却し、ポリテトラフルオロエチレ
ンフィルムを剥離し、厚さ4.5mmの本発明の繊維複
合体を得た。得られた繊維複合体を再度200℃まで加
熱し、厚さを測定して5.0mmになるようにプレス成
形し、成形品の曲げ強度を測定した。
This fiber composite is manufactured as follows. That is, length 50 mm, diameter 1
3 μm glass fiber and polypropylene fiber having a length of 50 mm and a diameter of 10 μm were supplied to a card machine at a weight ratio of 3: 1, and after disentanglement, needle punching was performed at 100 points per 1 cm 2 to obtain a thickness of 7 mm and an average weight of 550 g. A mat-like product having a thickness of / m 2 was obtained. Thickness 130μ on both sides of mat
m, a high-density polyethylene film having an average weight of 125 g / m 2 was laminated, and the obtained laminate was sandwiched between two polytetrafluoroethylene films, heated at 200 ° C. for 3 minutes, and then heated at 200 ° C. 5 kg /
Pressurized with cm 2 and compressed to 0.8 mm, while keeping the temperature at 200 ° C, vacuum suction the polytetrafluoroethylene film on both sides in the thickness direction and pull it to inflate the laminate to a thickness of 4.5 mm and then cool. Then, the polytetrafluoroethylene film was peeled off to obtain a fiber composite of the present invention having a thickness of 4.5 mm. The obtained fiber composite was heated again to 200 ° C., the thickness was measured, and press molding was performed so that the thickness was 5.0 mm, and the bending strength of the molded product was measured.

【0026】実施例4 この実施例の繊維複合体は、その重量が0.8kg/m
2 であるので、厚さを3.0mmとした以外は実施例3
と同様のものである。
Example 4 The fiber composite of this example has a weight of 0.8 kg / m.
Since it is 2 , Example 3 except that the thickness is 3.0 mm
Is similar to.

【0027】この繊維複合体は、積層物を真空吸引によ
り3.0mmまで膨らませた以外は実施例3と同様の製
造方法で得られたものである。その後厚さが5.0mm
になるようにプレス成形して成形品の曲げ強度を測定し
た。
This fiber composite was obtained by the same manufacturing method as in Example 3 except that the laminate was expanded to 3.0 mm by vacuum suction. Then the thickness is 5.0mm
Was press-molded so that the bending strength of the molded product was measured.

【0028】実施例5 この実施例の繊維複合体は、その重量が1.2kg/m
2 であるので、厚さを8.0mmとした以外は実施例1
と同様のものである。
Example 5 The fiber composite of this example has a weight of 1.2 kg / m.
2 is the same as Example 1 except that the thickness is 8.0 mm.
Is similar to.

【0029】この繊維複合体は、つぎのようにして製造
せられたものである。すなわち、長さ50mm、直径1
3μmのガラス繊維と、長さ50mm、直径10μmの
ポリプロピレン繊維を重量比3:1でカードマシンに供
給し、解繊した後1cm2 当り100箇所のニードルパ
ンチを行なって厚さ8mm、平均重量800g/m2
マット状物を得た。マット状物の両面に厚さ210μ
m、平均重量200g/m2 の高密度ポリエチレンフィ
ルムを積層し、得られた積層物を2枚のポリテトラフル
オロエチレンフィルムの間に挾んで、200℃で3分間
加熱した後、200℃に加熱したプレスにより5kg/
cm2 で加圧して1.2mmに圧縮し、200℃に保っ
たまま両面のポリテトラフルオロエチレンフィルムを厚
さ方向に真空吸引して引っぱり、厚さ7.0mmまで積
層物を膨らませた後冷却し、ポリテトラフルオロエチレ
ンフィルムを剥離して繊維複合体を得た。これを再度2
00℃まで加熱し、厚さを測定して8.0mmになるよ
うにプレス成形して、その曲げ強度を測定した。
This fiber composite is manufactured as follows. That is, length 50 mm, diameter 1
3 μm glass fiber and polypropylene fiber having a length of 50 mm and a diameter of 10 μm were supplied to a card machine at a weight ratio of 3: 1, and after disentanglement, needle punching was performed at 100 points per 1 cm 2 to obtain a thickness of 8 mm and an average weight of 800 g. A mat-like product having a thickness of / m 2 was obtained. 210μ thick on both sides of mat
m, a high-density polyethylene film having an average weight of 200 g / m 2 was laminated, and the obtained laminate was sandwiched between two polytetrafluoroethylene films, heated at 200 ° C. for 3 minutes, and then heated at 200 ° C. 5 kg /
Pressurized with cm 2 and compressed to 1.2mm, while keeping at 200 ° C, vacuum suction the polytetrafluoroethylene film on both sides in the thickness direction to pull it, expand the laminate to a thickness of 7.0mm, and then cool. Then, the polytetrafluoroethylene film was peeled off to obtain a fiber composite. This again 2
It was heated to 00 ° C., the thickness was measured, and press molding was performed so that the thickness was 8.0 mm, and the bending strength was measured.

