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JP3278269B2 - Plate-shaped laminated thermoplastic resin molding - Google Patents
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JP3278269B2 - Plate-shaped laminated thermoplastic resin molding - Google Patents

Plate-shaped laminated thermoplastic resin molding

Info

Publication number
JP3278269B2
JP3278269B2 JP30013093A JP30013093A JP3278269B2 JP 3278269 B2 JP3278269 B2 JP 3278269B2 JP 30013093 A JP30013093 A JP 30013093A JP 30013093 A JP30013093 A JP 30013093A JP 3278269 B2 JP3278269 B2 JP 3278269B2
Authority
JP
Japan
Prior art keywords
thermoplastic resin
plate
cross
flexural modulus
shaped laminated
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 - Fee Related
Application number
JP30013093A
Other languages
Japanese (ja)
Other versions
JPH07148875A (en
Inventor
靖夫 中村
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.)
Idemitsu Petrochemical Co Ltd
Original Assignee
Idemitsu Petrochemical 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 Idemitsu Petrochemical Co Ltd filed Critical Idemitsu Petrochemical Co Ltd
Priority to JP30013093A priority Critical patent/JP3278269B2/en
Publication of JPH07148875A publication Critical patent/JPH07148875A/en
Application granted granted Critical
Publication of JP3278269B2 publication Critical patent/JP3278269B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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  • Laminated Bodies (AREA)
  • Injection Moulding Of Plastics Or The Like (AREA)

Description

【発明の詳細な説明】DETAILED DESCRIPTION OF THE INVENTION

【0001】[0001]

【産業上の利用分野】本発明はソリの少ない板状積層熱
可塑性樹脂成形体に関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a plate-shaped laminated thermoplastic resin molded article having a small warp.

【0002】[0002]

【従来の技術】熱可塑性樹脂は、広範囲な分野において
各種成形体に加工されて使用されている。板状の熱可塑
性成形体は射出成形で製造されるのが一般的であり、例
えば、表面と裏面とが異なる材料特性を有する板状の熱
可塑性樹脂成形体は、最初に片面側に位置する熱可塑性
樹脂を成形した後、他方側の熱可塑性樹脂を成形すると
いう方法で製造されている。
2. Description of the Related Art Thermoplastic resins are used after being processed into various molded articles in a wide range of fields. Plate-shaped thermoplastic molded products are generally manufactured by injection molding.For example, a plate-shaped thermoplastic resin molded product having different material properties from the front surface and the back surface is located on one side first. It is manufactured by molding a thermoplastic resin and then molding the thermoplastic resin on the other side.

【0003】[0003]

【発明が解決しようとする課題】しかし、この方法で
は、先に成形した片側の熱可塑性樹脂は先に成形固化し
ているので既にある程度収縮しており、後に成形するも
う片側の熱可塑性樹脂は先に成形した熱可塑性樹脂があ
る程度収縮した後に成形されるために、これら両者の収
縮率には大きな差異が生じる。したがって、熱可塑性樹
脂成形体の形状が板状体である場合には、成形体は一定
時間が経過すると大きなそりを生じ、経時的な寸法精度
が極めて悪くなるという大きな欠点を有していた。そこ
で、板状積層熱可塑性樹脂成形体のそりを防止し、寸法
精度のよい成形体を得ることが大きな課題であった。
However, according to this method, the thermoplastic resin on one side molded earlier has already shrunk to some extent because it has been molded and solidified first, and the thermoplastic resin on the other side molded later has the same properties. Since the previously molded thermoplastic resin is molded after shrinking to some extent, there is a large difference in the shrinkage ratio between the two. Therefore, when the shape of the thermoplastic resin molded article is a plate-like body, the molded article has a great disadvantage that a large amount of warpage occurs after a certain period of time, and the dimensional accuracy over time becomes extremely poor. Therefore, it has been a major problem to prevent warpage of the plate-shaped laminated thermoplastic resin molded article and to obtain a molded article having good dimensional accuracy.

【0004】[0004]

【課題を解決するための手段】本発明者は上記した課題
に鑑み鋭意研究した結果、板状積層熱可塑性樹脂成形体
を構成する熱可塑性樹脂として曲げ弾性率の異なるもの
を使用し、且つ板厚方向に平行な平面で切断した断面で
の各樹脂の占める断面積等を特定の範囲の値とすること
によって、上記問題を解決できることを見いだし本発明
を提案するに至った。
Means for Solving the Problems The present inventor has conducted intensive studies in view of the above-mentioned problems, and as a result, using a thermoplastic resin having a different flexural modulus as a thermoplastic resin constituting a plate-like laminated thermoplastic resin molded article, The inventors have found that the above problem can be solved by setting the cross-sectional area occupied by each resin in a cross section cut along a plane parallel to the thickness direction to a value in a specific range, and have led to the present invention.

