JPH0144494B2 - - Google Patents
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- Publication number
- JPH0144494B2 JPH0144494B2 JP1877686A JP1877686A JPH0144494B2 JP H0144494 B2 JPH0144494 B2 JP H0144494B2 JP 1877686 A JP1877686 A JP 1877686A JP 1877686 A JP1877686 A JP 1877686A JP H0144494 B2 JPH0144494 B2 JP H0144494B2
- Authority
- JP
- Japan
- Prior art keywords
- pressure
- resin
- molding
- temperature
- thermoforming
- 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
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- Blow-Moulding Or Thermoforming Of Plastics Or The Like (AREA)
- Laminated Bodies (AREA)
Description
〔産業上の利用分野〕
本発明は圧空成形により電磁波遮蔽性を有する
筐体を製造する等に適した熱成形用積層板の成形
方法に関する。
〔従来技術〕
従来、電磁波遮蔽性を有する筐体を製造するに
は筐体に金属溶射を施すか、あるいは導電性塗料
を塗布する等の方法が行われている。しかし、前
者の方法は溶射された金属または合金が筐体本体
から剥離しやすく、また後者の方法は塗料中に含
有せしめた金属粒子が酸化するなどの経時変化が
生じ電磁波遮蔽能が劣化するものであつた。さら
に両者の方法はそれ自体高価となる欠点をも有す
るものであつた。そこで、金属箔と樹脂とを積層
した積層板を成形する方法が提案されたが、これ
ら積層板に使われる金属はFe箔、Al箔であるた
め、成形性が十分でなく、浅い成形しかできない
ものである。従つて、この積層板に用いる金属箔
としては超塑性をもつものが好ましく、これを樹
脂と一体のまま成形することが期待される。しか
し、超塑性合金としてはZn−Al合金、Pb−Sn合
金等が知られているが、これら超塑性合金を使用
した積層板は未だ市販されておらず、成形条件等
についても全く明らかになつていないのが現状で
ある。
〔発明が解決しようとする問題点〕
金属超塑性材の圧空成形に際しては、超塑性材
がある変形速度以下でしか大きな伸びを示さない
ことから成形時間が長くかかり、たとえばZn−
22%Al合金系の1mm厚の板の成形時間は1〜3
分程度となる。一方熱成形用樹脂板の成形では雌
型内を減圧して空気抜きをしつつ3Kg/cm2の定圧
をかける方法がとられており、60秒程度以内(多
くは10秒以内)の成形時間となつている。さらに
樹脂の圧空成形では成形開始直後に変形の大部分
が終了し、残りの成形時間はエツジをシヤープに
したり、細かい凹凸をつけるために必要とされ
る。例えば、厚み2mmのアクリル変性塩ビ(筒中
プラスチツク工業(株)製商品名カイダツク)で幅
100mm、長さ200mm、深さ35mmの筐体を成形するの
に温度160℃、圧力5Kg/cm2で10秒を要した。し
かし、上記条件で圧力を2秒かけて成形したもの
は、エツジがかなり丸くなつているものの形状と
しては、筐体になつており、変形量の90%以上は
既に終了していた。このように超塑性材と熱成形
用樹脂板とでは成形速度などの成形条件が大きく
異なる。そして、樹脂成形の従来法で上記積層板
を圧空成形すると、変形速度特に成形初期の変形
速度は超塑性合金板が大きな伸びを示す変形速度
に比べ速すぎるため、絞り比が浅い、エツジが丸
いなどごく限られた形状の型では成形できるもの
の、一般には超塑性金属の変形が樹脂においつか
ず、成形後金属板に亀裂が生じたり、樹脂板と金
属板の間に剥離が生じるものであつた。成形圧力
を下げることによりこのような金属板の亀裂や剥
離を防ぐことはできるが、この場合には型再現性
が不足するようになる。
〔問題を解決するための手段〕
本発明者らは、Pb−Sn系、Pb−Sn−Cd系お
よびZn−Al系等の超塑性合金と種々の熱成形用
樹脂を積層した熱成形用積層板について成形試験
を繰返した結果、上記積層板の圧空成形に際し、
成形圧力を多段に、もしくは無段階に変化させ、
初期成形圧力をその後の成形圧力に比べて低圧と
し、その後圧力を高め、もしくは順次高めながら
その以後の成形を行うことにより、積層板が良好
に成形されるという従来全く考え及ばない新規な
知見を得た。本発明はこれら知見に基づいて完成
したものである。
すなわち、本発明は超塑性合金と熱成用樹脂の
変形速度が異なることに着目し、まず超塑性合金
が変形し得る圧力で成形し、その後圧力を高め、
もしくは高めながら成形し、型再現性を得ること
を要点とするものである。従つて、本発明では初
期成形圧力は超塑性合金が変形可能で且つ熱成形
用樹脂が予備成形されるような比較的低圧である
ことを意味する。
これら、初期成形圧力およびそれ以後の圧力は
圧力を多段、好ましくは2段に変化させ、あるい
は無段階に変化させることによつて達成されるも
のである。
本発明における超塑性合金とは2相または3相
以上の合金系で微細な結晶粒を有することによ
り、熱成塑性樹脂(熱成形用樹脂)の一般的成形
温度である300℃以下の雰囲気温度で100%以上の
伸びを示すものをいう。具体的にはPb−Sn系合
金であつてSn含量が19〜97.5wt%のもの、Pn−
Sn−Cd系合金であつてSn含量が10〜62wt%で、
Cd含量が0.5〜30wt%のもの、あるいはZn−Al
系合金であつて、Al含量が21〜23wt%のものお
よびこれらにCu、Mg等を1%以下添加して改良
したもの等が挙げられる。そして、本発明はこれ
ら超塑性合金と熱成形用樹脂とを積層させた積層
板を圧空成形により筐体等に成形するものである
から、当然超塑性合金は樹脂の成形温度で超塑性
を示すものであり、また基本的には剛性をもつ必
要がないから穴があかない範囲でできるだけ薄
く、樹脂の成形についていかなければならない。
そのためには超塑性合金板の厚みは0.3〜0.01mm
程度とすることが好ましい。
また、本発明における熱成形用樹脂としては圧
空成形に適するシートで筐体とする場合はその主
要な機能を満たすものである必要があり、次の如
き樹脂が好適である。すなわちアクリル変性塩ビ
樹脂、またはこれに添加剤を加えたものからなる
群で、例えば商品名カイダツク(筒中プラスチツ
ク工業(株))、変形オレフイン樹脂、またはこれに
添加剤を加えたものからなる群で、例えば商品名
オレビツク(筒中プラスチツク工業(株))、芳香族
ポリエーテル樹脂、またはこれに添加剤を加えた
ものからなる群で、例えば商品名ノリル(筒中プ
ラスチツク工業(株))の他、ABC樹脂、PVC、ポ
リカーボネート等が挙げられる。これら熱成形用
樹脂のシートは厚さ0.1〜10mm程度のものが好ま