【0030】実施例6 この実施例の繊維複合体は、その重量が1.2kg/m
2 であるので、厚さを5.0mmとした以外は実施例5
と同様のものである。
Example 6 The fiber composite of this example has a weight of 1.2 kg / m.
Since it is 2 , Example 5 except that the thickness is 5.0 mm
Is similar to.

【0031】この繊維複合体は、積層物を真空吸引によ
り5.0mmまで膨らませた以外は実施例5と同様の製
造方法で得られたものである。その後厚さが8.0mm
になるようにプレス成形して成形品の曲げ強度を測定し
た。
This fiber composite was obtained by the same manufacturing method as in Example 5 except that the laminate was expanded to 5.0 mm by vacuum suction. Then the thickness is 8.0mm
Was press-molded so that the bending strength of the molded product was measured.

【0032】実施例7 この実施例の繊維複合体は、その重量が1.6kg/m
2 であるので、厚さを10.0mmとした以外は実施例
1と同様のものである。
Example 7 The fiber composite of this example has a weight of 1.6 kg / m.
2 is the same as in Example 1 except that the thickness is 10.0 mm.

【0033】この繊維複合体は、つぎのようにして製造
せられたものである。すなわち、長さ50mm、直径1
3μmのガラス繊維と、長さ50mm、直径10μmの
ポリプロピレン繊維を重量比3:1でカードマシンに供
給し、解繊した後1cm2 当り100箇所のニードルパ
ンチを行なって厚さ10mm、平均重量1000g/m
2 のマット状物を得た。マット状物の両面に厚さ315
μm、平均重量300g/m2 の高密度ポリエチレンフ
ィルムを積層し、得られた積層物を2枚のポリテトラフ
ルオロエチレンフィルムの間に挾んで、200℃で3分
間加熱した後、200℃に加熱したプレスにより5kg
/cm2 で加圧して1.6mmに圧縮し、200℃に保
ったまま両面のポリテトラフルオロエチレンフィルムを
厚さ方向に真空吸引して引っぱり、厚さ10.0mmま
で積層物を膨らませた後冷却し、ポリテトラフルオロエ
チレンフィルムを剥離して繊維複合体を得た。これを再
度200℃まで加熱し、厚さを測定して11.0mmに
なるようにプレス成形し、成形品の曲げ強度を測定し
た。
This fiber composite is manufactured as follows. That is, length 50 mm, diameter 1
Glass fiber of 3 μm and polypropylene fiber of 50 mm in length and 10 μm in diameter were supplied to the card machine at a weight ratio of 3: 1, and after being defibrated, needle punching was performed at 100 points per 1 cm 2 to obtain a thickness of 10 mm and an average weight of 1000 g. / M
2 mats were obtained. 315 thickness on both sides of mat
A high-density polyethylene film having a thickness of μm and an average weight of 300 g / m 2 was laminated, and the obtained laminate was sandwiched between two polytetrafluoroethylene films, heated at 200 ° C. for 3 minutes, and then heated at 200 ° C. 5kg by the pressed press
After pressurizing with a pressure of / cm 2 to 1.6 mm and keeping the temperature at 200 ° C., the polytetrafluoroethylene film on both sides is vacuum-sucked in the thickness direction and pulled to expand the laminate to a thickness of 10.0 mm. After cooling, the polytetrafluoroethylene film was peeled off to obtain a fiber composite. This was heated again to 200 ° C., the thickness was measured, and press molding was performed so that the thickness was 11.0 mm, and the bending strength of the molded product was measured.