【0005】即ち、本発明は、曲げ弾性率が異なり、且
つその曲げ弾性率比が0.5以下である2種の熱可塑性
樹脂が積層された板状成形体であって、その板厚方向に
平行な平面で切断した少なくとも一つの断面における2
種の熱可塑性樹脂の境界は凹凸を形成しており、且つ該
断面において下記(1)及び(2)式を同時に満足する
ことを特徴とする板状積層熱可塑性樹脂成形体である。
That is, the present invention relates to a plate-like molded product in which two kinds of thermoplastic resins having different flexural modulus and a flexural modulus ratio of 0.5 or less are laminated, 2 in at least one section cut in a plane parallel to
The boundary between the kinds of thermoplastic resins has unevenness, and the cross section satisfies the following expressions (1) and (2) at the same time.

【0006】 0.2<B/A≦1.6 ・・・ (1) 0.5≦(C×I)/(A×I′)<1 ・・・ (2) (ただし、上記式中、 A :曲げ弾性率の高い熱可塑性樹脂の占める断面積。0.2 <B / A ≦ 1.6 (1) 0.5 ≦ (C × I) / (A × I ′) <1 (2) (where, A: Cross-sectional area occupied by a thermoplastic resin having a high flexural modulus.

【0007】B :曲げ弾性率の低い熱可塑性樹脂の占
める断面積。
B: Cross-sectional area occupied by a thermoplastic resin having a low flexural modulus.

【0008】C :板状積層熱可塑性樹脂成形体の全断
面積。
C: Total cross-sectional area of the plate-shaped laminated thermoplastic resin molded article.

【0009】I :曲げ弾性率の高い熱可塑性樹脂の図
心を通り、且つ板厚方向に垂直で断面内に存在する軸に
関する曲げ弾性率の高い熱可塑性樹脂の断面二次モーメ
ント。
I: Secondary moment of area of the thermoplastic resin having a high flexural modulus with respect to an axis passing through the center of the thermoplastic resin having a high flexural modulus and perpendicular to the thickness direction and existing in the cross section.

【0010】I′:板状積層熱可塑性樹脂成形体の図心
を通り、且つ板厚方向に垂直で断面内に存在する軸に関
する板状積層熱可塑性樹脂成形体の断面二次モーメン
ト。)本発明の板状積層熱可塑性樹脂成形体を構成する
熱可塑性樹脂は、曲げ弾性率の異なるものであって、且
つこれら熱可塑性樹脂の曲げ弾性率の比が0.5以下の
ものである。つまり、板状積層熱可塑性樹脂成形体の一
方の面は曲げ弾性率の高い熱可塑性樹脂(以下、高剛性
熱可塑性樹脂ともいう。)であり、もう一方の面は曲げ
弾性率の低い熱可塑性樹脂(以下、低剛性熱可塑性樹脂
ともいう。)である。そして、低剛性熱可塑性樹脂と高
剛性熱可塑性樹脂のそれぞれの曲げ弾性率の比(低剛性
熱可塑性樹脂/高剛性熱可塑性樹脂)は0.5以下でな
ければならず、0.3以下であることが好ましい。曲げ
弾性率の比が0.5を越える場合には、高剛性熱可塑性
樹脂と低剛性熱可塑性樹脂の収縮の差による残留応力を
低剛性熱可塑性樹脂で緩和することができず、成形体の
ソリを防止することができない。
I ': Second moment of area of the plate-shaped laminated thermoplastic resin molded product with respect to an axis passing through the center of the plate-shaped laminated thermoplastic resin molded product and perpendicular to the plate thickness direction and existing in the cross section. The thermoplastic resin constituting the plate-shaped laminated thermoplastic resin molded article of the present invention has a different flexural modulus, and the ratio of the flexural modulus of these thermoplastic resins is 0.5 or less. . That is, one surface of the plate-shaped laminated thermoplastic resin molded article is a thermoplastic resin having a high flexural modulus (hereinafter, also referred to as a high rigidity thermoplastic resin), and the other surface is a thermoplastic resin having a low flexural modulus. Resin (hereinafter, also referred to as a low-rigidity thermoplastic resin). And, the ratio of the respective bending elastic moduli of the low-rigidity thermoplastic resin and the high-rigidity thermoplastic resin (low-rigidity thermoplastic resin / high-rigidity thermoplastic resin) must be 0.5 or less, and 0.3 or less. Preferably, there is. If the flexural modulus ratio exceeds 0.5, the residual stress due to the difference in shrinkage between the high-rigidity thermoplastic resin and the low-rigidity thermoplastic resin cannot be reduced by the low-rigidity thermoplastic resin, and We cannot prevent warpage.

【0011】本発明においては、積層する熱可塑性樹脂
は、両者の接着性を良好にするために、例えば、ポリオ
レフィン同士、ポリアミド同士のように同種の樹脂であ
ることが好ましい。また、高剛性熱可塑性樹脂として
は、曲げ弾性率が10,000〜100,000kg/
cm2の範囲のものを使用した場合に特に成形体のソリ
が大きくなる傾向があるために、そのような熱可塑性樹
脂を使用したときに本発明の効果が顕著となる。また、
上記した高剛性熱可塑性樹脂を使用したときは、ソリを
緩和する低剛性熱可塑性樹脂としては、曲げ弾性率40
0〜15,000kg/cm2の範囲のものを使用する
ことが好ましい。
In the present invention, the thermoplastic resins to be laminated are preferably of the same type, for example, polyolefins and polyamides, in order to improve the adhesion between the two. Further, as a high rigidity thermoplastic resin, the flexural modulus is 10,000 to 100,000 kg /.
Since the warpage of the molded article tends to be particularly large when a resin having a size in the range of cm 2 is used, the effect of the present invention becomes remarkable when such a thermoplastic resin is used. Also,
When the above-mentioned high-rigidity thermoplastic resin is used, the low-rigidity thermoplastic resin for reducing warpage may have a flexural modulus of 40.
It is preferable to use one in the range of 0 to 15,000 kg / cm 2 .

