JPH0593352A - Thermoformable core material and method for producing the same - Google Patents

Thermoformable core material and method for producing the same

Info

Publication number
JPH0593352A
JPH0593352A JP4000870A JP87092A JPH0593352A JP H0593352 A JPH0593352 A JP H0593352A JP 4000870 A JP4000870 A JP 4000870A JP 87092 A JP87092 A JP 87092A JP H0593352 A JPH0593352 A JP H0593352A
Authority
JP
Japan
Prior art keywords
thermoplastic resin
heat
mat
resin
sheet
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
JP4000870A
Other languages
Japanese (ja)
Other versions
JP3095503B2 (en
Inventor
Rikizo Tanaka
利喜蔵 田中
Fumio Nishitani
文男 西谷
Hiroshi Nasu
博至 那須
Katsuhiko Yamaji
克彦 山路
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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=26333977&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=JPH0593352(A) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Sekisui Chemical Co Ltd filed Critical Sekisui Chemical Co Ltd
Priority to JP04000870A priority Critical patent/JP3095503B2/en
Publication of JPH0593352A publication Critical patent/JPH0593352A/en
Application granted granted Critical
Publication of JP3095503B2 publication Critical patent/JP3095503B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Landscapes

  • Laminated Bodies (AREA)
  • Blow-Moulding Or Thermoforming Of Plastics Or The Like (AREA)
  • Inorganic Fibers (AREA)
  • Nonwoven Fabrics (AREA)

Abstract

PURPOSE:To obtain a thermoformable core material suitable as a substrate for formed ceiling and formed inner trim substrate for door of automobile, etc., by producing a sandwich laminate from inorganic resin and thermoplastic resin fiber and heat-treating the laminate under specific condition. CONSTITUTION:Both surfaces of a mat produced by using an inorganic fiber and a thermoplastic resin fiber are laminated with thermoplastic resin sheets (a) and (b). At least one surface of the obtained sandwiched laminate is laminated with a sheet made of a heat-resistant rigid resin (d) having a melting point higher than that of the thermoplastic resin fiber and the thermoplastic resin. The objective thermoformable core material is obtained by heating the laminated sheet at a temperature below the melting temperature of the heat- resistant rigid resin to melt the thermoplastic resin fiber and the thermoplastic resin and pressing the sheet to impregnate the thermoplastic resins (a) and (b) into the mat and bond the inorganic fibers with each other without impregnating the heat-resistant rigid resin (d) into the mat.

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、熱成形される複合材、
特に自動車等車両の成形天井の基材、ドアの成形内装基
材に使用される熱成形性芯材およびその製造方法に関す
る。
FIELD OF THE INVENTION The present invention relates to a thermoformed composite material,
In particular, the present invention relates to a thermoformable core material used as a base material for a molded ceiling of a vehicle such as an automobile and a molded interior base material for a door, and a method for producing the same.

【0002】[0002]

【従来の技術】従来、自動車等車両の内装材、特に熱成
形天井の基材に使用される熱成形性芯材には、軽量で、
剛性、耐熱性、熱賦形性などの性能が優れていることが
要求される。この種の材料として、例えば特開昭60−
83832号公報には、ガラス繊維などの無機繊維層の
両面にポリエチレン等の合成樹脂層を積層して基材を形
成し、この基材の樹脂層の表面に発泡体層を介して表皮
材を積層してなる熱成形性複合材料が開示されている。
ところが、このような熱成形性材料は、特に吸音性が低
く、また曲げ強度も充分でなく、例えば自動車天井材の
芯材として使用するには不十分であった。
2. Description of the Related Art Conventionally, a thermoformable core material used as a base material for an interior of a vehicle such as an automobile, especially a thermoformed ceiling, is lightweight,
Excellent performance such as rigidity, heat resistance, and heat shaping property is required. As this kind of material, for example, JP-A-60-
In Japanese Patent No. 83832, a base material is formed by laminating a synthetic resin layer such as polyethylene on both surfaces of an inorganic fiber layer such as glass fiber, and a skin material is provided on the surface of the resin layer of the base material via a foam layer. A thermoformable composite material formed by laminating is disclosed.
However, such a thermoformable material has particularly low sound absorbing property and insufficient bending strength, and is insufficient for use as a core material for an automobile ceiling material, for example.

【0003】かかる欠点を解消するために本発明者らは
既に、特開平1−56562号公報、特開平2−539
48号公報に、無機繊維が結着剤で部分的に結合され、
全体に亘って多数の空隙を有する成型体であって、両表
面から内部の空隙に連通する多数の細孔が形成された繊
維成形体や積層体を提案してきた。これら繊維成形体や
積層体は、耐熱性、熱賦形性、吸音性などが優れる利点
を有している。
In order to eliminate such a drawback, the present inventors have already disclosed in Japanese Patent Laid-Open Nos. 1-56562 and 2-539.
No. 48, the inorganic fibers are partially bound by a binder,
A fiber molded body or a laminated body, which is a molded body having a large number of voids throughout and in which a large number of pores communicating from both surfaces to internal voids is formed, has been proposed. These fiber moldings and laminates have the advantages of excellent heat resistance, heat shaping properties, sound absorption properties, and the like.

【0004】[0004]

【発明が解決しようとする課題】しかし、この種の積層
体などは、無機繊維が熱可塑性樹脂からなる結着剤で部
分的に結合しているが故、多数の細孔、空隙を有し、通
気性が有り、機械的強度、即ち剛性にも限界があった。
However, this type of laminate has a large number of pores and voids because the inorganic fibers are partially bound by a binder made of a thermoplastic resin. However, it has air permeability and its mechanical strength, that is, its rigidity, is limited.

【0005】したがって、この種の積層体などを例え
ば、自動車の成形天井の基材として使用する場合、これ
に積層される表皮材が例えば、ニット表皮、ニットウレ
タン表皮、不織布表皮など、それ自体が通気性を持つも
のを使用する場合には、表皮材表面が、温度変化などで
生ずる通気によって汚れてくるという問題があった。
Therefore, when this type of laminated body is used as a base material for a molded ceiling of an automobile, for example, the skin material laminated thereon is, for example, a knit skin, a knit urethane skin or a non-woven fabric skin. When a material having air permeability is used, there is a problem in that the surface of the skin material is contaminated by the air generated due to temperature changes.

【0006】このため、従来は表皮材を例えば塩化ビニ
ルレザー等の通気性の無いものに限定したり、通気性の
無いシート類を表皮材に付加するか、あるいは、車体構
造により天井が通気しないようにするなどの対策が必要
で、自動車の内装費用が高くなり、表皮材の選択幅が狭
くなったり、また、生産性が低下するなどの欠点があっ
た。
For this reason, conventionally, the skin material is limited to a non-breathable material such as vinyl chloride leather, non-breathable sheets are added to the skin material, or the ceiling does not vent due to the body structure. However, there are drawbacks such as an increase in automobile interior cost, a narrow selection range of skin materials, and a decrease in productivity.

【0007】このような欠点を解消すべく、特開昭64
−63113号公報には、複合成形体の製造方法が開示
されている。しかしながら、この方法によって得られる
複合成形体は、積層される耐熱樹脂シートを溶融するも
のではないため、無機繊維部分と耐熱樹脂シートの接合
強度が小さく、その後の二次加工時や経時的に剥離を生
じたりすることがあった。また、二次加工については熱
絞り成形が伴うことになるが、耐熱樹脂シートに熱絞り
成形によるシワが発生することが多かった。
In order to solve such a defect, Japanese Patent Laid-Open No. Sho 64-64
Japanese Patent Laid-Open No. 63113 discloses a method for manufacturing a composite molded body. However, since the composite molded body obtained by this method does not melt the heat-resistant resin sheet to be laminated, the bonding strength between the inorganic fiber portion and the heat-resistant resin sheet is small, and peeling occurs during the subsequent secondary processing or over time. May occur. Further, the secondary processing is accompanied by hot drawing, but wrinkles often occur in the heat resistant resin sheet due to hot drawing.

【0008】本発明の目的は、軽量性、耐熱性、熱賦形
性、および吸音性を損なうことなく、芯材自体が加熱賦
形した後も、完全な通気遮断性を有すると共に、芯材お
よび賦形後の芯材の機械的強度(剛性)を向上させた熱
成形性芯材およびその製造方法を提供することにある。
It is an object of the present invention to have a complete air-blocking property even after the core material itself is heated and shaped without impairing the lightness, the heat resistance, the heat shaping property, and the sound absorbing property, and the core material. Another object of the present invention is to provide a thermoformable core material with improved mechanical strength (rigidity) of the core material after shaping and a method for producing the same.