【0034】実施例8 この実施例の繊維複合体は、その重量が1.6kg/m
2 であるので、厚さを8.0mmとした以外は実施例7
と同様のものである。
Example 8 The fiber composite of this example has a weight of 1.6 kg / m.
Since the thickness is 2 , Example 7 except that the thickness is 8.0 mm.
Is similar to.

【0035】この繊維複合体は、積層物を真空吸引によ
り8.0mmまで膨らませた以外は、実施例7と同様の
製造方法で得られたものである。その後厚さが11.0
mmになるようにプレス成形して成形品の曲げ強度を測
定した。
This fiber composite was obtained by the same manufacturing method as in Example 7 except that the laminate was expanded to 8.0 mm by vacuum suction. Then the thickness is 11.0
Bending strength of the molded product was measured by press molding so as to have a thickness of mm.

【0036】比較例1 この比較例の繊維複合体は、その重量が0.6kg/m
2 であるにかかわらず厚さが4.5mmである以外は実
施例1と同様のものである。
Comparative Example 1 The fiber composite of this comparative example has a weight of 0.6 kg / m.
Despite being 2 , the same as Example 1 except that the thickness is 4.5 mm.

【0037】この繊維複合体は、積層物を真空吸引によ
り4.5mmまで膨らませた以外は、実施例5と同様の
製造方法で得られたものである。その後厚さが4.0m
mになるようにプレス成形して成形品の曲げ強度を測定
した。
This fiber composite was obtained by the same manufacturing method as in Example 5, except that the laminate was expanded to 4.5 mm by vacuum suction. After that the thickness is 4.0m
Bending strength of the molded product was measured by press molding so as to have m.

【0038】比較例2 この比較例の繊維複合体は、その重量が0.6kg/m
2 であるにかかわらず厚さが1.5mmである以外は実
施例1と同様のものである。
Comparative Example 2 The fiber composite of this comparative example has a weight of 0.6 kg / m.
Despite being 2 , the same as Example 1 except that the thickness is 1.5 mm.

【0039】この繊維複合体は、積層物を真空吸引によ
り1.5mmまで膨らませた以外は、実施例1と同様の
製造方法で得られたものである。その後実施例1と同様
に、加熱して厚さ2.9mmまで膨らませたが、4.0
mmにするようセットされたプレス機に対しては厚さ不
充分で、適正なプレス成形ができなかった。
This fiber composite was obtained by the same manufacturing method as in Example 1 except that the laminate was expanded to 1.5 mm by vacuum suction. Then, as in Example 1, the material was heated to inflate it to a thickness of 2.9 mm.
The thickness was insufficient for a press machine set to have a thickness of mm, and proper press molding could not be performed.

【0040】比較例3 この比較例の繊維複合体は、その重量が0.8kg/m
2 であるにかかわらず厚さが5.5mmである以外は実
施例1と同様のものである。
Comparative Example 3 The fiber composite of this comparative example had a weight of 0.8 kg / m.
Despite being 2 , the same as Example 1 except that the thickness is 5.5 mm.

【0041】この繊維複合体は、積層物を真空吸引によ
り5.5mmまで膨らませた以外は、実施例3と同様の
製造方法で得られたものである。その後厚さが5.0m
mになるようにプレス成形し、成形品の曲げ強度を測定
した。
This fiber composite was obtained by the same manufacturing method as in Example 3 except that the laminate was expanded to 5.5 mm by vacuum suction. Then the thickness is 5.0m
It was press-molded so as to have m, and the bending strength of the molded product was measured.