【0012】本発明に用いられる熱可塑性樹脂としては
特に制限されず、公知の熱可塑性樹脂を使用することが
できる。例えば、ポリエチレン、ポリプロピレン、ポリ
ブテンなどのポリオレフィン;ポリスチレン、AS樹脂
(アクリロニトリル−スチレン共重合体)、ABS樹脂
(アクリロニトリル−ブタジエン−スチレン共重合体)
などのスチレン系ポリマー;ナイロン6、ナイロン66
などのポリアミド;ポリ塩化ビニル、ポリ塩化ビニリデ
ンなどの含ハロゲンポリマー等を挙げることができる。
これらの熱可塑性樹脂はそれぞれ単独で、または混合し
て使用することができる。本発明においては、特にポリ
アミドやポリオレフィン等の結晶性樹脂が好適であり、
特にポリプロピレンを用いた場合にはソリの低減効果が
大きいために好適である。
[0012] The thermoplastic resin used in the present invention is not particularly limited, and a known thermoplastic resin can be used. For example, polyolefins such as polyethylene, polypropylene and polybutene; polystyrene, AS resin (acrylonitrile-styrene copolymer), ABS resin (acrylonitrile-butadiene-styrene copolymer)
Styrene polymers such as nylon; nylon 6, nylon 66
Polyamide; and halogen-containing polymers such as polyvinyl chloride and polyvinylidene chloride.
These thermoplastic resins can be used alone or in combination. In the present invention, a crystalline resin such as polyamide or polyolefin is particularly suitable,
In particular, when polypropylene is used, it is preferable because the effect of reducing warpage is large.

【0013】本発明の板状積層熱可塑性樹脂成形体は、
その板厚方向に平行な平面で切断した少なくとも一つの
断面において、上記した高剛性熱可塑性樹脂と低剛性熱
可塑性樹脂との境界が凹凸を形成している。本発明の板
状積層熱可塑性樹脂成形体の板厚方向に平行な平面で切
断した断面は、その平面の数に応じた数の断面が存在す
る。本発明においてはその断面のうち少なくとも1つの
断面について後述する要件を満足していれば、その他の
断面についてはその要件を必ずしも満足することを要し
ない。
The plate-shaped laminated thermoplastic resin molded article of the present invention comprises:
In at least one section cut along a plane parallel to the plate thickness direction, the boundary between the above-described high-rigidity thermoplastic resin and the low-rigidity thermoplastic resin has irregularities. The cross section of the plate-shaped laminated thermoplastic resin molded article of the present invention cut along a plane parallel to the plate thickness direction has a number of cross sections corresponding to the number of the planes. In the present invention, as long as at least one of the cross sections satisfies the requirements described later, the other cross sections do not necessarily have to satisfy the requirements.

【0014】上記の断面における境界の凹凸の形状は特
に制限されず、直線を組み合わせた形状、曲線を組み合
わせた形状のいずれでもよく、また、左右対象、非対象
のいずれであってもよい。具体的には、図13〜図17
に示すような櫛型、波型、およびこれらの組み合わせ等
の凹凸形状を挙げることができる。断面における境界が
凹凸ではなく図10に示すように一直線の場合は、高剛
性熱可塑性樹脂と低剛性熱可塑性樹脂の収縮の差による
残留応力を低剛性熱可塑性樹脂で緩和することができ
ず、成形体のソリを防止することができない。
The shape of the unevenness of the boundary in the above-mentioned cross section is not particularly limited, and may be any of a shape combining straight lines, a shape combining curves, and may be symmetrical or unsymmetrical. Specifically, FIGS.
And irregular shapes such as a comb shape, a wavy shape, and a combination thereof. When the boundary in the cross section is not uneven but straight as shown in FIG. 10, the residual stress due to the difference in contraction between the high-rigidity thermoplastic resin and the low-rigidity thermoplastic resin cannot be reduced by the low-rigidity thermoplastic resin, It is not possible to prevent warping of the molded body.

【0015】さらに、本発明においては、該断面におい
て下記(1)及び(2)式を同時に満足することを必要
とする。
Further, in the present invention, it is necessary to satisfy the following expressions (1) and (2) at the same time in the cross section.

【0016】 0.2<B/A≦1.6 ・・・ (1) 0.5≦(C×I)/(A×I′)<1 ・・・ (2) (ただし、上記式中、 A :曲げ弾性率の高い熱可塑性樹脂の占める断面積。0.2 <B / A ≦ 1.6 (1) 0.5 ≦ (C × I) / (A × I ′) <1 (2) A: Cross-sectional area occupied by a thermoplastic resin having a high flexural modulus.