【0009】本発明者らは、鋭意研究した結果、無機繊
維と熱可塑性樹脂繊維を主材料とするマット状物と耐熱
剛性樹脂層との間に、熱可塑性樹脂層を介在させ、これ
を加熱溶融・圧縮することによって、上記目的を達成で
きることを見出だし、その知見に基づいて本発明を完成
するに至った。
As a result of earnest studies, the inventors of the present invention intervene a thermoplastic resin layer between a heat-resistant and rigid resin layer and a mat-like material mainly composed of inorganic fibers and thermoplastic resin fibers and heat it. It was found that the above object can be achieved by melting and compressing, and the present invention has been completed based on the findings.

【0010】[0010]

【課題を解決するための手段】すなわち、本発明によれ
ば、無機繊維が熱可塑性樹脂により結着せられているマ
ット状物の少なくとも片面に、前記熱可塑性樹脂より溶
融温度の高い耐熱剛性樹脂(d) からなるシート状物が積
層され、無機繊維が厚み方向に拡開されていることを特
徴とする熱成形性芯材が提供せられる。
That is, according to the present invention, a heat-resistant and rigid resin having a melting temperature higher than that of the thermoplastic resin is provided on at least one surface of the mat-like material in which the inorganic fibers are bound by the thermoplastic resin. There is provided a thermoformable core material, characterized in that the sheet-like material consisting of d) is laminated and the inorganic fibers are expanded in the thickness direction.

【0011】また、本発明によれば、無機繊維と熱可塑
性樹脂繊維を主材料として形成されたマット状物の両面
に、熱可塑性樹脂シート状物(a) (b) を積層し、得られ
たサンドイッチ積層物の少なくとも片面に、前記熱可塑
性樹脂繊維および前記熱可塑性樹脂より溶融温度の高
い、耐熱剛性樹脂(d) からなるシート状物を積層した積
層シートを、前記耐熱剛性樹脂の溶融温度以下の温度で
加熱して、前記熱可塑性樹脂繊維と前記熱可塑性樹脂
を、各々、溶融させると共に圧縮して、前記熱可塑性樹
脂(a) (b) を前記マット状物内に含浸させて前記無機繊
維相互を結着させ、一方、前記耐熱剛性樹脂(d) は前記
マット状物内に含浸させないことを特徴とする熱成形性
芯材の製造方法が提供せられる。
According to the present invention, the thermoplastic resin sheet materials (a) and (b) are laminated on both surfaces of the mat-like material formed of inorganic fibers and thermoplastic resin fibers as main materials to obtain a mat-shaped material. A laminated sheet, in which a sheet material made of a heat-resistant and rigid resin (d) having a higher melting temperature than the thermoplastic resin fiber and the thermoplastic resin is laminated on at least one surface of the sandwich laminate, By heating at the following temperature, the thermoplastic resin fiber and the thermoplastic resin are respectively melted and compressed, the thermoplastic resin (a) (b) is impregnated in the mat-like material There is provided a method for producing a thermoformable core material, which comprises binding the inorganic fibers to each other, while not impregnating the heat-resistant and rigid resin (d) into the mat-like material.

【0012】以下、本発明について詳しく説明する。The present invention will be described in detail below.

【0013】本発明で使用するマット状物は、無機繊維
と熱可塑性樹脂繊維を主体としたものであり、無機繊維
としては、例えばガラス繊維、ロックウール等が挙げら
れる。無機繊維の長さは、マット状物の形成性の観点か
ら、5〜250mmが好ましく、より好ましくは、50〜
150mmのものが70重量%以上の分布をなすものであ
る。また、無機繊維の太さは、得られる熱成形芯材の曲
げ強度、厚み回復性の観点から、5〜20μmが好まし
く、より好ましくは7〜13μmである。
The mat-like material used in the present invention is mainly composed of inorganic fibers and thermoplastic resin fibers. Examples of the inorganic fibers include glass fibers and rock wool. The length of the inorganic fiber is preferably from 5 to 250 mm, more preferably from 50 to 50, from the viewpoint of forming the mat-like material.
The one having a diameter of 150 mm has a distribution of 70% by weight or more. Further, the thickness of the inorganic fiber is preferably 5 to 20 μm, more preferably 7 to 13 μm from the viewpoint of bending strength and thickness recovery of the thermoformed core material obtained.

【0014】また、熱可塑性樹脂繊維は、溶融され易く
ガラス繊維と結着する樹脂が好ましく例えば、ポリエチ
レン、ポリプロピレン、ポリスチレン等の樹脂からなる
繊維が挙げられる。熱可塑性樹脂繊維の長さおよび太さ
は、上記無機繊維に分散性よく混繊して容易にマット状
物を形成できる程度が好ましい。具体的には、長さは5
〜200mmが好ましく、より好ましくは20〜100mm
である。太さは5〜70μmが好ましく、より好ましく
は15〜40μmである。熱可塑性樹脂繊維としては、
芯材とホットメルト型の外装があるものでもよい。
The thermoplastic resin fiber is preferably a resin that is easily melted and bound to the glass fiber, and examples thereof include fibers made of a resin such as polyethylene, polypropylene and polystyrene. The length and thickness of the thermoplastic resin fiber are preferably such that the above-mentioned inorganic fiber can be easily mixed to form a mat-like material. Specifically, the length is 5
~ 200 mm is preferred, more preferably 20-100 mm
Is. The thickness is preferably 5 to 70 μm, more preferably 15 to 40 μm. As the thermoplastic resin fiber,
It may have a core material and a hot-melt type exterior.

【0015】無機繊維と熱可塑性樹脂繊維の配合割合
は、無機繊維の割合が少ないと、得られる熱成形性芯材
の耐熱性が低下し、多くなると無機繊維相互の結合部が
低下して機械的強度すなわち剛性が低下するので、無機
繊維と熱可塑性樹脂との重量比で5:1〜1:5の範囲
に設定するのが好ましい。
Regarding the blending ratio of the inorganic fibers and the thermoplastic resin fibers, if the proportion of the inorganic fibers is small, the heat resistance of the obtained thermoformable core material is lowered, and if the proportion is large, the joint portion between the inorganic fibers is lowered and the mechanical fibers are mechanical It is preferable to set the weight ratio of the inorganic fiber and the thermoplastic resin to be in the range of 5: 1 to 1: 5 because the mechanical strength, that is, the rigidity is lowered.

【0016】マット状物の製造方法は、任意の方法が採
用されてよく、一般的にはカードマシンに上記の無機繊
維と熱可塑性繊維を供給し、解繊してニードルパンチを
施して製造する。ニードルパンチは、マット状物及び得
られる熱成形性芯材の機械的強度を向上する為、1cm2
当り2〜100箇所打たれるのが好ましく、より好まし
くは10〜50箇所である。
Any method may be used for producing the mat-like material. Generally, the above-mentioned inorganic fiber and thermoplastic fiber are supplied to a card machine, defibrated and needle punched to produce the mat-like material. .. Needle punch is 1 cm 2 in order to improve the mechanical strength of the mat-like material and the resulting thermoformable core material.
The number of hits is preferably 2 to 100, and more preferably 10 to 50.

【0017】マット状物の密度は、大きくなるとマット
状物が重くなり、小さくなるとマット状物の機械的強度
が低下するので0.01〜0.2g/cm3 が好ましい。
マット状物の重さは、機械的強度を得るためには200
〜1500g/m2 が好ましく、より好ましくは300
〜800g/m2 がよい。
The density of the mat-like material is preferably 0.01 to 0.2 g / cm 3 because the mat-like material becomes heavier as the mat-like material becomes heavier and the mechanical strength as the mat-like material decreases as the mat-like material becomes smaller.
The weight of the mat is 200 to obtain the mechanical strength.
~ 1500 g / m 2 is preferred, more preferably 300
~ 800 g / m 2 is good.