【0042】比較例4 この比較例の繊維複合体は、その重量が0.8kg/m
2 であるにかかわらず厚さが2.0mmである以外は実
施例1と同様のものである。
Comparative Example 4 The fiber composite of this comparative example has a weight of 0.8 kg / m.
Despite being 2 , the same as Example 1 except that the thickness is 2.0 mm.

【0043】この繊維複合体は、積層物を真空吸引によ
り2.0mmまで膨らませた以外は、実施例3と同様の
製造方法で得られたものである。その後厚さが2.0m
mになるようにプレス成形した成形品の曲げ強度を測定
した。
This fiber composite was obtained by the same manufacturing method as in Example 3 except that the laminate was expanded to 2.0 mm by vacuum suction. Then the thickness is 2.0m
The bending strength of a molded product press-molded to have a thickness of m was measured.

【0044】比較例5 この比較例の繊維複合体は、その重量が1.2kg/m
2 であるにかかわらず厚さが9.0mmである以外は実
施例1と同様のものである。
Comparative Example 5 The fiber composite of this comparative example has a weight of 1.2 kg / m.
Despite being 2 , the same as Example 1 except that the thickness is 9.0 mm.

【0045】この繊維複合体は、積層物を真空吸引によ
り9.0mmまで膨らませた以外は、実施例5と同様の
製造方法で得られたものである。その後厚さが8.0m
mになるようにプレス成形し、成形品の曲げ強度を測定
した。
This fiber composite was obtained by the same manufacturing method as in Example 5 except that the laminate was expanded to 9.0 mm by vacuum suction. After that the thickness is 8.0m
It was press-molded so as to have m, and the bending strength of the molded product was measured.

【0046】比較例6 この比較例の繊維複合体は、その重量が1.2kg/m
2 であるにかかわらず厚さが4.0mmである以外は実
施例1と同様のものである。
Comparative Example 6 The fiber composite of this comparative example has a weight of 1.2 kg / m.
Despite being 2 , the same as Example 1 except that the thickness is 4.0 mm.

【0047】この繊維複合体は、積層物を真空吸引によ
り4.0mmまで膨らませた以外は、実施例5と同様の
製造方法で得られたものである。その後実施例5と同様
に加熱して厚さ6.9mmまで膨らませたが、8.0m
mにするようセットされたプレス機に対しては厚さ不充
分で、適正なプレス成形ができなかった。
This fiber composite was obtained by the same manufacturing method as in Example 5 except that the laminate was expanded to 4.0 mm by vacuum suction. After that, it was heated in the same manner as in Example 5 to inflate it to a thickness of 6.9 mm.
The thickness was not sufficient for the press machine set to m, and proper press molding could not be performed.

【0048】比較例7 この比較例の繊維複合体は、その重量が1.6kg/m
2 であるにかかわらず厚さが12.0mmである以外は
実施例1と同様のものである。
Comparative Example 7 The fiber composite of this comparative example has a weight of 1.6 kg / m.
Despite being 2 , the same as Example 1 except that the thickness is 12.0 mm.

【0049】この繊維複合体は、積層物を真空吸引によ
り12.0mmまで膨らませた以外は、実施例7と同様
の製造方法で得られたものである。その後厚さが11.
0mmになるようにプレス成形し、成形品の曲げ強度を
測定した。
This fiber composite was obtained by the same manufacturing method as in Example 7 except that the laminate was expanded to 12.0 mm by vacuum suction. Then the thickness is 11.
It was press-molded to have a thickness of 0 mm, and the bending strength of the molded product was measured.

【0050】比較例8 この比較例の繊維複合体は、その重量が1.6kg/m
2 であるにかかわらず厚さが6.0mmである以外は実
施例7と同様のものである。
Comparative Example 8 The fiber composite of this comparative example has a weight of 1.6 kg / m.
Despite being 2 , the same as Example 7 except that the thickness is 6.0 mm.