しい。
これら超塑性合金板および熱成形用樹脂シート
は添付の第1図に示されるように、超塑性合金板
1の両面に熱成形用樹脂シート2を低融点の熱可
塑性樹脂フイルムなどからなる接着剤もしくは粘
着剤3を介して、あるいは介在物無しで積層され
る。また積層板は第2図のように、超塑性合金板
1の片面にのみ熱成形用樹脂2を接着剤もしくは
粘着剤3を介して、もしくは介在物無しで積層さ
れたものであつてもよい。
上述の如き積層板は本発明に従つて、比較的低
圧の初期成形圧力により成形された後、初期成形
圧力よりも高い圧力で以後の成形が施される。
初期成形圧力は前述のように超塑性合金が超塑
性変性され且つ熱成形用樹脂が予備成形される範
囲とするが、具体的には0.1Kg/cm2未満の圧力で
は成形が不十分となり、5Kg/cm2を越えると合金
板に亀裂が生ずるため0.1〜5Kg/cm2とすること
が好ましい。また成形体の変形量が大きい場合に
は樹脂の変形に合金板の変形がおいつかないため
3Kg/cm2以下とすることが望ましい。さらに積層
板の構造が超塑性合金板の片面にのみ熱成形用樹
脂で積層されたものである場合には樹脂の変形に
拘束されて合金板も良く変形する効果が少なくな
るためか1.5Kg/cm2以内の圧力であることが望ま
しい。またこの初期成形圧は加圧である必然性が
あるわけではなく減圧によつて加えられてもよい
ことは自明のことである。これら初期成形圧力の
保持時間は1秒未満では積層板の変形量が少なく
低圧で変形する効果が不十分となり、また20秒を
越えると低圧で長時間をかけて成形することにな
り金型により積層板が冷却されるため、その後高
圧で成形しても型再現性が不足するようになるた
め1〜20秒とすることが好ましい。また必要以上
に低圧での成形時間をとることは全成形時間が長
くなることになり、工業的にも意味がない。
初期成形以後の成形圧力は型再現性の点から3
Kg/cm2以上とすることが好ましいが、型の形状お
よび模様によつては5Kg/cm2以上とすることが望
ましい。しかし10Kg/cm2を越えることは実際的で
はない。
超塑性合金としてPb−Sn系合金を用いた積層
板では、120〜183℃の成形温度とすることが望ま
しい。すなわち120℃未満の温度では超塑性が十
分発揮されず、183℃以上ではPb合金が溶解す
る。また絞り比が大きいなどの理由で十分な超塑
性を得たい場合には積層板の温度は150℃〜170℃
の温度範囲とすることがより望ましい。また、
Pb−Sn−Cd系超塑性合金を用いる場合には、積
層板の温度は110℃〜145℃とすることが望まし
い。すなわち110℃未満の温度では超塑性が十分
発揮されず、145℃以上ではPb合金が溶解する。
また、絞り比が大きいなどの理由で十分な超塑性
を得たい場合には125〜135℃の温度範囲が望まし
い。以上の例からもわかるように積層板の成形温
度の上限は用いる超塑性金属板が超塑性を示さな
くなる融点或いはZn−Al合金などのような場合
は変態点で上限が制限され、下限は要求される変
形速度を満たす温度によつて制限される。一方熱
可塑性樹脂の側から考えれば、積層板の下限温度
は樹脂の軟化が不十分となる温度で決定される。
また、金型温度は成形後の樹脂の硬化が不十分と
ならない温度あるいは成形中の積層板の冷却が著
しく型再現性が不足したり偏肉を生じる温度が下
限となり、樹脂の収縮を生じ型再現性に著しく悪
影響を及ぼす温度が上限となる。即ち、積層板の
樹脂としてアクリル変性塩ビ系樹脂を使用する場
合の積層板の温度は110℃以上、金型温度は10〜
70℃が適切であるが、種々の組合わせにより変動
することもあるのでこれに限定されるものではな
い。
同様に変形オレフイン系樹脂を使用する場合は
積層板温度は140℃以上金型温度は30〜120℃が適
切であり、芳香族ポリエーテル系樹脂を使用する
場合は、積層板温度は150℃以上、金型温度は30
〜130℃が適切であるが、種々の組合わせにより
変動することもあるのでこれに限定されるもので
はない。
〔作用〕
かくして本発明では熱成形用積層板の成形に際
し、初期成形圧力をその後の成形圧力に比べて低
圧とし、その後圧力を高め、もしくは順次高めな
がらそれ以後の成形を行うため、初期成形により
超塑性合金が超塑性変形され、同時に熱成形用樹
脂が大部分の変形が終了して予備成形が終り、そ
れ以後の高圧負荷により樹脂のエツジ部分等がさ
らにシヤープに成形されて型再現性が達成される
ことになる。
以下に実施例を示す。実施例1では二段成形の
実施例を、実施例2では多段成形の実施例を、そ
して実施例3では無段成形の実施例をそれぞれ示
す。なお、各実施例では幅100mm、長さ200mm、深
さ35mmで底面の一部に高さ約3mmの凹凸がある筐
体成形用の型を用いた。
実施例 1
熱成形用樹脂としては、アクリル変性塩ビ系の
ものとして商品名カイダツク(筒中プラスチツク
工業(株))、変形オレフイン系樹脂として商品名オ
レビツク(筒中プラスチツク工業(株))、芳香族ポ
リエーテル系樹脂としてポリフエニレンオキサイ
ド、商品名ノリル(筒中プラスチツク工業(株)製)
を用いた。超塑性合金としては16が0.2mm厚の70
%Pb−30%Sn合金板、10が0.1mm厚の38%Pb−62
%Sn合金板、22が0.2mm厚の64%Pb−16%Sn−20
%Cd合金板、21が0.1mm厚の64%Pd−16%Sn−20
%Cd合金板を用いた。又他の積層板にはすべて
0.2mm厚の38%Pb−62%Snの合金板を用いた。
積層法としては1〜17及び21、22については第
1図に示すように厚さ2mmと1mmのカイダツクの
間に超塑性合金をポリオレフイン系の接着フイル
ム(東セロ化学(株)製商品名アドマーフイルム
VE300)を介して装着した。また18〜20、23〜28
については第2図に示すように樹脂の片側に超塑
性合金を積層した。そして18〜20ではアドマーフ
イルムVE300と厚さ2mm厚のカイダツクを23〜25
ではポリオレフイン系接着フイルム(東セロ化学
(株)製、商品名アドマーフイルムXE070)と厚さ
1.5mmのオレビツクを、26〜28ではアドマーフイ
ルムXE070と厚さ2mmのノリルとを用いた。
実施例の結果を次に検討する。第一段の成形圧
力については低い例である14の場合でも成形が可
能となつている。又高すぎる例である1の場合
Pb合金板の超塑性変形が樹脂の変形に追いつか
ずPb合金板が破れた。なお第2図のような積層
法をとる場合にはPb合金板の変形が第1図のよ
うな場合にくらべ十分でなく、18のように3Kg/
cm2ではPb板に破れを生じ、樹脂とPb合金板との
間があいてしまうという密着性の不良現象が生じ
ることがある。第一段の成形の時間に関して短か
すぎる例である8の場合十分な一次成形がなされ
ないまま第二段目の圧力7Kg/cm2がかかつたので
Pb合金板に亀裂が生じている。また長すぎる例
である2、13、19の場合第二段成形の前に積層板
が金型により冷却されるため型再現性が不足とな
つた。第二段の圧力は例20に見るように5Kg/cm2
以上あればよいが、例2の場合から推測されるよ
うに2Kg/cm2のような低い圧力では十分な型再現
性が得られない。なお本発明法によらない例1、