【0018】本発明で用いる熱可塑性樹脂は、溶融させ
た状態でマット状物内に含浸されやすく、かつ、ガラス
繊維と結着しやすいものである。このような熱可塑性樹
脂としては例えば、ポリエチレン、ポリプロピレン、エ
チレン−酢酸ビニル共重合体、飽和ポリエステルおよび
これらの変性物(例えば、無水マレイン酸変性ポリエチ
レン)等の熱可塑性樹脂が挙げられる。
The thermoplastic resin used in the present invention is easily impregnated in the mat-like material in a molten state and is easily bound to the glass fiber. Examples of such a thermoplastic resin include thermoplastic resins such as polyethylene, polypropylene, ethylene-vinyl acetate copolymer, saturated polyester and modified products thereof (for example, maleic anhydride-modified polyethylene).

【0019】また、本発明で用いる耐熱剛性樹脂は、熱
可塑性樹脂繊維および熱可塑性樹脂より溶融温度の高い
ものであり、熱可塑性樹脂の溶融温度より、30℃以
上、好ましくは、50℃以上高いものである。このこと
により、積層シート全体を加熱して耐熱剛性樹脂以外の
樹脂を溶融させることができる。このような耐熱剛性樹
脂としては、例えば、ポリブチレンテレフタレート、飽
和ポリエステル、ポリカーボネートおよびこれらの変性
物などの耐熱剛性樹脂が挙げられる。
The heat-resistant and rigid resin used in the present invention has a melting temperature higher than that of the thermoplastic resin fiber and the thermoplastic resin, and is 30 ° C. or more, preferably 50 ° C. or more higher than the melting temperature of the thermoplastic resin. It is a thing. As a result, the entire laminated sheet can be heated to melt the resin other than the heat-resistant and rigid resin. Examples of such heat-resistant and rigid resins include heat-resistant and rigid resins such as polybutylene terephthalate, saturated polyester, polycarbonate, and modified products thereof.

【0020】また、本発明で用いる耐熱剛性樹脂は、無
機繊維層の表面に強靭かつ、完全な樹脂層を積層するこ
とにより、通気性の完全遮断を行なうとともに、芯材の
剛性を向上させるために、曲げ弾性率が15000kg/
cm2 以上のものが好ましい。より好ましくは20000
kg/cm2 以上の耐熱性剛性樹脂である。曲げ弾性率が1
5000kg/cm2 以下であると芯材の通気性の完全遮断
は可能だが、剛性の向上に寄与しにくくなる。
In addition, the heat-resistant and rigid resin used in the present invention has a strong and complete resin layer laminated on the surface of the inorganic fiber layer to completely block air permeability and improve the rigidity of the core material. And flexural modulus of 15000 kg /
It is preferably cm 2 or more. More preferably 20000
It is a heat-resistant and rigid resin with a weight of more than kg / cm 2 . Flexural modulus is 1
When it is 5000 kg / cm 2 or less, the air permeability of the core material can be completely cut off, but it becomes difficult to contribute to the improvement of rigidity.

【0021】また、本発明で用いる耐熱剛性樹脂は、良
好な熱成形性を得るために、熱成形絞り率(熱成形絞り
率は真空成形機にて円筒型に板状物を絞る際の直径Dと
高さHの比率H/Dにより規定する。)が0.5以上の
ものが好ましい。熱成形絞り率が0.5以下であると芯
材の熱成形性能、すなわち賦形性に問題が生じる。
The heat-resistant and rigid resin used in the present invention has a thermoforming drawing ratio (the thermoforming drawing ratio is the diameter when a plate-like material is drawn into a cylindrical shape by a vacuum forming machine). It is preferable that the ratio H / D of D to height H) is 0.5 or more. When the thermoforming drawing ratio is 0.5 or less, there is a problem in the thermoforming performance of the core material, that is, the shapeability.

【0022】次に、本発明において積層シート構造を得
る方法について説明する。
Next, a method for obtaining a laminated sheet structure in the present invention will be described.

【0023】まず第1の方法は、マット状物の両面に、
熱可塑性樹脂シート状物(a) (b) を積層し、得られたサ
ンドイッチ積層物の少なくとも片面に、耐熱剛性樹脂
(d) からなるシート状物を積層して積層シートを得る方
法である。
First, the first method is to apply the
Thermoplastic resin sheets (a) and (b) are laminated, and the heat-resistant and rigid resin is laminated on at least one side of the resulting sandwich laminate.
It is a method of obtaining a laminated sheet by laminating sheet-like materials comprising (d).

【0024】熱可塑性樹脂シート状物は溶融して、マッ
ト状物と耐熱剛性樹脂(例えば、ポリブチレンテレフタ
レート)シート状物との接合と、マット状物への含浸に
寄与する。また、マット状物が既に熱可塑性樹脂で十分
に含浸されているものであれば、熱可塑性樹脂シート状
物は、マット状物と耐熱剛性樹脂シート状物との接合に
主に寄与するようにしてもよい。
The thermoplastic resin sheet material melts and contributes to the joining of the mat-like material and the heat-resistant and rigid resin (for example, polybutylene terephthalate) sheet-like material and the impregnation of the mat-like material. Further, if the mat-like material is already sufficiently impregnated with the thermoplastic resin, the thermoplastic resin sheet-like material should mainly contribute to the joining of the mat-like material and the heat-resistant and rigid resin sheet-like material. May be.

【0025】第2の方法は、前記サンドイッチ積層物の
少なくとも片面に、耐熱剛性樹脂層(d) と熱可塑性樹脂
層(c) からなる多層シート状物[(d) /(c) ]を層(c)
が外側になるように積層して積層シートを得る方法であ
る。
In the second method, a multilayer sheet material [(d) / (c)] comprising a heat-resistant and rigid resin layer (d) and a thermoplastic resin layer (c) is formed on at least one surface of the sandwich laminate. (c)
It is a method of obtaining a laminated sheet by laminating the sheet so that it is on the outside.

【0026】第3の方法は、マット状物の一面に熱可塑
性樹脂シート状物(a) を積層し、マット状物の他の一面
に、耐熱剛性樹脂層(d) とこれをサンドイッチする熱可
塑性樹脂層(b) (c) からなる多層シート状物[(b) /
(d) /(c) ]を層(c) が外側になるように積層して積層
シートを得る方法である。
In the third method, the thermoplastic resin sheet material (a) is laminated on one surface of the mat-like material, and the heat-resistant and rigid resin layer (d) is sandwiched between the thermoplastic resin sheet material (a) and the other surface of the mat-like material. Multi-layer sheet material [(b) / consisting of plastic resin layers (b) and (c)]
(d) / (c)] is laminated so that the layer (c) is on the outer side to obtain a laminated sheet.

【0027】第4の方法は、マット状物の両面に、耐熱
剛性樹脂層(d) とこれをサンドイッチする熱可塑性樹脂
層(b) (c) からなる多層シート状物[(b) /(d) /(c)
]を層(c) が外側になるように積層して積層シートを
得る方法である。
A fourth method is a multilayer sheet material [(b) / (consisting of a heat-resistant and rigid resin layer (d) and thermoplastic resin layers (b) and (c) sandwiching the same on both surfaces of the mat-like material. d) / (c)
] Is laminated so that the layer (c) is on the outside to obtain a laminated sheet.

【0028】本発明では上記積層構成において、熱可塑
性樹脂層と耐熱剛性樹脂層とが互いに強固に接着しない
と、得られる熱成形性芯材から耐熱剛性樹脂層(シート
状物)が剥離するおそれがあり、接着強度を高めるため
に、耐熱剛性樹脂層(d) の少なくとも片面に接着性樹脂
層が設けられることが好ましい。すなわち、熱可塑性樹
脂層(a) 、(b) または(c) と耐熱剛性樹脂層(d) との間
にそれぞれ接着性樹脂を介在させることによって、接着
強度を高めることができる。この熱可塑性樹脂(a) また
は(b) と、耐熱剛性樹脂層(シート状物)の間の接着強
度(剥離強度)は、100g/15mm以上であることが
好ましく、より好ましくは150g/15mm以上、さら
に好ましくは200g/15mm以上である。この接着強
度が100g/15mm以下であると、芯材製造時や、例
えば自動車等の天井に加熱賦形時、および天井として使
用された際に剥離の問題を起こす。
In the present invention, in the above laminated structure, if the thermoplastic resin layer and the heat-resistant and rigid resin layer are not firmly adhered to each other, the heat-resistant and rigid resin layer (sheet-like material) may be peeled from the obtained thermoformable core material. Therefore, in order to increase the adhesive strength, it is preferable to provide an adhesive resin layer on at least one surface of the heat-resistant and rigid resin layer (d). That is, the adhesive strength can be increased by interposing an adhesive resin between the thermoplastic resin layer (a), (b) or (c) and the heat-resistant and rigid resin layer (d). The adhesive strength (peel strength) between the thermoplastic resin (a) or (b) and the heat-resistant and rigid resin layer (sheet-like material) is preferably 100 g / 15 mm or more, more preferably 150 g / 15 mm or more. And more preferably 200 g / 15 mm or more. If the adhesive strength is 100 g / 15 mm or less, there is a problem of peeling when manufacturing the core material, when heating the ceiling of an automobile or the like, and when used as a ceiling.