【0051】この繊維複合体は、積層物を真空吸引によ
り6.0mmまで膨らませた以外は、実施例7と同様の
製造方法で得られたものである。その後実施例7と同様
に加熱して厚さ9.2mmまで膨らませたが、11.0
mmにするようセットされたプレス機に対しては厚さ不
足で、適性なプレス成形ができなかった。
This fiber composite was obtained by the same manufacturing method as in Example 7 except that the laminate was expanded to 6.0 mm by vacuum suction. Then, it was heated in the same manner as in Example 7 to be inflated to a thickness of 9.2 mm.
The thickness was insufficient for a press machine set to have a thickness of mm, so that proper press molding could not be performed.

【0052】各実施例及び各比較例の成形品について曲
げ強度を測定した結果を表1に示す(JIS K722
1準拠)。
The results of measuring the flexural strength of the molded articles of Examples and Comparative Examples are shown in Table 1 (JIS K722).
1).

【0053】[0053]

【表1】 [Table 1]

【0054】[0054]

【発明の効果】本発明の繊維複合体によれば、重量が変
っても常に強度が大でしかもプレス成形性のよい厚さと
なすことができる。
EFFECTS OF THE INVENTION According to the fiber composite of the present invention, it is possible to obtain a thickness which is always high in strength and has good press formability even if the weight changes.

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

【図1】平均重量700g/m2 の繊維複合体の厚さと
加熱後に厚さ4mmにプレスした成形品の曲げ強度との
関係を示すグラフである。
FIG. 1 is a graph showing the relationship between the thickness of a fiber composite having an average weight of 700 g / m 2 and the bending strength of a molded product pressed into a thickness of 4 mm after heating.

───────────────────────────────────────────────────── フロントページの続き (51)Int.Cl.5 識別記号 庁内整理番号 FI 技術表示箇所 D04H 1/58 A 7199−3B // D06M 15/70 23/16 ─────────────────────────────────────────────────── ─── Continuation of the front page (51) Int.Cl. 5 Identification code Office reference number FI technical display location D04H 1/58 A 7199-3B // D06M 15/70 23/16

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】 厚さ方向に配向されているものを含む多
数の無機繊維が相互に部分的に熱可塑性樹脂で接合され
かつ全体にわたって多数の微細な空隙を有する繊維複合
体において、その厚さT(mm)が重量W(kg/
2 )の関数で 0.4≦W≦0.9のとき、4W−0.5≦T≦5W+
1 0.9<W≦1.7のとき、6W−2.3≦T≦8W−
1.7 の範囲にあることを特徴とする繊維複合体。
1. A fiber composite in which a large number of inorganic fibers including those oriented in the thickness direction are partially bonded to each other with a thermoplastic resin and have a large number of fine voids throughout. T (mm) is weight W (kg /
m 2 ), when 0.4 ≦ W ≦ 0.9, 4W−0.5 ≦ T ≦ 5W +
When 1 0.9 <W ≦ 1.7, 6W−2.3 ≦ T ≦ 8W−
A fiber composite characterized by being in the range of 1.7.
JP4342016A 1992-12-22 1992-12-22 Fiber composite Expired - Lifetime JP2960269B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP4342016A JP2960269B2 (en) 1992-12-22 1992-12-22 Fiber composite

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP4342016A JP2960269B2 (en) 1992-12-22 1992-12-22 Fiber composite

Publications (2)

Publication Number Publication Date
JPH06184901A true JPH06184901A (en) 1994-07-05
JP2960269B2 JP2960269B2 (en) 1999-10-06

Family

ID=18350533

Family Applications (1)

Application Number Title Priority Date Filing Date
JP4342016A Expired - Lifetime JP2960269B2 (en) 1992-12-22 1992-12-22 Fiber composite

Country Status (1)

Country Link
JP (1) JP2960269B2 (en)

Also Published As

Publication number Publication date
JP2960269B2 (en) 1999-10-06

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