2、18、19では良い結果が得られていない。
[Industrial Application Field] The present invention relates to a method for forming a thermoforming laminate suitable for manufacturing a housing having electromagnetic wave shielding properties by air pressure forming. [Prior Art] Conventionally, in order to manufacture a housing having electromagnetic wave shielding properties, methods such as applying metal spraying to the housing or coating the housing with a conductive paint have been used. However, in the former method, the sprayed metal or alloy tends to peel off from the housing body, and in the latter method, the metal particles contained in the paint undergo changes over time such as oxidation, which deteriorates the electromagnetic wave shielding ability. It was hot. Furthermore, both methods had the disadvantage of being expensive in themselves. Therefore, a method of forming a laminate made by laminating metal foil and resin was proposed, but since the metals used for these laminates are Fe foil and Al foil, the formability is insufficient and only shallow forming is possible. It is something. Therefore, it is preferable that the metal foil used for this laminate has superplasticity, and it is expected that it will be molded integrally with the resin. However, although Zn-Al alloy, Pb-Sn alloy, etc. are known as superplastic alloys, laminates using these superplastic alloys are not yet commercially available, and the forming conditions etc. are not completely clear. The current situation is that this is not the case. [Problems to be Solved by the Invention] When air-pressure forming metal superplastic materials, the forming time is long because the superplastic material exhibits large elongation only below a certain deformation rate.
The forming time for a 1 mm thick plate made of 22% Al alloy is 1 to 3.
It will take about a minute. On the other hand, when molding resin plates for thermoforming, a method is used in which a constant pressure of 3 kg/cm 2 is applied while reducing the pressure inside the female mold to remove air, and the molding time is within about 60 seconds (in most cases, within 10 seconds). It's summery. Furthermore, in pressure molding of resin, most of the deformation ends immediately after the start of molding, and the remaining molding time is required to sharpen edges and create fine irregularities. For example, use 2 mm thick acrylic modified PVC (trade name: Kaidatsu, manufactured by Tsutsunaka Plastic Industries Co., Ltd.) to
It took 10 seconds at a temperature of 160°C and a pressure of 5 kg/cm 2 to mold a casing of 100 mm, length 200 mm, and depth 35 mm. However, when molding was performed under the above conditions with pressure applied for 2 seconds, the edges were quite rounded, but the shape was a casing, and more than 90% of the deformation had already been completed. As described above, the molding conditions such as molding speed are significantly different between the superplastic material and the thermoforming resin plate. When the above-mentioned laminate is air-formed using the conventional resin molding method, the deformation speed, especially at the initial stage of molding, is