【0029】また、熱可塑性樹脂層((a) 、(b) 、(c)
)、耐熱剛性樹脂層(d) 、接着(樹脂)層の各層の厚
さは、とくに限定されるものではない。詳しくは、熱可
塑性樹脂層((a) 、(b) )はマット状物に充分溶融含浸
されて、マット状物内の熱可塑性樹脂繊維と共に無機繊
維を充分に結着させるに必要な厚さで、得ようとする熱
成形性芯材の重量の25〜40%が望ましく、一般には
50〜150μmが好ましい。熱可塑性樹脂層(c) は5
〜20μmが好ましい。また、耐熱剛性樹脂層(d) は熱
成形時の伸びに追従し部分的に切れてしまうことがな
く、かつ、高い剛性が得られる厚さであり、一般に5〜
50μm、好ましくは5〜40μm、より好ましくは1
0〜25μmである。5μm以下では通気性の完全遮断
を行ないにくく、また、50μm以上に厚くすることは
芯材の重量増と経済的な観点から好ましくない。接着
(樹脂)層は熱成形性芯材を製造する際さらに芯材を加
熱賦形する際の熱履歴、機械的応力(圧縮、拡厚、延伸
など)履歴および例えば自動車天井材としての使用にお
いて、十分な接着強度が得られる厚さで、一般には5〜
20μmが望ましい。
Further, the thermoplastic resin layers ((a), (b), (c)
), The heat-resistant and rigid resin layer (d), and the adhesive (resin) layer are not particularly limited in thickness. Specifically, the thermoplastic resin layers ((a) and (b)) are sufficiently melt-impregnated in the mat-like material to have a thickness necessary to sufficiently bind the inorganic fibers together with the thermoplastic resin fibers in the mat-like material. Then, 25 to 40% of the weight of the thermoformable core material to be obtained is desirable, and generally 50 to 150 μm is preferable. The thermoplastic resin layer (c) is 5
˜20 μm is preferred. In addition, the heat-resistant and rigid resin layer (d) has a thickness such that it does not follow the elongation during thermoforming and is not partially cut, and high rigidity is obtained.
50 μm, preferably 5 to 40 μm, more preferably 1
It is 0 to 25 μm. If the thickness is 5 μm or less, it is difficult to completely block the air permeability, and it is not preferable to increase the thickness to 50 μm or more from the viewpoint of an increase in weight of the core material and an economical viewpoint. The adhesive (resin) layer is used in the production of a thermoformable core material, the heat history when the core material is heated and shaped, the mechanical stress (compression, thickness expansion, stretching, etc.) history and the use as an automobile ceiling material , A thickness that provides sufficient adhesive strength, generally 5 to
20 μm is desirable.

【0030】尚、本発明においては、熱可塑性樹脂、耐
熱剛性樹脂および接着性樹脂には、適宜、酸化防止剤や
スリップ剤を必要に応じて混入可能である。
In the present invention, the thermoplastic resin, the heat-resistant and rigid resin and the adhesive resin may be appropriately mixed with an antioxidant or a slip agent, if necessary.

【0031】本発明においては、積層シート構造を製造
する方法はとくに限定されるものでなく、共押出し法、
押出しラミネート法、ドライラミネート法等が挙げられ
る。好ましい方法は共押出し法、すなわち、熱可塑性樹
脂と耐熱剛性樹脂との間に接着性樹脂を介し、同時押出
し、それに、常法であるTダイなどによって積層シート
を製造する方法であり、より経済的である。
In the present invention, the method for producing the laminated sheet structure is not particularly limited, and the coextrusion method,
An extrusion laminating method, a dry laminating method, etc. are mentioned. A preferred method is a co-extrusion method, that is, a method in which an adhesive resin is interposed between a thermoplastic resin and a heat-resistant and rigid resin, co-extrusion, and a laminated sheet is produced by a conventional method such as T-die. Target.

【0032】本発明においては、前記第1〜4の方法に
より得られる積層シートを、耐熱剛性樹脂の溶融温度の
以下の温度で加熱し、この加熱温度に保ったまま、圧縮
する。この圧縮圧力は2〜20Kg/cm、圧縮時間は2〜
10秒の範囲が好ましい。
In the present invention, the laminated sheet obtained by the first to fourth methods is heated at a temperature below the melting temperature of the heat-resistant rigid resin, and compressed while being kept at this heating temperature. The compression pressure is 2 to 20 kg / cm, and the compression time is 2 to
A range of 10 seconds is preferred.

【0033】この圧縮後、積層シート全体(マット状物
およびシート状物)の厚みを拡大する。厚みの拡大は、
無機繊維の弾力で回復させてもよいが、積層シートの外
側のシート状物を常温下で離形しやすくするためテフロ
ンコーティングされた、鋼板あるいはガラスクロスシー
トの両表面を真空吸引して強制的に行なってもよい。耐
熱剛性樹脂層(d) の外側に熱可塑性樹脂層(c) が設けら
れている場合には、外側の熱可塑性樹脂(c) は溶融され
ているので、鋼板あるいはガラスクロスシートとの密着
が良く、安定した厚みを拡大を行なうことができる。
After this compression, the thickness of the entire laminated sheet (mat-like material and sheet-like material) is increased. The increase in thickness is
It may be recovered by the elasticity of the inorganic fibers, but it is forced by vacuum suction on both surfaces of the Teflon coated steel sheet or glass cloth sheet to facilitate the release of the sheet-like material on the outside of the laminated sheet at room temperature. You may go to When the thermoplastic resin layer (c) is provided on the outside of the heat-resistant and rigid resin layer (d), the thermoplastic resin (c) on the outside is melted, so that the adhesion with the steel plate or the glass cloth sheet does not occur. Good and stable thickness can be expanded.

【0034】この加熱圧縮工程において、熱可塑性樹脂
(a) および(b) は溶融しマット状物内に含浸され、同様
に溶融する熱可塑性樹脂繊維とともに、無機繊維および
無機繊維相互を結着させる。一方、耐熱剛性樹脂(d) は
溶融せず、マット状物内に含浸することはない。また、
耐熱剛性樹脂(d) より外側の熱可塑性樹脂(c) は溶融さ
れるが、マット状物内に含浸はされない。
In this heat compression step, the thermoplastic resin
(a) and (b) are melted and impregnated in the mat-like material, and together with the thermoplastic resin fiber which is also melted, the inorganic fibers and the inorganic fibers are bound to each other. On the other hand, the heat-resistant and rigid resin (d) does not melt and does not impregnate into the mat-like material. Also,
The thermoplastic resin (c) outside the heat-resistant and rigid resin (d) is melted, but not impregnated into the mat-like material.

【0035】[0035]

【実施例】以下、実施例により本発明を具体的に説明す
るが、本発明はこれに限定されるものではない。
EXAMPLES The present invention will be specifically described below with reference to examples, but the present invention is not limited thereto.

【0036】[実施例1]長さが40〜75mm、直径9
μmのガラス繊維と、6デニール、50mmカットの高密
度ポリエチレン繊維とを、重量比で2:1の割合で配合
してカードマシンに供給し、解繊及び混繊して綿状物を
得た。次に、この綿状物に20箇所/cm2 の密度でニー
ドルパンチを打って、目付量約500g/m2 のマット
状物を得た。
[Example 1] Length 40 to 75 mm, diameter 9
Glass fiber of μm and high-density polyethylene fiber of 6 denier and 50 mm cut were blended at a weight ratio of 2: 1 and supplied to a card machine to be defibrated and mixed to obtain a cotton-like material. .. Next, the cotton-like material was needle punched at a density of 20 points / cm 2 to obtain a mat-like material having a basis weight of about 500 g / m 2 .