【0017】B :曲げ弾性率の低い熱可塑性樹脂の占
める断面積。
B: Cross-sectional area occupied by a thermoplastic resin having a low flexural modulus.

【0018】C :板状積層熱可塑性樹脂成形体の全断
面積。
C: Total cross-sectional area of the plate-shaped laminated thermoplastic resin molded article.

【0019】I :曲げ弾性率の高い熱可塑性樹脂の図
心を通り、且つ板厚方向に垂直で断面内に存在する軸に
関する曲げ弾性率の高い熱可塑性樹脂の断面二次モーメ
ント。
I: Second moment of area of the thermoplastic resin having a high flexural modulus with respect to an axis passing through the center of the thermoplastic resin having a high flexural modulus and perpendicular to the thickness direction and existing in the cross section.

【0020】I′:板状積層熱可塑性樹脂成形体の図心
を通り、且つ板厚方向に垂直で断面内に存在する軸に関
する板状積層熱可塑性樹脂成形体の断面二次モーメン
ト。)上記式中の図心は、断面形状における重心を表す
ものであり、断面二次モーメントは、機械工学便覧(昭
和63年5月15日、日本機械学会発行)A4編24頁
に定義されているもので、曲げ剛性強度を表す指標の1
つである。本発明において、断面二次モーメントは、市
販のソフトウェア、例えば、SDRC社製の「I−DE
AS VI.i」を用いて容易に算出することができ
る。また、比較的簡単な形状については、上記した機械
工学便覧A4編25〜26頁の表6に掲載された各種断
面形状についての計算式を用いて算出することもでき
る。
I ': The second moment of area of the plate-shaped laminated thermoplastic resin molded product with respect to the axis passing through the center of the plate-shaped laminated thermoplastic resin molded product and perpendicular to the plate thickness direction and existing in the cross section. The centroid in the above equation represents the center of gravity in the cross-sectional shape, and the second moment of area is defined in the Mechanical Engineering Handbook (May 15, 1988, published by The Japan Society of Mechanical Engineers), A4, page 24. Index of the flexural rigidity
One. In the present invention, the area moment of inertia is calculated using commercially available software such as “I-DE” manufactured by SDRC.
AS VI. i "can be easily calculated. A relatively simple shape can also be calculated using the above-mentioned formulas for various cross-sectional shapes listed in Table 6 on pages 25-26 of the Mechanical Engineering Handbook A4.

【0021】上式において、(1)式は高剛性熱可塑性
樹脂に対する低剛性熱可塑性樹脂の断面積比率を表す。
この値が小さくなると、高剛性熱可塑性樹脂が後から成
形される低剛性熱可塑性樹脂の収縮を抑制するため、板
状積層熱可塑性樹脂成形体のソリを抑制する効果が大き
いことを表す。また、(2)式は高剛性熱可塑性樹脂の
単位断面積当たりの断面二次モーメントを板状積層熱可
塑性樹脂成形体の単位断面積当たりの断面二次モーメン
トで除したものである。つまり、(2)式による算出値
が大きくなると、単位断面積当たりの曲げ剛性強度が上
昇し、該板状積層熱可塑性樹脂成形体のソリを抑制する
効果が大きいことを表す。
In the above equation, equation (1) represents the cross-sectional area ratio of the low-rigidity thermoplastic resin to the high-rigidity thermoplastic resin.
When this value is small, the high-rigidity thermoplastic resin suppresses the shrinkage of the low-rigidity thermoplastic resin to be molded later, which means that the effect of suppressing the warpage of the plate-shaped laminated thermoplastic resin molded article is large. Equation (2) is obtained by dividing the second moment of area per unit cross-sectional area of the high-rigidity thermoplastic resin by the second moment of area per unit cross-sectional area of the plate-shaped laminated thermoplastic resin molded product. That is, when the value calculated by the equation (2) increases, the flexural rigidity per unit cross-sectional area increases, indicating that the effect of suppressing the warpage of the plate-shaped laminated thermoplastic resin molded article is large.

【0022】本発明においては、上記式(1)で示され
るようにB/Aが0.2を越え1.6以下でなければな
らず、1以下であることが好ましい。B/Aが1.6を
越える場合には、高剛性熱可塑性樹脂と低剛性熱可塑性
樹脂の収縮の差による残留応力を、高剛性熱可塑性樹脂
が抑制する効果が低下するため板状積層熱可塑性樹脂成
形体のソリを防止することができない。B/Aが0.2
以下のときはソリの発生がほとんど起こらないために本
発明にしたがうまでもない。
In the present invention, B / A must be more than 0.2 and not more than 1.6 as shown by the above formula (1), and preferably not more than 1. If B / A exceeds 1.6, the effect of the high-rigidity thermoplastic resin to suppress the residual stress due to the difference in shrinkage between the high-rigidity thermoplastic resin and the low-rigidity thermoplastic resin decreases, so that the plate-like laminating heat is reduced. It is not possible to prevent warping of the plastic resin molded article. B / A is 0.2
In the following cases, warpage hardly occurs, and it goes without saying that the present invention is followed.