too fast compared to the deformation speed at which superplastic alloy sheets exhibit large elongation, resulting in shallow drawing ratios and rounded edges. Although molding is possible in very limited shapes such as molds, the deformation of the superplastic metal is generally not transferred to the resin, and cracks occur in the metal plate after molding, or separation occurs between the resin plate and the metal plate. . Although such cracking and peeling of the metal plate can be prevented by lowering the molding pressure, mold reproducibility becomes insufficient in this case. [Means for Solving the Problem] The present inventors have developed a thermoforming laminate in which superplastic alloys such as Pb-Sn, Pb-Sn-Cd, and Zn-Al are laminated with various thermoforming resins. As a result of repeated forming tests on the plates, we found that during pressure forming of the above laminate plate,
By changing the molding pressure in multiple stages or steplessly,
By setting the initial molding pressure to a lower pressure than the subsequent molding pressure, then increasing the pressure, or increasing the pressure sequentially while performing subsequent molding, we have discovered a completely new and previously unthinkable finding that laminates can be formed well. Obtained. The present invention was completed based on these findings. That is, the present invention focuses on the fact that the deformation rates of superplastic alloy and thermoforming resin are different, and first molds the superplastic alloy at a pressure that allows it to deform, then increases the pressure,
Alternatively, the key point is to mold while increasing the molding temperature and obtain mold reproducibility. Accordingly, in the present invention, the initial forming pressure is meant to be a relatively low pressure at which the superplastic alloy is deformable and the thermoforming resin is preformed. These initial molding pressures and subsequent pressures are achieved by changing the pressure in multiple steps, preferably in two steps, or by changing the pressure steplessly. In the present invention, the superplastic alloy is a two-phase or three-phase or more alloy system with fine crystal grains, so that it can be used at an ambient temperature of 300℃ or less, which is the general molding temperature for thermoplastic resins (thermoforming resins). This refers to something that shows a growth of 100% or more. Specifically, Pb-Sn alloys with a Sn content of 19 to 97.5 wt%, Pn-
It is a Sn-Cd alloy with a Sn content of 10 to 62 wt%,
Cd content 0.5~30wt% or Zn-Al
These include alloys with an Al content of 21 to 23 wt% and those improved by adding Cu, Mg, etc. in an amount of 1% or less. Since the present invention is to form a laminate made by laminating these superplastic alloys and a thermoforming resin into a housing or the like by pressure forming, the superplastic alloy naturally exhibits superplasticity at the molding temperature of the resin. Since it is a plastic material and basically does not need to be rigid, it must be made as thin as possible without holes and must be able to keep up with resin molding.