【0037】次に、このマット状物の両面に、高密度ポ
リエチレン樹脂(融点=135℃、MFR=7.0;J
IS K 6870による溶融流量)からなる厚さが約
100μmのシート状物を積層した。更にこの積層物の
片側面に、ポリブチレンテレフタレート樹脂(融点=2
20℃、熱絞り成形率H/D=1.5、曲げ弾性率=2
2000kg/cm2 )と、無水マレイン酸変性ポリエチレ
ン樹脂(MFR=0.91)と、高密度ポリエチレン樹
脂(融点=135℃、MFR=2.0)とを、層厚さ3
0μm/20μm/30μmで共押出ししたシート状物
(H/D=1.5)をポリブチレンテレフタレート樹脂
が外側になるように積層して、厚さ約7mm、重さ約80
0g/m2 の積層シートを作成した。
Next, a high-density polyethylene resin (melting point = 135 ° C., MFR = 7.0; J
Sheet-like materials having a thickness of about 100 μm formed by IS K 6870) were laminated. Furthermore, on one side of this laminate, polybutylene terephthalate resin (melting point = 2
20 ° C., hot drawing rate H / D = 1.5, flexural modulus = 2
2000 kg / cm 2 ), maleic anhydride-modified polyethylene resin (MFR = 0.91) and high-density polyethylene resin (melting point = 135 ° C., MFR = 2.0), layer thickness 3
Sheets (H / D = 1.5) coextruded at 0 μm / 20 μm / 30 μm are laminated so that the polybutylene terephthalate resin is on the outside, and the thickness is about 7 mm and the weight is about 80.
A 0 g / m 2 laminated sheet was prepared.

【0038】この積層シートについて、ポリエチレン樹
脂層とポリブチレンテレフタレート樹脂層間の剥離強度
(接着強度)を測定した結果、360g/15mmであっ
た。
The peel strength (adhesive strength) between the polyethylene resin layer and the polybutylene terephthalate resin layer of this laminated sheet was measured and found to be 360 g / 15 mm.

【0039】作成したこの積層シートを両面から、テフ
ロンコーティングされたガラスクロスシートで挾み、2
00℃の熱風加熱炉に供給し、5分間放置した後、20
0℃に加熱された平板プレスに移して、積層シートの厚
さが0.9mmになるように圧縮し、5秒間保持した。次
に、平板プレスの間隔が約7mmになるように広げ、積層
シートをガラスクロスシートで挾んだまま、平板状の真
空拡開装置に移して、ガラスシートを両側から0.5mm
/秒の速度で吸引して、吸引板の間隔が6mmまで拡開し
て吸引を解除し、取り出して、3分間空冷した。次に、
ガラスクロスシートを剥して、厚さ約5.5mm、重さ約
800g/m2 の平板状の熱成形性芯材を得た。
The laminated sheet thus prepared was sandwiched from both sides with a Teflon-coated glass cloth sheet, and 2
It is supplied to a hot air heating furnace at 00 ° C and left for 5 minutes, then 20
It was transferred to a flat plate press heated to 0 ° C., compressed so that the thickness of the laminated sheet was 0.9 mm, and held for 5 seconds. Next, the flat plate press is spread out so that the interval is about 7 mm, and while the laminated sheet is sandwiched by the glass cloth sheets, it is moved to a flat plate vacuum expansion device, and the glass sheets are moved from both sides by 0.5 mm.
Suction was performed at a speed of / sec, the suction plate interval was expanded to 6 mm, the suction was released, the product was taken out and air-cooled for 3 minutes. next,
The glass cloth sheet was peeled off to obtain a flat thermoformable core material having a thickness of about 5.5 mm and a weight of about 800 g / m 2 .

【0040】得られた熱成形性芯材の表面を拡大鏡で観
察すると、高密度ポリエチレン樹脂シート状物のみ積層
した面には、0.3mm以下の細孔が多数認められたが、
反対側の面には全く細孔は認められなかった。また、得
られた熱成形性芯材の一部を切り取って、断面を観察す
ると、ポリブチレンテレフタレート樹脂層がマット状物
のガラス繊維層に密着配置されているが、その他の樹脂
層は、ガラス繊維層内に溶融含浸され、溶融されたポリ
エチレン繊維と共に、ガラス繊維に結着し、また、ガラ
ス繊維相互の交点部に結着されており、更には、マット
状物の両側から、中心部に向うに従い、溶融含浸された
樹脂が少なくなり、空間部分が多くなっていた。また熱
成形性芯材片を採って、通気性と機械的強度(曲げ弾性
率)を測定した結果、表1に示すように通気が遮断さ
れ、剛性に優れていた。
When the surface of the obtained thermoformable core material was observed with a magnifying glass, a large number of pores of 0.3 mm or less were recognized on the surface on which only the high-density polyethylene resin sheet was laminated.
No pores were observed on the opposite surface. Further, by cutting a part of the obtained thermoformable core material and observing the cross section, the polybutylene terephthalate resin layer is closely adhered to the glass fiber layer of the mat-like material, but the other resin layers are glass. The fiber layer is melt-impregnated, and is bonded to the glass fiber together with the melted polyethylene fiber, and is also bonded to the intersections of the glass fibers. As it turned, the amount of resin melt-impregnated decreased and the space increased. Further, as a result of measuring the air permeability and the mechanical strength (flexural elastic modulus) of the thermoformable core material piece, as shown in Table 1, ventilation was blocked and the rigidity was excellent.

【0041】次に得られた熱成形性芯材の細孔が認めら
れた面(高密度ポリエチレン樹脂シート状物のみ積層し
た面)を上にして、周縁部を固定出来る枠にセットし、
遠赤外線炉に供給し、熱成形性芯材の表面温度が約17
0℃になるように加熱した。次いで、この熱成形性芯材
を枠に固定したまま、最大絞り深さ200mm、最小曲率
半径5mmの賦形面を持つ上下一対の金型(温度40℃)
で1分間加圧して凹形の賦形体を得た。
Next, the thermoformed core material obtained was set in a frame whose peripheral portion can be fixed, with the surface in which pores were observed (the surface on which only the high-density polyethylene resin sheet material was laminated) facing up.
When supplied to a far-infrared furnace, the surface temperature of the thermoformable core material is about 17
Heated to 0 ° C. Then, with the thermoformable core material fixed to the frame, a pair of upper and lower molds (temperature 40 ° C.) having a shaping surface with a maximum drawing depth of 200 mm and a minimum curvature radius of 5 mm.
It was pressurized for 1 minute to obtain a concave shaped body.

【0042】得られた賦形体は、金型の賦形形状とほぼ
同形状で、この賦形体の表面を詳しく観察すると凹面側
には、無数の細孔が認められたが、反対面には細孔が認
められなかった。更に、この賦形体から試料片を取っ
て、物性値を測定した結果表1に示すように通気性遮断
性、機械的強度が優れ、賦形性も良好であった。
The obtained shaped body had almost the same shape as the shape of the mold. When the surface of this shaped body was observed in detail, innumerable pores were recognized on the concave side, but on the opposite side. No pores were found. Further, as a result of measuring a physical property value by taking a sample piece from this shaped body, as shown in Table 1, the air permeability and mechanical strength were excellent, and the shapeability was also good.

【0043】[実施例2]実施例1に於ける、ポリブチ
レンテレフタレート樹脂をポリカーボネート樹脂(溶融
開始温度=210℃、MFR=3.0、H/D=2.
0、曲げ弾性率=20000kg/cm2 )に代えた以外は
実施例1と同様にして、積層シートを作成した。
Example 2 The polybutylene terephthalate resin used in Example 1 was replaced by a polycarbonate resin (melting start temperature = 210 ° C., MFR = 3.0, H / D = 2.
A laminated sheet was prepared in the same manner as in Example 1 except that the flexural modulus was 0, and the flexural modulus was 20000 kg / cm 2 .

【0044】この積層シートについて、ポリエチレン樹
脂層とポリカーボネート樹脂層の剥離強度を測定した結
果、40g/15mmであった。
The peel strength between the polyethylene resin layer and the polycarbonate resin layer of this laminated sheet was measured and found to be 40 g / 15 mm.

【0045】次に作成した積層シートから、実施例1と
同様にして、厚さ約6mm、重さ約800g/m2 の平板
状の熱成形性芯材を得た。
From the laminated sheet thus prepared, a flat thermoformable core material having a thickness of about 6 mm and a weight of about 800 g / m 2 was obtained in the same manner as in Example 1.