【0023】さらに、本発明においては、上記式(2)
で示されるように(C×I)/(A×I′)が0.5以
上1未満でなければならず、1に限りなく近づくことが
好ましいが、本発明の効果は0.7以上で顕著である。
また、上記式(2)の値が0.5未満の場合には、高剛
性熱可塑性樹脂及び低剛性熱可塑性樹脂が、互いのソリ
を抑制する効果が十分得られないため、積層成形体のソ
リを防止することができない。また、上記式(2)の値
が1以上になると、形状的に積層成形体を成形するのが
困難になるため好ましくない。また、上記式(2)が同
じ値の場合においては、上記断面における境界線の長い
方が好ましい。
Further, in the present invention, the above formula (2)
(C × I) / (A × I ′) must be 0.5 or more and less than 1 as shown by, and it is preferable that the value approaches 1 as much as possible, but the effect of the present invention is 0.7 or more. Notable.
When the value of the above formula (2) is less than 0.5, the high-rigidity thermoplastic resin and the low-rigidity thermoplastic resin cannot sufficiently obtain the effect of suppressing warpage between each other. We cannot prevent warpage. Further, when the value of the above formula (2) is 1 or more, it is not preferable because it is difficult to form a laminated molded body in shape. In addition, when the above equation (2) has the same value, it is preferable that the boundary line in the cross section be longer.

【0024】本発明で使用される熱可塑性樹脂には、従
来公知の熱安定剤、耐候剤、着色剤、帯電防止剤、滑
剤、核剤、ブルーミング防止剤などの添加剤;タルク、
炭酸カルシウム、マイカ、硫酸バリウム、ガラス繊維、
ガラスビーズ、ガラスバルーン、炭素繊維などの無機充
填剤;木粉、モミガラ粉、パルプなどの有機充填剤;デ
カブロムジフェニルエーテルに代表されるポリブロモジ
フェニルエーテル、TBA誘導体、TBS誘導体、含臭
素イソシアヌル酸誘導体などの含臭素有機系難燃剤;各
種リン酸系難燃剤;三酸化アンチモン、水酸化マグネシ
ウム、水酸化アルミニウム、赤リンなどの無機系難燃剤
を添加してもよい。
The thermoplastic resin used in the present invention may contain additives such as conventionally known heat stabilizers, weathering agents, coloring agents, antistatic agents, lubricants, nucleating agents, and blooming inhibitors;
Calcium carbonate, mica, barium sulfate, glass fiber,
Inorganic fillers such as glass beads, glass balloons, carbon fibers, etc .; organic fillers such as wood powder, fir powder, pulp; polybromodiphenyl ether represented by decabrom diphenyl ether; TBA derivatives; TBS derivatives; bromine-containing isocyanuric acid derivatives; Brominated organic flame retardants; various phosphoric acid flame retardants; and inorganic flame retardants such as antimony trioxide, magnesium hydroxide, aluminum hydroxide, and red phosphorus.

【0025】本発明の板状積層熱可塑性樹脂成形体にお
ける板状とは、縦、横の長さに比べて厚み方向の長さが
相対的に短いものであり、板厚方向に平行な方向から見
た形状は任意の形状、例えば、正方形、長方形のみなら
ず、三角形、四角形、五角形等の多角形、円形、中空円
形(ドーナツ型)、半円形、中空半円形、円弧形、中空
円弧形、馬蹄形、三日月形等であってよい。また、板厚
方向の断面の形状も任意の形状、例えば、長方形の他、
三角形、四角形、五角形等の多角形、長楕円形、弓形、
三日月型等であってよい。また、表面に特殊な凹凸加工
が施されたものであってもよく、概ね板状体の形状を保
持しているものであればよい。
The term “plate shape” in the plate-shaped laminated thermoplastic resin molded article of the present invention means that the length in the thickness direction is relatively shorter than the length in the vertical and horizontal directions, and the direction parallel to the thickness direction of the plate. Can be any shape, for example, not only a square and a rectangle, but also a polygon such as a triangle, a quadrangle, and a pentagon, a circle, a hollow circle (a donut shape), a semicircle, a hollow semicircle, an arc shape, and a hollow circle. It may be arc-shaped, horseshoe-shaped, crescent-shaped, or the like. In addition, the cross-sectional shape in the thickness direction is also an arbitrary shape, for example, in addition to a rectangle,
Polygons such as triangles, squares, pentagons, oblongs, bows,
It may be a crescent moon or the like. Further, the surface may be subjected to a special unevenness processing, and may be any as long as it has a substantially plate-like shape.

【0026】本発明の板状積層熱可塑性樹脂成形体の製
造方法は特に制限されず、公知の射出成形、プレス成
形、押出成形、スタンパブル成形などを採用することが
できる。特に、射出成形の中で、コアバック方式や2色
成形方法の場合、金型の一方側に高剛性熱可塑性樹脂を
充填後、金型コアを後退させ、又は金型を反転させた
後、もう一方側に低剛性熱可塑性樹脂を充填させる方法
を採用することができる。
The method for producing the plate-shaped laminated thermoplastic resin molded article of the present invention is not particularly limited, and known injection molding, press molding, extrusion molding, stampable molding and the like can be employed. In particular, in the injection molding, in the case of the core back method or the two-color molding method, after filling one side of the mold with a high-rigidity thermoplastic resin, after retracting the mold core, or after inverting the mold, A method of filling the other side with a low-rigidity thermoplastic resin can be adopted.