For this purpose, the thickness of the superplastic alloy plate is 0.3 to 0.01 mm.
It is preferable to set it as approximately. Further, the resin for thermoforming in the present invention must satisfy the main functions when a sheet suitable for pressure molding is used for the casing, and the following resins are suitable. In other words, it is a group consisting of acrylic modified PVC resin or additives added thereto, such as the product name Kaidatsu (trade name: Tsutsunaka Plastic Industries Co., Ltd.), modified olefin resin, or a group consisting of additives added thereto. , for example, a group consisting of the product name Orevikku (Tsutsunaka Plastics Co., Ltd.), aromatic polyether resin, or additives added thereto, such as the product name Noryl (Tsutsunaka Plastics Co., Ltd.), as well as ABC. Examples include resin, PVC, polycarbonate, etc. These thermoforming resin sheets preferably have a thickness of about 0.1 to 10 mm. As shown in the attached FIG. 1, these superplastic alloy plates and thermoforming resin sheets are made by attaching thermoforming resin sheets 2 to both sides of a superplastic alloy plate 1 using an adhesive made of a low melting point thermoplastic resin film or the like. Alternatively, they may be laminated via the adhesive 3 or without any inclusions. Further, the laminate may be one in which a thermoforming resin 2 is laminated only on one side of a superplastic alloy plate 1 via an adhesive or adhesive 3, or without any inclusions, as shown in FIG. . In accordance with the present invention, the laminate as described above is formed at a relatively low initial forming pressure and then subjected to subsequent forming at a pressure higher than the initial forming pressure. As mentioned above, the initial molding pressure is within the range where the superplastic alloy is superplastically modified and the thermoforming resin is preformed, but specifically, if the pressure is less than 0.1 Kg/ cm2 , the molding will be insufficient; If it exceeds 5 Kg/cm 2 , cracks will occur in the alloy plate, so it is preferably 0.1 to 5 Kg/cm 2 . Furthermore, if the amount of deformation of the molded body is large, the deformation of the alloy plate will not follow the deformation of the resin, so it is desirable that the amount of deformation be 3 kg/cm 2 or less. Furthermore, if the structure of the laminate is one in which thermoforming resin is laminated on only one side of a superplastic alloy plate, the alloy plate may be less effective at deforming due to the deformation of the resin. It is desirable that the pressure be within cm 2 . Furthermore, it is obvious that this initial molding pressure does not necessarily have to be increased pressure, but may be applied by reduced pressure. If the holding time of the initial molding pressure is less than 1 second, the amount of deformation of the laminate will be small and the effect of deforming at low pressure will be insufficient, and if it exceeds 20 seconds, molding will take a long time at low pressure and the mold will deteriorate. Since the laminate is cooled, the mold reproducibility becomes insufficient even if it is subsequently molded under high pressure, so the time is preferably 1 to 20 seconds. Moreover, taking a molding time at a lower pressure than necessary increases the total molding time, which is industrially meaningless. The molding pressure after the initial molding is set to 3 from the viewpoint of mold reproducibility.
It is preferable to set it to Kg/cm 2 or more, but depending on the shape and pattern of the mold, it is desirable to set it to 5 Kg/cm 2 or more. However, it is not practical to exceed 10 kg/cm 2 . For a laminate using a Pb-Sn alloy as a superplastic alloy, it is desirable to use a forming temperature of 120 to 183°C. That is, at temperatures below 120°C, superplasticity is not sufficiently exhibited, and at temperatures above 183°C, the Pb alloy melts. In addition, if you want to obtain sufficient superplasticity due to a large drawing ratio, etc., the temperature of the laminate should be 150℃ to 170℃.
It is more desirable to set the temperature range to . Also,
When using a Pb-Sn-Cd based superplastic alloy, the temperature of the laminate is preferably 110°C to 145°C. That is, at temperatures below 110°C, superplasticity is not sufficiently exhibited, and at temperatures above 145°C, the Pb alloy melts.