【0046】得られた熱成形性芯材の表面を拡大鏡で観
察すると、実施例1の場合と同様に、高密度ポリエチレ
ン樹脂シート状物のみ配した面には、0.3mm程度の細
孔が多数認められ、反対側の面には全く細孔は認められ
なかった。また、得られた熱成形性芯材の一部を切り取
って、断面を観察すると、実施例1の場合と同様に、ポ
リエチレンテレフタレート樹脂層がマット状物のガラス
繊維層に密着配置されているが、その他の樹脂層は、ガ
ラス繊維層内に溶融含浸され、溶融されたポリエチレン
繊維と共に、ガラス繊維に結着し、また、ガラス繊維相
互の交点部に結着されており、更には、マット状物の両
側から、中心部に向うに従い、溶融含浸された樹脂が少
なくなり、空間部分が多くなっていた。また熱成形性芯
材片を採って、通気性と機械的強度(曲げ弾性率)を測
定した結果、表1に示すように通気が遮断され、剛性に
優れていた。
When the surface of the obtained thermoformable core material is observed with a magnifying glass, as in the case of Example 1, the surface on which only the high-density polyethylene resin sheet-like material is arranged has pores of about 0.3 mm. Were observed, and no pores were observed on the opposite surface. Further, when a part of the obtained thermoformable core material was cut out and the cross section was observed, the polyethylene terephthalate resin layer was closely adhered to the glass fiber layer of the mat-like material as in Example 1. , The other resin layers are melt-impregnated into the glass fiber layer, and are bonded to the glass fibers together with the melted polyethylene fibers, and are also bonded to the intersections of the glass fibers, and further, the mat-like shape. From both sides of the product, the amount of resin that had been melt-impregnated decreased and the space increased as it went toward the center. Further, as a result of measuring the air permeability and the mechanical strength (flexural elastic modulus) of the thermoformable core material piece, as shown in Table 1, ventilation was blocked and the rigidity was excellent.

【0047】次いで、実施例1と同様にして賦形体を得
て、実施例1と同様にして観察すると、実施例1とほぼ
同じ状況であった。また、賦形体試料片の通気性、機械
的強度を測定した結果、表1に示すように、実施例1の
結果と同等に良好であった。
Then, a shaped body was obtained in the same manner as in Example 1 and was observed in the same manner as in Example 1. As a result, the situation was almost the same as in Example 1. In addition, as a result of measuring the air permeability and mechanical strength of the shaped sample piece, as shown in Table 1, it was as good as the result of Example 1.

【0048】[実施例3]実施例1で用いたのと同じマ
ット状物の一面に、無水マレイン酸変性高密度ポリエチ
レン樹脂(融点=135℃、MFR=7.0)からなる
厚さが約130μmのシート状物を積層した。一方、マ
ット状物の他の一面に、無水マレイン酸変性高密度ポリ
エチレン樹脂(融点=135℃、MFR=5.0)と、
接着性ポリエチレン樹脂(融点=105℃、MFR=
4.0)と、ポリブチレンテレフタレート樹脂(融点=
220℃、熱絞り成形率H/D=1.5、曲げ弾性率=
22000kg/cm2 )と、接着性ポリエチレン樹脂(融
点=105℃、MFR=4.0)と、無水マレイン酸変
性高密度ポリエチレン樹脂(融点=135℃、MFR=
5.0)とを、層厚さ90μm/10μm/20μm/
10μm/10μmで共押出ししたシート状物(H/D
=1.5)を、厚さ10μmのポリエチレン樹脂が外側
になるように積層して、厚さ約7mm重さ約800g/m
2 の積層シートを作成した。
[Example 3] On one surface of the same mat-like material as used in Example 1, a thickness of a maleic anhydride-modified high-density polyethylene resin (melting point = 135 ° C, MFR = 7.0) was about 10. Sheets having a thickness of 130 μm were laminated. On the other hand, on the other side of the mat-like material, maleic anhydride-modified high-density polyethylene resin (melting point = 135 ° C., MFR = 5.0),
Adhesive polyethylene resin (melting point = 105 ° C, MFR =
4.0) and polybutylene terephthalate resin (melting point =
220 ° C., hot drawing rate H / D = 1.5, flexural modulus =
22000 kg / cm 2 ), adhesive polyethylene resin (melting point = 105 ° C., MFR = 4.0), maleic anhydride modified high density polyethylene resin (melting point = 135 ° C., MFR =
5.0) and the layer thickness 90 μm / 10 μm / 20 μm /
Sheets (H / D) coextruded at 10 μm / 10 μm
= 1.5) is laminated so that the polyethylene resin with a thickness of 10 μm is on the outside, and the thickness is about 7 mm and the weight is about 800 g / m.
A laminated sheet of 2 was created.

【0049】この積層シートについて、ポリエチレン樹
脂層(厚さ90μm)とポリブチレンテレフタレート樹
脂層間の剥離強度(接着強度)を測定した結果、360
g/15mmであった。
With respect to this laminated sheet, the peel strength (adhesive strength) between the polyethylene resin layer (thickness 90 μm) and the polybutylene terephthalate resin layer was measured, and the result was 360.
It was g / 15 mm.

【0050】作成したこの積層シートから、実施例1と
同様にして、厚さ約5.5mm、重さ約800g/m2
平板状の熱成形性芯材を得た。
From the laminated sheet thus prepared, a flat thermoformable core material having a thickness of about 5.5 mm and a weight of about 800 g / m 2 was obtained in the same manner as in Example 1.

【0051】得られた熱成形性芯材の表面を拡大鏡で観
察すると、高密度ポリエチレン樹脂シート状物のみ積層
した面には、0.3mm以下の細孔が多数認められたが、
反対側の面には全く細孔は認められなかった。また、得
られた熱成形性芯材の一部を切り取って、断面を観察す
ると、ポリブチレンテレフタレート樹脂層がマット状物
のガラス繊維層に密着配置され、これより内側の樹脂層
(90μm/10μm)は、ガラス繊維層内に溶融含浸
され、溶融されたポリエチレン繊維と共に、ガラス繊維
に結着し、また、ガラス繊維相互の交点部に結着されて
おり、更には、マット状物の両側から、中心部に向うに
従い、溶融含浸された樹脂が少なくなり、空間部分が多
くなっていた。また熱成形性芯材片を採って、通気性と
機械的強度(曲げ弾性率)を測定した結果、表1に示す
ように通気が遮断され、剛性に優れていた。
When the surface of the obtained thermoformable core material was observed with a magnifying glass, a large number of pores of 0.3 mm or less were recognized on the surface on which only the high-density polyethylene resin sheet was laminated.
No pores were observed on the opposite surface. Further, when a part of the obtained thermoformable core material is cut out and the cross section is observed, the polybutylene terephthalate resin layer is closely adhered to the glass fiber layer of the mat-like material, and the resin layer inside (90 μm / 10 μm) ) Is melt-impregnated into the glass fiber layer, and is bonded to the glass fiber together with the melted polyethylene fiber, and is also bonded to the intersections of the glass fibers. As it went to the center, the amount of the resin melt-impregnated decreased and the space increased. Further, as a result of measuring the air permeability and the mechanical strength (flexural elastic modulus) of the thermoformable core material piece, as shown in Table 1, ventilation was blocked and the rigidity was excellent.

【0052】次に、実施例1と同様にして、凹形の賦形
体を得て、実施例1と同様にして観察すると、実施例1
とほぼ同じ状況であった。また、賦形体試料片の通気
性、機械的強度を測定した結果、表1に示すように、実
施例1の結果と同等に良好であった。
Then, a concave shaped body was obtained in the same manner as in Example 1 and observed in the same manner as in Example 1.
It was almost the same situation as. In addition, as a result of measuring the air permeability and mechanical strength of the shaped sample piece, as shown in Table 1, it was as good as the result of Example 1.

【0053】[比較例]実施例で用いたのと同じマット
状物の両面に、実施例3で用いたのと同じ無水マレイン
酸変性高密度ポリエチレン樹脂(融点=135℃、MF
R=7.0)からなる厚さが約130μmのシート状物
を積層して、厚さ約7mm、重さ約800g/m2 の積層
シートを作成した。
Comparative Example The same maleic anhydride-modified high-density polyethylene resin as used in Example 3 (melting point = 135 ° C., MF, MF)
R = 7.0) sheets having a thickness of about 130 μm were laminated to prepare a laminated sheet having a thickness of about 7 mm and a weight of about 800 g / m 2 .