【0027】また、一方の金型で、高剛性熱可塑性樹脂
を予め成形しておき、この成形体を取りだした後、もう
一方の金型に取り付け、低剛性熱可塑性樹脂を充填する
方法も採用できる。この方法を採用した場合、本発明に
したがった場合とそうでない場合の効果の差異が大き
く、本発明の効果が大きい。
Also, a method in which a high-rigidity thermoplastic resin is molded in one mold in advance, the molded body is taken out, and then attached to the other mold, and a low-rigidity thermoplastic resin is filled. it can. When this method is adopted, the difference between the effect according to the present invention and the effect otherwise is large, and the effect of the present invention is large.

【0028】[0028]

【発明の効果】本発明の板状積層熱可塑性樹脂成形体
は、ソリによる変形がなく寸法安定性のよい成形体であ
る。このような効果が得られる理由は、板状積層熱可塑
性樹脂成形体を構成する高剛性熱可塑性樹脂と低剛性熱
可塑性樹脂の曲げ弾性率の比が特定の値であり、また、
これら熱可塑性樹脂の断面における境界が凹凸形状であ
り、さらに、断面において特定の式を満足するものであ
るために、先に成形された高剛性熱可塑性樹脂の成形体
が後から成形した低剛性熱可塑性樹脂の成形体の収縮に
よる変形を抑制するためであると推定される。
The plate-shaped laminated thermoplastic resin molded article of the present invention is a molded article having good dimensional stability without deformation due to warpage. The reason why such an effect is obtained is that the ratio of the bending elastic modulus of the high-rigidity thermoplastic resin and the low-rigidity thermoplastic resin constituting the plate-shaped laminated thermoplastic resin molded article is a specific value,
Since the boundary in the cross section of these thermoplastic resins has an uneven shape, and furthermore, the cross section satisfies a specific formula, the molded article of the high rigid thermoplastic resin molded earlier has a low rigidity molded later. It is presumed that this is because deformation due to shrinkage of the molded article of the thermoplastic resin is suppressed.

【0029】したがって、本発明の板状積層熱可塑性樹
脂成形体は、寸法安定性の求められる各種部材として有
用である。例えば、バンパー、インストルーメントパネ
ル、ドアトリム等の自動車用部品;ワープロ、パソコ
ン、キーボード、コピー機、その他のOA機器のハウジ
ング;ドアパネル、サッシ、壁板等の住宅建材;便座、
便蓋等のサニタリー部品などに好ましく使用することが
できる。
Therefore, the plate-shaped laminated thermoplastic resin molded article of the present invention is useful as various members requiring dimensional stability. For example, automobile parts such as bumpers, instrument panels, and door trims; housings for word processors, personal computers, keyboards, copiers, and other OA equipment; housing materials such as door panels, sashes, and wall boards;
It can be preferably used for sanitary parts such as toilet lids.

【0030】[0030]

【実施例】本発明を更に具体的に説明するために、以下
に実施例及び比較例を掲げて説明するが、本発明はこれ
らの実施例に限定されるものでない。
EXAMPLES The present invention will be described more specifically with reference to examples and comparative examples, but the present invention is not limited to these examples.

【0031】なお、実施例及び比較例で示した熱可塑性
樹脂及び表中の記号で既に説明したものの他は以下のと
おりである。
The thermoplastic resins shown in Examples and Comparative Examples and those already described with reference to the symbols in the table are as follows.

【0032】 熱可塑性樹脂: 記号 材 質 曲げ弾性率(kg/cm2) イ:プロピレン単独重合体 20,000 ロ:エチレンプロピレンブロック共重合体 15,000 ハ:エチレンプロピレンランダム共重合体 10,000 ニ:エチレンプロピレンブロック共重合体 5,000 ホ:エチレンプロピレンブロック共重合体 3,000 表中の記号: L :断面における境界線長。Thermoplastic resin: Symbol Material Flexural modulus (kg / cm 2 ) A: Propylene homopolymer 20,000 B: Ethylene propylene block copolymer 15,000 C: Ethylene propylene random copolymer 10,000 D: Ethylene propylene block copolymer Polymer 5,000 E: Ethylene propylene block copolymer 3,000 Symbol in the table: L: Boundary line length in cross section.

【0033】L′:図1の(a)試験片の境界線長。L ': Boundary line length of the test piece in FIG.

【0034】実施例及び比較例 板状積層熱可塑性樹脂成形体の成形とソリの測定は以下
のようにして行なった。下記成形法に基づいて成形体を
得、ソリを測定し、その結果を表1に示した。なお、断
面二次モーメントはSDRC社製の「I−DEAS V
I.i」を用いて算出した。
Examples and Comparative Examples Molding of plate-shaped laminated thermoplastic resin molded articles and measurement of warpage were performed as follows. A molded product was obtained based on the following molding method, and warpage was measured. The results are shown in Table 1. In addition, the second moment of area is “I-DEAS V” manufactured by SDRC.
I. i ".