Further, when it is desired to obtain sufficient superplasticity due to reasons such as a large drawing ratio, a temperature range of 125 to 135°C is desirable. As can be seen from the above examples, the upper limit of the forming temperature of the laminate is limited by the melting point at which the superplastic metal plate used no longer exhibits superplasticity, or by the transformation point in the case of Zn-Al alloys, and the lower limit is set by the required temperature. The deformation rate is limited by the temperature that satisfies the deformation rate. On the other hand, from the perspective of the thermoplastic resin, the lower limit temperature of the laminate is determined at a temperature at which the resin is insufficiently softened.
In addition, the lower limit of the mold temperature is the temperature at which the resin does not harden sufficiently after molding, or the temperature at which the cooling of the laminate during molding significantly causes a lack of mold reproducibility or uneven thickness, which causes resin shrinkage and mold The upper limit is the temperature that has a significant negative effect on reproducibility. In other words, when using acrylic modified PVC resin as the resin for the laminate, the temperature of the laminate is 110℃ or higher, and the mold temperature is 10~
A temperature of 70°C is appropriate, but it is not limited to this as it may vary depending on various combinations. Similarly, when using modified olefin resin, the appropriate laminate temperature is 140°C or higher and the mold temperature is 30 to 120°C, and when aromatic polyether resin is used, the laminate temperature is 150°C or higher. , mold temperature is 30
A temperature of ~130°C is appropriate, but is not limited to this as it may vary depending on various combinations. [Function] Thus, in the present invention, when forming a thermoforming laminate, the initial forming pressure is set to be lower than the subsequent forming pressure, and then the pressure is increased, or the pressure is increased sequentially while subsequent forming is performed. The superplastic alloy is superplastically deformed, and at the same time, most of the thermoforming resin is deformed and preforming is completed, and the edges of the resin are further sharpened by high pressure loading after that, improving mold reproducibility. will be achieved. Examples are shown below. Example 1 shows an example of two-stage molding, Example 2 shows an example of multi-stage molding, and Example 3 shows an example of stepless molding. In each example, a mold for molding the casing was used, which had a width of 100 mm, a length of 200 mm, a depth of 35 mm, and a portion of the bottom surface had irregularities of about 3 mm in height. Example 1 Thermoforming resins include an acrylic modified PVC resin under the trade name Kaidatsu (Tsutsunaka Plastics Kogyo Co., Ltd.), a modified olefin resin under the trade name Orebitsuku (Tsutsunaka Plastics Kogyo Co., Ltd.), and an aromatic polyether. Polyphenylene oxide, trade name Noryl (manufactured by Tsutsunaka Plastics Co., Ltd.) as a system resin.
was used. As a superplastic alloy, 16 is 0.2mm thick 70
%Pb−30%Sn alloy plate, 10 is 38%Pb−62 with 0.1mm thickness
%Sn alloy plate, 22% 64%Pb−16%Sn−20 with 0.2mm thickness
%Cd alloy plate, 21% 64%Pd−16%Sn−20 with 0.1mm thickness
%Cd alloy plate was used. Also, for all other laminates
A 38%Pb-62%Sn alloy plate with a thickness of 0.2mm was used. As for the lamination method, as shown in Fig. 1, for 1 to 17, 21, and 22, a superplastic alloy is placed between the 2 mm and 1 mm thick adhesive films using a polyolefin-based adhesive film (trade name: Admar Film, manufactured by Tohcello Chemical Co., Ltd.).
VE300). Also 18-20, 23-28
As shown in Figure 2, a superplastic alloy was laminated on one side of the resin. And for 18-20, Admar film VE300 and 2mm thick Kaidatsuku for 23-25
Then, polyolefin adhesive film (Tohcello Chemical Co., Ltd.)
(manufactured by Co., Ltd., product name Admar Film XE070) and thickness
For 26 to 28, Admer film XE070 and 2 mm thick Noryl were used. The results of the examples will now be discussed. Regarding the first stage molding pressure, molding is possible even at a low pressure of 14. In case 1, which is an example of too high
The superplastic deformation of the Pb alloy plate could not keep up with the deformation of the resin, and the Pb alloy plate broke. In addition, when using the lamination method as shown in Figure 2, the deformation of the Pb alloy plate is not sufficient compared to the case as shown in Figure 1, and the deformation of the Pb alloy plate is less than 3 kg/18 as shown in Figure 1.
cm2 , the Pb plate may break and a gap may form between the resin and the Pb alloy plate, resulting in poor adhesion. In case 8, which is an example in which the first stage molding time was too short, the second stage pressure of 7 kg/cm 2 was applied without sufficient primary molding.