【0054】作成したこの積層シートから、実施例と同
様にして、厚さ約5.9mm、重さ約800g/m2 の平
板状の熱成形性芯材を得た。
From the laminated sheet thus prepared, a flat thermoformable core material having a thickness of about 5.9 mm and a weight of about 800 g / m 2 was obtained in the same manner as in the example.

【0055】得られた熱成形性芯材の表面を実施例と同
様に観察すると、芯材の両表面共に、直径0.3mm程度
の細孔が多数認められた。また、熱成形性芯材片を採っ
て、通気性と機械的強度(曲げ弾性率)を測定した結
果、表1に示すように通気性が認められた。
When the surface of the obtained thermoformable core material was observed in the same manner as in the examples, a large number of pores having a diameter of about 0.3 mm were recognized on both surfaces of the core material. Further, as a result of measuring the air permeability and the mechanical strength (flexural modulus) of the thermoformable core material piece, the air permeability was confirmed as shown in Table 1.

【0056】次に、実施例と同様にして、凹形の賦形体
を得た。得られた賦形体は、金型の賦形形状とほぼ同形
状で、この賦形体の表面を詳しく観察すると、賦形体の
両表面共に、直径0.5mm程度の無数の細孔が認められ
た。また、賦形体試料片の物性値を測定した結果、表1
に示すように、通気性が認められ、機械的強度および剛
性は実施例より劣っていた。
Then, a concave shaped body was obtained in the same manner as in the example. The obtained shaped body had almost the same shape as the shape of the mold, and when the surface of this shaped body was observed in detail, innumerable pores with a diameter of about 0.5 mm were recognized on both surfaces of the shaped body. .. In addition, as a result of measuring the physical property values of the shaped sample pieces, Table 1
As shown in FIG. 5, breathability was recognized, and mechanical strength and rigidity were inferior to those of the examples.

【0057】[0057]

【表1】 [Table 1]

【0058】[0058]

【発明の効果】本発明によると、無機繊維と熱可塑性樹
脂繊維を主材料とし、無機繊維が熱可塑性樹脂により結
着せられているマット状物の少なくとも片面に、強靭な
耐熱剛性樹脂層を積層配置するので、上述したように通
気遮断性および機械的強度に優れる熱成形性芯材が得ら
れる。さらに本発明によると、熱成形絞り率の大きな耐
熱剛性樹脂と接着強度が大きい接着樹脂層を配置するの
で、加熱賦形に好適な性能を有する熱成形性芯材が得ら
れる。また、本発明の製造方法によると、上述の効果を
有する熱成形性芯材を作業性よく製造することができ
る。
EFFECTS OF THE INVENTION According to the present invention, a tough heat-resistant and rigid resin layer is laminated on at least one surface of a mat-like material having inorganic fibers and thermoplastic resin fibers as main materials and inorganic fibers bound by a thermoplastic resin. Since they are arranged, as described above, the thermoformable core material which is excellent in ventilation blocking property and mechanical strength is obtained. Further, according to the present invention, since the heat-resistant and rigid resin having a large thermoforming reduction ratio and the adhesive resin layer having a large adhesive strength are arranged, a thermoformable core material having a performance suitable for heat shaping can be obtained. Further, according to the manufacturing method of the present invention, the thermoformable core material having the above-described effects can be manufactured with good workability.

───────────────────────────────────────────────────── 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 D01F 9/08 7199−3B D04H 1/54 J 7199−3B // B29L 9:00 4F ─────────────────────────────────────────────────── ─── Continuation of the front page (51) Int.Cl. 5 Identification number Office reference number FI technical display location D01F 9/08 7199-3B D04H 1/54 J 7199-3B // B29L 9:00 4F

Claims (11)