【0035】(A)成形方法 高剛性熱可塑性樹脂を用い日本製鋼所社製150Tベン
ト付射出成形機で下記条件にて幅60mm×長さ260
mmの各試験片を得た。
(A) Molding Method Using a high rigidity thermoplastic resin, an injection molding machine with a 150T vent manufactured by Nippon Steel Works, Ltd. under the following conditions, width 60 mm × length 260
mm test pieces were obtained.

【0036】 ・射出成形温度(シリンダー温度設定) 230℃ ・金型温度(冷却水温度設定) 40℃ これら試験片の板厚方向および幅方向に平行な平面で切
断した断面の形状は、それぞれ図1〜図9に示した
(a)、(b)、(c)、(d)、(e)、(f)、
(g)、(h)および(i)の9種類であった。断面の
寸法は各図に数字で示した。
Injection molding temperature (cylinder temperature setting) 230 ° C. Die temperature (cooling water temperature setting) 40 ° C. The cross-sectional shapes of these test pieces cut along a plane parallel to the plate thickness direction and the width direction are shown in FIG. (A), (b), (c), (d), (e), (f),
(G), (h) and (i). The dimensions of the cross section are indicated by numerals in each figure.

【0037】次に試験片の平な面を金型に密着させ、反
対側の凹凸面空間に新たに低剛性熱可塑性樹脂が充填さ
れる様に、幅60mm×長さ260mm×厚さ6mmの
金型に装着した。次いで上記と同一射出成形機で同一条
件にて低剛性熱可塑性樹脂を充填し、図10〜図18に
示す(a′)、(b′)、(c′)、(d′)、
(e′)、(f′)、(g′)、(h′)および
(i′)の幅60mm×長さ260mm×厚さ6mmの
各積層成形体を得た。なお、図10〜図18中、黒色部
分は高剛性熱可塑性樹脂であり、白色部分は低剛性熱可
塑性樹脂である。
Next, the flat surface of the test piece is brought into close contact with the mold, and a 60 mm wide × 260 mm long × 6 mm thick is formed so that the low-rigidity thermoplastic resin is newly filled in the uneven surface space on the opposite side. Attached to the mold. Next, a low-rigidity thermoplastic resin is filled with the same injection molding machine as above under the same conditions, and (a ′), (b ′), (c ′), (d ′),
(E '), (f'), (g '), (h') and (i ') were obtained, each having a width of 60 mm, a length of 260 mm and a thickness of 6 mm. In FIGS. 10 to 18, the black portion is a high-rigidity thermoplastic resin, and the white portion is a low-rigidity thermoplastic resin.

【0038】(B)成形体のソリ観察方法 上記の様にして得られた積層成形体を、成形後48時間
経過した後、水平な板の上に置き、水平面から該積層成
形体下面の一番離れた距離を測定した。
(B) Method of Observing Warpage of Molded Product After the laminated molded product obtained as described above has been molded for 48 hours, it is placed on a horizontal plate, and one side of the lower surface of the laminated molded product is measured from a horizontal plane. The farthest distance was measured.

【0039】[0039]

【表1】 [Table 1]

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

【図1】図1は、比較例の高剛性熱可塑性樹脂成形体の
断面図である。
FIG. 1 is a sectional view of a high-rigidity thermoplastic resin molded body of a comparative example.

【図2】図2は、実施例の高剛性熱可塑性樹脂成形体の
断面図である。
FIG. 2 is a cross-sectional view of a high-rigidity thermoplastic resin molded product of an example.

【図3】図3は、比較例の高剛性熱可塑性樹脂成形体の
断面図である。
FIG. 3 is a cross-sectional view of a high-rigidity thermoplastic resin molded body of a comparative example.

【図4】図4は、実施例の高剛性熱可塑性樹脂成形体の
断面図である。
FIG. 4 is a cross-sectional view of a high-rigidity thermoplastic resin molded product of an example.

【図5】図5は、実施例の高剛性熱可塑性樹脂成形体の
断面図である。
FIG. 5 is a sectional view of a high-rigidity thermoplastic resin molded product of an example.

【図6】図6は、実施例の高剛性熱可塑性樹脂成形体の
断面図である。
FIG. 6 is a sectional view of a high-rigidity thermoplastic resin molded product of an example.

【図7】図7は、実施例の高剛性熱可塑性樹脂成形体の
断面図である。
FIG. 7 is a cross-sectional view of a high-rigidity thermoplastic resin molded article of an example.

【図8】図8は、実施例の高剛性熱可塑性樹脂成形体の
断面図である。
FIG. 8 is a cross-sectional view of a high-rigidity thermoplastic resin molded product of an example.

【図9】図9は、実施例の高剛性熱可塑性樹脂成形体の
断面図である。
FIG. 9 is a sectional view of a high-rigidity thermoplastic resin molded product according to an example.

【図10】図10は、比較例の板状積層熱可塑性樹脂成
形体の断面図である。
FIG. 10 is a sectional view of a plate-shaped laminated thermoplastic resin molded product of a comparative example.