There are cracks in the Pb alloy plate. Furthermore, in the case of samples 2, 13, and 19, which are too long examples, the laminate was cooled by the mold before the second stage molding, resulting in insufficient mold reproducibility. The pressure in the second stage is 5Kg/cm 2 as shown in Example 20.
The above is sufficient, but as inferred from the case of Example 2, sufficient mold reproducibility cannot be obtained at a pressure as low as 2 Kg/cm 2 . Incidentally, Example 1 which is not based on the method of the present invention,
No good results were obtained for 2, 18, and 19.
【表】【table】
【表】
実施例 2
厚さ1mmのカイダツクと厚さ0.1mmのPb−62%
Sn合金板を第1図のごとく積層し、積層板温度
160℃、金型温度50℃で圧空成形を行つた。
5Kg/cm2の圧力を20秒間かけて成形したものは
Pb板に亀裂が生じた。
しかし表2に示すような圧力条件で三段階に分
けて成形したものはいずれも型再現性が良好で、
かつPb合金板の亀裂も生じなかつた。[Table] Example 2 1mm thick Kaidatsu and 0.1mm thick Pb-62%
Sn alloy plates are laminated as shown in Figure 1, and the temperature of the laminated plates is
Pressure forming was performed at 160°C and mold temperature of 50°C. The one molded under a pressure of 5Kg/ cm2 for 20 seconds is
A crack appeared in the Pb board. However, all molds molded in three stages under the pressure conditions shown in Table 2 had good mold reproducibility.
Moreover, no cracks occurred in the Pb alloy plate.
【表】
実施例 3
厚さ1.5mmのオレビツクと厚さ0.1mmのPb合金板
を第2図のごとく積層し、積層板温度160℃、金
型温度80℃で圧空成形を行つた。7Kg/cm2の圧力
を20秒間かけて成形したものは型再現性は良好で
あつたが、Pb合金板に亀裂が生じ、1Kg/cm2の
圧力で30秒間成形したものはPb合金板の亀裂は
なかつたが、型再現性は不十分であつた。しかし
成形スタート時の圧力が0.1Kg/cm2で成形開始直
後に0.1Kg/cm2から7Kg/cm2まで一定速度で20秒
間かけて徐々に圧力を7Kg/cm2まで上げて成形し
たものはPb合金板の伸び、型再現性共良好であ
つた。
〔発明の効果〕
以上のような本発明によれば、超塑性合金と熱
成形用樹脂とを積層した積層板を型再現性よく筐
体等の形状に効率よく成形し得る方法が得られ、
その効果は大きい。[Table] Example 3 A 1.5 mm thick Orebic sheet and a 0.1 mm thick Pb alloy plate were laminated as shown in Fig. 2, and pressure forming was performed at a laminate temperature of 160°C and a mold temperature of 80°C. The one molded under a pressure of 7 kg/cm 2 for 20 seconds had good mold reproducibility, but the Pb alloy plate had cracks, and the one molded under a pressure of 1 kg/cm 2 for 30 seconds had poor mold reproducibility. Although there were no cracks, the mold reproducibility was insufficient. However, when the pressure at the start of molding is 0.1Kg/ cm2 , the pressure is gradually increased from 0.1Kg/ cm2 to 7Kg/ cm2 over 20 seconds at a constant speed to 7Kg/ cm2 immediately after the start of molding. The elongation and mold reproducibility of the Pb alloy plate were both good. [Effects of the Invention] According to the present invention as described above, a method for efficiently molding a laminate of a superplastic alloy and a thermoforming resin into the shape of a casing or the like with good mold reproducibility is obtained.
The effect is great.
第1図および第2図は本発明に係る熱成形用積
層板の断面説明図である。
1……超塑性合金板、2……熱成形用樹脂シー
ト、3……接着剤または粘着剤。
FIGS. 1 and 2 are explanatory cross-sectional views of a thermoforming laminate according to the present invention. 1... Superplastic alloy plate, 2... Resin sheet for thermoforming, 3... Adhesive or adhesive.