【特許請求の範囲】[Claims] 【請求項1】 無機繊維が熱可塑性樹脂により結着せら
れているマット状物の少なくとも片面に、前記熱可塑性
樹脂より溶融温度の高い耐熱剛性樹脂(d) からなるシー
ト状物が積層され、無機繊維が厚み方向に拡開されてい
ることを特徴とする熱成形性芯材。
1. A sheet-shaped material made of a heat-resistant and rigid resin (d) having a melting temperature higher than that of the thermoplastic resin is laminated on at least one surface of a mat-shaped material in which inorganic fibers are bound by a thermoplastic resin. A thermoformable core material in which fibers are expanded in the thickness direction.
【請求項2】 マット状物が、熱可塑性樹脂繊維および
/または熱可塑性樹脂シート状物が溶融含浸されたもの
であることを特徴とする、請求項1に記載の熱成形性芯
材。
2. The thermoformable core material according to claim 1, wherein the mat-like material is obtained by melt-impregnating a thermoplastic resin fiber and / or a thermoplastic resin sheet-like material.
【請求項3】 シート状物が耐熱剛性樹脂層(d) と熱可
塑性樹脂層(c) からなり、熱可塑性樹脂層(c) が外側に
なるように積層されていることを特徴とする、請求項1
または2に記載の熱成形性芯材。
3. A sheet-like material comprising a heat-resistant and rigid resin layer (d) and a thermoplastic resin layer (c), which are laminated so that the thermoplastic resin layer (c) is on the outside. Claim 1
Alternatively, the thermoformable core material described in 2.
【請求項4】 耐熱剛性樹脂(d) が、耐熱剛性樹脂の熱
絞り成形率(H/D;H=高さ、D=直径)0.5以上
で、かつ、曲げ弾性率15000kg/cm2 以上のもので
ある、請求項1〜3のいずれか1項に記載の熱成形性芯
材。
4. The heat-resisting and rigid resin (d) has a heat-drawing ratio (H / D; H = height, D = diameter) of the heat-resisting and rigid resin of 0.5 or more, and a bending elastic modulus of 15000 kg / cm 2. The thermoformable core material according to any one of claims 1 to 3, which is as described above.
【請求項5】 マット状物とシート状物との間の剥離強
度が、100g/15mm幅以上であることを特徴とす
る、請求項1〜4のいずれか1項に記載の熱成形性芯
材。
5. The thermoformable core according to claim 1, wherein the peel strength between the mat-like material and the sheet-like material is 100 g / 15 mm width or more. Material.
【請求項6】 無機繊維と熱可塑性樹脂繊維を主材料と
して形成されたマット状物の両面に、熱可塑性樹脂シー
ト状物(a) (b) を積層し、得られたサンドイッチ積層物
の少なくとも片面に、前記熱可塑性樹脂繊維および前記
熱可塑性樹脂より溶融温度の高い、耐熱剛性樹脂(d) か
らなるシート状物を積層した積層シートを、前記耐熱剛
性樹脂の溶融温度以下の温度で加熱して、前記熱可塑性
樹脂繊維と前記熱可塑性樹脂を、各々、溶融させると共
に圧縮して、前記熱可塑性樹脂(a) (b) を前記マット状
物内に含浸させて前記無機繊維相互を結着させ、一方、
前記耐熱剛性樹脂(d) は前記マット状物内に含浸させな
いことを特徴とする熱成形性芯材の製造方法。
6. A thermoplastic resin sheet material (a) (b) is laminated on both sides of a mat-like material formed mainly of inorganic fibers and thermoplastic resin fibers, and at least a sandwich laminate obtained is obtained. A laminated sheet, on one side of which the thermoplastic resin fibers and a sheet-like material having a higher melting temperature than the thermoplastic resin and made of the heat-resistant and rigid resin (d) are laminated, is heated at a temperature not higher than the melting temperature of the heat-resistant and rigid resin. Then, the thermoplastic resin fiber and the thermoplastic resin are melted and compressed, respectively, and the thermoplastic resin (a) and (b) are impregnated in the mat-like material to bind the inorganic fibers to each other. Let me meanwhile,
The method for producing a thermoformable core material, wherein the heat-resistant and rigid resin (d) is not impregnated in the mat-like material.
【請求項7】 無機繊維と熱可塑性樹脂繊維を主材料と
して形成されたマット状物の両面に、熱可塑性樹脂シー
ト状物(a) (b) を積層し、得られたサンドイッチ積層物
の少なくとも片面に、前記熱可塑性樹脂繊維および前記
熱可塑性樹脂より溶融温度の高い、耐熱剛性樹脂層(d)
と熱可塑性樹脂層(c) からなる多層シート状物を層(c)
が外側になるように積層した積層シートを、前記耐熱剛
性樹脂の溶融温度以下の温度で加熱して、前記熱可塑性
樹脂繊維と前記熱可塑性樹脂を、各々、溶融させると共
に圧縮して、前記熱可塑性樹脂(a) (b) を前記マット状
物内に含浸させて前記無機繊維および無機繊維相互を結
着させ、一方、前記耐熱剛性樹脂(d) と前記マット状物
に接しない熱可塑性樹脂(c) は前記マット状物内に含浸
させないことを特徴とする熱成形性芯材の製造方法。
7. A thermoplastic resin sheet material (a) (b) is laminated on both surfaces of a mat-like material formed mainly of inorganic fibers and thermoplastic resin fibers, and at least a sandwich laminate obtained is obtained. On one side, the thermoplastic resin fiber and the melting temperature higher than the thermoplastic resin, heat-resistant rigid resin layer (d)
And a thermoplastic resin layer (c)
The laminated sheet laminated so that is on the outside is heated at a temperature equal to or lower than the melting temperature of the heat-resistant and rigid resin to melt and compress the thermoplastic resin fiber and the thermoplastic resin, respectively. A thermoplastic resin (a) (b) is impregnated into the mat-like material to bind the inorganic fibers and the inorganic fibers together, while the heat-resistant and rigid resin (d) is not in contact with the mat-like material. (c) is a method for producing a thermoformable core material, wherein the mat-like material is not impregnated.
【請求項8】 積層シートが、マット状物の一面に熱可
塑性樹脂シート状物(a) を積層し、前記マット状物の他
の一面には、前記熱可塑性樹脂繊維および前記熱可塑性
樹脂より溶融温度の高い、耐熱剛性樹脂層(d) とこれを
サンドイッチする熱可塑性樹脂層(b) (c) からなる多層
シート状物を層(c) が外側になるように積層したもので
あることを特徴とする、請求項7に記載の熱成形性芯材
の製造方法。
8. A laminated sheet, wherein a thermoplastic resin sheet material (a) is laminated on one surface of a mat-like material, and the thermoplastic resin fiber and the thermoplastic resin are laminated on the other surface of the mat-like material. It should be a laminate of multi-layered sheets consisting of a heat-resistant and rigid resin layer (d) with a high melting temperature and a thermoplastic resin layer (b) (c) sandwiching it, with the layer (c) facing outward. The method for producing a thermoformable core material according to claim 7, wherein
【請求項9】 積層シートが、マット状物の両面に、耐
熱剛性樹脂層(d) とこれをサンドイッチする熱可塑性樹
脂層(b) (c) からなる多層シート状物を層(c) が外側に
なるように積層したものであり、前記耐熱剛性樹脂の溶
融温度は前記熱可塑性樹脂繊維および前記熱可塑性樹脂
よりも高いことを特徴とする、請求項7に記載の熱成形
性芯材の製造方法。
9. A laminated sheet, wherein a layer (c) is provided on both sides of a mat-like material with a multilayer sheet-like material comprising a heat-resistant and rigid resin layer (d) and a thermoplastic resin layer (b) (c) sandwiching it. The thermoformable core material according to claim 7, wherein the heat-resistant rigid resin has a melting temperature higher than that of the thermoplastic resin fiber and the thermoplastic resin. Production method.
【請求項10】 耐熱剛性樹脂層(d) の少なくとも片面
に接着性樹脂層が設けられていることを特徴とする、請
求項6〜9のいずれか1項に記載の熱成形性芯材の製造
方法。
10. The thermoformable core material according to any one of claims 6 to 9, wherein an adhesive resin layer is provided on at least one surface of the heat-resistant and rigid resin layer (d). Production method.
【請求項11】 耐熱剛性樹脂(d) が耐熱剛性樹脂の熱
絞り成形率(H/D;H=高さ、D=直径)0.5以上
で、かつ、曲げ弾性率15000kg/cm2 以上のもので
ある、請求項6〜10のいずれか1項に記載の熱成形性
芯材の製造方法。
11. The heat-resisting and rigidifying resin (d) has a heat-drawing ratio (H / D; H = height, D = diameter) of the heat-resisting and rigidifying resin of 0.5 or more, and a bending elastic modulus of 15000 kg / cm 2 or more. The method for producing a thermoformable core material according to any one of claims 6 to 10, wherein
JP04000870A 1991-08-07 1992-01-07 Thermoformable core material and method for producing the same Expired - Lifetime JP3095503B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP04000870A JP3095503B2 (en) 1991-08-07 1992-01-07 Thermoformable core material and method for producing the same

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
JP3-197768 1991-08-07
JP19776891 1991-08-07
JP04000870A JP3095503B2 (en) 1991-08-07 1992-01-07 Thermoformable core material and method for producing the same

Publications (2)

Publication Number Publication Date
JPH0593352A true JPH0593352A (en) 1993-04-16
JP3095503B2 JP3095503B2 (en) 2000-10-03

Family

ID=26333977

Family Applications (1)

Application Number Title Priority Date Filing Date
JP04000870A Expired - Lifetime JP3095503B2 (en) 1991-08-07 1992-01-07 Thermoformable core material and method for producing the same

Country Status (1)

Country Link
JP (1) JP3095503B2 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH06226740A (en) * 1993-02-03 1994-08-16 Sekisui Chem Co Ltd Production of fiber composite
JP2021116513A (en) * 2020-01-29 2021-08-10 セイコーエプソン株式会社 Fiber structure manufacturing equipment, fiber structure manufacturing method, and fiber structure

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH06226740A (en) * 1993-02-03 1994-08-16 Sekisui Chem Co Ltd Production of fiber composite
JP2021116513A (en) * 2020-01-29 2021-08-10 セイコーエプソン株式会社 Fiber structure manufacturing equipment, fiber structure manufacturing method, and fiber structure

Also Published As

Publication number Publication date
JP3095503B2 (en) 2000-10-03

Similar Documents

Publication Publication Date Title
US4923547A (en) Process for producing composite molded articles from nonwoven mat
JP4154638B2 (en) Manufacturing method for interior materials
JP2004122545A (en) Thermoformable core material and automotive interior material using the same
JPH01207458A (en) Fiber molded article for heat molding and production thereof
JP3654821B2 (en) Thermoformable core material and manufacturing method thereof
JP3095503B2 (en) Thermoformable core material and method for producing the same
JP2582858B2 (en) Method for producing fiber molded article for thermoforming
JP2831673B2 (en) Method for producing fiber molded body
JP2872896B2 (en) Thermoformable core material, production method thereof and interior material
JPH01166946A (en) Manufacture of fibrous molding for thermoforming
JPH07102650B2 (en) Lightweight composite material manufacturing method
JP3853077B2 (en) Dispersion method stampable sheet expansion molded body and dispersion method stampable sheet
JPH06320559A (en) Production of interior part for car
JPH01165431A (en) Manufacture of fiber molding to be thermally molded
JP3050979B2 (en) Fiber composite material and method for producing the same
JP2536908B2 (en) Method for producing thermoformable composite material
JPH05222654A (en) Production of core material having thermoformability
JPH09123327A (en) Thermoformable composite material
JP2776615B2 (en) Method for producing porous composite material
JPH08188948A (en) Thermoformable core material
JPH08112816A (en) Thermoformable core material, manufacturing method thereof and interior material
JP2000167964A (en) Interior base material
JPH03161575A (en) Production of light weight composite material
JPH05311556A (en) Method for producing fiber composite
JPH0814065B2 (en) Method for producing fiber molding for thermoforming

Legal Events

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

Free format text: PAYMENT UNTIL: 20070804

Year of fee payment: 7

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

Free format text: PAYMENT UNTIL: 20080804

Year of fee payment: 8

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

Free format text: PAYMENT UNTIL: 20090804

Year of fee payment: 9

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

Free format text: PAYMENT UNTIL: 20090804

Year of fee payment: 9

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

Free format text: PAYMENT UNTIL: 20100804

Year of fee payment: 10

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

Free format text: PAYMENT UNTIL: 20110804

Year of fee payment: 11

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

Free format text: PAYMENT UNTIL: 20110804

Year of fee payment: 11

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

Free format text: PAYMENT UNTIL: 20120804

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: 20120804

Year of fee payment: 12