【図11】図11は、実施例の板状積層熱可塑性樹脂成
形体の断面図である。
FIG. 11 is a cross-sectional view of a plate-shaped laminated thermoplastic resin molded product of an example.

【図12】図12は、比較例の板状積層熱可塑性樹脂成
形体の断面図である。
FIG. 12 is a sectional view of a plate-shaped laminated thermoplastic resin molded product of a comparative example.

【図13】図13は、実施例の板状積層熱可塑性樹脂成
形体の断面図である。
FIG. 13 is a cross-sectional view of a plate-shaped laminated thermoplastic resin molded product of an example.

【図14】図14は、実施例の板状積層熱可塑性樹脂成
形体の断面図である。
FIG. 14 is a cross-sectional view of a plate-shaped laminated thermoplastic resin molded product of an example.

【図15】図15は、実施例の板状積層熱可塑性樹脂成
形体の断面図である。
FIG. 15 is a cross-sectional view of a plate-shaped laminated thermoplastic resin molded product of an example.

【図16】図16は、実施例の板状積層熱可塑性樹脂成
形体の断面図である。
FIG. 16 is a cross-sectional view of a plate-shaped laminated thermoplastic resin molded product of an example.

【図17】図17は、実施例の板状積層熱可塑性樹脂成
形体の断面図である。
FIG. 17 is a cross-sectional view of a plate-shaped laminated thermoplastic resin molded product of an example.

【図18】図18は、実施例の板状積層熱可塑性樹脂成
形体の断面図である。
FIG. 18 is a sectional view of a plate-shaped laminated thermoplastic resin molded product of an example.

Claims (1)

(57)【特許請求の範囲】(57) [Claims] 【請求項1】曲げ弾性率が異なり、且つその曲げ弾性率
比が0.5以下である2種の熱可塑性樹脂が積層された
板状成形体であって、その板厚方向に平行な平面で切断
した少なくとも一つの断面における2種の熱可塑性樹脂
の境界は凹凸を形成しており、且つ該断面において下記
(1)及び(2)式を同時に満足することを特徴とする
板状積層熱可塑性樹脂成形体。 0.2<B/A≦1.6 ・・・ (1) 0.5≦(C×I)/(A×I′)<1 ・・・ (2) (ただし、上記式中、 A :曲げ弾性率の高い熱可塑性樹脂の占める断面積。 B :曲げ弾性率の低い熱可塑性樹脂の占める断面積。 C :板状積層熱可塑性樹脂成形体の全断面積。 I :曲げ弾性率の高い熱可塑性樹脂の図心を通り、且
つ板厚方向に垂直で断面内に存在する軸に関する曲げ弾
性率の高い熱可塑性樹脂の断面二次モーメント。 I′:板状積層熱可塑性樹脂成形体の図心を通り、且つ
板厚方向に垂直で断面内に存在する軸に関する板状積層
熱可塑性樹脂成形体の断面二次モーメント。)
1. A plate-like molded product in which two kinds of thermoplastic resins having different flexural modulus and a flexural modulus ratio of 0.5 or less are laminated, and a plane parallel to the plate thickness direction. The boundary between the two types of thermoplastic resin in at least one cross section cut in step (a) has irregularities, and the cross section satisfies the following expressions (1) and (2) simultaneously. Plastic molded article. 0.2 <B / A ≦ 1.6 (1) 0.5 ≦ (C × I) / (A × I ′) <1 (2) (where, A: Cross-sectional area occupied by thermoplastic resin having high flexural modulus B: Cross-sectional area occupied by thermoplastic resin having low flexural modulus C: Total cross-sectional area of plate-shaped laminated thermoplastic resin molded article I: High flexural modulus Second moment of area of the thermoplastic resin having a high flexural modulus with respect to an axis passing through the centroid of the thermoplastic resin and perpendicular to the thickness direction and existing in the cross section I ': Drawing of plate-shaped laminated thermoplastic resin molded article The moment of inertia of the plate-shaped laminated thermoplastic resin article with respect to an axis passing through the center and perpendicular to the thickness direction and present in the cross section.)
JP30013093A 1993-11-30 1993-11-30 Plate-shaped laminated thermoplastic resin molding Expired - Fee Related JP3278269B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP30013093A JP3278269B2 (en) 1993-11-30 1993-11-30 Plate-shaped laminated thermoplastic resin molding

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP30013093A JP3278269B2 (en) 1993-11-30 1993-11-30 Plate-shaped laminated thermoplastic resin molding

Publications (2)

Publication Number Publication Date
JPH07148875A JPH07148875A (en) 1995-06-13
JP3278269B2 true JP3278269B2 (en) 2002-04-30

Family

ID=17881100

Family Applications (1)

Application Number Title Priority Date Filing Date
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Country Status (1)

Country Link
JP (1) JP3278269B2 (en)

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP5746882B2 (en) * 2011-02-25 2015-07-08 三豊化成株式会社 Manufacturing method for thick molded products

Also Published As

Publication number Publication date
JPH07148875A (en) 1995-06-13

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