Claims (1)
熱成形用積層板を圧空成形するに際し、初期成形
の圧力をその後の成形圧力に比べて低圧とし、そ
の後圧力を高め、もしくは順次高めながらそれ以
後の成形を行うことを特徴とする熱成形用積層板
の成形方法。 2 成形圧力を多段に変化させる特許請求の範囲
第1項記載の方法。 3 成形圧力を無段階に変化させる特許請求の範
囲第1項記載の方法。 4 成形初期の圧力が超塑性合金が超塑性変形さ
れ且つ熱成形用樹脂が予備成形される範囲とする
特許請求の範囲第1項〜第3項のいずれかに記載
の方法。 5 初期成形を圧力0.1〜5Kg/cm2で1〜20秒間
行い、それ以降の成形を3Kg/cm2以上で行う特許
請求の範囲第1項〜第4項のいずれかに記載の方
法。 6 初期成形圧力が0.1〜3Kg/cm2であり、それ
以降の成形圧力が5〜10Kg/cm2である特許請求の
範囲第5項記載の方法。 7 熱成形用積層板が超塑性合金板の片面にのみ
熱成形用樹脂が積層されたものであり、初期成形
圧力を0.1〜1.5Kg/cm2で行う特許請求の範囲第1
項〜第6項のいずれかに記載の方法。 8 熱成形用樹脂がアクリル変性塩ビ系樹脂であ
り、積層板の温度を110℃以上、金型温度を10〜
70℃とする特許請求の範囲第1項〜第7項のいず
れかに記載の方法。 9 熱成形用樹脂が変性オレフイン系樹脂であ
り、積層板の温度を140℃以上、金型温度を30〜
120℃とする特許請求の範囲第1項〜第7項のい
ずれかに記載の方法。 10 熱成形用樹脂が芳香族ポリエーテル系樹脂
であり、積層板の温度を150℃以上、金型温度を
30〜130℃とする特許請求の範囲第1項〜第7項
のいずれかに記載の方法。[Claims] 1. When pressure forming a thermoforming laminate made by laminating a superplastic alloy and a thermoforming resin, the initial forming pressure is lower than the subsequent forming pressure, and then the pressure is reduced. A method for forming a thermoforming laminate, characterized by performing subsequent forming while increasing the height or increasing the height sequentially. 2. The method according to claim 1, wherein the molding pressure is varied in multiple stages. 3. The method according to claim 1, wherein the molding pressure is changed steplessly. 4. The method according to any one of claims 1 to 3, wherein the pressure at the initial stage of molding is within a range in which the superplastic alloy is superplastically deformed and the thermoforming resin is preformed. 5. The method according to any one of claims 1 to 4, wherein initial molding is performed at a pressure of 0.1 to 5 kg/cm 2 for 1 to 20 seconds, and subsequent molding is performed at a pressure of 3 kg/cm 2 or more. 6. The method according to claim 5, wherein the initial molding pressure is 0.1 to 3 Kg/cm 2 and the subsequent molding pressure is 5 to 10 Kg/cm 2 . 7 The thermoforming laminate is a superplastic alloy plate with thermoforming resin laminated only on one side, and the initial molding pressure is 0.1 to 1.5 Kg/cm 2 Claim 1
6. The method according to any one of items 6 to 6. 8 The thermoforming resin is acrylic modified PVC resin, the temperature of the laminate is 110℃ or higher, and the mold temperature is 10~10℃.
The method according to any one of claims 1 to 7, wherein the temperature is 70°C. 9 The thermoforming resin is a modified olefin resin, the temperature of the laminate is 140℃ or higher, and the mold temperature is 30~30℃.
The method according to any one of claims 1 to 7, wherein the temperature is 120°C. 10 The thermoforming resin is an aromatic polyether resin, and the temperature of the laminate is 150℃ or higher and the mold temperature is
The method according to any one of claims 1 to 7, wherein the temperature is 30 to 130°C.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP1877686A JPS62176823A (en) | 1986-01-30 | 1986-01-30 | Method of molding laminated sheet for thermoforming |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP1877686A JPS62176823A (en) | 1986-01-30 | 1986-01-30 | Method of molding laminated sheet for thermoforming |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS62176823A JPS62176823A (en) | 1987-08-03 |
| JPH0144494B2 true JPH0144494B2 (en) | 1989-09-28 |
Family
ID=11981034
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP1877686A Granted JPS62176823A (en) | 1986-01-30 | 1986-01-30 | Method of molding laminated sheet for thermoforming |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS62176823A (en) |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5869412A (en) * | 1991-08-22 | 1999-02-09 | Minnesota Mining & Manufacturing Co. | Metal fibermat/polymer composite |
| JP4775593B2 (en) * | 2006-10-31 | 2011-09-21 | ソニーケミカル&インフォメーションデバイス株式会社 | Method for producing laminated soft magnetic sheet |
| JP4968481B2 (en) * | 2008-04-28 | 2012-07-04 | ソニーケミカル&インフォメーションデバイス株式会社 | Method for producing laminated soft magnetic sheet |
| JP5755971B2 (en) * | 2011-08-29 | 2015-07-29 | 三菱瓦斯化学株式会社 | Pressure forming method |
| JP5282921B2 (en) * | 2012-02-17 | 2013-09-04 | デクセリアルズ株式会社 | Method for producing laminated soft magnetic sheet |
-
1986
- 1986-01-30 JP JP1877686A patent/JPS62176823A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS62176823A (en) | 1987-08-03 |
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